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007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH -E1
E082-160620 REVIEW FJ44-2A LM REV 39
MTH -E2
E082-160620 REVIEW FJ44-2A LM REV 39
MTH -E1
E082-160920 REVIEW FJ44-2A LM REV40
MTH -E2
E082-160920 REVIEW FJ44-2A LM REV40
HRS
MTH
6125
09-Oct-2008 O/C0500001
UVA
INSPECT ADDL INFORMATION
WILLIAMS ENGINES INSTALLED PER SIERRA INDUSTRIES STC # SA09559AC OR STC# ST09559AC.
LDG
HRS
MTH
4922
7169.8
15-May-2020 12 31-May-2021 1 m 18 d051013G
UNK
INSPECT COMPASS SWING INSP
LDG
HRS
MTH
4930
7179.1
07-Oct-2020 12 31-Oct-2021 6 m 18 d053400
UNK
12 MONTH STAR AVIONICS INSPECTION
LDG
HRS
MTH
4873
7097.3
17-Jul-2019 24 31-Jul-2021 3 m 18 d053401 STAR AVIONICS 24 MONTH INSPECTION
LDG
HRS
MTH
4873
7097.3
03-Aug-2019 24 31-Aug-2021 4 m 18 d053402
UNK
STAR AVIONICS ALTITTUDE HOLD CHECK INSPECTION
LDG
HRS
MTH
4873
7097.3
10-Jul-2019
1200
36
8297.3
31-Jul-2022
1116.9
15 m 18 d053403
UNK
GMA 1347D TEST INSPECTION
LDG
HRS
MTH
4873
7097.3
10-Jul-2019
1200
36
8297.3
31-Jul-2022
1116.9
15 m 18 d053404
UNK
TAWS FUNCTION CHECK INSPECTION
LDG
HRS
MTH
4873
7097.3
15-Jul-2019 24 31-Jul-2021 3 m 18 d053405
UNK
GTX 33 TRANSPONDER TEST INSPECTION
LDG
HRS
MTH
4873
7097.3
15-Jul-2019 24 31-Jul-2021 3 m 18 d053406
UNK
PERFORM AIR DATA TEST INSPECTION
LDG
HRS
MTH
4866
7086.3
30-Mar-2019 60 31-Mar-2024 35 m 18 d053407
UNK
GRS 77 MAGNETIC VARIATION DATABASE UPDATE
LDG
HRS
MTH
4873
7097.3
15-Jul-2019
300
24
7397.3
31-Jul-2021
216.9
3 m 18 d053408
UNK
G950 FAILURE TEST INSPECTION
LDG
HRS
MTH
4873
7097.3
15-Jul-2019
300
24
7397.3
31-Jul-2021
216.9
3 m 18 d053409
UNK
INSPECT G950 COOLING FAN INSPECTION
LDG
HRS
MTH
4873
7097.3
10-Jul-2019
1200
36
8297.3
31-Jul-2022
1116.9
15 m 18 d053410
UNK
G950 MISCOMPARE INSPECTION
LDG
HRS
MTH
4873
7097.3
15-Jul-2019 24 31-Jul-2021 3 m 18 d053411
UNK
STATIC PRESSURE SYSTEM INSPECTION
LDG
HRS
MTH
4873
7097.3
17-Jul-2019 24 31-Jul-2021 3 m 18 d053412
UNK
ELETRONIC STANDBY INDICATOR INSPECTION
LDG
HRS
MTH
4873
7097.3
10-Jul-2019
1200
36
8297.3
31-Jul-2022
1116.9
15 m 18 d053413
UNK
G950 ELECTRICAL BONDING INSPECTION
LDG
HRS
MTH
4873
7097.3
10-Jul-2019
1200
36
8297.3
31-Jul-2022
1116.9
15 m 18 d053430
UNK
G950 VARIOUS VISUAL INSPECTIONS
Page 1 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
3000 9539.8 2359.4
053431
KUVA
G950 FUSELAGE EXTERIOR SKIN VISUAL INSPECTION
MTH 30-Apr-2003 O/C053490
SMF
INSPECT RVSM GMU TEST FLIGHT
LDG
HRS
MTH
4918
7162.7
10-Mar-2020
300
24
7462.7
31-Mar-2022
282.3
11 m 18 d055600
UNK
RIGHT COCKPIT SIDEWINDOW PRISM INSPECTION
LDG
HRS
MTH
4922
7169.8
23-Apr-2020
300
24
7469.8
30-Apr-2022
289.4
12 m 17 d051204
5-12-01
UNK
PHASE 1 INSPECTION
LDG
HRS
MTH
4922
7169.8
15-May-2020
300
24
7469.8
31-May-2022
289.4
13 m 18 d051205
5-12-02
UNK
PHASE 2 INSPECTION
LDG
HRS
MTH
4918
7162.7
10-Mar-2020
300
24
7462.7
31-Mar-2022
282.3
11 m 18 d051206
5-12-03
UNK
PHASE 3 INSPECTION
LDG
HRS
MTH
4922
7169.8
15-May-2020
300
24
7469.8
31-May-2022
289.4
13 m 18 d051207
5-12-04
UNK
PHASE 4 INSPECTION
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
1200
36
8380.4
30-Apr-2024
1200
36 m 17 d051210
5-12-05
UNK
PHASE 5 INSPECTION
LDG
HRS
DAYS
4935
7180.4
07-Apr-2021 90 06-Jul-2021 2 m 23 d051220
5-12-07
UNK
PHASE 7 INSPECTION
LDG
HRS
MTH
4924
7171
08-Jun-2020
150 7321 140.6051218
5-12-0B UNKPHASE B
LDG
HRS
MTH
4763
6915.3
18-Jan-2017
600
600
5363
7515.3
428
334.9051003
5-12-12
UNK
PHASE 12 INSPECTION
HRS
MTH
5085
26-Apr-2002
1000 10000 2819.6052013 : B
5-12-15
SJC 3915
PHASE 15 INSPECTION
HRS
MTH
0
30-Apr-1983
10000 10000 2819.6052013 : C
5-12-16
*CF
PHASE 16 INSPECTION
HRS
MTH
5085
26-Apr-2002
10000 15085 7904.6052013
5-12-17
SJC
PHASE 17 INSPECTION
LDG
HRS
MTH
4935
7180.4
07-Apr-2021 12 30-Apr-2022 12 m 17 d051005
5-12-18
UNK
PHASE 18 INSPECTION
LDG
HRS
MTH
4774
6945.1
21-Jul-2017 24
5-12-20
CYHM
PHASE 20 INSPECTION (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
LDG
HRS
MTH
4908
7147.4
01-Feb-2020 24 28-Feb-2022 10 m 15 d051220 : RVSM
A341007
UNK
INSPECT RVSM SKIN WAVINESS: PHASE 20 INSPECTION
LDG
HRS
MTH
4873
7097.3
15-Jul-2019 24 31-Jul-2021 3 m 18 d051220 : L
LEFT
B341005
UNK
LEAK TEST STATIC SYSTEM FAR 91.411: PHASE 20 INSPECTION
LDG
HRS
MTH
4873
7097.3
15-Jul-2019 24 31-Jul-2021 3 m 18 d051220 : R
RIGHT
B341005
UNK
LEAK TEST STATIC SYSTEM FAR 91.411: PHASE 20 INSPECTION
MTH 18-Jul-2019 241SW005959
011-01110-01 31-Jul-2021 3 m 18 d051007
NO. 1
B341008
UNK
CALIBRATION TEST AIR DATA COMPUTER FAR 91.411: PHASE 20 INSPECTION
Page 2 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 18-Jul-2019 241SW005986
011-01110-01 31-Jul-2021 3 m 18 d051220 : ADC#2
NO. 2
B341008
UNK
CALIBRATION TEST AIR DATA COMPUTER FAR 91.411: PHASE 20 INSPECTION
MTH 15-Jul-2019 2484810509
011-00779-21 31-Jul-2021 3 m 18 d051221 : R
NO. 1
B345001
UNK
CALIBRATION TEST ATC TRANSPONDER FAR 91.413: PHASE 20 INSPECTION
MTH 15-Jul-2019 2484810516
011-00779-21 31-Jul-2021 3 m 18 d051221
NO. 2
B345001
UNK
CALIBRATION TEST ATC TRANSPONDER FAR 91.413: PHASE 20 INSPECTION
LDG
HRS
MTH
4563
6608.9
22-Feb-2014 60
5-12-23
CYHM
PHASE 23 INSPECTION (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
HRS
MTH
0
30-Apr-1983
10000 10000 2819.6052013 : A
5-12-24
*CF
PHASE 24 INSPECTION
LDG
HRS
MTH
4924
7171
08-Jun-2020 6
5-12-34
UNK
PHASE 34 INSPECTION (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
MTH 23-Mar-2021 6E68634974
C352TS 30-Sep-2021 5 m 17 dCABIN
A262003
UNK
WEIGHT CHECK PORTABLE EXTINGUISHER : PHASE 34 INSPECTION
MTH 23-Mar-2021 6B-12490752
B385 30-Sep-2021 5 m 17 d051018 : F
COCKPIT
A262003
UNK
WEIGHT CHECK PORTABLE EXTINGUISHER : PHASE 34 INSPECTION
HRS
MTH
5085
26-Apr-2002
5000 10085 2904.6052010
5-12-37
SJC
PHASE 37 INSPECTION
MTH 30-Apr-1983 A/R052013 : E
5-12-40
*CF
PHASE 40 INSPECTION (NOT CURRENTLY USED)
MTH 30-Apr-1983 72
5-12-48 PHASE 48 INSPECTION (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
LDG
HRS
MTH
4935
7180.4
07-Apr-2021 72E68634974
C352TS 30-Apr-2027 72 m 17 dCABIN
B262004
UNK
EMPTY/INSPECT/RECHARGE PORTABLE EXTINGUISHER : PHASE 48 INSPECTION
LDG
HRS
MTH
4935
7180.4
07-Apr-2021 72B-12490752
B385 30-Apr-2027 72 m 17 d051019B : F
COCKPIT
B262004
UNK
EMPTY/INSPECT/RECHARGE PORTABLE EXTINGUISHER : PHASE 48 INSPECTION
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
1200
36
8380.4
30-Apr-2024
1200
36 m 17 d051210 : SJ
5-12-49
UNK
PHASE 49 INSPECTION
LDG
HRS
MTH
4427
6408
20-Feb-2012
2000 8408 1227.6051252
5-12-52
CYHM
PHASE 52 INSPECTION
PHASE 52 EXTENSION GRANTED IN ACCORDANCE WITH SL500-05-15,
LDG
HRS
MTH
4922
7169.8
15-May-2020 12 31-May-2021 1 m 18 d051253
5-12-53
UNK
PHASE 53 INSPECTION
LDG
HRS
MTH
4930
7179.1
07-Oct-2020
200
35-12-54
UNK
PHASE 54 INSPECTION
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
200
340896417
RG-380E/44
7380.4
31-Jul-2021
200
3 m 18 d
B243003
UNK
FUNCTIONAL CHECK BATTERY LEAD ACID BATTERY (CAPACITY CHECK): PHASE 54 INSPECTION
N/A5-12-56 PHASE 56 INSPECTION
Page 3 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4935
7180.4
07-Apr-2021 6 31-Oct-2021 6 m 18 d5-12-57
UNK
PHASE 57 INSPECTION
ACH
MTH
500 500 500
5-12-58 PHASE 58 INSPECTION
HRS
MTH
10000 10000 2819.6
5-12-59 PHASE 59 INSPECTION
LDG
HRS
MTH
4012
5085
26-Apr-2002
1000 5012 77
0512MA
5-12-MA
SJC
PHASE MA INSPECTION
LDG
HRS
MTH
4012
5085
26-Apr-2002
5000
0512MD
5-12-MD
SJC
PHASE MD INSPECTION (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
LDG
HRS
MTH
4012
5085
26-Apr-2002
5000
SN-UNKNOWN
5522720-1
9012 4077
LEFT
A574010 INSPECT LEFT MAIN LANDING GEAR SIDE BRACE FITTING: PHASE MD INSPECTION
LDG
HRS
MTH
4012
5085
26-Apr-2002
5000
SN-UNKNOWN
5522720-2
9012 4077
RIGHT
A574010 INSPECT RIGHT MAIN LANDING GEAR SIDE BRACE FITTING: PHASE MD INSPECTION
LDG
HRS
MTH
0
0
30-Apr-1983
224
5-12-MF PHASE MF INSPECTION (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
LDG
HRS
MTH
0
0
30-Apr-1983
425
5-12-MG PHASE MG INSPECTION (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
LDG
HRS
MTH
4647
6742.2
06-Aug-2015 N/A5-12-MH
CYHM
PHASE MH INSPECTION
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
300 (1169.2)7292.5 112.1E1
052001 UNKFJ44 CHECK 1
LDG
HRS
MTH
4803
6992.5
16-Feb-2018
300 (1170.2)7292.5 112.1E2
052001 UNKFJ44 CHECK 1
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
600 (1469.2)7592.5 412.1E1
052002 UNKFJ44 CHECK 2
LDG
HRS
MTH
4803
6992.5
16-Feb-2018
600 (1470.2)7592.5 412.1E2
052002 UNKFJ44 CHECK 2
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
600 (1469.2)7592.5 412.1E1
792025 UNKCHANGE OIL
LDG
HRS
MTH
4803
6992.5
16-Feb-2018
600 (1470.2)7592.5 412.1E2
792025 UNKCHANGE OIL
LDG
HRS
MTH
4234
6125.3
09-Oct-2008
10500 (1750)7873.3 692.9E1
052003 UVA
-8752
FJ44 CHECK 3
LDG
HRS
MTH
4235
6125.3
09-Oct-2008
10500 (1750)7872.3 691.9E2
052003 UVA
-8753
FJ44 CHECK 3
Page 4 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4234
6125.3
09-Oct-2008
10500 (3500)9623.3 2442.9E1
052004 UVA
-7002
FJ44 CHECK 4
LDG
HRS
MTH
4235
6125.3
09-Oct-2008
10500 (3500)9622.3 2441.9E2
052004 UVA
-7003
FJ44 CHECK 4
HRS
MTH
6123.3
09-Oct-2008
10500 (5250)11373.3 4192.9E1
052005
-5250
FJ44 CHECK 5
HRS
MTH
6122.3
09-Oct-2008
10500 (5250)11372.3 4191.9E2
052005
-5250
FJ44 CHECK 5
HRS
MTH
6123.3
09-Oct-2008
10500 (7000)13123.3 5942.9E1
052006
-3500
FJ44 CHECK 6
HRS
MTH
6122.3
09-Oct-2008
10500 (7000)13122.3 5941.9E2
052006
-3500
FJ44 CHECK 6
HRS
MTH
6123.3
09-Oct-2008
10500 (8750)14873.3 7692.9E1
052007
-1750
FJ44 CHECK 7
HRS
MTH
6122.3
09-Oct-2008
10500 (8750)14872.3 7691.9E2
052007
-1750
FJ44 CHECK 7
HRS
MTH
6123.3
09-Oct-2008
10500 (10500)16623.3 9442.9E1
052008 FJ44 CHECK 8
HRS
MTH
6122.3
09-Oct-2008
10500 (10500)16622.3 9441.9E2
052008 FJ44 CHECK 8
HRS
MTH
6123.3
09-Oct-2008
12250 (12250)18373.3 11192.9E1
052009 FJ44 CHECK 9
HRS
MTH
6122.3
09-Oct-2008
12250 (12250)18372.3 11191.9E2
052009 FJ44 CHECK 9
HRS
MTH
6123.3
09-Oct-2008
14000 (14000)20123.3 12942.9E1
052010 FJ44 CHECK 10
HRS
MTH
6122.3
09-Oct-2008
14000 (14000)20122.3 12941.9E2
052010 FJ44 CHECK 10
HRS
MTH
3338
09-Sep-1994 O/C129999
SMF
INSPECT AIRCRAFT SURVEY
MTH 30-Apr-1983 N/A
B213003 OPERATIONAL CHECK PRESSURIZATION (AIRPLANES -0001 THRU -0213 NOT INCORPORATING SB500-21-09): PHASE 5 INSPECTION
MTH 06-Apr-2019 72LOT # ESD18F725-001
13083-5 30-Jun-2024 38 m 17 d262003 : AL
AFT LEFT
262037
UNK
-10REPLACE ENGINE FIRE EXTINGUISHER CARTRIDGE (SERVICE LIFE)
MTH 06-Apr-2019 72LOT # ESD18F725-001
13083-5 30-Jun-2024 38 m 17 d262003 : AR
AFT RIGHT
262038
UNK
-10REPLACE ENGINE FIRE EXTINGUISHER CARTRIDGE (SERVICE LIFE)
MTH 06-Apr-2019 72LOT # ESD18F725-001
13083-5 30-Jun-2024 38 m 17 d262003 : FL
FORWARD LEFT
262039
UNK
-10REPLACE ENGINE FIRE EXTINGUISHER CARTRIDGE (SERVICE LIFE)
MTH 06-Apr-2019 72LOT # ESD18F725-001
13083-5 30-Jun-2024 38 m 17 d262003 : FR
FORWARD RIGHT
262040
UNK
-10REPLACE ENGINE FIRE EXTINGUISHER CARTRIDGE (SERVICE LIFE)
MTH 30-Apr-2019 60
B13585
3040110230-Apr-2024 36 m 17 d
121001 : A
AFT
B262002
UNK
HYDROSTATIC TEST ENGINE FIRE EXTINGUISHER
MTH 06-Apr-2019 60
B13308
3040110230-Apr-2024 36 m 17 d
121001 : F
FORWARD
B262002
UNK
HYDROSTATIC TEST ENGINE FIRE EXTINGUISHER
Page 5 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 01-Jun-2019 144
E68634974
C352TS30-Jun-2031 122 m 17 d
CABIN
B262003
UNK
HYDROSTATIC TEST PORTABLE EXTINGUISHER
MTH 01-Jan-2016 144
B-12490752
B38531-Jan-2028 81 m 18 d
051019 : F
COCKPIT
B262003
UNK
HYDROSTATIC TEST PORTABLE EXTINGUISHER
MTH 24-Mar-2021 36
2159
2311132131-Mar-2024 35 m 18 d
051227
B326003
UNK
HYDROSTATIC TEST EMERGENCY GEAR AIR BOTTLE
MTH 07-May-2020 36K906486
176126-64 31-May-2023 25 m 18 d051226 : C
B350004
UNK
HYDROSTATIC TEST OXYGEN CYLINDER (DOT 3HT1850 OR 3FC1850)
MTH 09-Oct-2008 A/RE1
710010 COMPRESSOR CLEANING
MTH 09-Oct-2008 A/RE2
710010 COMPRESSOR CLEANING
Page 6 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/C253
224465-2211002
*CF
EMERGENCY PRESSURIZATION VALVE
LDG
HRS
MTH
4427
6408
20-Feb-2012
010001133A
BC61A901-2
7608 427.6CABIN
212002
9912323-2 CYHM
AFT OVERHEAD BLOWER
MTH 30-Apr-1983 O/CSN-UNKNOWN
1H56-1212003
*CF
AIR INLET DOOR ACTUATOR
MTH 30-Apr-1983 O/CSN-UNKNOWN
WS2107F30
LEFT CABIN
212005 *CFCOOLING FAN
MTH 30-Apr-1983 O/CSN-UNKNOWN
WS2107F30
RIGHT CABIN
212005 *CFCOOLING FAN
MTH 30-Apr-1983 O/C405
5705-1
CABIN
212006
*CF
UNDERFLOOR BLOWER
MTH 30-Apr-1983 O/CSN-UNKNOWN
5A3032212010
9910059-3 *CF
DOOR ACTUATOR MOTOR ASSEMBLY
MTH 30-Apr-1983 O/C17048
C668511-0102
CABIN
213001
3001J14 *CF
PRESSURE INDICATOR
MTH 30-Apr-1983 O/C11566
130356-5213002
*CF
PRESSURIZATION CONTROLLER
MTH 30-Apr-1983 O/CW1154H
C668513-0101
CABIN
213003
35060-1128 *CF
RATE OF CLIMB INDICATOR
MTH 30-Apr-1983 O/C424312
102466-1
LEFT CABIN
213005
9912055-1 *CF
ALTITUDE LIMIT VALVE
MTH 30-Apr-1983 O/C424281
102466-1
RIGHT CABIN
213005
9912055-1 *CF
ALTITUDE LIMIT VALVE
LDG
HRS
MTH
4803
6992.5
22-Feb-2018 O/C49-609
103576-13213006
UNK
SAFETY OUTFLOW VALVE
MTH 30-Apr-1983 O/C89711
103576-12213007
*CF
NORMAL OUTFLOW VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
2101701-1213008
*CF
MANUAL DUMP VALVE
MTH 30-Apr-1983 O/C459
225645-2
LEFT
213009
9912109-1 *CF
BLEED AIR FLOW CONTROL VALVE
MTH 30-Apr-1983 O/C478
225645-2
RIGHT
213009
9912109-1 *CF
BLEED AIR FLOW CONTROL VALVE
HRS
MTH
2908
10-Nov-1992
0O/C
SN-UNKNOWN
130358-1213013 JHBPNEUMATIC RELAY
MTH 30-Apr-1983 O/C52733
738443-13215001
9912069-21 *CF
REFRIGERATION UNIT
MTH 30-Apr-1983 O/CSN-UNKNOWN
740730-2215002
*CF
ASPIRATOR AND FAN HOUSING
LDG
HRS
MTH
4884
7108.4
31-Oct-2019
0
0
2
500081997
738384-8
12108.4 4928
215004
UNK
AIR CYCLE MACHINE
RECOMMENDED ECONOMIC OVERHAUL PERIOD DEFINED BY HAMILTON STANDARD.
MTH 30-Apr-1983 O/CSN-UNKNOWN
754751-1215005
9912069-1
*CFBYPASS VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
746833-1215006 *CFOVERHEAT SWITCH
MTH 30-Apr-1983 O/C628
225655215007
9912068-3 *CF
GROUND OPERATION VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
5518118-3216001
*CF
CABIN TEMPERATURE SELECTOR
MTH 30-Apr-1983 O/CSN-UNKNOWN
754661-5216002
9912069-22 *CF
TEMPERATURE CONTROL UNIT
Page 7 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/CSN-UNKNOWN
754691-1216003
9912069-14 *CF
DUCT TEMPERATURE SENSOR
MTH 30-Apr-1983 O/CSN-UNKNOWN
754681-1216004
9912069-15 *CF
CABIN TEMPERATURE SENSOR
HRS
MTH
5719
25-Nov-2005
0O/C
1258
19A2338216005
9912070-1 YHM
CENTRIFUGAL BLOWER
HRS
MTH
3061
22-Oct-1993
0O/C
SN-UNKNOWN
0221-003216006
FMN
CABIN TEMPERATURE INDICATOR
MTH 30-Apr-1983 O/C031639
4008519-911221008
SP-200 *CF
AUTOPILOT COMPUTER
MTH 30-Apr-1983 O/C122026
4018639-901221009
PC-500 *CF
AUTOPILOT CONTROLLER
MTH 30-Apr-1983 O/C028408
4006719-904
AILERON
221010
SM-200
*CFSERVO ACTUATOR
MTH 30-Apr-1983 O/C078909
4006719-904
ELEVATOR
221010
SM-200
*CFSERVO ACTUATOR
MTH 30-Apr-1983 O/C119035
4006719-906
RUDDER
221010
SM-200
*CFSERVO ACTUATOR
MTH 30-Apr-1983 O/C2835
622-2883-001231002
PWR-200
*CFHF PA/PS UNIT
MTH 30-Apr-1983 O/C2094
622-5337-001231003
TCR-220 *CF
HF RECEIVER-EXCITER
LDG
HRS
MTH
4511
6539.8
29-Jun-2013 O/C
8951
013-00244-00NO. 1
231004
GA-36 UVA
HIGH FREQUENCY COMMUNICATION ANTENNA
MTH 30-Apr-1983 O/C2713
622-4545-005231005 *CFHF CONTROL HEAD
MTH 30-Apr-1983 O/C1196
VF10-108-1
NO. 2
232002
9912084-1 *CF
VHF COMMUNICATION ANTENNA
MTH 30-Apr-1983 O/C1515
VFS10-90-5
NO. 1
232003
*CF
VHF COMMUNICATION ANTENNA
MTH 30-Apr-1983 O/C
18974
622-1879-002NO. 2
232010
VHF-20A *CF
BOTTOM COMMUNICATION TRANSCEIVER
MTH 30-Apr-1983 O/C512A
1U434-001232011
*CF
COMMUNICATION CONTROL
MTH 30-Apr-1983 O/CSN-UNKNOWN
48FU2103
CABIN
235003 *CFSPEAKERS
MTH 30-Apr-1983 O/CSN-UNKNOWN
48FU2103
COCKPIT
235003 *CFSPEAKERS
MTH 30-Apr-1983 O/CSN-UNKNOWN
C596502-0202
LEFT
235005
60837-23
*CFMICROPHONE
MTH 30-Apr-1983 O/CSN-UNKNOWN
C596502-0202
RIGHT
235005
60837-23
*CFMICROPHONE
MTH 30-Apr-1983 O/CSN-UNKNOWN
62629-00
LEFT
235006 *CFTELEX HEADSET
MTH 30-Apr-1983 O/CSN-UNKNOWN
62629-00
RIGHT
235006 *CFTELEX HEADSET
HRS
MTH
5170
16-Sep-2002
0O/C
162
PC17-3B
NO. 1
242001 SMFAC INVERTER
MTH 30-Apr-1983 O/C229
PC17-3B
NO. 2
242001 *CFAC INVERTER
Page 8 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4470
6464.6
30-Oct-2012
0
0O/C1251
1371-1242002 CYHMAC FAIL MONITOR-
LDG
HRS
MTH
4883
7108.2
16-Oct-2019
0
983.2
0
1000875
23080-001-1CHJ
8108.2 927.8NO. 1
243001
9912038-8 UNK
ENGINE STARTER/GENERATOR
LDG
HRS
MTH
4883
7108.2
16-Oct-2019
0
0
8
10001904
23080-001-1
8108.2 927.8NO. 2
243001
9912038-4 UNK
ENGINE STARTER/GENERATOR
HRS
MTH
6125
18-Dec-2008
0O/C
7723A
51509-006BR
LEFT
243003
9912039-3 UVA
GENERATOR CONTROL UNIT
HRS
MTH
6125
18-Dec-2008
0O/C
10486A
51509-006BR
RIGHT
243003
9912039-3 UVA
GENERATOR CONTROL UNIT
MTH 30-Apr-1983 O/C3624
C662501-0102
LEFT
243004 *CFAMMETER
HRS
MTH
3538
01-Aug-1995
0O/C
1568
C662501-0102
RIGHT
243004 SJCAMMETER
MTH 30-Apr-1983 O/C1077
C662502-0101243005
153LV30
*CFVOLTMETER
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
148
215
43O/C40896417
RG-380E/44243007 UNKBATTERY
MTH 30-Apr-1983 O/C1140
1529-1243008
*CF
BATTERY TEMPERATURE MODULE
MTH 30-Apr-1983 O/C1121
1229-1243009
*CF
BATTERY TEMPERATURE GAUGE
MTH 30-Apr-1983 O/CV4702
1166-1
G
243010
*CF
GAGE TEMP SENSOR --
MTH 30-Apr-1983 O/CH4704
1166-1
W
243010
*CF
OVR HEAT TEMP SENSOR --
MTH 30-Apr-1983 O/C1111
1301-1243011
*CF
CURRENT / VOLT CONTROLLER
HRS
MTH
5484
12-Feb-2004
314O/C
790A
1302-1243012 SJCCURRENT SENSOR
MTH 30-Apr-1983 O/CSN-UNKNOWN
AN3380-1
K11
244001 *CF400 AMP RELAY
MTH 30-Apr-1983 O/CSN-UNKNOWN
AN3380-1
K12
244001 *CF400 AMP RELAY
MTH 30-Apr-1983 O/CSN-UNKNOWN
AN3380-1
K13
244001 *CF400 AMP RELAY
MTH 30-Apr-1983 O/CSN-UNKNOWN
AN3380-1
K1
244001 *CF400 AMP RELAY
MTH 30-Apr-1983 O/CSN-UNKNOWN
AN3380-1
K7
244001 *CF400 AMP RELAY
MTH 30-Apr-1983 O/CSN-UNKNOWN
AN3380-1
K8
244001 *CF400 AMP RELAY
MTH 30-Apr-1983 O/C1639
1505-1
CENTER
245001
*CF
5 VOLT LIGHT DIMMER
MTH 30-Apr-1983 O/C3565
1505-1
LEFT
245001
*CF
5 VOLT LIGHT DIMMER
MTH 30-Apr-1983 O/C3596
1505-1
RIGHT
245001
*CF
5 VOLT LIGHT DIMMER
Page 9 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/CSN-UNKNOWN
CM4033
LEFT
251001 *CFINERTIA REEL
MTH 30-Apr-1983 O/CSN-UNKNOWN
CM4033
RIGHT
251001 *CFINERTIA REEL
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
0
0
156019121570019
P01074-101 31-Jan-2025 45 m 18 dNO. 1
256001 UNKLIFE JACKET
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
0
0
156019121570298
P01074-101 31-Jan-2025 45 m 18 dNO. 2
256001 UNKLIFE JACKET
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
0
0
156019121570442
P01074-101 31-Jan-2025 45 m 18 dNO. 3
256001 UNKLIFE JACKET
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
0
0
156020100401387
P01074-101 31-Jan-2025 45 m 18 dNO. 4
256001 UNKLIFE JACKET
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
0
0
156020100400231
P01074-101 31-Jan-2025 45 m 18 dNO. 5
256001 UNKLIFE JACKET
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
0
0
156020100400606
P01074-101 31-Jan-2025 45 m 18 dNO. 6
256001 UNKLIFE JACKET
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
0
0
156019121570018
P01074-101 31-Jan-2025 45 m 18 dNO. 7
256001 UNKLIFE JACKET
LDG
HRS
MTH
4922
7169.8
15-May-2020 O/C02001
453-5002
344008
256019
UNK
EMERGENCY LOCATER TRANSMITTER
LDG
HRS
MTH
4697
6833.7
11-Mar-2016
0
0
0
DUE
DUE
DUE
DUE
367648-061
452-013331-Mar-2021 -13 d
344010
256025 EMERGENCY LOCATER TRANSMITTER BATTERY
Over Due
HRS
MTH
6125
18-Dec-2008
0O/C
080607
244-18882
NO. 1 ENGINE
261001
9912036-3 UVA
FIRE DETECTION SENSOR
HRS
MTH
4725
11-Aug-2000
0O/C
SN-UNKNOWN
244-18882
NO. 2 ENGINE
261001
9912036-3 SJC
FIRE DETECTION SENSOR
MTH 30-Apr-1983 O/C250007
377-02808
NO. 1 ENGINE
261002
9912036-2 *CF
FIRE DETECTION CONTROL
MTH 30-Apr-1983 O/C750067
377-02808
NO. 2 ENGINE
261002
9912036-2 *CF
FIRE DETECTION CONTROL
LDG
HRS
MTH
4866
7086.3
09-Apr-2019
0
0
487O/CB13585
30401102
AFT
262001
9912048-2 UNK
ENGINE FIRE EXTINGUISHER
LDG
HRS
MTH
4866
7086.3
09-Apr-2019
0
0
491O/CB13308
30401102
FORWARD
262001
9912048-2 UNK
ENGINE FIRE EXTINGUISHER
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
117
167.2
36O/CE68634974
C352TS
CABIN
262002
UNK
PORTABLE EXTINGUISHER
LDG
HRS
MTH
4935
7180.4
07-Apr-2021
190
282.9
53O/CB-12490752
B385
COCKPIT
262002
UNK
PORTABLE EXTINGUISHER
Page 10 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4866
7086.3
09-Apr-2019
0
072
LOT # ESD18F725-001
13083-530-Jun-2024 38 m 17 d
AFT LEFT
262003
UNK
ENGINE FIRE EXTINGUISHER CARTRIDGE
Manufacture Date: 01-Jun-2018
LDG
HRS
MTH
4866
7086.3
09-Apr-2019
0
072
LOT # ESD18F725-001
13083-530-Jun-2024 38 m 17 d
AFT RIGHT
262003
UNK
ENGINE FIRE EXTINGUISHER CARTRIDGE
Manufacture Date: 01-Jun-2018
LDG
HRS
MTH
4866
7086.3
09-Apr-2019
0
072
LOT # ESD18F725-001
13083-530-Jun-2024 38 m 17 d
FORWARD LEFT
262003
UNK
ENGINE FIRE EXTINGUISHER CARTRIDGE
Manufacture Date: 01-Jun-2018
LDG
HRS
MTH
4866
7086.3
09-Apr-2019
0
072
LOT # ESD18F725-001
13083-530-Jun-2024 38 m 17 d
FORWARD RIGHT
262003
UNK
ENGINE FIRE EXTINGUISHER CARTRIDGE
Manufacture Date: 01-Jun-2018
HRS
MTH
5719
25-Nov-2005
0O/C
052002
5565450-72271001
YHM
AILERON TRIM TAB ACTUATOR
HRS
MTH
4215
14-Jan-1998
0O/C
SN-UNKNOWN
5565450-71272001
SJC
RUDDER TRIM TAB ACTUATOR
MTH 11-Feb-2005 O/C
042297-0
5115231-30
273002
SJC
ELEVATOR TRIM ELECTRICAL ACTUATOR
HRS
MTH
5719
25-Nov-2005
0O/C
092702
5565450-92273003
YHM
ELEVATOR TRIM TAB ACTUATOR
HRS
MTH
5170
16-Sep-2002
0O/C
1143
FS30-5
LEFT
275001
9910055-4
SMFFLAP MOTOR
HRS
MTH
5170
16-Sep-2002
0O/C
1363
FS30-5
RIGHT
275001
9910055-4
SMFFLAP MOTOR
LDG
HRS
MTH
4767
6938.7
07-Apr-2017
03000412900
5565175-38
9938.7 2758.3LEFT
275002 UNKFLAP GEARBOX
LDG
HRS
MTH
4767
6938.7
07-Apr-2017
03000121395-2
5565175-38
9938.7 2758.3RIGHT
275002 UNKFLAP GEARBOX
HRS
MTH
5820
01-Jul-2006
0O/C
2881DA
5527230-1
LEFT
276001
YHM
SPEED BRAKE ACTUATOR
MTH 30-Apr-1983 O/C111618
5527230-1
RIGHT
276001
*CF
SPEED BRAKE ACTUATOR
HRS
MTH
3185
23-Feb-1994
0O/C
1269
2710970276002
FMN
SPEED BRAKE CONTROL VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
LEFT AFT
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
LEFT CENTER AFT
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
LEFT CENTERFORWARD
281002
9912083-1
*CFFUEL DRAIN VALVE
Page 11 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
LEFT FORWARD
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
LEFT MID
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
RIGHT AFT
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
RIGHT CENTERAFT
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
RIGHT CENTERFORWARD
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
RIGHT FORWARD
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/CSN-UNKNOWN
6904-079
RIGHT MID
281002
9912083-1
*CFFUEL DRAIN VALVE
MTH 30-Apr-1983 O/C2H426A
1C7-12
LEFT
282001
9912017-2
*CFFUEL BOOST PUMP
HRS
MTH
5632
16-Sep-2004
0O/C
8AY7
1C7-12
RIGHT
282001
9912017-2
SJCFUEL BOOST PUMP
HRS
MTH
6125
18-Dec-2008
0O/C
C129
LR45020D
L
282005 UVAEJECTOR PUMP --
HRS
MTH
6125
18-Dec-2008
0O/C
C130
LR45020D
R
282005 UVAEJECTOR PUMP --
HRS
MTH
5885
24-Oct-2006
0O/C
6968
L15H-3
LEFT
284001
YHM
LOW FUEL LEVEL SWITCH
MTH 30-Apr-1983 O/CSN-UNKNOWN
L15H-3
RIGHT
284001
*CF
LOW FUEL LEVEL SWITCH
MTH 30-Apr-1983 O/C14497P
300047-13001
LEFT
284002
9912019-4 *CF
FUEL QUANTITY COMPENSATOR
MTH 30-Apr-1983 O/C14488P
300047-13001
RIGHT
284002
9912019-4 *CF
FUEL QUANTITY COMPENSATOR
MTH 30-Apr-1983 O/C
1604D
391046-218LEFT WING
284003
9912019-8 *CF
SECTION (61.00) FUEL QUANTITY PROBE
MTH 30-Apr-1983 O/C
1557D
391046-218RIGHT WING
284003
9912019-8 *CF
SECTION (61.00) FUEL QUANTITY PROBE
MTH 30-Apr-1983 O/C
2415D
391046-219LEFT WING
284004
9912019-7 *CF
SECTION (129.00) FUEL QUANTITY PROBE
MTH 30-Apr-1983 O/C
2425D
391046-219RIGHT WING
284004
9912019-7 *CF
SECTION (129.00) FUEL QUANTITY PROBE
MTH 30-Apr-1983 O/C
2502D
391046-220LEFT WING
284005
9912019-6 *CF
SECTION (171.50) FUEL QUANTITY PROBE
MTH 30-Apr-1983 O/C
2521D
391046-220RIGHT WING
284005
9912019-6 *CF
SECTION (171.50) FUEL QUANTITY PROBE
MTH 30-Apr-1983 O/C
2478D
391046-221LEFT WING
284006
9912019-5 *CF
SECTION (211.00) FUEL QUANTITY PROBE
MTH 30-Apr-1983 O/C
2419D
391046-221RIGHT WING
284006
9912019-5 *CF
SECTION (211.00) FUEL QUANTITY PROBE
Page 12 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
3999
11-Apr-1997
0O/C
SN-UNKNOWN
7140-5291001
9912052-12 SJC
HYDRAULIC RESERVOIR
HRS
MTH
6125
09-Oct-2008
0O/C
097
SI360-686-1
291002W : L
NO. 1 ENGINE
291002 UVAHYDRAULIC PUMP
LDG
HRS
MTH
4464
6459.6
14-Sep-2012
0O/C
110
SI360-686-1
291002W : R
NO. 2 ENGINE
291002 CYHMHYDRAULIC PUMP
MTH 30-Apr-1983 O/C1656
3520020100-4
LEFT
291005
9912194-3 *CF
HYDRAULIC W/FLW DET CHECK VALVE
MTH 30-Apr-1983 O/C1637
3520020100-4
RIGHT
291005
9912194-3 *CF
HYDRAULIC W/FLW DET CHECK VALVE
MTH 30-Apr-1983 O/C1173
2710971291012
- *CF
OPEN CENTER BYPASS VALVE
LDG
HRS
MTH
4495
6510.8
01-Mar-2013
0
0O/CNAE5780
25S-7D5059-07
LEFT WING
301001 KCAKDE-ICE BOOT
HRS
MTH
6148
19-Mar-2009
0O/C
MZFY420
25S-7D5059-08
RIGHT WING
301002 CAKDE-ICE BOOT
HRS
MTH
6148
19-Mar-2009
0O/C
MAHC380
29S-7D5059-13LEFT
301003
CAK
HORIZONTAL STABILIZER DE-ICE BOOT
HRS
MTH
6148
19-Mar-2009
0O/C
MAHC390
29S-7D5059-13RIGHT
301003
CAK
HORIZONTAL STABILIZER DE-ICE BOOT
HRS
MTH
6148
19-Mar-2009
0O/C
MAJY710
25S-7D5059-05
VERTICALSTABILIZER
301004 CAKDE-ICE BOOT
MTH 30-Apr-1983 O/C505
2E1469-1
LEFT
301005
9912081-7
*CFANTI-ICE ELEMENT
MTH 30-Apr-1983 O/C533
2E1469-8
RIGHT
301006
9912081-8
*CFANTI-ICE ELEMENT
MTH 30-Apr-1983 O/C1885
1106P55
AFT
301007
*CF
DE-ICE PRESSURE SWITCH
MTH 30-Apr-1983 O/C1887
1106P55
FORWARD
301007
*CF
DE-ICE PRESSURE SWITCH
MTH 30-Apr-1983 O/C5774
3D2314-62
LEFT WING
301008 *CFDE-ICE VALVE
MTH 30-Apr-1983 O/C5788
3D2314-62
RIGHT WING
301008 *CFDE-ICE VALVE
MTH 30-Apr-1983 O/C5794
3D2314-62301008
*CF
STABILIZER AND FIN DE-ICE VALVE
MTH 30-Apr-1983 O/C914
76-1A301009
*CF
AIRFOIL DE-ICE TIMER
MTH 30-Apr-1983 O/CSN-UNKNOWN
5528007-207
LEFT WING
301010
*CF
ANTI-ICE ASSEMBLY
MTH 30-Apr-1983 O/CSN-UNKNOWN
5528007-208
RIGHT WING
301010
*CF
ANTI-ICE ASSEMBLY
HRS
MTH
3024
03-Sep-1993
0O/C
U0160
3E1870-01
RIGHT
301013
9912106-1 FMN
ANTI-ICE TEMPERATURE CONTROL
HRS
MTH
6125
18-Dec-2008
0O/C
0063
5573-00-1
LEFT
302001
UVA
INLET ANTI-ICE VALVE --
Page 13 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
6125
18-Dec-2008
0O/C
0062
5573-00-1
RIGHT
302001
UVA
INLET ANTI-ICE VALVE --
MTH 30-Apr-1983 O/CSN-UNKNOWN
476411302001 *CFALCOHOL PUMP
MTH 30-Apr-1983 O/CSN-UNKNOWN
85300302002
*CF
BLEED AIR CHECK VALVE
HRS
MTH
5885
24-Oct-2006
665O/C
0168
226395
LEFT
302003
9912086-1 YHM
ANTI-ICE SOLENOID VALVE
HRS
MTH
5885
24-Oct-2006
0O/C
157452
1946-00-16
RIGHT
302003
9912402-16 YHM
ANTI-ICE SOLENOID VALVE
HRS
MTH
3937
24-Jan-1997
0O/C
SN-UNKNOWN
21548-2-19-6
NO. 2 ENGINE
302004 SJCANTI-ICE SWITCH
MTH 30-Apr-1983 O/CSN-UNKNOWN
PH502
LEFT
303001 *CFPITOT TUBE
MTH 30-Apr-1983 O/CSN-UNKNOWN
PH502
RIGHT
303001 *CFPITOT TUBE
MTH 30-Apr-1983 O/CSN-UNKNOWN
CM2933-7
LEFT LOWER
303002 *CFPILOT STATIC PORT
MTH 30-Apr-1983 O/CSN-UNKNOWN
CM2933-7
RIGHT LOWER
303002
*CF
COPILOT STATIC PORT
MTH 30-Apr-1983 O/CSN-UNKNOWN
CM2933-7
LEFT UPPER
303003
*CF
COPILOT STATIC PORT
MTH 30-Apr-1983 O/CSN-UNKNOWN
CM2933-7
RIGHT UPPER
303003 *CFPILOT STATIC PORT
MTH 30-Apr-1983 O/C1225
1169-1304001
*CF
HOT AIR TEMPERATURE MONITOR-
MTH 30-Apr-1983 O/C4J0079
27241287304005
9912085-1 *CF
TEMPERATURE CONTROL VALVE
MTH 30-Apr-1983 O/C4J0043
27231272304006
9912085-2 *CF
TEMPERATURE CONTROLLER
MTH 30-Apr-1983 O/C0J0267
27221274
LEFT
304007
9912085-3 *CF
TEMPERATURE SENSOR
MTH 30-Apr-1983 O/C910
1115P25304008 *CFPRESSURE SWITCH
MTH 30-Apr-1983 O/C
629
226395-1
304009
9912086-2 *CF
WINDSHIELD ANTI-ICE BLEED AIR SOLENOID VALVE
HRS
MTH
3061
22-Oct-1993 0O/CSN-UNKNOWN
811-BATT-1
LEFT
312002 FMNCLOCK BATTERY
HRS
MTH
3061
22-Oct-1993
9O/C
SN-UNKNOWN
C664503-0102313001
15136 FMN
FLIGHT HOUR METER
HRS
MTH
4487
09-Mar-1999
0O/C
008175
7000992313003
AG-222
SJCACCELEROMETER
HRS
MTH
6125
18-Dec-2008
0O/C
85267084900001
85-267-1313005
UVA
DATA ACQUISITION UNIT --
HRS
MTH
6125
18-Dec-2008
0O/C
0449003
84-142-1
LEFT
313006
UVA
ENGINE DISPLAY UNIT --
HRS
MTH
6125
18-Dec-2008
0O/C
0440007
84-142-1
RIGHT
313006
UVA
ENGINE DISPLAY UNIT --
Page 14 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/C166
6541000-27
LEFT MAINLANDING GEAR
321001 *CFASSEMBLY
MTH 30-Apr-1983 O/C166
6541000-28
RIGHT MAINLANDING GEAR
321002 *CFASSEMBLY
LDG
MTH
0
30-Apr-1983
0410001140
5542000-7
41000 36065NOSE GEAR
322001 *CFASSEMBLY
HRS
MTH
5719
25-Nov-2005 O/C700-11X
5543001-11
NOSE LANDINGGEAR
322002 YHMSHIMMY DAMPER
MTH 30-Apr-1983 O/CSN-UNKNOWN
5542300-1
NOSE LANDINGGEAR
322004 *CFFORK
MTH 30-Apr-1983 O/CSN-UNKNOWN
5511169-1
NOSE LANDINGGEAR
322005 *CFACTUATOR FITTING
LDG
HRS
MTH
3725
4870
16-Apr-2001
022500
SN-UNKNOWN
5513056-5
26225 21290
LEFT NOSELANDING GEAR
322006
SJC
TRUNNION SUPPORT ASSEMBLY
LDG
HRS
MTH
3725
4870
16-Apr-2001
022500
SN-UNKNOWN
5513056-6
26225 21290
RIGHT NOSELANDING GEAR
322006
SJC
TRUNNION SUPPORT ASSEMBLY
LDG
MTH
0
30-Apr-1983
022500SN-UNKNOWN
5542301-5
22500 17565NOSE LANDINGGEAR
322007 *CFTRUNION
LDG
MTH
0
30-Apr-1983
191541600SN-UNKNOWN
5541205-3
41600 36665LEFT MAIN GEAR
322008
*CF 1915
TRUNNION ATTACH PIN
LDG
MTH
0
30-Apr-1983
191541600SN-UNKNOWN
5541205-4
41600 36665RIGHT MAIN GEAR
322008
*CF 1915
TRUNNION ATTACH PIN
LDG
MTH
0
30-Apr-1983
191541600SN-UNKNOWN
6527213-2
41600 36665LEFT MAIN GEAR
322009 *CF
1915
ACTUATOR PIN
LDG
MTH
0
30-Apr-1983
191541600SN-UNKNOWN
6527213-2
41600 36665RIGHT MAIN GEAR
322009 *CF
1915
ACTUATOR PIN
LDG
HRS
MTH
3246
3708
16-Jan-1996
028600
SN-UNKNOWN
6541204-5
31846 26911
LEFT MAIN GEAR
322010
SJC
ACTUATOR ATTACH STUD
LDG
HRS
MTH
3246
3708
16-Jan-1996
028600
SN-UNKNOWN
6541204-5
31846 26911
RIGHT MAIN GEAR
322010
SJC
ACTUATOR ATTACH STUD
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541306-4
28600 23665LEFT MAIN GEAR
322011 *CF
1915
TRUNNION
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541306-4
28600 23665RIGHT MAIN GEAR
322011 *CF
1915
TRUNNION
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
6541200-1
28600 23665LEFT MAIN GEAR
322012 *CF
1915
AXLE
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
6541200-1
28600 23665RIGHT MAIN GEAR
322012 *CF
1915
AXLE
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541310-3
28600 23665LEFT MAIN GEAR
322013
*CF 1915
UPPER PISTON BEARING
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541310-3
28600 23665RIGHT MAIN GEAR
322013
*CF 1915
UPPER PISTON BEARING
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541304-9
28600 23665LEFT MAIN GEAR
322014
*CF 1915
UPPER TORQUE LINK
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541304-10
28600 23665RIGHT MAIN GEAR
322014
*CF 1915
UPPER TORQUE LINK
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541304-11
28600 23665LEFT MAIN GEAR
322015
*CF 1915
LOWER TORQUE LINK
Page 15 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
MTH
0
30-Apr-1983
191541600SN-UNKNOWN
5541304-6
41600 36665322015L : RL
RIGHT MAIN GEAR
322015
*CF 1915
LOWER TORQUE LINK
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
6541212-2
28600 23665LEFT MAIN GEAR
322016
*CF 1915
TORQUE LINK SHAFT
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
6541212-2
28600 23665RIGHT MAIN GEAR
322016
*CF 1915
TORQUE LINK SHAFT
LDG
MTH
0
30-Apr-1983
191541600SN-UNKNOWN
5541220-2
41600 36665LEFT MAIN GEAR
322017 *CF
1915
TORQUE LINK BOLT
LDG
MTH
0
30-Apr-1983
191541600SN-UNKNOWN
5541220-2
41600 36665RIGHT MAIN GEAR
322017 *CF
1915
TORQUE LINK BOLT
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
MS17825-8
28600 23665LEFT MAIN GEAR
322018 *CF
1915
TORQUE LINK NUT
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
MS17825-8
28600 23665RIGHT MAIN GEAR
322018 *CF
1915
TORQUE LINK NUT
MTH 30-Apr-1983 O/CSN-UNKNOWN
5542105-3
NOSE GEAR
322019 *CFPISTON ASSEMBLY
LDG
MTH
0
30-Apr-1983
191522500SN-UNKNOWN
5542100-3
22500 17565NOSE GEAR
322020
*CF 1915
CYLINDER BRAZE ASSEMBLY
LDG
MTH
0
30-Apr-1983
191522500SN-UNKNOWN
5542223-1
22500 17565NOSE GEAR
322021 *CF
1915
AXLE SPACER
LDG
MTH
0
30-Apr-1983
191522500SN-UNKNOWN
5542208-3
22500 17565NOSE GEAR
322022
*CF 1915
TORQUE LINK SHAFT
LDG
HRS
MTH
4012
5085
26-Apr-2002
037500
DA873
2-7442-1
41512 36577
LEFT MAINLANDING GEAR
323001
9912053-17 SJC
ACTUATOR ASSEMBLY
LDG
HRS
MTH
4012
5085
26-Apr-2002
037500
DA103
2-7442-2
41512 36577
RIGHT MAINLANDING GEAR
323002
9912053-18 SJC
ACTUATOR ASSEMBLY
LDG
HRS
MTH
4012
5085
26-Apr-2002
88332600
49B
1523200-1
35729 30794
NOSE LANDINGGEAR
323003
9912063-13 SJC
ACTUATOR ASSEMBLY
MTH 30-Apr-1983 O/C140
5527504-2
LEFT MAINLANDING GEAR
323004 *CFUPLOCK ACTUATOR
MTH 30-Apr-1983 O/C108
5527504-2
NOSE LANDINGGEAR
323004 *CFUPLOCK ACTUATOR
HRS
MTH
5719
25-Nov-2005 O/CWMP126
5527504-2
RIGHT MAINLANDING GEAR
323004 YHMUPLOCK ACTUATOR
LDG
HRS
MTH
4935
7180.4
07-Apr-2021 1141802159
23111321 31-Oct-2026 66 m 18 d323006
9912103-1 UNK
EMERGENCY GEAR AIR BOTTLE
MTH 30-Apr-1983 O/C1199
2710969323007
*CF
LANDING GEAR CONTROL VALVE
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541320-4
28600 23665RIGHT MAINLANDING GEAR
323008
*CF 1915
CYLINDER ASSEMBLY
LDG
MTH
0
30-Apr-1983
191528600SN-UNKNOWN
5541320-3
28600 23665LEFT MAINLANDING GEAR
323014
*CF 1915
CYLINDER ASSEMBLY
LDG
HRS
MTH
3552
4215
14-Jan-1998
017200
27
6541000-41
20752 15817
LEFT MAINLANDING GEAR
323018
SJC
PISTON BRAZE OR WELD ASSEMBLY
LDG
HRS
MTH
3552
4215
14-Jan-1998
017200
19
6541000-42
20752 15817
RIGHT MAINLANDING GEAR
323018
SJC
PISTON BRAZE OR WELD ASSEMBLY
MTH 30-Apr-1983 0O/CSN-UNKNOWN
2341128323019
*CF
EMERGENCY AIR BOTTLE GAGE
Page 16 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4506
6534.3
17-Apr-2013 O/C3088
3-1490-1
LEFT MAINLANDING GEAR
324001
9912222-11
CYHMWHEEL ASSEMBLY
LDG
HRS
MTH
4506
6534.3
17-Apr-2013 O/C3092
3-1490-1
RIGHT MAINLANDING GEAR
324001
9912222-11
CYHMWHEEL ASSEMBLY
LDG
HRS
MTH
4076
5885
24-Oct-2006
0
O/C93117544
9544207-7
NOSE LANDINGGEAR
324002 YHMWHEEL ASSEMBLY
LDG
HRS
MTH
4767
6938.7
07-Apr-2017
0
0
12O/C0681
2-1528-6
LEFT MAINLANDING GEAR
324003
9912246-27
UNKBRAKE ASSEMBLY
LDG
HRS
MTH
4767
6938.7
07-Apr-2017
0
0
12O/C0403R
2-1528-6
RIGHT MAINLANDING GEAR
324004
9912246-27
UNKBRAKE ASSEMBLY
LDG
HRS
MTH
4803
6992.5
22-Feb-2018
0
0
0O/C71122496
220K08-3
LEFT MAIN GEAR
324005 UNKTIRE
LDG
HRS
MTH
4803
6992.5
22-Feb-2018
0
0
0O/C71122104
220K08-3
RIGHT MAIN GEAR
324005 UNKTIRE
LDG
HRS
MTH
4076
5885
24-Oct-2006
0
O/C6197W00315
031-613-8
NOSE LANDINGGEAR
324006
9914070-1
YHMTIRE
MTH 30-Apr-1983 O/C2544
12A085-9
COPILOTINBOARD
324011
9912050-9 *CF
BRAKE MASTER CYLINDER
MTH 30-Apr-1983 O/C2550
12A085-9
PILOT OUTBOARD
324011
9912050-9 *CF
BRAKE MASTER CYLINDER
MTH 30-Apr-1983 O/C2508
12A085-10
COPILOTOUTBOARD
324012
9912050-10 *CF
BRAKE MASTER CYLINDER
MTH 30-Apr-1983 O/C2525
12A085-10
PILOT INBOARD
324012
9912050-10 *CF
BRAKE MASTER CYLINDER
MTH 30-Apr-1983 0O/C1008
AS20800-1324013
*CF
PARKING BRAKE VALVE
MTH 23-Mar-1995 O/C828
895232-0875324014
PDX
EMERGENCY BRAKE VALVE
MTH 30-Apr-1983 O/C653
42-547324020
*CF
ANTI SKID CONTROL BOX
MTH 30-Apr-1983 O/C679
38-581-3324021
*CF
POWER BRAKE RELAY VALVE
MTH 30-Apr-1983 O/C130
57C57640324023 *CFACCUMULATOR
MTH 30-Apr-1983 O/C1292
40-955
LEFT MAINLANDING GEAR
324024
9912305-2 *CF
WHEEL TRANSDUCER
MTH 30-Apr-1983 O/C1287
40-955
RIGHT MAINLANDING GEAR
324024
9912305-2 *CF
WHEEL TRANSDUCER
Page 17 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
5150
06-Aug-2002
0O/C
2055
MP50B1324026
SJC
POWER BRAKE MOTOR
MTH 30-Apr-1983 O/CSN-UNKNOWN
A2948326001
9910080-1 *CF
GEAR WARNING HORN
MTH 30-Apr-1983 O/C2182
D3474-13331001
9912167-13 *CF
ANNUNCIATOR PANEL
MTH 30-Apr-1983 O/C161
EM2044331011
*CF
ELECTRICAL PANEL LIGHT INVERTER
MTH 30-Apr-1983 O/CSN-UNKNOWN
1941-4331012
*CF
MASTER WARNING SWITCH
MTH 30-Apr-1983 O/C5841
40-0100-1334002
*CF
VERTICAL FIN ANTI-COLLISION LIGHT
MTH 30-Apr-1983 O/C9857
60-2799-1
LEFT
334003
9910368-2 *CF
STROBE POWER SUPPLY
HRS
MTH
5719
25-Nov-2005
0O/C
1414
60-2799-1
RIGHT
334003
9910368-2 YHM
STROBE POWER SUPPLY
MTH 30-Apr-1983 0O/CSN-UNKNOWN
24621-3335001
*CF
EMERGENCY LIGHTING BATTERY
MTH 29-Jun-2013 O/CNOT INSTALLED
PN
LEFT
341001 AIRSPEED INDICATOR
MTH 29-Jun-2013 O/CNOT INSTALLED
PN
RIGHT
341001 AIRSPEED INDICATOR
MTH 29-Jun-2013 O/CNOT INSTALLED
PN
PILOT
341002 ALTIMETER
HRS
MTH
6125
18-Dec-2008
0O/C
06143
5518108-7341006
UVA
OVERSPEED WARNING HORN
HRS
MTH
4880
26-Apr-2001
0O/C
PC2049
SLZ9686-1341010
SJC
ANGLE OF ATTACK INDICATOR
MTH 30-Apr-1983 O/CSN-UNKNOWN
MOD202-5K341012
*CF
ANGLE OF ATTACK POTENTIOMETER
MTH 30-Apr-1983 O/CU1499C
SLZ9386341013
*CF
ANGLE OF ATTACK TRANSMITTER
MTH 30-Apr-1983 O/CSN-UNKNOWN
SLZ9374341014
*CF
ANGLE OF ATTACK INDEXER
MTH 30-Apr-1983 O/C021968
7000839-903
RIGHT
341021
*CF
RADIO ALTIMETER IND --
LDG
HRS
MTH
4803
6992.5
02-Mar-2018 O/C1732512
GB300NA161341036
9910095-6
BAROMATIC. PRESSURE SWITCH
MTH 30-Apr-1983 O/CSN-UNKNOWN
C660501-0301342001
*CF
MAGNETIC COMPASS
MTH 30-Apr-1983 O/C123881
4018369-905
NO. 1
342041
FZ-500 *CF
FLIGHT DIRECTOR COMPUTER
MTH 30-Apr-1983 O/C111208
4020570-901
RIGHT
342042
MS-205 *CF
AP/FD MODE SELECTOR
MTH 30-Apr-1983 O/C071777
7000622-901
NO. 1
342043
VG-14A
*CFVERTICAL GYRO
LDG
HRS
MTH
4511
6539.8
29-Jun-2013 O/C1SW005959
011-01110-01
NO. 1
342048
UVA
AIR DATA COMPUTER
Page 18 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4511
6539.8
29-Jun-2013 O/C1SW005986
011-01110-01
NO. 2
342048
UVA
AIR DATA COMPUTER
HRS
MTH
3962
03-Mar-1997
0O/C
90074660
4020577-3
LEFT
342049
C-14D SJC
DIR GYRO SYN COMPASS
MTH 30-Apr-1983 O/C097112
2593379-1342052
CS-412 *CF
DUAL REMOTE COMPENSATOR
MTH 30-Apr-1983 O/C121558
7000469-901
NO. 2
342053
RD-650A
*CFHSI INDICATOR
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C88957245
011-00972-10
NO. 1
343000 KUVANO. 1 GDU (PFD)
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C88957247
011-00972-10
NO. 2
343000 KUVANO. 2 GDU (PFD)
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C14Z005324
011-01440-40
NO. 3
343000 KUVANO. 3 GDU MFD
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C6324
305-468-00
NO. 1
343001 KUVANO. 1 FAN COCKPIT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C6333
305-468-00
NO. 2
343001 KUVANO. 2 FAN COCKPIT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C6336
305-468-00
NO. 3
343001 KUVANO. 3 FAN COCKPIT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/CIHQ008296
011-01105-20
NO. 1
343002 KUVANO. 1 GIA 63W
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/CIHQ008321
011-01105-20
NO. 2
343002 KUVANO. 2 GIA 63W
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C17107502
011-01257-20
NO. 1
343003
KUVA
NO. 1 GMA AUDIO PANEL
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C17107508
011-01257-20
NO. 2
343003
KUVA
NO. 2 GMA AUDIO PANEL
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C2225
962830-3A343004 KUVAADC 2000
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C42023569
011-00868-10
NO. 1
343005 KUVANO. 1 GRS 77 AHRS
Page 19 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C42023570
011-00868-10
NO. 2
343005 KUVANO. 2 GRS 77 AHRS
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C1SW005959
011-01110-01
NO. 1
343006 KUVANO. 1 GDC 74B ADC
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C1SW005986
011-01110-01
NO. 2
343006 KUVANO. 2 GDC 74B ADC
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/CICM010146
011-00870-00
NO. 1
343007 KUVANO. 1 GMU 44 MAGS
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/CICM010147
011-00870-00
NO. 2
343007 KUVANO. 2 GMU 44 MAGS
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C47922777
011-00978-00
NO. 1
343008 KUVANO. 1 GTP59 OAT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C47922783
011-00978-00
NO. 2
343008 KUVANO. 2 GTP59 OAT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C47204498
011-00883-20343009 KUVAGWX 68 RADAR
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C84810509
011-00779-21
NO. 1
343010 KUVANO. 1 GTX 33D
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C84810516
011-00779-21
NO. 2
343010 KUVANO. 2 GTX 33D
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C131430
DMNI-50-2
TOP LEFT
343011
KUVA
TRANS. ANTENNA TOP LEFT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C132432
DMNI-50-2
TOP RIGHT
343011
KUVA
TRANS. ANTENNA TOP RIGHT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C293
04060002-21343012 KUVAADC 602 SKYLIGHT
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C1786
9200-32500-0021
#2
343013
KUVA
#2 ESI 2000 STDBY INDICATOR
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C1784
9200-32500-0021343013
KUVA
#1 ESI 2000 STDBY INDICATOR
Page 20 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C17837
1049-4000-03343014 KUVAGDC 31
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C5510
071-1055-00343015 KUVAKA 52
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C1EA005495
011-01446-00343017 KUVAGTS 820
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C140050745
011-01347-00343018
KUVA
GPA 65 POWER AMP
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C124009093
011-01346-00
BOTTOM
343019
KUVA
GA 58 ANTENNA BOTTOM
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C124009091
011-01346-00
TOP
343019
KUVA
GA 58 ANTENNA TOP
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C10077
305467-00
NO. 1
343020 KUVANO. 1 FAN NOSE
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C10078
305467-00
NO. 2
343020 KUVANO. 2 FAN NOSE
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C47708192
011-00986-00343021 KUVAGDL69
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C10757
013-00245-00343022 KUVAGA37 ANTENNA
LDG
HRS
MTH
4511
6539.8
29-Jun-2013
0
0
0O/C8951
013-00244-00343023 KUVAGA36 ANTENNA
MTH 30-Apr-1983 O/C1308
MI585343344002
DI-4002 *CF
RADAR INDICATOR SCREEN
MTH 30-Apr-1983 O/C
3542
MI585200
344004
RT-4001 *CF
WEATHER RADAR RECEIVER/TRANSMITTER
MTH 30-Apr-1983 O/C3463
MI585202344005
AP-4001 *CF
WEATHER RADAR ANTENNA
MTH 30-Apr-1983 O/C084485
4004437-901344022
RT-220 *CF
RADIO ALTIMETER TRANSCEIVER
MTH 30-Apr-1983 O/C091918
4010504
AFT
344023
AT-224 *CF
RADIO ALTITUDE ANTENNA
MTH 30-Apr-1983 O/C091914
4010504
FORWARD
344023
AT-224 *CF
RADIO ALTITUDE ANTENNA
MTH 30-Apr-1983 O/C19117
DMN4-17-1B345010 *CFNAV ANTENNA KIT
Page 21 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/C12569
622-2362-001
NO. 2
345011
ADF-60A
*CFADF RECEIVER
HRS
MTH
3144
13-Jan-1994
0O/C
29801
622-2363-001
NO. 1
345014
APA-80 ICT
ADF LOOP ANTENNA
MTH 30-Apr-1983 O/C12536
622-2363-001
NO. 2
345014
APA-80 *CF
ADF LOOP ANTENNA
MTH 30-Apr-1983 O/CSN-UNKNOWN
16D00400-2345017
*CF
MARKER BEACON ANTENNA
MTH 30-Apr-1983 O/C8719
RGS1048345018
*CF
GLIDESLOPE ANTENNA
MTH 30-Apr-1983 O/C22952
622-0876-001
BOTTOM
345032
VIR-30 *CF
NO. 2 NAVIGATION RECEIVER
MTH 30-Apr-1983 O/C23648
622-0876-001
TOP
345032
VIR-30 *CF
NO. 1 NAVIGATION RECEIVER
LDG
HRS
MTH
4511
6539.8
29-Jun-2013 O/C84810509
011-00779-21
NO. 1
345034 UVAATC TRANSPONDER
LDG
HRS
MTH
4511
6539.8
29-Jun-2013 O/C84810516
011-00779-21
NO. 2
345034 UVAATC TRANSPONDER
MTH 30-Apr-1983 O/C3839
622-2012-201
NO. 1
345035 *CFDME INDICATOR
MTH 30-Apr-1983 O/C1981
11444-1345042
*CF
VLF LOOP COUPLER --
MTH 30-Apr-1983 O/C5027
11455-2345053 *CFVLF ANTENNA
MTH 30-Apr-1983 O/C1684
11600-2345054
*CF
VLF CONTROL DISPLAY
MTH 30-Apr-1983 O/C891
10070-1345055
*CF
VLF COURSE DEVIATION INDICATOR
MTH 30-Apr-1983 O/C2810
10050-3-3B1345056
*CF
VLF RECEIVER COMPUTER UNIT
MTH 30-Apr-1983 O/C3497
10600-2-202345057
*CF
VLF OPERATIONAL EQUIPMENT UNIT
HRS
MTH
3104
03-Dec-1993
0O/C
SN-UNKNOWN
066-04031-0211345132
KLN-90 GJT
GPS RECEIVER/ SENSOR
MTH 30-Apr-1983 0O/C4351
C668512-0101351001
MD-97 *CF
OXYGEN PRESSURE GAUGE
LDG
HRS
MTH
4823
7016.9
04-Jul-2018
0
0
072119784
MC10-16-101 31-Jul-2024 39 m 18 dCOPILOT
351004 UNKOXYGEN MASK
LDG
HRS
MTH
4823
7016.9
04-Jul-2018
0
0
072116569
MC10-16-101 31-Jul-2024 39 m 18 dPILOT
351004 UNKOXYGEN MASK
MTH 30-Apr-1983 0O/C5809
ZR807351005
9912057-2 *CF
OXYGEN REGULATOR
LDG
HRS
MTH
4922
7169.8
15-May-2020 152288K906486
176126-64 30-Sep-2031 125 m 17 d351006
ZC369-64
UNKOXYGEN CYLINDER
LDG
HRS
MTH
4515
6544
10-Jul-2013 O/CNA
MJV3361001
UVA
DOOR SEAL CONTROL VALVE
MTH 30-Apr-1983 O/C1196U
38E85-5C361003
9912043-2 *CF
DEICE BOOT REGULATOR
Page 22 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/C
SN-UNKNOWN
2102702-5
361004
*CF
PNUEMATIC (BLEED AIR) PRESSURE REGULATOR
HRS
MTH
6125
09-Oct-2008
0O/C
0099
5404-00-1
LEFT
361004W
UVA
REGULATOR BA PRESS --
HRS
MTH
6125
09-Oct-2008
0O/C
0096
5404-00-1
RIGHT
361004W
UVA
REGULATOR BA PRESS --
HRS
MTH
6125
09-Oct-2008
0O/C
0084
5473-00-1
LEFT
361005W
UVA
PRESSURE CONTROL VALVE --
HRS
MTH
6125
09-Oct-2008
0O/C
0098
5473-00-1
RIGHT
361005W
UVA
PRESSURE CONTROL VALVE --
HRS
MTH
5556
04-Jun-2004
0O/C
1AY5
3H64-4
BOTTOM
361006 INSTRUMENT PRESSURE REGULATOR
HRS
MTH
5556
04-Jun-2004
0O/C
10AW8
3H64-4
TOP
361006 INSTRUMENT PRESSURE REGULATOR
HRS
MTH
6125
09-Oct-2008
0O/C
GO22876
6607A5-99
LEFT
361006W
UVA
PNEUMATIC PRESSURE SWITCH --
HRS
MTH
6125
09-Oct-2008
0O/C
FO30182
6607A5-99
RIGHT
361006W
UVA
PNEUMATIC PRESSURE SWITCH --
MTH 30-Apr-1983 O/CSN-UNKNOWN
CM2939-4-15361007
*CF
PRESSURE DOOR SEAL HOSE
HRS
MTH
6125
18-Dec-2008
0O/C
6BD14
1H95-1
LEFT
361008 UVACHECK VALVE
LDG
HRS
MTH
4370
6324.9
19-Dec-2010
0
0O/C7BF4
1H95-1
RIGHT
361008 CYHMCHECK VALVE
HRS
MTH
3338
14-Sep-1994
0O/C
SN-UNKNOWN
S15501-1
CABIN
521001
9912075-4
SMFDOOR SEAL
HRS
MTH
5484
12-Feb-2004
0O/C
SN-UNKNOWN
S-17563-2521002
SJC
EMERGENCY EXIT SEAL
MTH 30-Apr-1983 O/C387
6519009-33
CABIN
526001 *CFDOOR STEP
HRS
MTH
6125
18-Dec-2008
0O/C
9554
E149000-101
LEFT MAIN
561001
9912064-15 UVA
WINDSHIELD ASSY, (LH)
MTH 30-Apr-1983 O/C116034
CES-507-018-0
RIGHT MAIN
561002
9912064-8 *CF
WINDSHIELD ASSY, (LH)
MTH 30-Apr-1983 O/CSN-UNKNOWN
5511275-7561003
*CF
FOUL WEATHER WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5511285-6
COPILOTINBOARD
561005 *CFWINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5511285-4
COPILOTOUTBOARD
561005 *CFWINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5511285-5
PILOT INBOARD
561005 *CFWINDOW
Page 23 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/CSN-UNKNOWN
5511285-3
PILOT OUTBOARD
561005 *CFWINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-5
LEFT AFT
562001 *CFCABIN WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-5
LEFT CENTER AFT
562001 *CFCABIN WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-5
LEFT CENTERFORWARD
562001 *CFCABIN WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-6
LEFT FORWARD
562001
*CF
CABIN MAIN DOOR WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-5
RIGHT AFT
562001 *CFCABIN WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-5
RIGHT CENTERAFT
562001 *CFCABIN WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-5
RIGHT CENTERFORWARD
562001 *CFCABIN WINDOW
MTH 30-Apr-1983 O/CSN-UNKNOWN
5591005-5
RIGHT FORWARD
562001
*CF
CABIN EMERGENCY DOOR WINDOW
LDG
MTH
0
30-Apr-1983
020000SN-UNKNOWN
5522700-1
20000 15065LEFT FORWARD
572001
*CF
TRUNNION FITTING ASSEMBLY
LDG
MTH
0
30-Apr-1983
020000SN-UNKNOWN
5522700-2
20000 15065RIGHT FORWARD
572002
*CF
TRUNNION FITTING ASSEMBLY
LDG
MTH
0
30-Apr-1983
041600SN-UNKNOWN
5522710-11
41600 36665LEFT AFT
574001
*CF
TRUNNION FITTING ASSEMBLY
LDG
MTH
0
30-Apr-1983
041600SN-UNKNOWN
5522710-12
41600 36665RIGHT AFT
574002
*CF
TRUNNION FITTING ASSEMBLY
MTH 30-Apr-1983 O/CSN-UNKNOWN
5522720-1
LEFT
574003
*CF
SIDEBRACE FITTING ASSEMBLY
MTH 30-Apr-1983 O/CSN-UNKNOWN
5522720-2
RIGHT
574004
*CF
SIDEBRACE FITTING ASSEMBLY
MTH 30-Apr-1983 O/CSN-UNKNOWN
5555030-18
LEFT ENGINE
710002
*CF
BY-PASS NOZZLE ASSEMBLY
MTH 30-Apr-1983 O/CSN-UNKNOWN
5555030-18
RIGHT ENGINE
710002
*CF
BY-PASS NOZZLE ASSEMBLY
HRS
MTH
6125
18-Dec-2008
03500NSN
SI360-161-3
9625 2444.6LEFT ENGINE AFT
712001 UVAISOLATOR MOUNT
HRS
MTH
6125
18-Dec-2008
03500NSN
SI360-161-3
9625 2444.6RIGHT ENGINEAFT
712001 UVAISOLATOR MOUNT
HRS
MTH
6125
18-Dec-2008
035000203
96094-01
9625 2444.6LEFT ENGINEFORWARDBOTTOM
712002 UVAISOLATOR MOUNT
HRS
MTH
6125
18-Dec-2008
035000201
96094-01
9625 2444.6LEFT ENGINEFORWARD TOP
712002 UVAISOLATOR MOUNT
HRS
MTH
6125
18-Dec-2008
035000200
96094-01
9625 2444.6RIGHT ENGINEFORWARDBOTTOM
712002 UVAISOLATOR MOUNT
HRS
MTH
6125
18-Dec-2008
035000202
96094-01
9625 2444.6RIGHT ENGINEFORWARD TOP
712002 UVAISOLATOR MOUNT
HRS
MTH
6125
09-Oct-2008
0E/C
116077
56000-104
710001 : E1**L
NO. 1
71EN1
FJ44-2A
UVAENGINE
Page 24 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
6125
09-Oct-2008
0E/C
116076
56000-104
710001 : E2**R
NO. 2
71EN2
FJ44-2A
UVAENGINE
HRS
MTH
6125
18-Dec-2008
0O/C
LH2A0717
89954ASSY111E9114G703E1
710002W
UVA
ENGINE COMPUTER --
HRS
MTH
6125
18-Dec-2008
0O/C
LH2A0733
89954ASSY111E9114G703E2
710002W
UVA
ENGINE COMPUTER --
HRS
MTH
6125
09-Oct-2008
0O/C
AU21150
72165
E1
720007W
UVA
NOZZLE-1ST LP TURBINE --
HRS
MTH
6125
09-Oct-2008
0O/C
AU21147
72165
E2
720007W
UVA
NOZZLE-1ST LP TURBINE --
LDG
HRS
MTH
4228
6125
09-Oct-2008
010000
AU21288
65502
(10000)14228 9293
E1
723001 UVAFAN ROTOR
LDG
HRS
MTH
4226
6125
09-Oct-2008
010000
AU21306
65502
(10000)14226 9291
E2
723001 UVAFAN ROTOR
LDG
HRS
MTH
4228
6125
09-Oct-2008
06000
HW29927
61964
(8000)12228 7293
E1
723010
UVA
2000
HP COMPRESSOR ROTOR
LDG
HRS
MTH
4226
6125
09-Oct-2008
06000
HW29099
61964
(8000)12226 7291
E2
723010
UVA
2000
HP COMPRESSOR ROTOR
HRS
MTH
6125
09-Oct-2008 O/CHW29451
69986
E1
723015
UVA
IP COMPRESSOR ROTOR
HRS
MTH
6125
09-Oct-2008 O/CHW27925
69986
E2
723015
UVA
IP COMPRESSOR ROTOR
HRS
MTH
6125
09-Oct-2008
0O/C
AU20867
110164
E1
723022
UVA
DIFFUSER CASE ASSEMBLY
HRS
MTH
6125
09-Oct-2008
0O/C
AU20863
110164
E2
723022
UVA
DIFFUSER CASE ASSEMBLY
HRS
MTH
6125
09-Oct-2008
0O/C
RX07RT1801
64711
E1
723061
UVA
HIGH PRESSURE SHAFT
HRS
MTH
6125
09-Oct-2008
0O/C
RX07RT1913
64711
E2
723061
UVA
HIGH PRESSURE SHAFT
HRS
MTH
6125
09-Oct-2008
0O/C
RX07TN31
110697
E1
723092
UVA
COMPLETE LP SHAFT ASSEMBLY
HRS
MTH
6125
09-Oct-2008
0O/C
RX07TN0032
110697
E2
723092
UVA
COMPLETE LP SHAFT ASSEMBLY
HRS
MTH
6125
09-Oct-2008
0O/C
AU21287
55608
E1
724045
280 UVA
SEAL AND FUEL SLINGER ASSEMBLY
HRS
MTH
6125
09-Oct-2008
0O/C
AU21285
55608
E2
724045
280 UVA
SEAL AND FUEL SLINGER ASSEMBLY
LDG
HRS
MTH
4228
6125
09-Oct-2008
0
0
8000
HW29550
67093
(8000)12228 7293
E1
725010 UVAHP TURBINE DISK
Page 25 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4226
6125
09-Oct-2008
0
0
8000
HW29546
67093
(8000)12226 7291
E2
725010 UVAHP TURBINE DISK
LDG
HRS
MTH
4228
6125
09-Oct-2008
010000
HW28997
72037
(10000)14228 9293
E1
725020
UVA
1ST LP TURBINE DISK
LDG
HRS
MTH
4226
6125
09-Oct-2008
010000
HW29786
72037
(10000)14226 9291
E2
725020
UVA
1ST LP TURBINE DISK
LDG
HRS
MTH
4228
6125
09-Oct-2008
010000
HW29056
66993
(10000)14228 9293
E1
725030
UVA
2ND LP TURBINE DISK
LDG
HRS
MTH
4226
6125
09-Oct-2008
010000
HW29847
66993
(10000)14226 9291
E2
725030
UVA
2ND LP TURBINE DISK
HRS
MTH
6125
09-Oct-2008
0O/C
HW29550
73458
E1
725102W
UVA
ROTOR ASSY-HP TURBIN --
HRS
MTH
6125
09-Oct-2008
0O/C
HW29546
73458
E2
725102W
UVA
ROTOR ASSY-HP TURBIN --
HRS
MTH
6125
09-Oct-2008
0O/C
AU20222
78824E1
726011
UVA
ACCESSORY DRIVE GEARBOX ASSEMBLY
HRS
MTH
6125
09-Oct-2008
0O/C
AU20224
78824E2
726011
UVA
ACCESSORY DRIVE GEARBOX ASSEMBLY
HRS
MTH
5090
31-May-2002
0O/C
20506
1103P0448
NO. 1 ENGINE
731004
9912033-2 SJC
LOW FUEL PRESSURE SWITCH
MTH 30-Apr-1983 O/CSN-UNKNOWN
1103P92
NO. 2 ENGINE
731004
9912033-1 *CF
LOW FUEL PRESSURE SWITCH
HRS
MTH
6125
18-Dec-2008
0O/C
703259
3268005-0101
NO. 1 ENGINE
733003
9912031-4
UVAFUEL FLOWMETER
HRS
MTH
6125
18-Dec-2008
0O/C
08B451
3268005-0101
NO. 2 ENGINE
733003
9912031-4
UVAFUEL FLOWMETER
LDG
HRS
MTH
4803
6992.5
17-Feb-2018 O/CBCC1CAD419
50817
E1
730002W
UNK
NOZZLE ASSEMBLY, FUEL --
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
0
0
0O/CBCC-00002924
50817
E2
730002W
UNK
NOZZLE ASSEMBLY, FUEL --
HRS
MTH
6125
09-Oct-2008
04000YYK0700
59863
(4002)10125 2944.6E1
731001 UVAFUEL PUMP
HRS
MTH
6125
09-Oct-2008
04000YYK0699
59863
(4003)10125 2944.6E2
731001 UVAFUEL PUMP
MTH 09-Oct-2008 0O/CSN-UNKNOWN
PN
E1
731046 FUEL MANIFOLD ASSEMBLY
MTH 09-Oct-2008 0O/CSN-UNKNOWN
PN
E2
731046 FUEL MANIFOLD ASSEMBLY
LDG
HRS
MTH
4423
6396.7
25-Nov-2011
0
0O/CGE4794
57847
E1
732301W
CYHM
IND-FUEL FILTER,ELEC --
Page 26 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4423
6396.7
25-Nov-2011
0
0O/CGE4799
57847
E2
732301W
CYHM
IND-FUEL FILTER,ELEC --
HRS
MTH
6125
09-Oct-2008
04000RF13444714
78186
(4002)10125 2944.6E1
732401
UVA
FUEL CONTROL (HMU) UNIT
HRS
MTH
6125
09-Oct-2008
04000RF13444715
78186
(4003)10125 2944.6E2
732401
UVA
FUEL CONTROL (HMU) UNIT
HRS
MTH
6125
09-Oct-2008
0O/C
BL17675
73489
E1 INBOARD
741010 UVAIGNITION EXCITER
HRS
MTH
6125
09-Oct-2008
0O/C
BL17726
73489
E2 INBOARD
741010 UVAIGNITION EXCITER
HRS
MTH
6125
09-Oct-2008
0O/C
BL17656
73489
E1 OUTBOARD
741020 UVAIGNITION EXCITER
HRS
MTH
6125
09-Oct-2008
0O/C
BL17658
73489
E2 OUTBOARD
741020 UVAIGNITION EXCITER
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
0
0
0O/CCK1701949
68032
E1 INBOARD
742201 UNKIGNITOR
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
0
0
0O/CCK1701948
68032
E2 INBOARD
742201 UNKIGNITOR
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
0
0
0O/CCK1701932
68032
E1 OUTBOARD
742202 UNKIGNITOR
LDG
HRS
MTH
4803
6992.5
17-Feb-2018
0
0
0O/CCK1701946
68032
E2 OUTBOARD
742202 UNKIGNITOR
MTH 30-Apr-1983 O/CSN-UNKNOWN
31A402
LEFT INBOARD
750001
9912025-4 *CF
BLEED AIR FLEX JOINT COUPLING
MTH 30-Apr-1983 O/CSN-UNKNOWN
31A402
LEFT OUTBOARD
750001
9912025-4 *CF
BLEED AIR FLEX JOINT COUPLING
MTH 30-Apr-1983 O/CSN-UNKNOWN
31A402
RIGHT INBOARD
750001
9912025-2 *CF
BLEED AIR FLEX JOINT COUPLING
MTH 30-Apr-1983 O/CSN-UNKNOWN
31A402
RIGHT OUTBOARD
750001
9912025-2 *CF
BLEED AIR FLEX JOINT COUPLING
HRS
MTH
6125
09-Oct-2008
0O/C
AU21234
69885
E1
753020
UVA
HP COMPRESSOR COVER ASSY
HRS
MTH
6125
09-Oct-2008
0O/C
AU21184
69885
E2
753020
UVA
HP COMPRESSOR COVER ASSY
MTH 30-Apr-1983 O/C
SN-UNKNOWN
5565810-1
761001
*CF
ENGINE CONTROL QUADRANT ASSEMBLY
MTH 30-Apr-1983 O/CSN-UNKNOWN
411D0315-3
NO. 1 ENGINE
761002
*CF
MAIN THROTTLE CONTROL CABLE
MTH 30-Apr-1983 O/CSN-UNKNOWN
411D0315-3
NO. 2 ENGINE
761002
*CF
MAIN THROTTLE CONTROL CABLE
MTH 30-Apr-1983 O/CSN-UNKNOWN
7-42346-1
NO. 1 ENGINE
761003
*CF
NACELLE THROTTLE CONTROL CABLE
Page 27 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 O/CSN-UNKNOWN
7-42346-2
NO. 2 ENGINE
761004
*CF
NACELLE THROTTLE CONTROL CABLE
MTH 30-Apr-1983 O/C
SN-UNKNOWN
U-183238-001
761005
9912110-1 *CF
DEPLOY INTERLOCK SOLENOID ASSEMBLY
MTH 30-Apr-1983 O/C4656
22A623
LEFT BOTTOM
771001
*CF
N2 TACH GENERATOR
HRS
MTH
3010
26-Aug-1993
0O/C
65200
22A623
LEFT TOP
771001
FMN
N1 TACH GENERATOR
MTH 30-Apr-1983 O/C7109
22A623
RIGHT BOTTOM
771001
*CF
N2 TACH GENERATOR
HRS
MTH
5719
25-Nov-2005
0O/C
89855
AG34
RIGHT TOP
771001
9912034-1 YHM
N1 TACH GENERATOR
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020978
62141
LEFT NO. 1
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020979
62141
LEFT NO. 2
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020977
62141
LEFT NO. 3
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020976
62141
LEFT NO. 4
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020980
62141
LEFT NO. 5
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020975
62141
LEFT NO. 6
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020972
62141
RIGHT NO. 1
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020973
62141
RIGHT NO. 2
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020971
62141
RIGHT NO. 3
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020970
62141
RIGHT NO. 4
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020974
62141
RIGHT NO. 5
772001W UVAITT PROBE --
HRS
MTH
6125
09-Oct-2008
0O/C
YYF020969
62141
RIGHT NO. 6
772001W UVAITT PROBE --
HRS
MTH
6125
18-Dec-2008
0O/C
LR10276
24235SOCN59715-A
LEFT
772002 UVATT2 SENSOR --
HRS
MTH
6125
18-Dec-2008
0O/C
LR10351
24235SOCN59715-A
RIGHT
772002 UVATT2 SENSOR --
HRS
MTH
6125
09-Oct-2008
0O/C
MD0118783
57355
E1
771005
UVA
N1 DUAL MAGNETIC SPEED SENSOR
Page 28 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
6125
09-Oct-2008
0O/C
MD0118781
57355
E2
771005
UVA
N1 DUAL MAGNETIC SPEED SENSOR
HRS
MTH
6125
09-Oct-2008
0O/C
MD0119197
54831
E1
771015
UVA
N2 DUAL MAGNETIC SPEED SENSOR
HRS
MTH
6125
09-Oct-2008
0O/C
MD0119199
54831
E2
771015
UVA
N2 DUAL MAGNETIC SPEED SENSOR
HRS
MTH
6125
18-Dec-2008
0O/C
89
VSDL-OC204G793003
9912147-3 UVA
OIL PRESSURE INDICATOR
HRS
MTH
6125
18-Dec-2008
0O/C
40399
123479
RIGHT ENGINE
793004
9912164-1 UVA
OIL PRESSURE TRANSMITTER
HRS
MTH
6125
18-Dec-2008
0O/C
0097
1103P1133
LEFT ENGINE
793006
UVA
LOW OIL PRESSURE SWITCH
HRS
MTH
6125
18-Dec-2008
0O/C
0099
1103P1133
RIGHT ENGINE
793006
UVA
LOW OIL PRESSURE SWITCH
HRS
MTH
6125
18-Dec-2008
0O/C
1285
10623
E1
792004
UVA
HEAT EXCHANGER --
HRS
MTH
6125
18-Dec-2008
0O/C
1272
10623
E2
792004
UVA
HEAT EXCHANGER --
HRS
MTH
6125
09-Oct-2008
0O/C
PP0192
110718
E1
792201W
UVA
COOLER-LUBE OIL --
HRS
MTH
6125
09-Oct-2008
0O/C
PP0191
110718
E2
792201W
UVA
COOLER-LUBE OIL --
HRS
MTH
6125
09-Oct-2008
05000MX20323
110590
(5002)11125 3944.6E1
792401
UVA
LUBE AND SCAVENGE PUMP
HRS
MTH
6125
09-Oct-2008
05000MX20320
110590
(5003)11125 3944.6E2
792401
UVA
LUBE AND SCAVENGE PUMP
Page 29 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-INFORMATIONAL
SL CIL-03-01 CERTIFICATION REQUIREMENTS - SUPPLEMENTAL TYPE CERTIFICATE (STC)
MOC :
-RECOMMENDED
SL CIL-99-03 R01 MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)
MOC :
MTH -RECOMMENDED
SL CIL-99-03 MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM (CPCP) (SUPERSEDED BY CIL-99-03 REV 01)
MOC :
-INFORMATIONAL
SL 500-03-01 R01 CERTIFICATION REQUIREMENTS - SUPPLEMENTAL TYPE CERTIFICATE (STC) (SUPERSEDED BY CIL-03-01)
MOC :
-INFORMATIONALSL 500-99-09 R07 CESCOM PRICING
MOC :
A/RINFORMATIONAL
SL 500-99-12 MISCELLANEOUS - CESSNA PART NUMBER SUFFIXES FOR REMANUFACTURED PARTS
MOC :
A/RINFORMATIONAL
SL 500-99-13 MISCELLANEOUS - CESSNA SERVICE DOCUMENT CHANGE NOTIFICATION
MOC :
-INFORMATIONAL
SL CIL-99-04 MISCELLANEOUS - INCREMENTAL LIBRARY UPDATES FOR CESVIEW
MOC :
-INFORMATIONALE1
SB FJ44-05-002R01
UNSERVICEABLE PARTS - NOTIFICATION (SUPERSEDED BY FJ44-05-002 R02)
MOC :
-INFORMATIONALE2
SB FJ44-05-002R01
UNSERVICEABLE PARTS - NOTIFICATION (SUPERSEDED BY FJ44-05-002 R02)
MOC :
-INFORMATIONAL
E1
SB FJ44-05-002R04
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
-INFORMATIONAL
E2
SB FJ44-05-002R04
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
-CANCELLEDE1
SB FJ44-05-002R05-CN
SUPERSEDED - UNSERVICEABLE PARTS - NOTIFICATION (THIS SERVICE DOCUMENT HAS BEEN SUPERSEDED BY WIPSID-05-1000)
MOC :
-CANCELLEDE2
SB FJ44-05-002R05-CN
SUPERSEDED - UNSERVICEABLE PARTS - NOTIFICATION (THIS SERVICE DOCUMENT HAS BEEN SUPERSEDED BY WIPSID-05-1000)
MOC :
-INFORMATIONAL
E1
SB FJ44-05-002R05
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
-INFORMATIONAL
E2
SB FJ44-05-002R05
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
Page 30 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-INFORMATIONALE1
SB FJ44-05-002 UNSERVICEABLE PARTS - NOTIFICATION (SUPERSEDED BY FJ44-05-002 R01)
MOC :
-INFORMATIONALE2
SB FJ44-05-002 UNSERVICEABLE PARTS - NOTIFICATION (SUPERSEDED BY FJ44-05-002 R01)
MOC :
-CANCELLEDE1
SL WI-05-1015-CN CANCELED - TIME LIMITS/MAINTENANCE CHECKS - AIRWORTHINESS LIMITATIONS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-CANCELLEDE2
SL WI-05-1015-CN CANCELED - TIME LIMITS/MAINTENANCE CHECKS - AIRWORTHINESS LIMITATIONS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E1
SL WI-05-1015 TIME LIMITS/MAINTENANCE CHECKS - AIRWORTHINESS LIMITATIONS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E2
SL WI-05-1015 TIME LIMITS/MAINTENANCE CHECKS - AIRWORTHINESS LIMITATIONS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E1
SL WI-05-1020 TIME LIMITS/MAINTENANCE CHECKS - SCHEDULED MAINTENANCE CHECKS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E2
SL WI-05-1020 TIME LIMITS/MAINTENANCE CHECKS - SCHEDULED MAINTENANCE CHECKS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E1
SL WI-05-1022 TIME LIMITS/MAINTENANCE CHECKS - UNSERVICEABLE PARTS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E2
SL WI-05-1022 TIME LIMITS/MAINTENANCE CHECKS - UNSERVICEABLE PARTS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
HRS
MTH
3144
13-Jan-1994 A/ROPTIONAL Complete11SB-4
SB 500-11-04
ICT
MODEL 500 CONVERSION TO MODEL 501 (SUPERSEDED BY 500-11-04REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL11SL-2
SL 500-11-02
JHB
PLACARDS AND MARKINGS - DATA PLATE RELOCATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
-INFORMATIONAL
SL CIL-99-01 REV01
USE OF CORROSION INHIBITING COMPOUNDS
MOC :
-INFORMATIONAL
SL CIL-99-01 REV02
USE OF CORROSION INHIBITING COMPOUNDS
MOC :
-INFORMATIONAL
SL CIL-99-01 USE OF CORROSION INHIBITING COMPOUNDS (SUPERSEDED BY CIL-99-01 REV 01)
MOC :
MTH -RECOMMENDED
SL CIL-99-02 MISCELLANEOUS - AVOID OPERATIONS ON RUNWAYS TREATED WITH RUNWAY DE-ICE (RDI) FLUIDS. AIRCRAFT WASHING RECOMMENDED AFTEREXPOSURE TO RDI FLUIDS
MOC :
Page 31 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-INFORMATIONAL
SL CIL-20-01 REV02
STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL
MOC :
-INFORMATIONAL
SL CIL-20-01 STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL(SUPERSEDED BY CIL-20-01 REV 01)
MOC :
A/RINFORMATIONAL
SL 500-20-02 R27 STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY SL500-20-02 R28)
MOC :
-INFORMATIONAL
SL 500-20-04 STANDARD PRACTICES - CESSNA STANDARD PRACTICES MANUAL
MOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete21SB-8
SB 500-21-08 SUPPLEMENTAL FLIGHT COMPARTMENT VENTILATION SYSTEM INSTALLATION (SUPERSEDED BY 500-21-08 REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL21SB-15
SB 500-21-15 FREON AIR CONDITIONING SYSTEM INSTALLATION (SUPERSEDED BY 500-21-15 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL21SB-16
SB 500-21-16 AIRCONDITIONING - COCKPIT AIR DISTRIBUTION - ADD SUPPLEMENTARY AIR OUTLETS ON SIDE CONSOLES
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL21SB-19
SB 500-21-19 AIR CONDITIONING - NOSE GEAR DOORS MODIFICATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
4513
29-Jul-1999 A/ROPTIONAL Complete21SB-20
SB 500-21-20
SJC
CABIN VENTILATION MOTOR REPLACEMENT (SUPERSEDED BY 500-21-20 REV 01)
COMPLIED WITHMOC :
HRS
MTH
3144
13-Jan-1994 A/R Complete21SB-21
SB 500-21-21
ICT
OUTFLOW VALVE REPLACEMENT
COMPLIED WITHMOC :
MTH A/ROPTIONAL21SB-22
SB 500-21-22
*CF
AIR CONDITIONING - ALTERNATE FLOW CONTROL VALVE INSTALLATION
MOC :
HRS
MTH
3708
16-Jan-1996 -MANDATORY
Complete21SB-23
SB 500-21-23
SJC
ADDITIONAL OUTFLOW VALVE REPLACEMENTS
COMPLIED WITHMOC :
MTH A/RDISCRETIONARY21SB-24
SB 500-21-24 AIR CONDITIONING - CABIN FAN AND DEFOG BLOWER WIRING IMPROVEMENT
MOC :
A/ROPTIONAL
SB 500-21-25 AIR CONDITIONING - TEMPERATURE CONTROLLER IMPROVEMENT
MOC :
Page 32 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-INFORMATIONAL
SL CIL-21-01 COMPRESSOR MOTOR BRUSH LIFE LIMIT
MOC :
MTH 17-Aug-2015 -MANDATORY
SL CIL-21-02 REV01
AIR CONDITIONING - ENVIRONMENTAL HOUR METER INSTALLATION
DEFERRED - OWNER DOES NOT WISH TO COMPLY AT THIS TIME.MOC :
-OPTIONAL
SL CIL-21-02 ENVIRONMENTAL HOUR METER INSTALLATION (SUPERSEDED BY CIL-21-02 REV 01)
MOC :
HRS
MTH
300
RECOMMENDED21SL-20
SL 500-21-20
JHB
AIR CONDITIONING - COMPRESSOR DRIVE MOTOR BRUSH INSPECTION/REPLACEMENT (FORT WORTH AIRWORKS INC. - ZEPHYR AIR CONDITIONING)
NOT APPLICABLE
MOC :
HRS
MTH
4487
09-Mar-1999 A/ROPTIONAL Complete22SB-7
SB 500-22-07
SJC
AUTO FLIGHT - SINGLE AND DUAL ACCELEROMETER INSTALLATION
COMPLIED WITHMOC :
HRS
MTH
5345
19-Jun-2003 A/ROPTIONAL Complete22SB-9
SB 500-22-09
SMF
AUTO FLIGHT - FLIGHT DIRECTOR COMPUTER VERTICAL SPEED HOLD WIRING MODIFICATION
COMPLIED WITHMOC :
MTH A/ROPTIONAL23SB-10
SB 500-23-10 COMMUNICATION - FLITEFONE III INSTALLATION (SUPERSEDED BY 500-23-10 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL23SB-15
SB 500-23-15
JHB
STATIC DISCHARGE IMPROVEMENT (SUPERSEDED BY 500-23-15 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL23SB-16
SB 500-23-16
*CF
COMMUNICATIONS - STATIC WICK REPLACEMENT
MOC :
MTH A/ROPTIONAL23SB-17 : REV1
SB 500-23-17 REV01
COLLINS 8.33 KHZ COMMUNICATION RADIO INSTALLATION
MOC :
HRS
MTH
4546
15-Oct-1999 A/RMANDATORY Complete23SB-18
SB 500-23-18
SJC
COMMUNICATION - VLF NOISE FILTER CAPACITOR REMOVAL/REPLACEMENT (SUPERSEDED BY 500-23-18 REV 01)
COMPLIED WITH - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :
HRS
MTH
300
RECOMMENDED23SL-14
SL 500-23-14
JHB
COMMUNICATION - 66 TRA MICROPHONE CORD REPLACEMENT PROGRAM
OPERATOR DOES NOT WISH TO COMPLY AT THIS TIME
MOC :
MTH A/ROPTIONAL23SL-15
SL 500-23-15
JHB
COMMUNICATION - STATIC DISCHARGE WICK MODIFICATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
Page 33 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete24SB-5
SB 500-24-05 ELECTRICAL - BATTERY TEMPERATURE MONITOR GAUGE SYSTEM (SUPERSEDED BY 500-24-05 REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL24SB-16 : REV1
SB 500-24-16 REV01
ELECTRICAL POWER - CONTROL WHEEL ELECTRICAL CABLE REPLACEMENT
MOC :
MTH A/RRECOMMENDED24SB-17 : REV2
SB 500-24-17 REV02 JHB
GENERATOR CONTROL UNIT START CIRCUIT MODIFICATION (SUPERSEDED BY 500-24-17 REV 03)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
3768
26-Mar-1996 A/RRECOMMENDED Complete24SB-18
SB 500-24-18
SJC
ELECTRICAL POWER - WING TIP WIRE BUNDLE PROTECTIVE COVER INSTALLATION
COMPLIED WITHMOC :
MTH A/ROPTIONAL24SB-20 : REV1
SB 500-24-20 REV01
ELECTRICAL POWER - OVERVOLTAGE MONITOR SYSTEM INSTALLATION
MOC :
MTH A/ROPTIONAL24SB-21
SB 500-24-21 ELECTRICAL POWER - BATTERY DISCONNECT RELAY ACCESS IMPROVEMENT
MOC :
MTH A/ROPTIONAL24SB-22
SB 500-24-22 ELECTRICAL POWER - SEALED LEAD ACID BATTERY INSTALLATION
MOC :
A/ROPTIONAL
SB 500-24-23 ELECTRICAL POWER - MAGNETIC CIRCUIT BREAKER MODIFICATION
MOC :
MTH A/ROPTIONAL25SB-17
SB 500-25-17 AFT PORTABLE SEAT INSTALLATION (SUPERSEDED BY 500-25-17 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL25SB-20
SB 500-25-20 EQUIPMENT/FURNISHINGS - STRETCHER INSTALLATION (SUPERSEDED BY 500-25-20 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL25SB-22
SB 500-25-22 THREE PLACE SIDE FACING COUCH INSTALLATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL25SB-26
SB 500-25-26
JHB
EQUIPMENT/FURNISHINGS CREW SEAT BACK MODIFICATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
3085
19-Nov-1993 A/RMANDATORY Complete25SB-27
SB 500-25-27
FMN
EQUIPMENT/FURNISHINGS - LOCATOR BEACON RESET CIRUIT VOLTAGE LIMIT RESISTOR REMOVAL
COMPLIED WITHMOC :
Page 34 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH A/ROPTIONAL
25SB-28 : REV1
SB 500-25-28 REV01 JHB
FOUR-POINT RESTRAINT SYSTEM INSTALLATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
A/ROPTIONAL25SB-31 : REV2
SB 500-25-31 REV02
EQUIPMENT/FURNISHINGS - ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT) (SUPERSEDED BY 500-25-31 REV 03)
MOC :
A/ROPTIONAL
SB 500-25-31 REV03
ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATORTRANSMITTER (ELT)
MOC :
HRS
MTH
3085
19-Nov-1993 A/RMANDATORY Complete25SL-3
SL 500-25-03
FMN
INSPECTION/MODIFICATION OF PERSONAL FLOTATION DEVICES
COMPLIED WITHMOC :
HRS
MTH
256
01-Feb-1984 A/RMANDATORY Complete25SL-4
SL 500-25-04
JHB
MODIFICATION OF INERTIA REEL ON CREW SEATS WITH 4 AND 5 POINT RESTRAINT
COMPLIED WITHMOC :
HRS
MTH
150INFORMATIONAL25SL-5
SL 500-25-05
JHB
SWITLIK INFLATABLE LIFE PRESERVER INSPECTION
NOT APPLICABLE
MOC :
HRS
MTH
3937
24-Jan-1997 -MANDATORY Complete
25SL-08
SL 500-25-08
SJC
TRANSMITTAL OF EASTERN AERO MARINE SERVICE BULLETIN SBV-25-2, EQUIPMENT/FURNISHINGS - LIFE PRESERVERS AND INDIVIDUAL FLOTATIONDEVICES REPLACEMENT OF CO2 INFLATOR
COMPLIED WITHMOC :
HRS
MTH
4870
16-Apr-2001 A/RRECOMMENDED Complete25SL-09
SL 500-25-09
SJC
EQUIPMENT/FURNISHINGS - GLARESHIELD ATTACHMENT SCREW(S) INSPECTION/REPLACEMENT
COMPLIED WITHMOC :
HRS
MTH
5820
01-Jul-2006 A/RMANDATORY Complete26SB-02 : REV1
SB 500-26-02 REV01 YHM
FIRE PROTECTION - FIRE BOTTLE WIRE IDENTIFICATION SLEEVE INSTALLATION
COMPLIED WITHMOC :
HRS
MTH
5979
02-Aug-2007 A/RMANDATORY Complete26ASL02
ASL 500-26-02
YHM
FIRE PROTECTION - TRANSMITTAL OF MEGGITT SAFETY SYSTEMS SERVICE BULLETIN 26-36 - THERMISTORS DETECTORS
COMPLIED WITHMOC :
MTH -MANDATORY
SL CIL-26-01 REV01
FIRE PROTECTION - FIRE EXTINGUISHER BOTTLE CARTRIDGE GROUND STUD TORQUING
MOC :
-SUPERSEDED
SL CIL-26-01 FIRE PROTECTION - FIRE EXTINGUISHER BOTTLE CARTRIDGE GROUND STUD TORQUING (SUPERSEDED BY CIL-26-01 REV 01)
MOC :
HRS
MTH
305
15-Mar-1984 A/RRECOMMENDED Complete26SL-1
SL 500-26-01
JHB
ENGINE FIRE WARNING TRAY
COMPLIED WITHMOC :
Page 35 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
305
14-Mar-1984 A/RRECOMMENDED Complete27SB-10
SB 500-27-10
JHB
FLIGHT CONTROLS - AILERON ACTUATOR CABLE GUARD MODIFICATION (SUPERSEDED BY 500-27-10 REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL27SB-11
SB 500-27-11
JHB
FLIGHT CONTROLS - FLAP BEARING AND ROLLER REPLACEMENT (SUPERSEDED BY 500-27-11 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL27SB-13
SB 500-27-13 FLIGHT CONTROLS - SPEED BRAKE PUSH ROD REPLACEMENT
MOC :
MTH A/ROPTIONAL27SB-14
SB 500-27-14
*CF
FLIGHT CONTROLS - FLAP MOTOR CONNECTOR INSTALLATION (SUPERSEDED BY 500-27-14 REV 01)
MOC :
HRS
MTH
3937
24-Jan-1997 -RECOMMENDED Complete27SB-15 : REV1
SB 500-27-15 REV01 SJC
FLAP GEARBOX REPLACEMENT (SUPERSEDED BY 500-27-15 REV 02)
COMPLIED WITHMOC :
HRS
MTH
3937
24-Jan-1997 -RECOMMENDED
Complete27SB-16
SB 500-27-16
SJC
ELEVATOR ELECTRIC TRIM ACTUATOR REPLACEMENT
COMPLIED WITH - NOT APPLICABLE BY DATE OF MANUFACTUREMOC :
HRS
MTH
4605
31-Jan-2000 -CANCELLED Complete27SB-18
SB 500-27-18
SJC
AILERON FASTENERS INSPECTION/INSTALLATION (SUPERSEDED BY 500-27-18 REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL27SB-19
SB 500-27-19 FLIGHT CONTROLS - TRIM TAB ACTUATOR GREASE FITTING INSTALLATION
MOC :
HRS
MTH
111
25-Aug-1983 A/RMANDATORY
Complete27SL-6
SL 500-27-06
JHB
INSPECTION OF ELEVATOR AND RUDDER TRIM SYSTEM
COMPLIED WITHMOC :
HRS
MTH
6002
22-Dec-2007 A/RRECOMMENDED Complete27SL-11
SL 500-27-11
THM
FLIGHT CONTROLS - RUDDER PEDAL SUPPORT INSPECTION
COMPLIED WITHMOC :
MTH A/ROPTIONAL28SB-09
SB 500-28-09 FUEL - IMPROVED FUEL CROSSFEED SELECT KNOB AVAILABILITY
MOC :
HRS
MTH
3937
24-Jan-1997 A/ROPTIONAL Complete28SB-10
SB 500-28-10
SJC
WING FUEL CELL FOAM BLOCK REMOVAL (SUPERSEDED BY 500-28-10 REV 01)
COMPLIED WITHMOC :
HRS
MTH
4870
16-Apr-2001 A/RRECOMMENDED Complete28SB-11 : 500
SB 500-28-11
SJC
FUEL - TANK BRACKET AND CLAMP INSTALLATION/INSPECTION
COMPLIED WITHMOC :
Page 36 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
5820
01-Jul-2006 A/RMANDATORY
Complete28SB-12
SB 500-28-12
YHM
WING FUEL BOOST PUMP WIRE ROUTING IMPROVEMENT
COMPLIED WITHMOC :
HRS
MTH
3937
24-Jan-1997 A/RMANDATORY Complete28SLA09 : REV1
ASL 500-28-09 REV01
SJC
FUEL - TRANSMITTAL OF PARKER HANNIFIN CORPORATION - AIRBORNE AIR & FUEL PRODUCTS SERVICE LETTER NO. 41, RAPCO FLEET SUPPORTINC. OVERHAUL OF AIRBORNE FUEL PUMPS
COMPLIED WITHMOC :
HRS
MTH
3937
24-Jan-1997 A/RMANDATORY Complete28SL-08
SL 500-28-08
SJC
FUEL - FUEL CELL INSPECTION REQUIREMENTS (SUPERSEDED BY SL500-28-08 R01)
COMPLIED WITHMOC :
-INFORMATIONAL
SL CIL-30-01 REV01
APPROVED DEICING PROGRAM UPDATES
MOC :
MTH A/ROPTIONAL30SL-6
SL 500-30-06 EROSION SHOES FOR WING TIP PYLON LEADING EDGE, HORIZONTAL STABILIZER/VERTICAL FIN TIPS (SUPERSEDED BY SL500-30-06 R01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
-INFORMATIONAL
SL CIL-31-01 INDICATING/RECORDING SYSTEMS - CVR, FDR, AND CVDR 90-DAY BATTERY UNDERWATER LOCATOR BEACON (ULB) INSTALLATION
MOC :
MTH A/ROPTIONAL32SB-27
SB 500-32-27 LANDING GEAR - GRAVEL RUNWAY SYSTEM INSTALLATION (SUPERSEDED BY 500-32-27 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete32SB-28
SB 500-32-28 ANTI-SKID BRAKE SYSTEM INSTALLATION (SUPERSEDED BY 500-32-28 REV 01)
COMPLIED WITHMOC :
HRS
MTH
198
15-Nov-1983 A/RMANDATORY Complete32SB-37
SB 500-32-37
JHB
LANDING GEAR - MAIN GEAR ACTUATOR ATTACH STUD REPLACEMENT
COMPLIED WITHMOC :
HRS
MTH
2815
06-Aug-1992 A/ROPTIONAL Complete32SB-38 : REV2
SB 500-32-38 REV02 JHB
BFGOODRICH BRAKES AND WHEELS INSTALLATION (SUPERSEDED BY 500-32-38 REV 03)
COMPLIED WITHMOC :
MTH A/ROPTIONAL32SB-41
SB 500-32-41
JHB
LANDING GEAR - BFGOODRICH BRAKE BLEEDER BLOCK INSTALLATION AND HOSE REPLACEMENT (SUPERSEDED BY 500-32-41 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
3768
26-Mar-1996 A/RRECOMMENDED Complete32SB-42
SB 500-32-42
SJC
LANDING GEAR - MLG WHEEL WELL AFT SPAR BOX HYDRAULIC/PNEUMATIC LINES GROMMET REPLACEMENT
COMPLIED WITHMOC :
Page 37 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
3708
16-Jan-1996 -RECOMMENDED Complete32SB-43
SB 500-32-43
SJC
MAIN LANDING GEAR SIDE BRACE STUD INSPECTION/REPLACEMENT
COMPLIED WITHMOC :
HRS
MTH
4215
14-Jan-1998 -RECOMMENDED Complete32SB-45
SB 500-32-45
SJC
POWER BRAKE HYDRAULIC PUMP SCREW REPLACEMENT
COMPLIED WITHMOC :
LDG
HRS
MTH
4820
7014.3
08-Jun-2018 A/RMANDATORY N/A32SB-48 : REV3
SB 500-32-48 REV03
UNK
LANDING GEAR - TRANSMITTAL OF BFGOODRICH SERVICE BULLETIN 2-1528-32-2, LANDING GEAR - BRAKE ASSEMBLY POSSIBLE CRACKED STATORSDISKS
NOT APPLICABLE - BOTH BRAKE ASSYS O/H BY BF GOODRICH APRIL 2016MOC :
HRS
MTH
4859
28-Feb-2001 -MANDATORY
Complete32SB-48 : 500
LEFT
SB 500-32-48
SJC
TRANSMITTAL OF BFGOODRICH SERVICE BULLETIN 2-1528-32-2, LANDING GEAR - BRAKE ASSEMBLY POSSIBLE CRACKED STATORS DISKS(SUPERSEDED BY 500-32-48 REV 01)
COMPLIED WITHMOC :
HRS
MTH
4859
28-Feb-2001 -MANDATORY
Complete32SB-48 : 500
RIGHT
SB 500-32-48
SJC
TRANSMITTAL OF BFGOODRICH SERVICE BULLETIN 2-1528-32-2, LANDING GEAR - BRAKE ASSEMBLY POSSIBLE CRACKED STATORS DISKS(SUPERSEDED BY 500-32-48 REV 01)
COMPLIED WITHMOC :
MTH 10-Apr-2014 -RECOMMENDED Complete
SB 500-32-51 REV01 CYHM
REPLACEMENT OF BLEEDER SCREWS AND FITTINGS WITH BLEEDER PLUGS
COMPLIED WITH - PREVIOUSLY COMPLIED WITH ON APRIL 10/2014 UNDER EMI WO# 0248MOC :
LDG
HRS
MTH
4579
6639.5
11-Apr-2014 -RECOMMENDED Complete
SB 500-32-51
CYHM
REPLACEMENT OF BLEEDER SCREWS AND FITTINGS WITH BLEEDER PLUGS (SUPERSEDED BY 500-32-51 REV 01)
COMPLIED WITH - SB 500-32-51 CARRIED OUT WITH NEW BRAKE HOSE ASSEMBLIES.MOC :
HRS
MTH
148
28-Sep-1983 A/RMANDATORY Complete32SLA34
ASL 500-32-34
JHB
MAIN GEAR ACTUATOR TO STRUT ATTACH STUD INSPECTION (SUPERSEDED BY ASL500-32-34 REV 01)
COMPLIED WITHMOC :
HRS
MTH
3490
26-Jun-1995 A/RMANDATORY Complete32SLA62
ASL 500-32-62
UVA
LANDING GEAR - MAIN LANDING GEAR ACTUATOR STUD(S) INSPECTION/REPLACEMENT
COMPLIED WITHMOC :
-INFORMATIONAL
SL CIL-32-01 LANDING GEAR - IMPROVED NOSE WHEEL GREASE SEAL
MOC :
LDG
HRS
MTH
4642
6732.4
23-Jun-2015 -RECOMMENDED
CompleteSL CIL-32-03
CYHM
NLG UPLOCK ROLLER BRACKET INSPECTION
COMPLIED WITH - NO FAULLT NOTED-ORIENTATION IS CORRECT AT THIS TIMEMOC :
-INFORMATIONAL
SL CIL-32-04 WIRELESS TIRE PRESSURE MONITORING SYSTEM INSTALLATION
MOC :
Page 38 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-INFORMATIONAL
SL CIL-32-06 LANDING GEAR - WIRELESS TIRE PRESSURE SENSOR FILL VALVE TORQUE VERIFICATION
MOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL
Complete32SL-14
SL 500-32-14 EXTENDED BRAKE LIFE MODIFICATION
COMPLIED WITHMOC :
HRS
MTH
256
30-Jan-1984 A/R Complete32SL-33
SL 500-32-33
JHB
M/G STRUT O-RINGS
COMPLIED WITHMOC :
HRS
MTH
198
15-Nov-1983 A/RRECOMMENDED Complete32SL-35
SL 500-32-35
JHB
AIR STORAGE BOTTLE
COMPLIED WITHMOC :
HRS
MTH
1775
01-Jun-1988 A/RRECOMMENDED Complete32SL-38
SL 500-32-38
JHB
NOSE GEAR STEERING LOWER JOINT BEARING INSPECTION
COMPLIED WITHMOC :
HRS
MTH
3085
19-Nov-1993 A/RRECOMMENDED Complete32SL-41
SL 500-32-41
FMN
LANDING GEAR - UPLOCK ACTUATOR HYDRAULIC LINE INSPECTION
COMPLIED WITHMOC :
HRS
MTH
2815
06-Aug-1992 A/RRECOMMENDED Complete32SL-42
SL 500-32-42
JHB
LANDING GEAR - MAIN LANDING GEAR AXLE INTERNAL CORROSION INSPECTION
COMPLIED WITHMOC :
HRS
MTH
2815
06-Aug-1992 A/RRECOMMENDED Complete32SL-48
SL 500-32-48
JHB
LANDING GEAR - LANDING GEAR EMERGENCY EXTENSION CONTROL ASSEMBLY PIN INSPECTION
COMPLIED WITHMOC :
HRS
MTH
3085
19-Nov-1993 A/RRECOMMENDED Complete32SL-53
SL 500-32-53
FMN
LANDING GEAR - NOSE LANDING GEAR UPLOCK LINE INSPECTION
COMPLIED WITHMOC :
HRS
MTH
3085
19-Nov-1993 A/RRECOMMENDED Complete32SL-54
SL 500-32-54
FMN
LANDING GEAR - LANDING GEAR HANDLE LOCKING SOLENOID INSPECTION
COMPLIED WITHMOC :
HRS
MTH
3504
07-Jul-1995 A/RRECOMMENDED
Complete32SL-57 : REV1
SL 500-32-57 R01
SJC
LANDING GEAR - TEIJIN SEIKI MAIN AND NOSE LANDING GEAR ACTUATOR DOWN AND LOCKED SWITCH INSPECTION/ REPLACEMENT (SUPERSEDEDBY SL500-32-57 R02)
COMPLIED WITH - NOT APPLICABLE BY TYPE MANUFACTURERMOC :
HRS
MTH
3504
07-Jul-1995 A/RRECOMMENDED Complete32SL-66
SL 500-32-66
SJC
LANDING GEAR - NOSE LANDING GEAR WHEEL AND TIRE ASSEMBLY ATTACH HARDWARE INSPECTION / REPLACEMENT
COMPLIED WITHMOC :
MTH A/ROPTIONAL32SL-71 : REV1
SL 500-32-71 R01 NOSE LANDING GEAR ICE PROTECTION BOOT INSTALLATION
MOC :
Page 39 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
6222
12-Dec-2009 A/RMANDATORY Complete32SL-76
SL 500-32-76
YHM
LANDING GEAR - EMERGENCY GEAR RELEASE INSPECTION
COMPLIED WITHMOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete33SB-3
SB 500-33-03 LIGHTS - WING TIP RECOGNITION LIGHT INSTALLATION (SUPERSEDED BY 500-33-03 REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL33SB-4
SB 500-33-04 RUDDER MOUNTED OSCILLATING BEACON INSTALLATION (SUPERSEDED BY 500-33-04 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL33SB-8 : REV6
SB 500-33-08 REV06 JHB
LIGHTS - RUDDER MOUNTED OSCILLATING BEACON REPLACEMENT
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL33SB-09
SB 500-33-09 LIGHTS - LANDING LIGHT ELECTRICAL CIRCUIT MODIFICATION (SUPERSEDED BY 500-33-09 REV 01)
MOC :
MTH A/ROPTIONAL
33SB-10
SB 500-33-10
*CF
LIGHTS - EXIT SIGN REPLACEMENT
MOC :
MTH A/ROPTIONAL33SB-11
SB 500-33-11 LIGHTS - WING TIP NAV/COLLISION LIGHT MODIFICATION (SUPERSEDED BY 500-33-11 REV 01)
MOC :
MTH A/ROPTIONAL33SB-12
SB 500-33-12 LIGHTS - LANDING LIGHT CIRCUIT SWITCH MODULE INSTALLATION
MOC :
MTH A/ROPTIONAL33SB-13 : REV1
SB 500-33-13 REV01
LIGHTS - EMERGENCY LIGHTING BATIERY PACK UPGRADE
MOC :
MTH A/ROPTIONAL33SB-14
SB 500-33-14 LIGHTS - LED TAIL POSITION LIGHT INSTALLATION
MOC :
HRS
MTH
3144
13-Jan-1994 -MANDATORY
Complete33SL-04 : REV1
SL 500-33-04 R01
ICT
LANDING LIGHT SWITCH INSPECTION/REPLACEMENT
COMPLIED WITHMOC :
MTH A/ROPTIONAL34SB-7
SB 500-34-07 NAVIGATION - INSTALLATION OF COLLINS RADIO ALTIMETER (SUPERSEDED BY 500-34-07 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete34SB-15
SB 500-34-15 9500 POUND ZERO FUEL WEIGHT INSTALLATION (SUPERSEDED BY 500-34-15 REV 01)
COMPLIED WITHMOC :
Page 40 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH A/ROPTIONAL34SB-29
SB 500-34-29 NAVIGATION - AREA NAVIGATION ADAPTER CABLE INSTALLATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete34SB-31
SB 500-34-31 NAVIGATION - INSTALLATION OF ANGLE-OF-ATTACK SYSTEM (SUPERSEDED BY 500-34-31 REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL34SB-32
SB 500-34-32 NAVIGATION - AREA NAV (RNS-3500) SYSTEM INSTALLATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL34SB-49
SB 500-34-49
JHB
NAVIGATION - VLF SYSTEM H-FIELD LOOP ANTENNA INSTALLATION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL34SB-55
SB 500-34-55
JHB
NAVIGATION - STANDBY GYRO EMERGENCY LIGHTING
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
HRS
MTH
3085
19-Nov-1993 A/RRECOMMENDED Complete34SB-57
SB 500-34-57
FMN
NAVIGATION - STARTER-GENERATOR AND GCU FILTER INSTALLATION
COMPLIED WITHMOC :
HRS
MTH
3144
13-Jan-1994 A/RMANDATORY
Complete
34SBA58 : REV1
ASB 500-34-58REV 01 ICT
NAVIGATION - VG14A VERTICAL GYRO INSPECTION
COMPLIED WITHMOC :
MTH A/ROPTIONAL34SB-59 : REV1
SB 500-34-59 REV01 JHB
NAVIGATION - VN-212 SIGNAL GROUND WIRING MODIFICATION
MOC :
HRS
MTH
5170
16-Sep-2002 A/ROPTIONAL Complete34SB-65
SB 500-34-65
SMF
NAVIGATION - REDUCED VERTICAL SEPARATION MINIMUM (RVSM) OPERATION MODIFICATION
COMPLIED WITHMOC :
MTH A/ROPTIONAL34SB-66
SB 500-34-66 NAVIGATION - SANDEL TERRAIN AWARENESS WARNING SYSTEM (TAWS) INSTALLATION
MOC :
MTH A/ROPTIONAL34SB-67
SB 500-34-67 NAVIGATION - SIGMA-TEK CONTROL PANEL INSTALLATION
MOC :
HRS
MTH
4215
14-Jan-1998 A/RMANDATORY Complete34SLA41
ASL 500-34-41
SJC
NAVIGATION - KLN 89B, KLN 90B AND KLN 900 GPS INSTRUMENT LANDING SYSTEM APPROACH RESTRICTIONS
COMPLIED WITHMOC :
Page 41 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH A/RRECOMMENDED34SL-37
SL 500-34-37
JHB
DORNE AND MARGOLIN DMN4-17-4 NAV ANTENNA COUPLER INSPECTION
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
-OPTIONAL
SB 500-35-04 REV04
OXYGEN - INSTALLATION OF 64 CUBIC FOOT OXYGEN SYSTEM
MOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete35SB-4
SB 500-35-04 OXYGEN - INSTALLATION OF 64 CUBIC FOOT OXYGEN SYSTEM (SUPERSEDED BY 500-35-04 REV 01)
COMPLIED WITHMOC :
MTH A/ROPTIONAL
35SB-06 : REV1
SB 500-35-06 REV01
OXYGEN - EROS OXYGEN MASK INSTALLATION
MOC :
MTH A/ROPTIONAL35SB-06
SB 500-35-06
JHB
OXYGEN - EROS OXYGEN MASK INSTALLATION (SUPERSEDED BY 500-35-06 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
LDG
HRS
DAYS
MTH
4697
6833.7
11-Mar-2016 -MANDATORY Complete
SL CIL-35-05
CYHM
OXYGEN - TRANSMITTAL OF ZODIAC AEROSPACE SB MCF-SBU-35-001
COMPLIED WITH - PREVIOUSLY COMPLIED WITH IN ACCORDANCE WITH SB MCF-SBU- REV 1 ON FEB 3/2016MOC :
MTH A/RINFORMATIONAL
SL 500-35-06 OXYGEN - OXYGEN BOTTLE INSPECTION
MOC :
LDG
HRS
MTH
4478
6477
26-Nov-2012 -MANDATORY Complete
SL 500-35-07
CYHM
OXYGEN - TRANSMITTAL OF INTERTECHNIQUE SERVICE BULLETIN MXH-35-240
COMPLIED WITH - COMPLIED WITH AND NO ACTIONS REQUIRED DUE TO THE DATA ON BOTH THE L/H AND R/H CREWOXYGEN MASKS- SEE EMI WO# 01913968967
MOC :
HRS
MTH
4353
23-Sep-1998 A/ROPTIONAL Complete36SB-04
SB 500-36-04
SJC
PNEUMATIC - ENGINE BLEED AIR CONNECTOR IMPROVEMENT
COMPLIED WITHMOC :
MTH A/ROPTIONAL
36SB-05 : REV1
SB 500-36-05 REV01
PNEUMATIC - DOOR SEAL VALVE REPLACEMENT
MOC :
HRS
MTH
1775
01-Jun-1988 A/RRECOMMENDED Complete52SB-16
SB 500-52-16
JHB
DOORS - ENTRY STEP ASSEMBLY IMPROVEMENT (SUPERSEDED BY 500-52-16 REV 01)
COMPLIED WITHMOC :
HRS
MTH
6125
18-Dec-2008 A/RRECOMMENDED Complete52SB-18
SB 500-52-18
UVA
DOOR - BAGGAGE DOOR POSITIVE SAFETY LOCK INSTALLATION (SUPERSEDED BY 500-52-18 REV 01)
COMPLIED WITH - OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
Page 42 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
3708
16-Jan-1996 A/RRECOMMENDED Complete52SB-19
SB 500-52-19
SJC
DOORS - ENTRY DOOR STEP CATCH COVER INSTALLATION (WITH STANDARD DOOR AND STEP)
COMPLIED WITHMOC :
LDG
HRS
DAYS
4427
6408
20-Feb-2012 A/RMANDATORY
CompleteASL 500-52-04
CYHM
DOORS - EMERGENCY EXIT INSPECTION
COMPLIED WITH - NO FAULTS NOTEDMOC :
HRS
MTH
3085
19-Nov-1993 A/RMANDATORY Complete52SL-03
SL 500-52-03
FMN
DOOR - EMERGENCY EXIT INNER HANDLE ATTACH SCREW INSPECTION/REPLACEMENT
COMPLIED WITHMOC :
HRS
MTH
10
30-Apr-1983 A/ROPTIONAL Complete53SB-3
SB 500-53-03 FUSELAGE - DRAG CHUTE INSTALLATION (SUPERSEDED BY 500-53-03 REV 01)
COMPLIED WITHMOC :
HRS
MTH
3937
24-Jan-1997 A/RRECOMMENDED Complete53SB-20
SB 500-53-20
SJC
FUSELAGE - FLIGHT CREW SEAT RAIL AND BEAM RIVETS INSPECTION/INSTALLATION
COMPLIED WITHMOC :
MTH A/ROPTIONAL53SB-22
SB 500-53-22 FUSLEAGE - DORSAL FIN INSTALLATION AND MATERIAL IMPROVEMENT
MOC :
HRS
MTH
5085
26-Apr-2002 -RECOMMENDED
Complete53SB-23
SB 500-53-23
SJC
AN3-5A BOLT INSPECTION/REPLACEMENT
COMPLIED WITHMOC :
MTH A/ROPTIONAL53SB-26
SB 500-53-26 FUSELAGE - WHEEL WELL BOX IMPROVEMENT
MOC :
HRS
MTH
5885
24-Oct-2006 A/RRECOMMENDED
Complete53SL-05 : REV1
SL 500-53-05 R01
YHM
FUSELAGE - INTERCOSTAL DRAINAGE PATH INSPECTION
COMPLIED WITHMOC :
HRS
MTH
3085
19-Nov-1993 A/R Complete55SL-01 : REV1
SL 500-55-01 R01
FMN
STABILIZERS - RUDDER TORQUE TUBE INTERNAL CORROSION INSPECTION
COMPLIED WITHMOC :
HRS
MTH
2815
06-Aug-1992 A/RRECOMMENDED Complete55SL-01
SL 500-55-01
JHB
STABILIZERS - RUDDER TORQUE TUBE INTERNAL CORROSION INSPECTION (SUPERSEDED BY SL500-55-01 R01)
COMPLIED WITHMOC :
HRS
MTH
2815
06-Aug-1992 A/RRECOMMENDED Complete57SL-04
SL 500-57-04
JHB
WIRE BUNDLE ROUTING IMPROVEMENT (SUPERSEDED BY SL500-57-04 R01)
COMPLIED WITHMOC :
-CANCELLEDE1
SL WI-71-1064-CN CANCELED - POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL
MOC :
Page 43 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-CANCELLEDE2
SL WI-71-1064-CN CANCELED - POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL
MOC :
-E1
SL WI-71-1064 POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL
MOC :
-E2
SL WI-71-1064 POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL
MOC :
-CANCELLEDE1
SL WI-71-1129 CANCELED - POWER PLANT - BIT NO. 50 FAULT TROUBLESHOOTING -REVISION TO MAINTENANCE MANUAL
MOC :
-CANCELLEDE2
SL WI-71-1129 CANCELED - POWER PLANT - BIT NO. 50 FAULT TROUBLESHOOTING -REVISION TO MAINTENANCE MANUAL
MOC :
HRS
MTH
1505
09-Jul-1987 A/R Complete72SL-3
SL 500-72-03
JHB
ENGINE - JT15D FAN BLADE INSPECTION
COMPLIED WITHMOC :
HRS
MTH
150
RECOMMENDED72SL-04
SL 500-72-04 ENGINE - INTRODUCTION OF NEW IMPROVED GAS GENERATOR CASE
P&WC SB 7286 REV2 RECOMMENDS ACCOMPLISHMENT AT ENGINE OVERHA UL AFTER 5-04-90.
MOC :
HRS
MTH
6016
23-Jan-2008 A/RRECOMMENDED N/A72SL-10 : E1**L
LEFT ENGINE
SL 500-72-10
YHM
ENGINE - TRANSMITTAL OF PRATT & WHITNEY CANADA (P&WC) SERVICE BULLETIN JT15D-72-7590, TURBOFAN ENGINE BORESCOPE INSPECTION OFIMPELLER REAR FACE AND COMMERCIAL SUPPORT PROGRAM NOTIFICATION (CSPN) C03001R1
NOT APPLICABLE - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :
HRS
MTH
6016
23-Jan-2008 A/RRECOMMENDED N/A72SL-10 : E2**R
RIGHT ENGINE
SL 500-72-10
YHM
TRANSMITTAL OF PRATT & WHITNEY CANADA (P&WC) SERVICE BULLETIN JT15D-72-7590, TURBOFAN ENGINE BORESCOPE INSPECTION OF IMPELLERREAR FACE AND COMMERCIAL SUPPORT PROGRAM NOTIFICATION (CSPN) C03001R1
NOT APPLICABLE - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :
-INFORMATIONAL
E1
SB FJ44-05-002R02
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
-INFORMATIONAL
E2
SB FJ44-05-002R02
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
-INFORMATIONAL
E1
SB FJ44-05-002R03
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
-INFORMATIONAL
E2
SB FJ44-05-002R03
UNSERVICEABLE PARTS - NOTIFICATION
MOC :
-MANDATORY
E1
SB FJ44-71-002R02
ENGINE - HP COMPRESSOR - BORESCOPE INSPECTION
MOC :
Page 44 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-MANDATORY
E2
SB FJ44-71-002R02
ENGINE - HP COMPRESSOR - BORESCOPE INSPECTION
MOC :
-RECOMMENDEDE1
SB FJ44-72-022R02
FRONT BYPASS DUCT - REPAIR RIGHT-HAND SERVICE ADAPTER INSERT
MOC :
-RECOMMENDEDE2
SB FJ44-72-022R02
FRONT BYPASS DUCT - REPAIR RIGHT-HAND SERVICE ADAPTER INSERT
MOC :
-OPTIONAL
E1
SB FJ44-72-042R06
INSTALL REAR MOUNT SLEEVE
MOC :
-OPTIONAL
E2
SB FJ44-72-042R06
INSTALL REAR MOUNT SLEEVE
MOC :
-RECOMMENDED
E1
SB FJ44-72-051R04
REWORK NAMEPLATE
MOC :
-RECOMMENDED
E2
SB FJ44-72-051R04
REWORK NAMEPLATE
MOC :
-RECOMMENDED
E1
SB FJ44-72-051R05
NAMEPLATE - REWORK
MOC :
-RECOMMENDED
E2
SB FJ44-72-051R05
NAMEPLATE - REWORK
MOC :
-RECOMMENDEDE1
SB FJ44-72-054R04
ENGINE - GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER (SUPERSEDED BY FJ44-72-054 R05)
MOC :
-RECOMMENDEDE2
SB FJ44-72-054R04
ENGINE - GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER (SUPERSEDED BY FJ44-72-054 R05)
MOC :
-RECOMMENDEDE1
SB FJ44-72-054R06
GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER
MOC :
-RECOMMENDEDE2
SB FJ44-72-054R06
GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER
MOC :
-CANCELLEDE1
SB FJ44-72-064R02
CANCELLED - ENGINE - 1ST REDUCTION BEVEL GEAR BEARING SUPPORT - REWORK OR REPLACE
MOC :
-CANCELLEDE2
SB FJ44-72-064R02
CANCELLED - ENGINE - 1ST REDUCTION BEVEL GEAR BEARING SUPPORT - REWORK OR REPLACE
MOC :
Page 45 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDEDE1
SB FJ44-72-066R02
ENGINE - HOUSING, CARBON RING SEAL AND BEARING (NO. 3 BEARING RETAINER) - REPLACE (SUPERSEDED BY FJ44-72-066 R03)
MOC :
-RECOMMENDEDE2
SB FJ44-72-066R02
ENGINE - HOUSING, CARBON RING SEAL AND BEARING (NO. 3 BEARING RETAINER) - REPLACE (SUPERSEDED BY FJ44-72-066 R03)
MOC :
-RECOMMENDEDE1
SB FJ44-72-066R03
ENGINE - HOUSING, CARBON RING SEAL AND BEARING (NO. 3 BEARING RETAINER) - REPLACE SERVICE BULLETIN (SUPERSEDED BY FJ44-72-066R04)
MOC :
-RECOMMENDEDE2
SB FJ44-72-066R03
ENGINE - HOUSING, CARBON RING SEAL AND BEARING (NO. 3 BEARING RETAINER) - REPLACE SERVICE BULLETIN (SUPERSEDED BY FJ44-72-066R04)
MOC :
-RECOMMENDEDE1
SB FJ44-72-066R05
ENGINE - CARBON RING SEAL AND BEARING HOUSING - REPLACE (SUPERSEDED BY FJ44-72-066 R06)
MOC :
-RECOMMENDEDE2
SB FJ44-72-066R05
ENGINE - CARBON RING SEAL AND BEARING HOUSING - REPLACE (SUPERSEDED BY FJ44-72-066 R06)
MOC :
-RECOMMENDED
E1
SB FJ44-72-066R06
CARBON RING SEAL AND BEARING HOUSING - REPLACE
MOC :
-RECOMMENDED
E2
SB FJ44-72-066R06
CARBON RING SEAL AND BEARING HOUSING - REPLACE
MOC :
-OPTIONALE1
SB FJ44-72-077R02
ENGINE - IP COMPRESSOR STATOR (STAGE 1-2) - REWORK (SUPERSEDED BY FJ44-72-077 R03)
MOC :
-OPTIONALE2
SB FJ44-72-077R02
ENGINE - IP COMPRESSOR STATOR (STAGE 1-2) - REWORK (SUPERSEDED BY FJ44-72-077 R03)
MOC :
-OPTIONALE1
SB FJ44-72-077R03
IP COMPRESSOR STATOR (STAGE 1-2) - REWORK (SUPERSEDED BY FJ44-72-077 R04)
MOC :
-OPTIONALE2
SB FJ44-72-077R03
IP COMPRESSOR STATOR (STAGE 1-2) - REWORK (SUPERSEDED BY FJ44-72-077 R04)
MOC :
-OPTIONAL
E1
SB FJ44-72-077R04
IP COMPRESSOR STATOR (STAGE 1-2) - REWORK
MOC :
-OPTIONAL
E2
SB FJ44-72-077R04
IP COMPRESSOR STATOR (STAGE 1-2) - REWORK
MOC :
Page 46 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-INFORMATIONALE1
SB FJ44-72-079R02
CANCELLED - ENGINE - MPI - TIME EXTENSION FOR TAP ENGINES
MOC :
-INFORMATIONALE2
SB FJ44-72-079R02
CANCELLED - ENGINE - MPI - TIME EXTENSION FOR TAP ENGINES
MOC :
-RECOMMENDEDE1
SB FJ44-72-080R01
ENGINE - 2ND REDUCTION BEVEL GEAR BALL BEARING (GEARBOX ASSEMBLY) - REPLACE
MOC :
-RECOMMENDEDE2
SB FJ44-72-080R01
ENGINE - 2ND REDUCTION BEVEL GEAR BALL BEARING (GEARBOX ASSEMBLY) - REPLACE
MOC :
HRS -RECOMMENDED (3500)9623.3 2442.9E1
SB FJ44-72-080R02
2ND REDUCTION BEVEL GEAR BALL BEARING (GEARBOX ASSEMBLY) - REPLACE
MOC :
HRS -RECOMMENDED (3500)9622.3 2441.9E2
SB FJ44-72-080R02
2ND REDUCTION BEVEL GEAR BALL BEARING (GEARBOX ASSEMBLY) - REPLACE
MOC :
-OPTIONALE1
SB FJ44-72-082R02
UPGRADE FJ44-2A GEARBOX (8K SPRING-LOADED) TO IMPROVED CONFIGURATION
MOC :
-OPTIONALE2
SB FJ44-72-082R02
UPGRADE FJ44-2A GEARBOX (8K SPRING-LOADED) TO IMPROVED CONFIGURATION
MOC :
-OPTIONALE1
SB FJ44-72-084R02
ENGINE- UPGRADE FJ44-2A GEARBOX (8K MAGSEAL) TO SPRING LOADED CONFIGURATION (SUPERSEDED BY FJ44-72-084 R03)
MOC :
-OPTIONALE2
SB FJ44-72-084R02
ENGINE- UPGRADE FJ44-2A GEARBOX (8K MAGSEAL) TO SPRING LOADED CONFIGURATION (SUPERSEDED BY FJ44-72-084 R03)
MOC :
-OPTIONALE1
SB FJ44-72-084R03
UPGRADE FJ44-2A GEARBOX (8K MAGSEAL) TO SPRING LOADED CONFIGURATION
MOC :
-OPTIONALE2
SB FJ44-72-084R03
UPGRADE FJ44-2A GEARBOX (8K MAGSEAL) TO SPRING LOADED CONFIGURATION
MOC :
-RECOMMENDEDE1
SB FJ44-72-085R01
ENGINE - IP BLEED VALVE - REPLACE (SUPERSEDED BY FJ44-72-085 R02)
MOC :
-RECOMMENDEDE2
SB FJ44-72-085R01
ENGINE - IP BLEED VALVE - REPLACE (SUPERSEDED BY FJ44-72-085 R02)
MOC :
Page 47 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDEDE1
SB FJ44-72-085R04
ENGINE - IP BLEED VALVE - REPLACE (SUPERSEDED BY FJ44-72-085 R05)
MOC :
-RECOMMENDEDE2
SB FJ44-72-085R04
ENGINE - IP BLEED VALVE - REPLACE (SUPERSEDED BY FJ44-72-085 R05)
MOC :
-RECOMMENDEDE1
SB FJ44-72-085R05
ENGINE - IP BLEED VALVE - REPLACE (SUPERSEDED BY FJ44-72-085 R06)
MOC :
-RECOMMENDEDE2
SB FJ44-72-085R05
ENGINE - IP BLEED VALVE - REPLACE (SUPERSEDED BY FJ44-72-085 R06)
MOC :
-RECOMMENDED
E1
SB FJ44-72-085R06
ENGINE - IP BLEED VALVE - REPLACE
MOC :
-RECOMMENDED
E2
SB FJ44-72-085R06
ENGINE - IP BLEED VALVE - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-72-086R02
ENGINE - BLEED VALVE SHAFT - REPLACE (SUPERSEDED BY FJ44-72-086 R03)
MOC :
-RECOMMENDEDE2
SB FJ44-72-086R02
ENGINE - BLEED VALVE SHAFT - REPLACE (SUPERSEDED BY FJ44-72-086 R03)
MOC :
-RECOMMENDED
E1
SB FJ44-72-086R03
ENGINE - BLEED VALVE SHAFT - REPLACE
MOC :
-RECOMMENDED
E2
SB FJ44-72-086R03
ENGINE - BLEED VALVE SHAFT - REPLACE
MOC :
HRS
DUE
DUERECOMMENDED (3500)9623.3 2442.9E1
SB FJ44-72-098 ENGINE - 1ST REDUCTION BEVEL GEAR BEARING SUPPORT - REWORK OR REPLACE
MOC :
HRS
DUE
DUERECOMMENDED (3500)9622.3 2441.9E2
SB FJ44-72-098 ENGINE - 1ST REDUCTION BEVEL GEAR BEARING SUPPORT - REWORK OR REPLACE
MOC :
-CANCELLEDE1
SB FJ44-72-108R01-CN
SUPERSEDED - ACCESSORY DRIVE SHAFT - REPLACE (THIS SERVICE DOCUMENT IS NO LONGER AVAILABLE)
MOC :
-CANCELLEDE2
SB FJ44-72-108R01-CN
SUPERSEDED - ACCESSORY DRIVE SHAFT - REPLACE (THIS SERVICE DOCUMENT IS NO LONGER AVAILABLE)
MOC :
Page 48 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDEDE1
SB FJ44-72-108R01
ACCESSORY DRIVE SHAFT - REPLACE (SUPERSEDED BY SB WISB-72-1037 R01)
MOC :
-RECOMMENDEDE2
SB FJ44-72-108R01
ACCESSORY DRIVE SHAFT - REPLACE (SUPERSEDED BY SB WISB-72-1037 R01)
MOC :
-RECOMMENDEDE1
SB FJ44-72-108 ACCESSORY DRIVE SHAFT - REPLACE (SUPERSEDED BY FJ44-72-108 R01)
MOC :
-RECOMMENDEDE2
SB FJ44-72-108 ACCESSORY DRIVE SHAFT - REPLACE (SUPERSEDED BY FJ44-72-108 R01)
MOC :
HRS
DUE
DUERECOMMENDED (3500)9623.3 2442.9E1
SB FJ44-72-109 ENGINE - 1ST REDUCTION BEVEL GEAR BALL BEARING - REPLACE
MOC :
HRS
DUE
DUERECOMMENDED (3500)9622.3 2441.9E2
SB FJ44-72-109 ENGINE - 1ST REDUCTION BEVEL GEAR BALL BEARING - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-72-111R01
ENGINE - 1ST LP TURBINE NOZZLE - INSPECTION (SUPERSEDED BY FJ44-72-111 R02)
MOC :
-RECOMMENDEDE2
SB FJ44-72-111R01
ENGINE - 1ST LP TURBINE NOZZLE - INSPECTION (SUPERSEDED BY FJ44-72-111 R02)
MOC :
-RECOMMENDED
E1
SB FJ44-72-111R02
ENGINE - 1ST LP TURBINE NOZZLE - INSPECTION
MOC :
-RECOMMENDED
E2
SB FJ44-72-111R02
ENGINE - 1ST LP TURBINE NOZZLE - INSPECTION
MOC :
-RECOMMENDEDE1
SB FJ44-72-111 ENGINE - 1ST LP TURBINE NOZZLE - INSPECTION (SUPERSEDED BY FJ44-72-111 R01)
MOC :
-RECOMMENDEDE2
SB FJ44-72-111 ENGINE - 1ST LP TURBINE NOZZLE - INSPECTION (SUPERSEDED BY FJ44-72-111 R01)
MOC :
HRS
MANDATORY(3500)9623.3 2442.9
E1
SB FJ44-72-115 ENGINE - DAMPENER BRACKET ASSEMBLY - INSTALL
MOC :
HRS
MANDATORY(3500)9622.3 2441.9
E2
SB FJ44-72-115 ENGINE - DAMPENER BRACKET ASSEMBLY - INSTALL
MOC :
HRS
DUE
DUERECOMMENDED
(3500)9623.3 2442.9E1
SB FJ44-72-116 DIFFUSER CASE ASSEMBLY - REWORK OR REPLACE
MOC :
HRS
DUE
DUERECOMMENDED
(3500)9622.3 2441.9E2
SB FJ44-72-116 DIFFUSER CASE ASSEMBLY - REWORK OR REPLACE
MOC :
Page 49 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDED
E1
SB FJ44-72-119 HP COMPRESSOR ROTOR - REWORK
MOC :
-RECOMMENDED
E2
SB FJ44-72-119 HP COMPRESSOR ROTOR - REWORK
MOC :
-OPTIONALE1
SB FJ44-72-120R02
OIL BREATHER TUBE ASSEMBLY, FRONT BYPASS DUCT ASSEMBLY, AND BREATHER TUBE ASSEMBLY - INSTALL (SUPERSEDED BY FJ44-72-120 R03)
MOC :
-OPTIONALE2
SB FJ44-72-120R02
OIL BREATHER TUBE ASSEMBLY, FRONT BYPASS DUCT ASSEMBLY, AND BREATHER TUBE ASSEMBLY - INSTALL (SUPERSEDED BY FJ44-72-120 R03)
MOC :
-OPTIONALE1
SB FJ44-72-120R03
OIL BREATHER TUBE ASSEMBLY, FRONT BYPASS DUCT ASSEMBLY, AND BREATHER TUBE ASSEMBLY - INSTALL (SUPERSEDED BY FJ44-72-120 R04)
MOC :
-OPTIONALE2
SB FJ44-72-120R03
OIL BREATHER TUBE ASSEMBLY, FRONT BYPASS DUCT ASSEMBLY, AND BREATHER TUBE ASSEMBLY - INSTALL (SUPERSEDED BY FJ44-72-120 R04)
MOC :
-OPTIONALE1
SB FJ44-72-120R04
OIL BREATHER TUBE ASSEMBLY, FRONT BYPASS DUCT ASSEMBLY, AND BREATHER TUBE ASSEMBLY - INSTALL
MOC :
-OPTIONALE2
SB FJ44-72-120R04
OIL BREATHER TUBE ASSEMBLY, FRONT BYPASS DUCT ASSEMBLY, AND BREATHER TUBE ASSEMBLY - INSTALL
MOC :
-RECOMMENDEDE1
SB FJ44-72-125R02
HP TURBINE BLADES - REPLACE AT CHECK 3 (SUPERSEDED BY FJ44-72-125 R03)
MOC :
-RECOMMENDEDE2
SB FJ44-72-125R02
HP TURBINE BLADES - REPLACE AT CHECK 3 (SUPERSEDED BY FJ44-72-125 R03)
MOC :
-RECOMMENDEDE1
SB FJ44-72-125R03
HP TURBINE BLADES - REPLACE (SUPERSEDED BY WISB-72-1009 R02)
MOC :
-RECOMMENDEDE2
SB FJ44-72-125R03
HP TURBINE BLADES - REPLACE (SUPERSEDED BY WISB-72-1009 R02)
MOC :
-RECOMMENDEDE1
SB FJ44-72-125 HP TURBINE BLADES - REPLACE AT CHECK 3 (SUPERSEDED BY FJ44-72-125 R01)
MOC :
-RECOMMENDEDE2
SB FJ44-72-125 HP TURBINE BLADES - REPLACE AT CHECK 3 (SUPERSEDED BY FJ44-72-125 R01)
MOC :
-MANDATORYE1
SB FJ44-72-129R01
INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE
MOC :
Page 50 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-MANDATORYE2
SB FJ44-72-129R01
INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-72-130R01
HP COMPRESSOR ROTOR - INSPECTION (SUPERSEDED BY FJ44-72-130 R02)
MOC :
-RECOMMENDEDE2
SB FJ44-72-130R01
HP COMPRESSOR ROTOR - INSPECTION (SUPERSEDED BY FJ44-72-130 R02)
MOC :
-RECOMMENDED
E1
SB FJ44-72-130R02
HP COMPRESSOR ROTOR - INSPECTION
MOC :
-RECOMMENDED
E2
SB FJ44-72-130R02
HP COMPRESSOR ROTOR - INSPECTION
MOC :
-RECOMMENDEDE1
SB FJ44-72-130 HP COMPRESSOR ROTOR - INSPECTION (SUPERSEDED BY FJ44-72-130 R01)
MOC :
-RECOMMENDEDE2
SB FJ44-72-130 HP COMPRESSOR ROTOR - INSPECTION (SUPERSEDED BY FJ44-72-130 R01)
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9623.3 2442.9E1
SB FJ44-72-133R01
REPLACE 1ST LP TURBINE NOZZLE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9622.3 2441.9E2
SB FJ44-72-133R01
REPLACE 1ST LP TURBINE NOZZLE
MOC :
-RECOMMENDEDE1
SB FJ44-72-133 REPLACE 1ST LP TURBINE NOZZLE (SUPERSEDED BY FJ44-72-133 R01)
MOC :
-RECOMMENDEDE2
SB FJ44-72-133 REPLACE 1ST LP TURBINE NOZZLE (SUPERSEDED BY FJ44-72-133 R01)
MOC :
-RECOMMENDEDE1
SB FJ44-72-134 1ST LP TURBINE NOZZLE HEATSHIELD HOUSING ASSEMBLY - REPLACE
MOC :
-RECOMMENDEDE2
SB FJ44-72-134 1ST LP TURBINE NOZZLE HEATSHIELD HOUSING ASSEMBLY - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-72-142R01
NO. 1 CARBON SEAL ASSEMBLY & SEAL RUNNER - REPLACE
MOC :
-RECOMMENDEDE2
SB FJ44-72-142R01
NO. 1 CARBON SEAL ASSEMBLY & SEAL RUNNER - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-72-142 NO. 1 CARBON SEAL ASSEMBLY & SEAL RUNNER - REPLACE
MOC :
Page 51 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDEDE2
SB FJ44-72-142 NO. 1 CARBON SEAL ASSEMBLY & SEAL RUNNER - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9623.3 2442.9E1
SB FJ44-72-143R01
BLEED VALVE SHAFT - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9622.3 2441.9E2
SB FJ44-72-143R01
BLEED VALVE SHAFT - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9623.3 2442.9
E1
SB FJ44-72-143 BLEED VALVE SHAFT - REPLACE (SUPERSEDED BY FJ44-72-143 R01)
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9622.3 2441.9
E2
SB FJ44-72-143 BLEED VALVE SHAFT - REPLACE (SUPERSEDED BY FJ44-72-143 R01)
MOC :
HRS
MTH -RECOMMENDED
(1750)7873.3 692.9
E1
SB FJ44-72-145 GEARBOX ASSEMBLY - INSTALL WASHER & SPRING CARTRIDGE ASSEMBLY
MOC :
HRS
MTH -RECOMMENDED
(1750)7872.3 691.9
E2
SB FJ44-72-145 GEARBOX ASSEMBLY - INSTALL WASHER & SPRING CARTRIDGE ASSEMBLY
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED (3500)9623.3 2442.9E1
SB FJ44-72-146 DIFFUSER CASE ASSEMBLY - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED (3500)9622.3 2441.9E2
SB FJ44-72-146 DIFFUSER CASE ASSEMBLY - REPLACE
MOC :
-RECOMMENDED
E1
SB FJ44-72-147R01
DIFFUSER CASE ASSEMBLY - INSPECTION
MOC :
-RECOMMENDED
E2
SB FJ44-72-147R01
DIFFUSER CASE ASSEMBLY - INSPECTION
MOC :
-RECOMMENDEDE1
SB FJ44-72-147 DIFFUSER CASE ASSEMBLY - INSPECTION
MOC :
-RECOMMENDEDE2
SB FJ44-72-147 DIFFUSER CASE ASSEMBLY - INSPECTION
MOC :
-RECOMMENDEDE1
SB FJ44-72-149R01
SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
Page 52 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDEDE2
SB FJ44-72-149R01
SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-72-149R02
SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-RECOMMENDEDE2
SB FJ44-72-149R02
SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-72-149 SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-RECOMMENDEDE2
SB FJ44-72-149 SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-RECOMMENDED
E1
SB FJ44-72-150R01
LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-RECOMMENDED
E2
SB FJ44-72-150R01
LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-
E1
SB FJ44-72-150R02
LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
-
E2
SB FJ44-72-150R02
LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
HRS
MTH
MPI
MPI
MPIRECOMMENDED (1750)7873.3 692.9
E1
SB FJ44-72-150R03
LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
HRS
MTH
MPI
MPI
MPIRECOMMENDED (1750)7872.3 691.9
E2
SB FJ44-72-150R03
LP REAR BEARING SEAL RETAINER - REPLACE
MOC :
MTH -RECOMMENDEDE1
SB FJ44-72-150 LP REAR BEARING SEAL RETAINER - REPLACE (SUPERSEDED BY FJ44-72-150 R01)
MOC :
MTH -RECOMMENDEDE2
SB FJ44-72-150 LP REAR BEARING SEAL RETAINER - REPLACE (SUPERSEDED BY FJ44-72-150 R01)
MOC :
-CANCELLEDE1
SB FJ44-72-56-CN CANCELED - ENGINE - CONVERSION - FJ44-2A (P/N 56000) TO FJ44-2A (56000-104)
MOC :
-CANCELLEDE2
SB FJ44-72-56-CN CANCELED - ENGINE - CONVERSION - FJ44-2A (P/N 56000) TO FJ44-2A (56000-104)
MOC :
Page 53 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-CANCELLEDE1
SB WI-72-1008 R01-CN
CANCELED - ENGINE - HIGH PRESSURE TURBINE ROTOR - REPLACE
MOC :
-CANCELLEDE2
SB WI-72-1008 R01-CN
CANCELED - ENGINE - HIGH PRESSURE TURBINE ROTOR - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUEMANDATORY
(1750)7873.3 692.9
E1
SB WI-72-1008 R01 HIGH PRESSURE TURBINE BLADES - REPLACE (SUPERSEDED BY SB WISB-72-1040)
MOC :
HRS
MTH
DUE
DUE
DUEMANDATORY
(1750)7872.3 691.9
E2
SB WI-72-1008 R01 HIGH PRESSURE TURBINE BLADES - REPLACE (SUPERSEDED BY SB WISB-72-1040)
MOC :
-MANDATORYE1
SB WI-72-1008 HIGH PRESSURE TURBINE ROTOR - REPLACE (SUPERSEDED BY WISB-72-1008 R01)
MOC :
-MANDATORYE2
SB WI-72-1008 HIGH PRESSURE TURBINE ROTOR - REPLACE (SUPERSEDED BY WISB-72-1008 R01)
MOC :
-RECOMMENDED
E1
SB WI-72-1009 R02 TURBINE BLADES - REPLACE
MOC :
-RECOMMENDED
E2
SB WI-72-1009 R02 TURBINE BLADES - REPLACE
MOC :
-MANDATORY
E1
SB WI-72-1009 TURBINE BLADES - REPLACE
MOC :
-MANDATORY
E2
SB WI-72-1009 TURBINE BLADES - REPLACE
MOC :
-MANDATORYE1
SB WI-72-1032 R01 HIGH PRESSURE TURBINE DISK - REPLACE
MOC :
-MANDATORYE2
SB WI-72-1032 R01 HIGH PRESSURE TURBINE DISK - REPLACE
MOC :
LDG
MTH
130MANDATORY (821)5049 114E1
SB WI-72-1032 R02 HIGH PRESSURE TURBINE DISK - REPLACE
MOC :
LDG
MTH
130MANDATORY (823)5049 114E2
SB WI-72-1032 R02 HIGH PRESSURE TURBINE DISK - REPLACE
MOC :
-MANDATORYE1
SB WI-72-1032 HIGH PRESSURE TURBINE DISK - REPLACE
MOC :
-MANDATORYE2
SB WI-72-1032 HIGH PRESSURE TURBINE DISK - REPLACE
MOC :
-RECOMMENDEDE1
SB WI-72-1037 R01 ACCESSORY DRIVE TOWERSHAFT - REPLACE
MOC :
Page 54 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDEDE2
SB WI-72-1037 R01 ACCESSORY DRIVE TOWERSHAFT - REPLACE
MOC :
MTH
CSI
CSIRECOMMENDED
New ReqE1
SB WI-72-1037 R02 ACCESSORY DRIVE TOWERSHAFT - REPLACE
MOC :
MTH
CSI
CSIRECOMMENDED
New ReqE2
SB WI-72-1037 R02 ACCESSORY DRIVE TOWERSHAFT - REPLACE
MOC :
-RECOMMENDEDE1
SB WI-72-1040 R01 HIGH PRESSURE TURBINE BLADES - REPLACE
MOC :
-RECOMMENDEDE2
SB WI-72-1040 R01 HIGH PRESSURE TURBINE BLADES - REPLACE
MOC :
MTH
MPI
MPIRECOMMENDED
New ReqE1
SB WI-72-1040 R02 HIGH PRESSURE TURBINE BLADES - REPLACE
MOC :
MTH
MPI
MPIRECOMMENDED
New ReqE2
SB WI-72-1040 R02 HIGH PRESSURE TURBINE BLADES - REPLACE
MOC :
-RECOMMENDEDE1
SB WI-72-1040 HIGH PRESSURE TURBINE BLADES - REPLACE
MOC :
-RECOMMENDEDE2
SB WI-72-1040 HIGH PRESSURE TURBINE BLADES - REPLACE
MOC :
MTH
MPI
MPIRECOMMENDEDE1
SB WI-72-1041 HEAT EXCHANGER CLAMP ASSEMBLY - REPLACE
MOC :
MTH
MPI
MPIRECOMMENDEDE2
SB WI-72-1041 HEAT EXCHANGER CLAMP ASSEMBLY - REPLACE
MOC :
-CANCELLEDE1
SL WI-72-1032-CN APPROVED ENGINE FUELS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-CANCELLEDE2
SL WI-72-1032-CN APPROVED ENGINE FUELS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E1
SL WI-72-1080 VISUALLY INSPECT THE 2ND LP TURBINE NOZZLE ASSEMBLY - REVISION TO ENGINE MANUAL
MOC :
-E2
SL WI-72-1080 VISUALLY INSPECT THE 2ND LP TURBINE NOZZLE ASSEMBLY - REVISION TO ENGINE MANUAL
MOC :
-E1
SL WI-72-1128 FAN ROTOR - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E2
SL WI-72-1128 FAN ROTOR - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-CANCELLEDE1
SL WI-72-1132-CN CANCELED - ENGINE - APPROVED ENGINE FUELS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
Page 55 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-CANCELLEDE2
SL WI-72-1132-CN CANCELED - ENGINE - APPROVED ENGINE FUELS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E1
SL WI-72-1132 APPROVED ENGINE FUELS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E2
SL WI-72-1132 APPROVED ENGINE FUELS - REVISION TO LINE MAINTENANCE MANUAL
MOC :
-E1
SL WI-72-1140 INDUCTION HEATING - REVISION TO ENGINE MANUAL
MOC :
-E2
SL WI-72-1140 INDUCTION HEATING - REVISION TO ENGINE MANUAL
MOC :
A/RRECOMMENDEDE1
SB FJ44-73-017R05
ENGINE FUEL AND CONTROL ¿ FUEL CONTROL UNIT ¿ REMOVE, INSTALL
MOC :
A/RRECOMMENDEDE2
SB FJ44-73-017R05
ENGINE FUEL AND CONTROL ¿ FUEL CONTROL UNIT ¿ REMOVE, INSTALL
MOC :
-OPTIONALE1
SB FJ44-73-041R01
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R02)
MOC :
-OPTIONALE2
SB FJ44-73-041R01
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R02)
MOC :
-OPTIONALE1
SB FJ44-73-041R02
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R03)
MOC :
-OPTIONALE2
SB FJ44-73-041R02
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R03)
MOC :
-OPTIONALE1
SB FJ44-73-041R03
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R04)
MOC :
-OPTIONALE2
SB FJ44-73-041R03
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R04)
MOC :
-OPTIONALE1
SB FJ44-73-041R04
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R05)
MOC :
-OPTIONALE2
SB FJ44-73-041R04
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R05)
MOC :
-OPTIONALE1
SB FJ44-73-041R05
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R06)
MOC :
Page 56 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-OPTIONALE2
SB FJ44-73-041R05
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE (SUPERSEDED BY FJ44-73-041 R06)
MOC :
-OPTIONALE1
SB FJ44-73-041R06
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE
MOC :
-OPTIONALE2
SB FJ44-73-041R06
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE
MOC :
-OPTIONALE1
SB FJ44-73-041R07
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE
MOC :
-OPTIONALE2
SB FJ44-73-041R07
ENGINE FUEL AND CONTROL - ECU - INSTALL CP317.03 SOFTWARE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(1169.2)7292.5 112.1E1
SB FJ44-73-062R01
ENGINE FUEL AND CONTROL - FUEL FLOW TO OIL COOLER TUBE ASSEMBLY - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(1170.2)7292.5 112.1E2
SB FJ44-73-062R01
ENGINE FUEL AND CONTROL - FUEL FLOW TO OIL COOLER TUBE ASSEMBLY - REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-73-062 ENGINE FUEL AND CONTROL - FUEL FLOW TO OIL COOLER TUBE ASSEMBLY - REPLACE
MOC :
-RECOMMENDEDE2
SB FJ44-73-062 ENGINE FUEL AND CONTROL - FUEL FLOW TO OIL COOLER TUBE ASSEMBLY - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9623.3 2442.9
E1
SB WI-73-1000 R01 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED
(3500)9622.3 2441.9
E2
SB WI-73-1000 R01 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE
MOC :
-RECOMMENDEDE1
SB WI-73-1000 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE
MOC :
-RECOMMENDEDE2
SB WI-73-1000 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE
MOC :
HRS
MTH
1775
01-Jun-1988 A/ROPTIONAL
Complete74SB-1
SB 500-74-01
JHB
IGNITION - DUAL IGNITION EXCITER BOX INSTALLATION
COMPLIED WITHMOC :
Page 57 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
DAYS
4543
6582.8
20-Sep-2013 -MANDATORY N/A
SL CIL-74-01 REV01 CYHM
INSPECTION OF IGNITION CABLE AND THROTTLE LINKAGE
NOT APPLICABLE - N/A DUE TO EQUIPMENT NOT INSTALLED.MOC :
LDG
HRS
DAYS
4543
6582.8
20-Sep-2013 -MANDATORY N/A
SL CIL-74-01
CYHM
INSPECTION OF IGNITION CABLE AND THROTTLE LINKAGE (SUPERSEDED BY CIL-74-01 REV 01)
NOT APPLICABLE - N/A DUE TO EQUIPMENT NOT INSTALLEDMOC :
HRS
MTH
4870
16-Apr-2001 A/RRECOMMENDED
Complete74SL-04
SL 500-74-04
SJC
IGNITION - TRANSMITTAL OF PRATT & WHITNEY CANADA SERVICE BULLETIN 7567R1 TURBOFAN ENGINE IGNITER BOX GROUNDING STRAP -INTRODUCTION OF
COMPLIED WITH - SERVICE INFORMATION ITEM COMPLIED WITH PREVIOUSLY. DATE AND OR HOURS UNKNOWN.MOC :
-MANDATORYE1
SB WI-74-1002 R01 IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT (SUPERSEDED BY WISB-74-1002 R02)
MOC :
-MANDATORYE2
SB WI-74-1002 R01 IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT (SUPERSEDED BY WISB-74-1002 R02)
MOC :
LDG
HRS
MTH
4873
7097.3
17-Jul-2019 -MANDATORY CompleteE1
SB WI-74-1002 R02
UNK
IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT
COMPLIED WITHMOC :
LDG
HRS
MTH
4873
7097.3
17-Jul-2019 -MANDATORY CompleteE2
SB WI-74-1002 R02
UNK
IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT
COMPLIED WITHMOC :
-MANDATORYE1
SB WI-74-1002 IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT (SUPERSEDED BY WISB-74-1002 R01)
MOC :
-MANDATORYE2
SB WI-74-1002 IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT (SUPERSEDED BY WISB-74-1002 R01)
MOC :
-RECOMMENDEDE1
SB FJ44-75-002R02
ENGINE - COMPRESSOR BLEED VALVE RETURN SPRING - REPLACE
MOC :
-RECOMMENDEDE2
SB FJ44-75-002R02
ENGINE - COMPRESSOR BLEED VALVE RETURN SPRING - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED (3500)9623.3 2442.9E1
SB WI-75-1001 R01 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED (3500)9622.3 2441.9E2
SB WI-75-1001 R01 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE
MOC :
Page 58 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-RECOMMENDEDE1
SB WI-75-1001 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE
MOC :
-RECOMMENDEDE2
SB WI-75-1001 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE
MOC :
-CANCELLEDE1
SL WI-76-1001-CN CANCELED - ENGINE CONTROLS - VISUALLY INSPECT THE LP SHAFT TRIP SENSOR SYSTEM - REVISION TO THE LINE MAINTENANCE MANUAL
MOC :
-CANCELLEDE2
SL WI-76-1001-CN CANCELED - ENGINE CONTROLS - VISUALLY INSPECT THE LP SHAFT TRIP SENSOR SYSTEM - REVISION TO THE LINE MAINTENANCE MANUAL
MOC :
-E1
SL WI-76-1001 ENGINE CONTROLS - VISUALLY INSPECT THE LP SHAFT TRIP SENSOR SYSTEM - REVISION TO THE LINE MAINTENANCE MANUAL
MOC :
-E2
SL WI-76-1001 ENGINE CONTROLS - VISUALLY INSPECT THE LP SHAFT TRIP SENSOR SYSTEM - REVISION TO THE LINE MAINTENANCE MANUAL
MOC :
-E1
SB FJ44-77-006R02
ENGINE INDICATING - ENGINE EFCU HARNESS ASSEMBLY - REWORK CONNECTOR/BACKSHELL
MOC :
-E2
SB FJ44-77-006R02
ENGINE INDICATING - ENGINE EFCU HARNESS ASSEMBLY - REWORK CONNECTOR/BACKSHELL
MOC :
MTH A/ROPTIONAL78SB-1
SB 500-78-01 EXHAUST - THRUST REVERSER INSTALLATION (SUPERSEDED BY 500-78-01 REV 01)
- OPERATOR DOES NOT WISH TO COMPLY AT THIS TIMEMOC :
MTH A/ROPTIONAL78SB-12 : 500
SB 500-78-12 EXHAUST - THRUST REVERSER THROTTLE STOP SOLENOID GROUND IMPROVEMENT
MOC :
-RECOMMENDEDE1
SB FJ44-79-007R03
ENGINE - LUBE PUMP - REWORK TO P/N 110487 (SUPERSEDED BY FJ44-79-007 R04)
MOC :
-RECOMMENDEDE2
SB FJ44-79-007R03
ENGINE - LUBE PUMP - REWORK TO P/N 110487 (SUPERSEDED BY FJ44-79-007 R04)
MOC :
-RECOMMENDED
E1
SB FJ44-79-007R04
ENGINE - LUBE PUMP - REWORK TO P/N 110487
MOC :
-RECOMMENDED
E2
SB FJ44-79-007R04
ENGINE - LUBE PUMP - REWORK TO P/N 110487
MOC :
Page 59 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4626
6711.2
01-Mar-2015 -RECOMMENDED N/AE1
SB FJ44-79-008R01 CYHM
ENGINE - OIL FILLER CAP AND DIPSTICK ASSEMBLY - REPLACE (SUPERSEDED BY FJ44-79-008 R02)
NOT APPLICABLE - N/A DUE TO ENGINE SERIAL NUMBER EFFECTIVITYMOC :
LDG
HRS
MTH
4626
6711.2
02-Mar-2015 -RECOMMENDED N/AE2
SB FJ44-79-008R01 CYHM
ENGINE - OIL FILLER CAP AND DIPSTICK ASSEMBLY - REPLACE (SUPERSEDED BY FJ44-79-008 R02)
NOT APPLICABLE - N/A DUE TO ENGINE SERIAL NUMBER EFFECTIVITYMOC :
LDG
HRS
MTH
4626
6711.2
01-Mar-2015 -RECOMMENDED
N/A
E1
SB FJ44-79-008R02 CYHM
OIL FILLER CAP AND DIPSTICK ASSEMBLY - REPLACE
NOT APPLICABLE - N/A DUE TO ENGINE SERIAL NUMBER EFFECTIVITYMOC :
LDG
HRS
MTH
4626
6711.2
02-Mar-2015 -RECOMMENDED
Complete
E2
SB FJ44-79-008R02 CYHM
OIL FILLER CAP AND DIPSTICK ASSEMBLY - REPLACE
COMPLIED WITH - N/A DUE TO ENGINE SERIAL NUMBER EFFECTIVITYMOC :
HRS
MTH
DUE
DUE
DUEMANDATORY
(3500)9623.3 2442.9E1
SB FJ44-79-011R01
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R02)
MOC :
HRS
MTH
DUE
DUE
DUEMANDATORY
(3500)9622.3 2441.9E2
SB FJ44-79-011R01
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R02)
MOC :
-MANDATORYE1
SB FJ44-79-011R02
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R03)
MOC :
-MANDATORYE2
SB FJ44-79-011R02
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R03)
MOC :
-MANDATORYE1
SB FJ44-79-011R03
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R04)
MOC :
-MANDATORYE2
SB FJ44-79-011R03
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R04)
MOC :
-MANDATORY
E1
SB FJ44-79-011R04
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE
MOC :
-MANDATORY
E2
SB FJ44-79-011R04
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE
MOC :
-MANDATORY
E1
SB FJ44-79-011R05
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE
MOC :
Page 60 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-MANDATORY
E2
SB FJ44-79-011R05
OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE
MOC :
HRS
DUE
DUEMANDATORY (3500)9623.3 2442.9E1
SB FJ44-79-011 OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R01)
MOC :
HRS
DUE
DUEMANDATORY (3500)9622.3 2441.9E2
SB FJ44-79-011 OIL - MAGNETIC SELF-CLOSING VALVE - REPLACE (SUPERSEDED BY FJ44-79-011 R01)
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED (3500)9623.3 2442.9
E1
SB FJ44-79-012R01
OIL - LUBE OIL COOLER - REWORK OR REPLACE
MOC :
HRS
MTH
DUE
DUE
DUERECOMMENDED (3500)9622.3 2441.9
E2
SB FJ44-79-012R01
OIL - LUBE OIL COOLER - REWORK OR REPLACE
MOC :
-RECOMMENDEDE1
SB FJ44-79-012 OIL - LUBE OIL COOLER - REWORK OR REPLACE (SUPERSEDED BY FJ44-79-012 R01)
MOC :
-RECOMMENDEDE2
SB FJ44-79-012 OIL - LUBE OIL COOLER - REWORK OR REPLACE (SUPERSEDED BY FJ44-79-012 R01)
MOC :
-RECOMMENDED
E1
SB FJ44-79-015 CANCELLED - OIL - LUBE AND SCAVENGE PUMP ASSEMBLY - TIME EXTENSION OF TIME BETWEEN OVERHAUL (TBO) FOR TOTAL ASSURANCEPROGRAM (TAP)
MOC :
-RECOMMENDED
E2
SB FJ44-79-015 CANCELLED - OIL - LUBE AND SCAVENGE PUMP ASSEMBLY - TIME EXTENSION OF TIME BETWEEN OVERHAUL (TBO) FOR TOTAL ASSURANCEPROGRAM (TAP)
MOC :
-RECOMMENDEDE1
SL 44-79-013 R02 OIL FILLER CAP AND DIPSTICK ASSEMBLY - ADDITIONAL OIL LEVEL MARKS
MOC :
-RECOMMENDEDE2
SL 44-79-013 R02 OIL FILLER CAP AND DIPSTICK ASSEMBLY - ADDITIONAL OIL LEVEL MARKS
MOC :
-E1
SL WI-79-1008 OIL - LOW OIL LEVEL SENSOR - REVISION TO ILLUSTRATED PARTS CATALOG
MOC :
-E2
SL WI-79-1008 OIL - LOW OIL LEVEL SENSOR - REVISION TO ILLUSTRATED PARTS CATALOG
MOC :
HRS
MTH
187
18-Oct-1983 A/RRECOMMENDED
Complete80SB-4
SB 500-80-04
JHB
STARTING - START CIRCUIT WIRING MODIFICATION
COMPLIED WITHMOC :
MTH A/ROPTIONAL80SB-05
SB 500-80-05 STARTING - REPLACEMENT OF SUPPRESSION DIODE WITH TRANSZORB
MOC :
-CANCELLED
SL CIL-99-01 R03 MISCELLANEOUS - USE OF CORROSION INHIBITING COMPOUNDS
MOC :
Page 61 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-CANCELLED
SL CIL-99-02 R01 MISCELLANEOUS - AVOID OPERATIONS ON RUNWAYS TREATED WITH RUNWAY DE-ICE (RDI) FLUIDS. AIRCRAFT WASHING RECOMMENDED AFTEREXPOSURE TO RDI FLUIDS
MOC :
-CANCELLED
SL CIL-99-03 R02 MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)
MOC :
-CANCELLED
SL CIL-99-04 R01 MISCELLANEOUS - INCREMENTAL LIBRARY UPDATES FOR CESVIEW
MOC :
Page 62 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
5719
25-Nov-2005 -MANDATORY Complete
30AD-02
FAA 1998-04-38
YHM
TO MINIMIZE THE POTENTIAL HAZARDS ASSOCIATED WITH OPERATING THE AIRPLANE IN SEVERE ICING CONDITIONS BY PROVIDING MORE CLEARLYDEFINED PROCEDURES AND LIMITATIONS ASSOCIATED WITH SUCH CONDITIONS
COMPLIED WITHMOC :
HRS
MTH
5719
25-Nov-2005 -MANDATORY N/A34AD-26
FAA 2001-23-17
YHM
APPLIANCE AD - GNS 430 UNITS, PART NUMBER 011-00280-00; REFER TO AD FOR SERIAL NUMBER EFFECTIVITY.
NOT APPLICABLE - NOT APPLICABLE BY COMPONENT PART NUMBER.MOC :
HRS
MTH
5820
01-Jul-2006 - Complete
26AD-02
FAA 2006-04-10
YHM
THIS AD REQUIRES INSTALLING IDENTIFICATION SLEEVES ON THE WIRES FOR THE POSITIVE AND NEGATIVE STUDS OF THE ENGINE AND/ OR (APU)FIRE EXTINGUISHING BOTTLES, AS APPICABLE, AND RECONNECTING THE WIRES TO THE CORRECT TERMINAL STUDS. (SUPERSEDED BY AD 2007-11-17)
COMPLIED WITHMOC :
HRS
MTH
5719
25-Nov-2005 A/R N/A34AD-28
FAA 2004-08-15
YHM
APPLIANCE AD - PREVENT THE LOADING OF THE BARO SET POTENTIOMETER, WHICH COULD RESULT IN AN UNACCEPTABLE ALTITUDE ERROR.
NOT APPLICABLE - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :
LDG
HRS
MTH
4230
6121
20-Sep-2008 - Complete32AD-01
FAA 2004-09-05
YHM
PREVENT JAMMING OF THE WHEEL/TIRE ASSEMBLY
COMPLIED WITHMOC :
MTH 01-Jun-1990 -MANDATORY Complete21AD-01
FAA 1990-07-10R01 *CF
FREON AIR CONDITIONERS INSTALLED IN THE AFT SECTION OF THE BAGGAGECOMPARTMENT.
COMPLIED WITHMOC :
HRS
MTH
3768
26-Mar-1996 -MANDATORY Complete21AD-02
FAA 1995-25-10
SJC
REPLACE THE OUTFLOW SAFETY VALVE IN ACCORDANCE WITH ALLIED SIGNAL SEVICE BULLETIN 103576-21-4056.
COMPLIED WITHMOC :
LDG
HRS
DAYS
4521
6554.8
16-Jul-2013 -MANDATORY N/A
FAA 2013-09-11PARA (G)
CYHM
AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR DEACTIVATION OF THEA/C SYSTEM INSPECTION FOR PART NUMBER (P/N)
NOT APPLICABLE - N/A DUE TO THE APPLICABILITY OF EQUIPMENT INSTALLED AT THIS TIME( P/N 61108-1COMPRESSORMOTOR)
MOC :
LDG
HRS
DAYS
4521
6554.8
16-Jul-2013 -MANDATORY N/A
FAA 2013-09-11PARA (H)
CYHM
AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR DEACTIVATION OF THEA/C SYSTEM INSPECTION A\C COMPRESSOR HOUR METER AND MAINTENANCE RECORDS
NOT APPLICABLE - N/A DUE TO THE APPLICABILITY OF EQUIPMENT INSTALLED AT THIS TIME( P/N 61108-1COMPRESSORMOTOR)
MOC :
Page 63 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4521
6554.8
16-Jul-2013 -MANDATORY N/A
FAA 2013-09-11PARA (I) & (J)
CYHM
AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR DEACTIVATION OF THEA/C SYSTEM REPLACEMENT OF A/C COMPRESSOR MOTOR BRUSHES AND RELATED MAINTENANCE MANUAL INFORMATION
NOT APPLICABLE - N/A DUE TO THE APPLICABILITY OF EQUIPMENT INSTALLED AT THIS TIME( P/N 61108-1COMPRESSORMOTOR)
MOC :
LDG
HRS
MTH
4521
6554.8
16-Jul-2013 A/RMANDATORY N/A
FAA 2013-09-11PARA (K)
CYHM
AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR DEACTIVATION OF THEA/C SYSTEM DEACTIVATION OF A/C SYSTEM
NOT APPLICABLE - N/A DUE TO THE APPLICABILITY OF EQUIPMENT INSTALLED AT THIS TIME( P/N 61108-1COMPRESSORMOTOR)
MOC :
LDG
HRS
MTH
4521
6554.8
16-Jul-2013 A/RMANDATORY N/A
FAA 2013-09-11PARA (L)
CYHM
AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR DEACTIVATION OF THEA/C SYSTEM REACTIVATION OF A/C SYSTEM
NOT APPLICABLE - N/A DUE TO THE APPLICABILITY OF EQUIPMENT INSTALLED AT THIS TIME( P/N 61108-1COMPRESSORMOTOR)
MOC :
LDG
HRS
DAYS
4521
6554.8
16-Jul-2013 -MANDATORY N/A
FAA 2013-09-11PARA (M)
CYHM
AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR DEACTIVATION OF THEA/C SYSTEM PARTS RETURN AND REPORTING REQUIREMENTS
NOT APPLICABLE - N/A DUE TO THE APPLICABILITY OF EQUIPMENT INSTALLED AT THIS TIME( P/N 61108-1COMPRESSORMOTOR)
MOC :
LDG
HRS
MTH
4521
6554.8
16-Jul-2013 -MANDATORY
N/A
FAA 2013-09-11
CYHM
AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON A/C COMPRESSOR MOTORS, PART NOS. 1134104-1/1134104-5, OR DEACTIVATION OF THEA/C SYSTEM
NOT APPLICABLE - N/A DUE TO THE APPLICABILITY OF EQUIPMENT INSTALLED AT THIS TIME( P/N 61108-1COMPRESSORMOTOR)
MOC :
LDG
HRS
DAYS
4668
6782
06-Nov-2015 -MANDATORY N/A
FAA 2015-17-12PARA (G) CYHM
INSPECT THE A/C COMPRESSOR MOTOR TO DETERMINE WHETHER P/N FWA1134104-1 OR P/N FWA1134104-5 IS INSTALLED
NOT APPLICABLE - FOUND TO BE NOT APPLICABLE DUE TO PART NUMBER EFFECTIVITY- PART NUMBER INSTALLED AT THISTIME IS 61108-1. VAPOR CYCLE COOLING SYSTEM HOUR METER NOT INSTALLED ON 501-0320#667 AS PEROWNERSREQUEST.
MOC :
LDG
HRS
DAYS
4668
6782
06-Nov-2015 -MANDATORY N/A
FAA 2015-17-12PARA (H)
CYHM
DETERMINE THE HOUR READING ON THE A/C COMPRESSOR HOUR METER (IF, DURING THE INSPECTION REQUIRED BY PARA (G) OF THIS AD, ANY A/CCOMPRESSOR MOTOR HAVING P/N FWA1134104-1 OR P/N FWA1134104-5 IS FOUND
NOT APPLICABLE - FOUND TO BE NOT APPLICABLE DUE TO PART NUMBER EFFECTIVITY- PART NUMBER INSTALLED AT THISTIME IS 61108-1. VAPOR CYCLE COOLING SYSTEM HOUR METER NOT INSTALLED ON 501-0320#667 AS PEROWNERSREQUEST.
MOC :
Page 64 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4668
6782
06-Nov-2015 -MANDATORY N/A
FAA 2015-17-12PARA (I)
CYHM
REPLACE THE A/C COMPRESSOR MOTOR BRUSHES WITH NEW BRUSHES (USING THE HOUR READING ON THE A/C COMPRESSOR HOUR METERDETERMINED IN PARA (H) OF THIS AD)
NOT APPLICABLE - FOUND TO BE NOT APPLICABLE DUE TO PART NUMBER EFFECTIVITY- PART NUMBER INSTALLED AT THISTIME IS 61108-1. VAPOR CYCLE COOLING SYSTEM HOUR METER NOT INSTALLED ON 501-0320#667 AS PEROWNERSREQUEST.
MOC :
LDG
HRS
MTH
4668
6782
06-Nov-2015 -MANDATORY N/A
FAA 2015-17-12PARA (K) CYHM
DEACTIVATE THE A/C SYSTEM (IN LIEU OF REPLACING THE A/C COMPRESSOR MOTOR BRUSHES AS REQUIRED BY THIS AD)
NOT APPLICABLE - FOUND TO BE NOT APPLICABLE DUE TO PART NUMBER EFFECTIVITY- PART NUMBER INSTALLED AT THISTIME IS 61108-1. VAPOR CYCLE COOLING SYSTEM HOUR METER NOT INSTALLED ON 501-0320#667 AS PEROWNERSREQUEST.
MOC :
LDG
HRS
MTH
4668
6782
06-Nov-2015 -MANDATORY N/A
FAA 2015-17-12PARA (L)
CYHM
IF THE A/C SYSTEM IS DEACTIVATED, AS SPECIFIED IN PARA (K), PRIOR TO THE A/C SYSTEM BEING REACTIVATED: PERFORM THE INSPECTIONSPECIFIED IN PARA (H), AND DO THE REPLACEMENTS SPECIFIED IN PARA (I), AT THE TIMES SPECIFIED IN PARA (I). RETURN THE A/C SYSTEM TOSERVICE
NOT APPLICABLE - FOUND TO BE NOT APPLICABLE DUE TO PART NUMBER EFFECTIVITY- PART NUMBER INSTALLED AT THISTIME IS 61108-1. VAPOR CYCLE COOLING SYSTEM HOUR METER NOT INSTALLED ON 501-0320#667 AS PEROWNERSREQUEST.
MOC :
LDG
HRS
DAYS
4668
6782
06-Nov-2015 -MANDATORY N/A
FAA 2015-17-12PARA (M) CYHM
SEND THE REMOVED BRUSHES TO CESSNA AIRCRAFT COMPANY
NOT APPLICABLE - FOUND TO BE NOT APPLICABLE DUE TO PART NUMBER EFFECTIVITY- PART NUMBER INSTALLED AT THISTIME IS 61108-1. VAPOR CYCLE COOLING SYSTEM HOUR METER NOT INSTALLED ON 501-0320#667 AS PEROWNERSREQUEST.
MOC :
LDG
HRS
MTH
4668
6782
06-Nov-2015 -MANDATORY N/A
FAA 2015-17-12
CYHM
AIR CONDITIONING - INSPECTIONS TO DETERMINE IF CERTAIN A/C COMPRESSOR MOTORS ARE INSTALLED AND TO DETERMINE THE ACCUMULATEDHOURS ON CERTAIN A/C COMPRESSOR MOTOR ASSEMBLIES; AND REPETITIVE REPLACEMENT OF THE BRUSHES IN THE A/C COMPRESSOR MOTORASSEMBLY, OR, AS AN OPTION TO THE BRUSH REPLACEMENT, DEACTIVATION OF THE A/C SYSTEM AND PLACARD INSTALLATION; AND RETURN OFREPLACED BRUSHES TO CESSNA
NOT APPLICABLE - FOUND TO BE NOT APPLICABLE DUE TO PART NUMBER EFFECTIVITY- PART NUMBER INSTALLED AT THISTIME IS 61108-1. VAPOR CYCLE COOLING SYSTEM HOUR METER NOT INSTALLED ON 501-0320#667 AS PEROWNERSREQUEST.
MOC :
LDG
HRS
DAYS
4543
6582.8
20-Sep-2013 -MANDATORY N/A
TCCA CF-2013-25
CYHM
APPLIANCE AD - EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING INSTALLATION DISCREPANCIES
NOT APPLICABLE - N/A DUE TO EQUIPMENT NOT INSTALLEDMOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2013-0020R04 (1)
CYHM
INSPECT THE MARKINGS OF SAFETY BELTS AND/OR TORSO RESTRAINT SYSTEMS, TO DETERMINE IF THEY HAVE BEEN MAINTAINED OR REPAIREDBY ORGANISATIONS OTHER THAN THE DESIGN APPROVAL HOLDER
NOT APPLICABLE - N/A DUE TO PREVIOUS WORK CARRIED OUT BY C&M MARINE AVIATION SERVICES INC WHICH ISAPPROVED UNDER SIL SSP-006
MOC :
Page 65 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2013-0020R04 (2)
CYHM
VERIFY IF THE ORGANISATION IS LISTED AMONG THE AUTHORIZED MAINTENANCE OR REPAIR ORGANISATION REFERENCE DOCUMENTS QUOTED INTHE REF. PUBLICATIONS SECTION OF THIS AD
NOT APPLICABLE - N/A DUE TO PREVIOUS WORK CARRIED OUT BY C&M MARINE AVIATION SERVICES INC WHICH ISAPPROVED UNDER SIL SSP-006
MOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2013-0020R04 (3) CYHM
REMOVE AND REPLACE BELTS NOT MEETING THE CERTIFICATION REQUIREMENTS OR MAKE RELEVANT SEAT INOPERATIVE
NOT APPLICABLE - N/A DUE TO PREVIOUS WORK CARRIED OUT BY C&M MARINE AVIATION SERVICES INC WHICH ISAPPROVED UNDER SIL SSP-006
MOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2013-0020R04 (4)
CYHM
AFTER 14 FEBRUARY 2013 [THE EFFECTIVE DATE OF THE ORIGINAL ISSUE OF THIS AD], DO NOT INSTALL SAFETY BELTS OR TORSO RESTRAINTSYSTEMS ON ANY AIRCRAFT, UNLESS INSPECTED AND CORRECTED IN COMPLIANCE WITH THE REQUIREMENTS OF THIS AD
NOT APPLICABLE - N/A DUE TO PREVIOUS WORK CARRIED OUT BY C&M MARINE AVIATION SERVICES INC WHICH ISAPPROVED UNDER SIL SSP-006
MOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2013-0020R04 CYHM
APPLIANCE AD - EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENT
NOT APPLICABLE - N/A DUE TO PREVIOUS WORK CARRIED OUT BY C&M MARINE AVIATION SERVICES INC WHICH ISAPPROVED UNDER SIL SSP-006
MOC :
-MANDATORY
EASA 2014-0187PARA (1)
INSPECT THE SAFETY BELT ATTACHMENT BOLTS
MOC :
-MANDATORY
EASA 2014-0187PARA (2)
IF, DURING THE INSPECTION AS REQUIRED BY PARAGRAPH (1) OF THIS AD, DETACHED OR LOOSENED SAFETY BELT ATTACHMENT BOLTS AREFOUND, BEFORE NEXT FLIGHT, RE-TORQUE THE AFFECTED BOLTS TO THE VALUE AS DEFINED IN, AND IN ACCORDANCE WITH THE INSTRUCTIONSOF, GEVEN SB NO. D103-25-004 REVISION 2.
MOC :
-MANDATORY
EASA 2014-0187PARA (3)
FOR SPECIFIC D1-03 SEAT ASSEMBLIES (P/N AS IDENTIFIED IN TABLE 1.1.1 OF GEVEN SB NO. D103-25-004 REVISION 2, EFF CODE FROM AAA TO AUC),WITHIN 6 MONTHS AFTER THE EFFECTIVE DATE OF THIS AD, MODIFY THE SEAT BELT ATTACHMENT ASSEMBLY ON THE AISLE SIDE SPREADER OFSTANDARD AND LAST ROW SEATS IN ACCORDANCE WITH THE INSTRUCTIONS OF GEVEN SB NO. D103-25-004 REVISION 2.
MOC :
-MANDATORY
EASA 2014-0187PARA (4)
AS AN ALTERNATIVE TO THE CORRECTIVE ACTIONS AS REQUIRED BY PARAGRAPH (1) OR (2) OF THIS AD, AS APPLICABLE, BEFORE NEXT FLIGHT,BLOCK EACH AFFECTED SEAT FOR OCCUPANCY, PENDING ACCOMPLISHMENT OF THE APPLICABLE CORRECTIVE ACTION(S).
MOC :
-MANDATORY
EASA 2014-0187 APPLIANCE AD - EQUIPMENT & FURNISHINGS – SAFETY BELT ATTACHMENT BOLTS – INSPECTION / REPLACEMENT
MOC :
HRS
MTH
2908
10-Nov-1992 - Complete
25AD-1
FAA 1983-01-06
JHB
APPLIANCE AD - TO DETECT LIFE PRESERVERS AND FLOTATION DEVICES WHICH HAVE CO2 INFLATION VALVE MANIFOLDS THAT MAY OPERATEIMPROPERLY, AND TO CORRECT THE DEFICIENCY, PERFORM THE FOLLOWING IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS,PARAGRAPH 2, OF SWITLIK PARACHUTE COMPANY, INC., SERVICE BULLETIN 25-00-16, DATED APRIL 1, 1982:
COMPLIED WITHMOC :
Page 66 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
2908
10-Nov-1992 -MANDATORY Complete
25AD-02
FAA 1989-06-01
JHB
APPLIANCE AD - PREVENT THE IMPROPER FUNCTIONING OF THE CARBON DIOXIDE (CO2) INFLATORS ON TSO-C13, LIFE PRESERVERS AND TSO-C72INDIVIDUAL FLOTATION DEVICES
COMPLIED WITHMOC :
MTH 17-Mar-1999 A/RMANDATORY Complete25AD-03
FAA 1998-25-10
SJC
APPLIANCE AD - SEAT RESTRAINT SYSTEM (SUPERSEDED BY 1998-25-10 R01)
COMPLIED WITHMOC :
LDG
HRS
MTH
4842
7041.9
02-Nov-2018 - N/A
FAA 2017-16-01PARA (G)
UNK
PERFORM GENERAL VISUAL INSPECTIONS OF THE ELT FOR DISCREPANCIES; CHECKS , TESTS AND VERIFICATIONS AS APPLICABLE, TO ENSURETHE ELT IS FUNCTIONING, AND ALL APPLICABLE CORRECTIVE ACTIONS
NOT APPLICABLE - N/A DUE TO P/NMOC :
LDG
HRS
MTH
4842
7041.9
02-Nov-2018 -MANDATORY N/A
FAA 2017-16-01PARA (J) UNK
OPTIONAL TERMINATING ACTION: REPLACE ELT WITH A SERVICEABLE FAA-APPROVED ELT
NOT APPLICABLE - N/A DUE TO P/NMOC :
LDG
HRS
MTH
4842
7041.9
02-Nov-2018 -MANDATORY N/A
FAA 2017-16-01
UNK
APPLIANCE AD - EQUIPMENT / FURNISHINGS - AMERI-KING CORPORATION MODEL AK-450() AND AK-451() SERIES EMERGENCY LOCATORTRANSMITTERS - REPETATIVE INSPECTIONS, CHECKS, TESTS AND VERIFICATIONS
NOT APPLICABLE - N/A DUE TO P/NMOC :
MTH -MANDATORY
FAA 2021-07-13PARA (E)(1)
INSPECT THE BUCKLE HANDLE FOR A CRACK AND IF CRACKED, BEFORE FURTHER FLIGHT, REPLACE IT WITH AN AIRWORTHY BUCKLE
MOC :
MTH -MANDATORY
FAA 2021-07-13PARA (E)(2)
MEASURE THE THICHNESS OF THE BUCKLE HANDLE VANE; IF THICKNESS IS 0.125 INCH OR GREATER, BEFORE FURTHER FLIGHT, REMOVE THEBUCKLE FROM SERVICE AND REPLACE IT WITH AN AIRWORTHY BUCKLE
MOC :
-MANDATORY
FAA 2021-07-13PARA (E)(3)
DO NOT INSTALL A BUCKLE OR RESTRAINT SYSTEM WITH A BUCKLE P/N 1111430 OR 1111475, ALL DASH NUMBERS, WITH A HANDLE VANE THICKNESSOF 0.125 INCH OR GREATER
MOC :
-MANDATORY
FAA 2021-07-13 APPLIANCE AD - EQUIPMENT AND FURNISHING - SEAT RESTRAINT SYSTEM PLASTIC ROTARY BUCKLE HANDLE - INSPECTION/REPLACEMENT
MOC :
-MANDATORY
EASA 2016-0024PARA (1)
INSPECT EACH SIEMENS SMOKE DETECTOR TO DETERMINE WHETHER IT IS AN AFFECTED PART
MOC :
-MANDATORY
EASA 2016-0024PARA (2.1)
REPLACE CARGO COMPARTMENT SMOKE DETECTORS, IDENTIFIED IN PARAGRAPH (1), IN ACCORDANCE WITH TABLE 1 OR TABLE 2
MOC :
-MANDATORY
EASA 2016-0024PARA (2.2)
REPLACE PASSENGER, CABIN OR ANY OTHER ON BOARD LOCATION SMOKE DETECTORS, IDENTIFIED IN PARAGRAPH (1), IN ACCORDANCE WITHTABLE 3
MOC :
Page 67 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-MANDATORY
EASA 2016-0024PARA (2.3)
REPLACE REPAIRED SMOKE DETECTOR IDENTIFIED IN APPENDIX 1
MOC :
-MANDATORY
EASA 2016-0024PARA (3)
FROM THE EFFECTIVE DATE OF THIS AD, DO NOT INSTALL ON ANY AEROPLANE AN AFFECTED P/N SMOKE DETECTOR UNLESS THE UNIT (GMC ONLY)IS MARKED 'SIL PMC-26-002'
MOC :
MTH -MANDATORY
EASA 2016-0024 APPLIANCE AD - FIRE PROTECTION - OPTICAL AND AMBIENT SMOKE DETECTORS - IDENTIFICATION / REPLACEMENT
MOC :
MTH -MANDATORY
EASA 2016-0044PARA (1)
INSPECT EACH FIRE EXTINGUISHER, EXCEPT THOSE HAVING P/N 57333 SERIES, INSTALLED ON BAE146 AND RJ AEROPLANES, AND THOSE HAVINGP/N57183 SERIES, INSTALLED ON ATP AEROPLANES, AND DEPENDING ON FINDINGS, ACCOMPLISH CORRECTIVE ACTIONS IN ACCORDANCE WITHTHE INSTRUCTIONS OF KG SB 26-080 REVISION 1
MOC :
-MANDATORY
EASA 2016-0044PARA (2)
ACCOMPLISHMENT OF AN OVERHAUL (SEE NOTE 2 OF THIS AD) OF A FIRE EXTINGUISHER BY KIDDE GRAVINER OR HUGEN, OR IN ACCORDANCEWITH THE INSTRUCTIONS OF KG SIL 01-10 OR IN ACCORDANCE WITH KG CMM 26-21-40 REVISION 14 OR LATER OR KG CMM 26-21-52 REVISION 13 ORLATER (AS APPLICABLE TO FIRE EXTINGUISHER P/N) IS ACCEPTABLE TO COMPLY WITH THE REQUIREMENT OF PARAGRAPH (1).
MOC :
-MANDATORY
EASA 2016-0044PARA (3)
FROM THE EFFECTIVE DATE OF THIS AD DO NOT INSTALL ON ANY AIRCRAFT AN AFFECTED FIRE EXTINGUISHER, UNLESS IT IS NEW, OR HAS PASSEDAN INSPECTION IN ACCORDANCE WITH THE INSTRUCTIONS OF KG SB 26-080 REVISION 1, OR IT HAS BEEN OVERHAULED (SEE NOTE 2) BY KG, OR BYHUGEN OR IN ACCORDANCE WITH THE INSTRUCTIONS OF KG SIL 01-10 OR IN ACCORDANCE WITH THE INSTRUCTIONS OF KG CMM 26-21-40REVISION 14, OR OF KG CMM 26-21-52 REVISION 13, AS APPLICABLE TO FIRE EXTINGUISHER P/N
MOC :
MTH -MANDATORY
EASA 2016-0044 APPLIANCE AD - ATA 26 - FIRE PROTECTION - ENGINE AND AUXILIARY POWER UNIT AUTOMATIC FIRE EXTINGUISHERS - INSPECTION/OVERHAUL
MOC :
HRS
MTH
5970
12-Jun-2007 A/RMANDATORY
Complete26AD-03
FAA 2007-11-17 IDENTIFY WIRES FOR FIRE EXTINGUISHING BOTTLES
COMPLIED WITHMOC :
LDG
HRS
DAYS
4353
6298.1
21-Sep-2010 A/RMANDATORY N/A26AD-06
FAA 2010-04-16PARA (G) CYHM
REPLACE TYPE H1-10 AIR HALON 1211 (BCF) PORTABLE FIRE EXTINGUISHERSMANUFACTURED BY SICLI WITH SERVICABLE UNIT
NOT APPLICABLE - 2010-04-16 IS NOT APPLICABLE DUE TO THE PORTABLE FIRE EXTINGUISHERS MAKE AND MODELNUMBERS
MOC :
LDG
HRS
MTH
4353
6298.1
21-Sep-2010 A/RMANDATORY N/A
FAA 2010-04-16 APPLIANCE AD - TYPE H1-10 AIR HALON 1211 (BCF) PORTABLE FIRE EXTINGUISHERSMANUFACTURED BY SICLI
NOT APPLICABLE - 2010-04-16 IS NOT APPLICABLE DUE TO THE PORTABLE FIRE EXTINGUISHERS MAKE AND MODELNUMBERS
MOC :
HRS
MTH
5820
01-Jul-2006 -MANDATORY Complete28AD-01
FAA 2006-06-03
YHM
PREVENT FUEL VAPOR IGNITION
COMPLIED WITHMOC :
-MANDATORY
EASA 2015-0093PARA (1)
AMEND THE AFM OF THE AIRCRAFT BY INSERTING A TEMPORARY REVISION (TR) TO THE AFM (SUPPLEMENT)
MOC :
Page 68 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-MANDATORY
EASA 2015-0093PARA (2)
MODIFY THE AIRCRAFT BY REPLACING EACH AHRS UNIT HAVING A P/N SPECIFIED AS ‘OLD’ IN TABLE 2 OF THIS AD WITH A MODIFIED UNIT, HAVING AP/N SPECIFIED AS ‘NEW’ IN TABLE 2 OF THIS AD
MOC :
-MANDATORY
EASA 2015-0093PARA (3)
CONCURRENT WITH MODIFICATION OF AN AIRCRAFT AS REQUIRED BY PARAGRAPH (2) OF THIS AD, THE AFM CHANGE, IF REQUIRED BY PARAGRAPH(1) OF THIS AD (SEE NOTE 1 OF THIS AD), CAN BE REMOVED FROM THAT AIRCRAFT
MOC :
-MANDATORY
EASA 2015-0093PARA (4)
DO NOT INSTALL ON ANY AIRCRAFT A LCR-100 AHRS UNIT, HAVING A P/N SPECIFIED AS ‘OLD’ IN TABLE 1 OF THIS AD
MOC :
MTH -MANDATORY
EASA 2015-0093 APPLIANCE AD - NAVIGATION – ATTITUDE HEADING REFERENCE SYSTEM – MODIFICATION / REPLACEMENT
MOC :
HRS
MTH
5719
25-Nov-2005 - N/A
34AD-2
FAA 1980-09-09
YHM
APPLIES TO THE FOLLOWING AIRPLANES, EQUIPPED WITH CESSNA INSTALLED DUAL FLIGHT DIRECTOR INDICATORS, UNLESS MODIFIED TOPROVIDE INDEPENDENT POWER SOURCES, DISTRIBUTION AND BUS SYSTEMS FOR THE DUAL FLIGHT DIRECTOR INSTALLATION OR BY RELOCATINGTHE COPILOT'S SECOND ATTITUDE INDICATOR TO THE TOP CENTER POSITION OF THE COPILOT PANEL INSTRUMENT "T".
NOT APPLICABLE - NOT APPLICABLE BY AIRCRAFT MODEL SERIAL AND/OR UNIT NUMBER.MOC :
MTH 17-Mar-1999 -MANDATORY
Complete
34AD-22
FAA 1998-25-02
SJC
APPLIANCE AD - TO PREVENT THE DISPLAY OF TARGET INDICATORS ON THE WRONG SIDE OF THE AIRCRAFT CAUSED BY AN INTERNALCOMPONENT FAILURE IN THE SKY497 INSTALLATIONS WITH A TOP-MOUNTED ANTENNA, WHICH COULD RESULT IN THE PILOT MAKING ANINCORRECT INITIAL MANEUVER BASED ON THE DISPLAYED INFORMATION WHILE TRYING TO VISUALLY ACQUIRE THE AIRCRAFT.
COMPLIED WITHMOC :
HRS
MTH
5719
25-Nov-2005 -MANDATORY Complete34AD-27
FAA 2003-13-08
YHM
APPLIANCE AD - GOODRICH AVIONICS SYSTEMS, INC. TAWS8000 TERRAIN AWARENESS WARNING SYSTEM
COMPLIED WITH - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :
HRS
MTH
5885
24-Oct-2006 -SUPERSEDED N/A34AD-35
FAA 2006-16-18
YHM
APPLIANCE AD - PREVENT A BEARING ERROR (SUPERSEDED BY 2006-16-18 R01)
NOT APPLICABLE - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
FAA 2014-18-01
CYHM
APPLIANCE AD - NAVIGATION - ROCKWELL COLLINS, INC. MODE S TRANSPONDERS - INSPECTION / MODIFICATION
NOT APPLICABLE - N/A DUE TO ROCKWELL COLLINS EQUIPMENT NOT INSTALLED AT THIS TIMEMOC :
-MANDATORY
FAA 2015-10-51-E APPLIANCE/EMERGENCY AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS SECTIONOF THE AFM OR AFMS.
MOC :
LDG
HRS
MTH
4655
6755.2
25-Sep-2015 -MANDATORY
N/A
FAA 2015-10-51
CYHM
APPLIANCE AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS SECTION OF THE AFMOR AFMS
NOT APPLICABLE - N/A DUE TO AVIDYNE IFD EQUIPMENT NOT INSTALLED ON THIS AIRCRAFT.MOC :
Page 69 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4398
6366.9
12-Jun-2011 - N/A
EASA 2011-0090
CYHM
OXYGEN – OXYGEN MASK REGULATOR INFLATABLE HARNESS – IDENTIFICATION /REPLACEMENT
NOT APPLICABLE - EASA AD 2011-0090 FOUND TO BE NOT APPLICABLE TO THE PILOT AND COPILOT OXYGEN INFLATABLEHARNESSES DUE TO THE YEAR OF MANUFACTURE.
MOC :
MTH -MANDATORY
EASA 2014-0142PARA (1)
ACCOMPLISH ACCOMPLISH THE ACTIONS AS SPECIFIED IN PARAGRAPHS (1.1) AND (1.2) OF THIS AD - DETERMINE THE DATE OF MANUFACTURING /REPLACE THE HARNESS INFLATION HOSE P/N 445952 WITH A SERVICEABLE PART, OR REMOVE THE INFLATABLE HARNESS FROM THE MASKREGULATOR AND REPLACE IT WITH A SERVICEABLE HARNESS
MOC :
-MANDATORY
EASA 2014-0142PARA (2)
ACCOMPLISH AN OXYGEN MASK REGULATOR EQUIPPED WITH A P/N MXH21-1 INFLATABLE HARNESS HAVING A DMF CODE OF NOVEMBER 2008 (0845-S OR 08/45-S) OR EARLIER, AND THOSE WITH A DMF OF JANUARY 2011 (1101-S OR 11/01-S) OR LATER, IS EXCLUDED FROM THE INSPECTION ANDREPLACEMENT REQUIREMENTS OF PARAGRAPH (1) OF THIS AD
MOC :
-MANDATORY
EASA 2014-0142PARA (3)
ACCOMPLISH IT IS ALLOWED TO INSTALL ON AN AEROPLANE A FLIGHT CREW OXYGEN MASK REGULATOR, HAVING A P/N AS IDENTIFIED IN SECTION1.A.(1) OF ZODIAC AEROTECHNICS SB MC10-35-274, PROVIDED IT HAS BEEN DETERMINED THAT A P/N MXH21-31 INFLATABLE HARNESS IS INSTALLED,OR THAT THE P/N MXH21-1 INFLATABLE HARNESS INSTALLED ON THAT FLIGHT CREW OXYGEN MASK REGULATOR HAS BEEN CORRECTED, ASREQUIRED BY THIS AD.
MOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2014-0142R01 (1)
CYHM
ACCOMPLISH ACCOMPLISH THE ACTIONS AS SPECIFIED IN PARAGRAPHS (1.1) AND (1.2) OF THIS AD - DETERMINE THE DATE OF MANUFACTURING /REPLACE THE HARNESS INFLATION HOSE P/N 445186 OR P/N 445952, AS APPLICABLE, WITH A SERVICEABLE PART, OR REMOVE THE INFLATABLEHARNESS FROM THE MASK REGULATOR AND REPLACE IT WITH A SERVICEABLE HARNESS
NOT APPLICABLE - N/A DUE TO YEAR OF MANUFACTUREMOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2014-0142R01 (2)
CYHM
ACCOMPLISH AN OXYGEN MASK REGULATOR EQUIPPED WITH A P/N MXH20-1 OR P/N MXH21-1 INFLATABLE HARNESS HAVING A DMF CODE OFNOVEMBER 2008 (0845-S OR 08/45-S) OR EARLIER, AND THOSE WITH A DMF OF JANUARY 2011 (1101-S OR 11/01-S) OR LATER, IS EXCLUDED FROMTHE INSPECTION AND REPLACEMENT REQUIREMENTS OF PARAGRAPH (1) OF THIS AD
NOT APPLICABLE - N/A DUE TO YEAR OF MANUFACTUREMOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2014-0142R01 (3)
CYHM
ACCOMPLISH IT IS ALLOWED TO INSTALL ON AN AEROPLANE A FLIGHT CREW OXYGEN MASK REGULATOR, HAVING A P/N AS IDENTIFIED IN SECTION1.A.(1) OF ZODIAC AEROTECHNICS SB MC10-35-274, PROVIDED IT HAS BEEN DETERMINED THAT A P/N MXH21-31 INFLATABLE HARNESS IS INSTALLED,OR THAT THE P/N MXH20-1 OR P/N MXH21-1 INFLATABLE HARNESS INSTALLED ON THAT FLIGHT CREW OXYGEN MASK REGULATOR HAS BEENCORRECTED, AS REQUIRED BY THIS AD
NOT APPLICABLE - N/A DUE TO YEAR OF MANUFACTUREMOC :
LDG
HRS
MTH
4611
6684
21-Oct-2014 -MANDATORY N/A
EASA 2014-0142R01 CYHM
APPLIANCE AD - OXYGEN ¿ OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE ¿ IDENTIFICATION / REPLACEMENT
NOT APPLICABLE - N/A DUE TO YEAR OF MANUFACTUREMOC :
-MANDATORY
EASA 2014-0142 APPLIANCE AD - OXYGEN - OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE - IDENTIFICATION / REPLACEMENT (SUPERSEDEDBY 2014-0142 R01)
MOC :
Page 70 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
3490
26-Jun-1995 -MANDATORY Complete35AD-04
FAA 1994-19-06
UVA
APPLIANCE AD - TO PREVENT THE FLIGHT CREW FROM EXPERIENCING DIFFICULTY IN EXHALING INTO THE AFFECTED CREW OXYGEN MASKS.
COMPLIED WITHMOC :
HRS
MTH
4546
15-Oct-1999 -MANDATORY Complete35AD-02
FAA 1999-08-21
SJC
APPLIANCE AD - PREVENT REDUCED OXYGEN CONSUMPTIOIN WHEN PASSENGERS ARE REQUIRED TO USE DEFECTIVE OXYGEN MASKS
COMPLIED WITHMOC :
LDG
HRS
MTH
4731
6875.4
31-Aug-2016 -MANDATORY N/A
FAA 2016-11-20PARA (G)
UNK
PHYSICALLY INSPECT THE PBE POUCH TO DETERMINE IF IT HAS AN INTACT VACUUM SEAL IN ACCORDANCE WITH B/E AEROSPACE SERVICEBULLETIN NO. 119003-35-011, REV .000, DATED FEBRUARY 4, 2015, PARA III.A..1 SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - NO PBE INSTALLEDMOC :
LDG
HRS
MTH
4731
6875.4
31-Aug-2016 -MANDATORY N/A
FAA 2016-11-20PARA (H.1)
UNK
REPLACEMENT OF A PBE POUCH, FOUND DURING THE INSPECTION IN PARAGRAPH (G) OF THIS AD, THAT DOES NOT HAVE AN INTACT VACUUMSEAL. SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - NO PBE INSTALLEDMOC :
LDG
HRS
MTH
4731
6875.4
31-Aug-2016 -MANDATORY
N/A
FAA 2016-11-20PARA (H.2)
UNK
REPLACEMENT OF A PBE POUCH, FOUND DURING THE INSPECTION IN PARAGRAPH (G) OF THIS AD, WHERE THE VACUUM SEAL IS INTACT.SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - NO PBE INSTALLEDMOC :
LDG
HRS
MTH
4731
6875.4
31-Aug-2016 -MANDATORY N/A
FAA 2016-11-20
UNK
APPLIANCE AD - OXYGEN - INSPECTION AND REPLACEMENT OF B/E AEROSPACE PROTECTIVE BREATHING EQUIPMENT (PBE), PART NUMBER 119003-11 THAT ARE INSTALLED ON AIRPLANES. SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - NO PBE INSTALLEDMOC :
LDG
HRS
MTH
4803
6992.5
20-Feb-2018 -MANDATORY N/A
FAA 2017-18-12PARA (G) UNK
INSPECTION RETAINED FROM AD 2016-11-20 FOR AIRPLANES WITH PBE, P/N 119003-11, INSTALLED
NOT APPLICABLE - THE PBE PART NUMBER IS NOT INSTALLED IN THIS AIRCRAFT P/N V745584MOC :
LDG
HRS
MTH
4803
6992.5
20-Feb-2018 -MANDATORY N/A
FAA 2017-18-12PARA (H) UNK
REPLACEMENT RETAINED FROM AD 2016-11-20 FOR AIRPLANES WITH PBE, P/N 119003-11, INSTALLED
NOT APPLICABLE - THE PBE PART NUMBER IS NOT INSTALLED IN THIS AIRCRAFT P/N V745584MOC :
LDG
HRS
MTH
4803
6992.5
20-Feb-2018 -MANDATORY N/A
FAA 2017-18-12PARA (I) & (J)
UNK
INSPECT TO DETERMINE IF THE S/N OF THE INSTALLED PBE, P/N 119003-21, IS WITHIN THE RANGE OF 004-14768M THROUGH 004-21093M OR 004-02393M THROUGH 004-03033M AND IF FOUND WITHIN THE S/N RANGE REPLACE IT.
NOT APPLICABLE - THE PBE PART NUMBER IS NOT INSTALLED IN THIS AIRCRAFT P/N V745584MOC :
Page 71 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
4803
6992.5
20-Feb-2018 -MANDATORY N/A
FAA 2017-18-12
UNK
APPLIANCE AD - OXYGEN - INSPECTION AND REPLACEMENT OF B/E AEROSPACE PROTECTIVE BREATHING EQUIPMENT (PBE), PART NUMBER 119003-11 AND 119003-21 THAT ARE INSTALLED ON AIRPLANES
NOT APPLICABLE - THE PBE PART NUMBER IS NOT INSTALLED IN THIS AIRCRAFT P/N V745584MOC :
HRS
MTH
5719
25-Nov-2005 A/RMANDATORY N/A57AD-1
FAA 1979-12-06
YHM
VISUALLY INSPECT THE UPPER AND LOWER SPAR CAP STEMS AT WING STATION 37.0
NOT APPLICABLE - NOT APPLICABLE BY AIRCRAFT MODEL SERIAL AND/OR UNIT NUMBER.MOC :
HRS
MTH
5719
25-Nov-2005 - CompleteAD 72-1
YHM
JT15D FAN BLADE INSP
COMPLIED WITHMOC :
MTH 25-Nov-2005 - CompleteE1
AD 72-04
YHM
HPT BLADE SHIFT INSP
COMPLIED WITH - FOUND PREVIOUSLY COMPLIED WITH.MOC :
MTH 25-Nov-2005 - CompleteE2
AD 72-04
YHM
HPT BLADE SHIFT INSP
COMPLIED WITH - FOUND PREVIOUSLY COMPLIED WITH.MOC :
MTH 25-Nov-2005 - N/AE1
AD 72-05
YHM
PRATT & WHITNEY IMPELLER
NOT APPLICABLE - NOT APPLICABLE BY COMPONENT PART NUMBER.MOC :
MTH 25-Nov-2005 - N/AE2
AD 72-05
YHM
PRATT & WHITNEY IMPELLER
NOT APPLICABLE - NOT APPLICABLE BY COMPONENT PART NUMBER.MOC :
HRS
MTH
5719
25-Nov-2005 - N/ALEFT ENGINE
AD 73-1
YHM
UACL SI3-74 FCU INSP
NOT APPLICABLE - NOT APPLICABLE BY COMPONENT PART NUMBER.MOC :
HRS
MTH
5719
25-Nov-2005 - N/ARIGHT ENGINE
AD 73-1
YHM
UACL SI3-74 FCU INSP
NOT APPLICABLE - NOT APPLICABLE BY COMPONENT PART NUMBER.MOC :
HRS
MTH
5719
25-Nov-2005 A/RMANDATORY N/A78AD-01
FAA 1993-05-15
YHM
TO PREVENT SEVERELY REDUCED CONTROLLABILITY OF ENGINE POWER AUTHORITY.
NOT APPLICABLE - NOT APPLICABLE-EQUIPMENT NOT INSTALLEDMOC :
Page 72 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Factory Installed
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 -
FO
06A21FO-01 : A
21FO-01A
*CF
INDICATOR-CABIN TEMP FACTORY OPTION
MTH 30-Apr-1983 -
FO
179A21FO-04 : A
21FO-04A
*CF
COCKPIT AIR SUPPLEMENTAL FACTORY OPTION
MTH 30-Apr-1983 -
FO
631G23FO-01 : G
23FO-01G
*CF
HF COM SYSTEM COLLIN HF-220 FACTORY OPTION
MTH 30-Apr-1983 -
FO
12B24FO-01 : B
24FO-01B
*CF
BATTERY & MONITOR FOR 20 CELL FACTORY OPTION
MTH 30-Apr-1983 -FO
26C24FO-02 : C
24FO-02C
*CF
INVERTER 600 VA DUAL EXH FWD SGL FLT DIR FACTORY OPTION
MTH 30-Apr-1983 -FO
104J25FO-05 : J
25FO-05J
*CF
STRGE DRAWER #3 AFT FCG SEAT LATERL TRAK FACTORY OPTION
MTH 30-Apr-1983 -
FO
121E25FO-18 : E
25FO-18E
*CF
SEAT #3 AFT FACING FACTORY OPTION
MTH 30-Apr-1983 -FO
124G25FO-20 : G
25FO-20G
*CF
EXECUTIVE TABLE USED W/STD & OPT A FACTORY OPTION
MTH 30-Apr-1983 -FO
124H25FO-20 : H
25FO-20H
*CF
EXECUTIVE TABLE USE W/STD AND A STG FACTORY OPTION
MTH 30-Apr-1983 -
FO
132
25FO-23
*CF
TAILORING SEAT-CITATION 2 FACTORY OPTION
MTH 30-Apr-1983 -
FO
136A25FO-25 : A
25FO-25A
*CF
CARPET RUNNER CABIN AISLE FACTORY OPTION
MTH 30-Apr-1983 -FO
16625FO-37
*CF
CHIMES UNIT FACTORY OPTION
MTH 30-Apr-1983 -FO
3628FO-01
*CF
FUEL CAP LOCKING FACTORY OPTION
MTH 30-Apr-1983 -FO
182
31FO-02
*CF
CLOCK-DIGITAL ELECTRIC 24 HOUR RH FACTORY OPTION
MTH 30-Apr-1983 -
FO
182B31FO-02 : B
31FO-02B
*CF
CLOCK DIGITAL ELECTRIC 24 HOUR LH FACTORY OPTION
MTH 30-Apr-1983 -
FO
10
32FO-01
*CF
ANTI SKID MAIN WHEEL BRAKE FACTORY OPTION
MTH 30-Apr-1983 -
FO
93
32FO-02
*CF
BRAKES EXTENDED LIFE FACTORY OPTION
MTH 30-Apr-1983 -FO
49B33FO-02 : B
33FO-02B
*CF
LIGHT-RECOGNITION WING-TIP MOUNTED FACTORY OPTION
MTH 30-Apr-1983 -
FO
01C34FO-01 : C
34FO-01C
*CF
ALTIMETER MILLIBAR RH EXCH FACTORY OPTION
MTH 30-Apr-1983 -
FO
11
34FO-02
*CF
INDICATOR-ANGLE OF ATTACK FACTORY OPTION
Page 73 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
007-Apr-20217091058.1ENG 2
007-Apr-20217071057.1ENG 1
007-Apr-202149357180.4AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
C-GTOLReg No:
13-Apr-2021 2:27PM
30-Apr-1983
Owner: TECHNISONIC INDUSTRIES LTD.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 501 - MODEL 501
Unit:
501-0320
0667
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Factory Installed
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 30-Apr-1983 -
FO
175
34FO-04
*CF
LOCATOR BEACON EMERGENCY FACTORY OPTION
MTH 30-Apr-1983 -FO
185A34FO-06 : A
34FO-06A
*CF
9500 LB ZERO FUEL WT W/SURFACE DE-ICE FACTORY OPTION
MTH 30-Apr-1983 -FO
658N34FO-12 : N
34FO-12N
*CF
2ND ADF COLLINS ADF 60 WO/HF COMM FWD FACTORY OPTION
MTH 30-Apr-1983 -FO
679B34FO-15 : B
34FO-15B
*CF
FLIGHT DIRECTOR LH-5" SINGLE CUE SPERRY FACTORY OPTION
MTH 30-Apr-1983 -FO
693P
34FO-20 : P
34FO-20P
*CF
TRUE AIRSPEED FACTORY OPTION
MTH 30-Apr-1983 -FO
671J34FO-95 : J
34FO-95J
*CF
RADIO ALTIMETER-AA215 W/SEP COPIL INDICATOR FACTORY OPTION
MTH 30-Apr-1983 -
FO
632A34FO-96 : A
34FO-96A
*CF
RADAR-PRIMUS 400 SL-COLOR FACTORY OPTION
MTH 30-Apr-1983 -
FO
58B35FO-01 : B
35FO-01B
*CF
QUICK DONNING OXYGEN MASKS FACTORY OPTION
MTH 30-Apr-1983 -
FO
66B35FO-02 : B
35FO-02B
*CF
OXYGEN SYSTEM-64 CUBIC FEET FACTORY OPTION
MTH 30-Apr-1983 -FO
18853FO-01
*CF
DRAG CHUTE FACTORY OPTION
MTH 30-Apr-1983 -FO
76
73FO-01
*CF
ENGINE SYNCHRONIZING INSTRUMENT FACTORY OPTION
Page 74 of 74NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.