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ATR72-500
S.NO SHEET # DATE ISSUE #1 LEP 1 23/04/2018 INITIAL2 A SHEET 1 23/04/2018 INITIAL3 A SHEET 2 23/04/2018 INITIAL4 B SHEET 1 23/04/2018 INITIAL5 B SHEET 2 23/04/2018 INITIAL6 B SHEET 3 23/04/2018 INITIAL7 C SHEET 1 23/04/2018 INITIAL8 C SHEET 2 23/04/2018 INITIAL9 C SHEET 3 23/04/2018 INITIAL
10 C SHEET 4 23/04/2018 INITIAL11 C SHEET 4A 23/04/2018 INITIAL12 C SHEET 4B 23/04/2018 INITIAL13 C SHEET 4C 23/04/2018 INITIAL14 C SHEET 4D 23/04/2018 INITIAL15 C SHEET 4E 23/04/2018 INITIAL16 C SHEET 5 23/04/2018 INITIAL17 C SHEET 6 23/04/2018 INITIAL18 C SHEET 7 23/04/2018 INITIAL19 C SHEET 8 23/04/2018 INITIAL20 C SHEET 8A 23/04/2018 INITIAL21 C SHEET 9 23/04/2018 INITIAL22 C SHEET 10 23/04/2018 INITIAL
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ALL (FUEL DENSITY 0.78 Kg / litre)ALL (FUEL DENSITY 0.79 Kg / litre)
ALL (FUEL DENSITY 0.81 Kg / litre)ALL (FUEL DENSITY 0.82 Kg / litre)
ALL (FUEL DENSITY 0.80 Kg / litre)
LIST OF EFFECTIVE PAGES ISSUE # 00
EFFECTIVITY
ALL (FUEL DENSITY 0.77 Kg / litre)
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EDP EXCHANGE FOR SEMI PERMANENT DATAFOR CHECK IN AND LOAD CONTROL
LEP 1 Date: 23/04/2018
21 C SHEET 9 23/04/2018 INITIAL22 C SHEET 10 23/04/2018 INITIAL23 C SHEET 11 23/04/2018 INITIAL24 C SHEET 12 23/04/2018 INITIAL25 C SHEET 13 23/04/2018 INITIAL26 C SHEET 14 23/04/2018 INITIAL27 C SHEET 15 23/04/2018 INITIAL28 D SHEET 1 23/04/2018 INITIAL29 D SHEET 2 23/04/2018 INITIAL
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LEP 1 Date: 23/04/2018
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
COMMUNICATION ADDRESSES
A SHEET 1
CARRIER PK
1. HANDLING AGENT’S CONTACT ADDRESS Completed sheets and changes of basic data and procedure must be forwarded to:
MAILING ADDRESS:
TELETYPE ADDRESS:
EMAIL ADDRESS:
REMARKS: 2. CARRIER’S CONTACT ADDRESS
MAILING ADDRESS: OPERATIONS ENGINEERING TECHNICAL DIVISION FLIGHT OPERATIONS DEPARTMENT PIA HEAD OFFICE, JINNAH INTERNATIONAL AIRPORT KARACHI, 75200, PAKISTAN. TELETYPE ADDRESS: KHIOLPK KHIOXPK EMAIL ADDRESS: [email protected] REMARKS:
mailto:[email protected]
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
COMMUNICATION ADDRESSES
A SHEET 2
CARRIER PK
3. AUTOMATICALLY PRODUCED DOCUMENTS
(Tick as required) � NOTAC � SEATPLAN � LOADPLAN � PASSENGER INFO LIST � LOAD SHEET � LOADING INSTRUCTION/REPORT
4. MESSAGE REQUIREMENTS
(Tick as required) � LPM Load Planning Message AHM 580 � LDM Load Message AHM 583 � ALI Abbreviated Load Information Message AHM 584 � CPM Container/Pallet Distribution Message AHM 587 � UCM ULD Control Message AHM 388(Dispatch Only) � MVT Movement Messages AHM 011 and 780 � DIV Diversion Message AHM 781 � SOM Seat Occupied Message RP 1712 � PTM Passenger Transfer Message RP1718 � PSM Passenger Service Message RP 1715 (Despatch Only) � TPM Teletype Passenger Manifest RP 1717 (Despatch only) � PFS Passenger Final Sales Message RP 1719 (Despatch) � IDM Industry Discount Message RP 1714 � RQL Request List Message RP 1709 (despatch) � PNL/ADL Passenger Name List, and Additions and Deletions List (RP 1708) (acceptance Only) � SAL Seats Available List RP 1713(Acceptance Only) � SLS Statistical Load Summary AHM 588 � RQM Request Information Message AHM 783 � UWS ULD/Bulk Load Weight signal AHM 581 (Acceptance Only)
5. MESSAGE ADDRESSES
Attach a complete address list for all messages mentioned under paragraph 4 above
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No.: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
GENERAL INFORMATION
B SHEET 1
CARRIER PK
1. PASSENGER AND BAGGAGE WEIGHTS 1.1 Passenger weights
Adult male 75 KG Adult female 75 KG Child 38 KG Infant 15 KG
Remarks: 1.2 Cabin Baggage Weight
YES NO Cabin weight is included in the above mentioned passenger weights. If NO; Actual cabin baggage weight must be used. Remarks:
1.3 Checked Baggage Weight
Weight per piece ACTUAL Weight per passenger ACTUAL
Enter “actual” if standard weight not permitted. Remarks:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 20/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA B SHEET 2
CARRIER PK
ALL WEIGHTS IN KILOGRAMS (KG)
2. CREW AND CREW BAGGAGE WEIGHTS 2.1 Crew Weights
Cockpit crew 81 Cabin crew 75
YES NO Crew baggage is included in the above crew weights: If NO: Crew baggage weight must be specified in 2.2 Remarks: 2.2 Crew Baggage Weights
For check purposes add list of valid weights and indices.
COCKPIT CABIN SHORTHAUL 30 20 LONGHAUL 30 20 OTHER’S *
* Specify conditions as appropriate Remarks: For International flights include crew baggage.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
GENERAL INFORMATION
B SHEET 3
CARRIER PK
3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS
(Tick as appropriate)
DOW DOI Remarks
Item Incl Excl Incl Excl
Basic Weight (EMPTY WEIGHT) Crew Weight Crew Baggage Pantry Containers
Pallets
CONFIG Weight
FLIGHT PACK
REMARKS:-
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 1
A/C TYPE ATR72-500
CARRIER PK
1. BALANCE AND SPECIAL INFORMATION - OUTPUT ON LOADSHEET
1.1 Balance output
Please mark your requirements in respective box. Remarks Basic index BI Dry operating index DOI Dead load index DLI Dead load MAC MACDLW Loaded Index at zero fuel weight LIZFW Loaded index at take-off weight LITOW Loaded Index at landing weight LILAW MAC – at zero fuel weight MACZFW MAC - at takeoff weight MACTOW MAC at landing weight MACLAW Stabilizer trim setting at take-off STABTO *
* specify ANU or AND as appropriate. Passenger trim output
Please mark your requirements in respective box. Remarks Class Trim Cabin Area Trim Seat Row Trim
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 2
A/C TYPE ATR72-500
CARRIER PK
ALL WEIGHTS IN KILOGRAMS (KG)
1.3 Seating Conditions
State below how the seating conditions are to be shown on the load sheet in the respective box (give example).
1.4 Special Information Specify the information to be entered in the lower parts of the EDP Load sheet.
1.4.1 Captain’s information/notes, Centre of Gravity limits, ramp weight, etc. (give examples). 1.4.2 Load message before LMC, if required, to be shown.
2. AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS
DRY OPERATING WEIGHT � BASIC WEIGHT √ (tick as appropriate) For check purpose add list of valid weights and indices.
Standard Fleet Weight: 13224 Standard Fleet Index: 46.2
Registration
Weight Adjustment
Index Adjustment
Registration
Weight Adjustment
Index Adjustment
AP-BKZ
-165
4.6
AP-BKY
15
-1.0
AP-BKV
-33
-1.6
AP-BKW
104
0.2
AP-BKX
79
-2.0
NOTE: Notification for data changes at short notice may also be made by means of data exchange message (AHM 052). PK does not take Fleet Average Basic Weight; Weight must be taken Tail Wise.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 3
A/C TYPE ATR72-500
CARRIER PK
3. BASIC INDEX AND MAC FORMULA 3.1 Examples and definitions
Index = W * (Sta - Ref. Sta) + K C
C*(I – K) + Ref.Sta - LEMAC W %MAC = MAC 100 W = Weight Actual Sta. = Station, horizontal distance in inches or metres from station zero to the location Ref. Sta. = Reference station/axis. Selected station around which all index values are calculated K = Constant used as a plus value to avoid negative index figures. C = Constant used as a denominator to convert moment values into index values. I = Index value corresponding to respective weight. MAC = Length of Mean Aerodynamic Chord in inches or meters. LEMAC = Horizontal distance in inches or meters from the station zero to location of the Leading Edge of MAC.
3.2 Index formula Ref. Sta at = 14.180 Meters from zero K (constant) = 50 C (constant) = 150
3.3 MAC Information
Length of MAC = 2.303 Meters LEMAC at = 13.604 Meters from zero
3.4 Stabilizer trim setting
MAC Range Min 14% Max 37% STAB Range Min 2.5 Max 0
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4
A/C TYPE ATR72-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading � Fuel Usage � Standard Procedure � Non-standard Procedure � FUEL DENSITY: 0.77 kg/litre
Fuel Weight Index value
Fuel Weight Index value
+/-
100
10
1
+/-
100
10
1
1 8 9 0 0 7 4 9 + 0 1 1 3 2 9 + 0 2 1 8 9 9 + 0 3 2 4 5 8 + 0 4 3 0 2 8 + 0 5 3 5 9 7 + 0 6 4 2 4 1 + 0 7 4 9 0 5 + 0 8
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4A
A/C TYPE ATR72-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading � Fuel Usage � Standard Procedure � Non-standard Procedure � FUEL DENSITY: 0.78 kg/litre
Fuel Weight Index value
Fuel Weight Index value
+/-
100
10
1
+/-
100
10
1
1 8 8 0 0 7 4 8 + 0 1 1 3 2 7 + 0 2 1 8 9 8 + 0 3 2 4 5 6 + 0 4 3 0 2 8 + 0 5 3 5 9 3 + 0 6 4 2 2 7 + 0 7 4 9 6 9 + 0 8
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4B
A/C TYPE ATR72-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.79 kg/litre
Fuel Weight Index value
Fuel Weight Index value
+/-
100
10
1
+/-
100
10
1
1 8 7 0 0 7 4 6 + 0 1 1 3 2 6 + 0 2 1 8 9 7 + 0 3 2 4 5 4 + 0 4 3 0 2 8 + 0 5 3 5 8 8 + 0 6 4 2 1 3 + 0 7 5 0 3 2 + 0 8
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4C
A/C TYPE ATR72-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading � Fuel Usage � Standard Procedure � Non-standard Procedure � FUEL DENSITY: 0.80 kg/litre
Fuel Weight Index value
Fuel Weight Index value
+/-
100
10
1
+/-
100
10
1
1 8 6 0 0 7 4 4 + 0 1 1 3 2 4 + 0 2 1 8 9 6 + 0 3 2 4 5 2 + 0 4 3 0 2 8 + 0 5 3 5 9 2 + 0 6 4 2 0 0 + 0 7 5 0 9 6 + 0 8
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4D
A/C TYPE ATR72-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading � Fuel Usage � Standard Procedure � Non-standard Procedure � FUEL DENSITY: 0.81 kg/litre
Fuel Weight Index value
Fuel Weight Index value
+/-
100
10
1
+/-
100
10
1
1 8 6 0 0 7 4 3 + 0 1 1 3 2 2 + 0 2 1 8 9 5 + 0 3 2 4 5 0 + 0 4 3 0 2 8 + 0 5 3 5 9 2 + 0 6 4 1 8 8 + 0 7 5 0 0 6 + 0 8
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4E
A/C TYPE ATR72-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.82 kg/litre
Fuel Weight Index value
Fuel Weight Index value
+/-
100
10
1
+/-
100
10
1
1 8 5 0 0 7 4 1 + 0 1 1 3 2 1 + 0 2 1 8 9 4 + 0 3 2 4 4 9 + 0 4 3 0 2 8 + 0 5 3 5 9 1 + 0 6 4 1 7 6 + 0 7 4 9 5 1 + 0 8 5 2 2 3 + 0 9
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 5
A/C TYPE ATR72-500
CARRIER PK
5. COCKPIT 5.1 Number of seats and average station
Maximum number of cockpit seats
Length of arm from reference station Index influence
± Inch / metre ± per 1 kg
CAPT -
4.540 -
0 . 0 6 4 2 7
F/O
-
4.540 -
0 . 0 6 4 2 7
OBSERVER
-
5.500 - 0 . 0 5 7 8 7
Remarks:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 6
A/C TYPE ATR72-500
CARRIER PK
6. LIMITATIONS 6.1 Aircraft Weight Limitations Maximum weight for:
Aircraft Reg.
Or Subtype Nr. Ramp/Taxi Design take-off
wet* Design take-off
dry Zero fuel Design landing
AP-BKZ
AP-BKV
AP-BKW
AP-BKY
AP-BKY
22970
22970
22970
22970
22970
N O T
A P P L I C A B L E
22800
22800
22800
22800
22800
20800
20800
20800
20800
20800
22350
22350
22350
22350
22350
*Valid for take-off with water- injection
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 7
A/C TYPE ATR72-500
CARRIER PK
6.2. CG – Limits for Loadsheet
Purposes
Enter the forward and the aft balance limits in the boxes commencing at the lowest weight and terminating at the highest weight to be checked. IMPORTANT – If limits are affected and / or determined by passenger / fuel / version / or other conditions specify each set of limits on a separate sheet entering the special condition(s) in the box.
FORWARD AFT
Special condition if applicable
Special condition if applicable
Specify Applicability * Weight
Index value Specify
Applicability * Weight
Index value
± 10
0
10
1 0.1
0.01
± 10
0
10
1 0.1
0.01
ZFW 1 3 0 0 0 + 3 2 0 0 ZFW 1 3 0 0 0 + 5 9 0 0 1 4 7 0 0 + 3 6 0 0 2 0 8 0 0 + 7 6 0 0 1 8 0 0 0 + 2 8 0 0 2 0 8 0 0 + 3 6 0 0
TOGW 1 3 0 0 0 + 3 2 0 0 TOGW 1 3 0 0 0 + 5 9 0 0 1 4 7 0 0 + 3 6 0 0 2 2 8 0 0 + 8 1 0 0 1 8 0 0 0 + 2 8 0 0
2 2 8 0 0 + 4 4 0 0
*Zero Fuel, Taxi, Take-off, In-flight, Landing NOTE: Attach a balance chart for check purposes. Remarks :
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
7. PASSENGER SEATS
Class codes :
(e.g. F, Y, C, M etc.) Class 1 YP Class 4
Class 2 Y Class 5
Class 3
NOTE: Fill in one table for each cabin configuration code.
Name of cabin section
Number of seats Total per cabin section Class 1
Class 2
Class 3
Class 4
Class 5
ZONE A 12 8Y
ZONE B - 32
ZONE C - 18
12 58
Remarks
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 8
Cabin-Configuration (s) 12YP/58Y
A/C TYPE ATR72-500 .
CARRIER PK
Sub total Total per Class
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
7. PASSENGER SEATS
Class codes :
(e.g. F, Y, C, M etc.) Class 1 YP Class 4
Class 2 Y Class 5
Class 3
NOTE: Fill in one table for each cabin configuration code.
Name of cabin section
Number of seats Total per cabin section Class 1
Class 2
Class 3
Class 4
Class 5
ZONE A - 20
ZONE B - 32
ZONE C - 18
- 70
Remarks
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 8 A
Cabin-Configuration (s) 70Y
A/C TYPE ATR72-500 .
CARRIER PK
Sub total Total per Class
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 9
Cabin-Configuration(s) 12YP/58Y OR 70Y
A/C TYPE ATR72-500
CARRIER PK
8. Average Station 8.1 Class / Cabin Sections
Class / Cabin section Length of arm from
reference station Index influence
± Inch / metre ± per 1 kg ZONE A - 4.161 - . 0 2 7 7 4 ZONE B + 0.792 + . 0 0 5 2 8 ZONE C + 5.576 + . 0 3 7 1 7
8.2 Seating Layout
Show the passenger seating layout for the configurations given in the box at the top by inserting the seat row numbers and letters in the following table. For special seats use the facility codes listed below. B = Bassinet position P = Stretcher location C = Crew seat Q = Quiet zone E = Emergency exit S = Smoking G = Groups T = Near toilet H = Incapacitated passenger U = Unaccompanied minor I = Infant preference rows / seats V = Seat left vacant / offered last J = Rear facing seats W = No movie K = Near galley X = No facility seat, e.g. no distinction L = Leg space seat between smoking and non – smoking M = Wheel chair Y = Not fitted N = No smoking Z = Buffer zone O = Over wing seat A = Aisle Alpha / Characters --- D, F, R, Blank, not used.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No:
INITIAL
Date: 23/04/2018
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 10
CABIN CONFIGURATION(S) 12YP/58Y OR 70Y
A/C TYPE ATR72-500
CARRIER PK
8.2.1 Seat plan Layout / Facilities and Row Index Influence.
SEC
TIO
N
RO
W N
O
ROW LETTER Index influence per seat row ± per 1 kg
A B C D
A A A A A B B B B B B B B C C C C C
1 X X X X - . 0 2 7 7 42 X X X X - . 0 2 7 7 43 X X X X - . 0 2 7 7 44 X X X X + . 0 2 7 7 4
5 X X X X + . 0 2 7 7 46 X X X X + . 0 0 5 2 87 X X X X + . 0 0 5 2 88 X X X X + . 0 0 5 2 89 X X X X + . 0 0 5 2 810 X X X X + . 0 0 5 2 811 X X X X + . 0 0 5 2 812 X X X X + . 0 0 5 2 813 X X X X + . 0 0 5 2 814 X X X X + . 0 3 7 1 715 X X X X + . 0 3 7 1 716 X X X X + . 0 3 7 1 717 X X X X + . 0 3 7 1 718 X X + . 0 3 7 1 7
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 11
Cabin-configuration(s) 12YP/58Y OR 70Y
A/C TYPE ATR72-500
CARRIER PK
8.3 Cabin Crew Seats
Crew seats location Max. No. of seats
Length of arm from reference station Index influence
± Inch / metre ± per 1 kg FWD 1 + 7.75 - . 0 4 2 8 7AFT 1 + 22.34 + . 0 5 4 4 1
Remarks: 8.4 Galleys
Galley locations Length of arm from
reference station
Index influence
± Inch / metre ± per 1 kg FWD + 21.47 + . 0 4 8 6 1 AFT + 23.09 + . 0 5 9 4 3
Remarks:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 12
Cabin-Configuration(s) 12YP/58Y OR 70Y
A/C TYPE ATR72-500
CARRIER PK
8.5 Pantry Weight / Pantry Code (normally used for above mentioned cabin configurations). NOTE: The columns “Pantry Weight” and “Location” must be filled in only if Basic Weight is specified under paragraph 2.
Pantry Code Pantry Weight Location *
International
Domestic
Test & Training
467 KG
364 KG
45 KG
* Use the locations as under paragraph 8.4.
REMARKS:
8.6 Crew Distribution / Crew Code (normally used for above mentioned cabin configurations). NOTE: The column “Location” is to be filled in only if Basic Weight is specified under paragraph 2.
Crew Code Cockpit Crew Cabin Crew Location *
Location of Crew Baggage
REFER ENCLOSED PAGE FOR CREW
IN RH FWD HOLD
* Use the location as under paragraph 8.3.
Total
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 13
Cabin-Configuration(s) 12YP/58Y OR 70Y
A/C TYPE ATR72-500
CARRIER PK
9. DETAILS FOR COMPARTMENT TRIM
Compartment Number Description
Maximum Capacity
Index value ± per 1 kg Gross Weight
(kg) Volume *
(m3) RH FWD COMPT BULK 480
3 - . 0 4 9 8 9
LH FWD COMPT BULK 448
2.8 - . 0 4 9 8 9
FWD PART AFT COMPT BULK 195
1.23 + . 0 6 0 4 4
AFT PART AFT COMPT BULK 442 2.75 + . 0 6 7 5 3
* Volume information required for bulk compartments only.
Remarks: IN CASE OF CATERING IS LOADED IN REAR CARGO GALLEY, ONLY AFT PART OF THE AFT HOLD WILL BE USED FOR BULK BAGGAGE AND CARGO LOADING AND FWD PART OF AFT HOLD WILL REMAIN EMPTY DUE TO CATERING LOADING AND UNLOADING IN THE REAR CARGO COMPARTMENT GALLEY. 9.1 Combined Load Limitations. Attach relevant company regulations.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
10. DETAILS FOR BAY / SECTION TRIM
Bay / Section Maximum Capacity Index value
± per 1 kg
Gross Weight (kg)
Volume * (m3)
FWD HOLD FWD RH COMPT 480 3 - . 0 4 9 8 9 FWD LH COMPT 448 2.8 - . 0 4 9 8 9
AFT HOLD
AFT PART AFT COMPT 442 2.75 + 0 6 7 5 3
* Volume information required for bulk compartments only. NOTE 1: Attach a plan for each compartment configuration. NOTE 2: Use additional sheets as required.
10.1 Unsymmetrical Load Limitations.
Attach relevant company regulations.
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 14
Cabin-Configuration(s) 12YP/58Y OR 70Y (WITH PANTRY LOADED IN REAR CARGO GALLEY)
A/C TYPE ATR72-500
CARRIER PK
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 23/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 15
A/C TYPE ATR72-500
CARRIER PK
11. BALLAST
FIXED PROVISIONS FOR CARRYING BALLAST.
Specify or attach a table.
Remarks:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 28/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
LOADPLANNING-DATA D SHEET 1
A/C TYPE ATR72-500
CARRIER PK
1. UNIT LOAD DEVICES DETAILS
MAXIMUM CAPACITY TYPE CODE TARE WEIGHT GROSS WEIGHT VOLUME * REMARKS
------------- NOT -------------------- APPLICABLE --------------------
* Containers / lgloos only Note: For pallets, specify Lower Deck or Main Deck.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: INITIAL
Date: 28/04/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
LOADPLANNING-DATA D SHEET 2
A/C TYPE ATR72-500
CARRIER PK
2. SPECIAL LOAD
Attach relevant company regulations for special load (AVI, Dangerous Goods, etc.). PLEASE REFER TO PIA WEIGHT AND BALANCE MANUAL AND CARGO HANDLING MANUAL.
LEP AHM50 ISSUE 00.xlssheet a 1ASHEET 1
COMMUNICATIONADDRESSESPK
sheet a 2ASHEET 2
COMMUNICATIONADDRESSESPK
sheet b 1BSHEET 1PK
GENERAL INFORMATION
sheet b 2BSHEET 2
AIRCRAFT DATAPK
sheet b 3BSHEET 3
GENERAL INFORMATIONPK
sheet c 1CSHEET 1
AIRCRAFT DATAPKATR72-500
sheet c 2CSHEET 2
AIRCRAFT DATAPKATR72-500
sheet c 3CSHEET 3
AIRCRAFT DATAPKATR72-500
sheet c 4CSHEET 4
AIRCRAFT DATAPKATR72-500
sheet c 4aCSHEET 4A
AIRCRAFT DATAPKATR72-500
sheet c 4bsheet c 4cCSHEET 4C
AIRCRAFT DATAPKATR72-500
sheet c 4dCSHEET 4D
AIRCRAFT DATAPKATR72-500
sheet c 4esheet c 5CSHEET 5
AIRCRAFT DATAATR72-500PK
sheet c 6CSHEET 6
AIRCRAFT DATAPKN
ATR72-500
sheet c 7sheet c 8CSHEET 8ATR72-500PK
AIRCRAFT DATAClass codes :(e.g. F, Y, C, M etc.) Class 1 YP Class 4Class 2 Y Class 5Class 3Remarks
sheet c 8asheet c 9CSHEET 912YP/58Y OR 70Y
ATR72-500PK
AIRCRAFT DATA
sheet c 10sheet c 11sheet c 12sheet c 13CSHEET 1312YP/58Y OR 70Y
AIRCRAFT DATAPKATR72-500
sheet c 14sheet c 15CSHEET 15
AIRCRAFT DATAFIXED PROVISIONS FOR CARRYING BALLAST.Specify or attach a table.Remarks:
sheet d 1DSHEET 1
LOADPLANNING-DATAPKATR72-500
sheet d 2DSHEET 2
LOADPLANNING-DATAAttach relevant company regulations for special load (AVI, Dangerous Goods, etc.).