View
1
Download
0
Category
Preview:
Citation preview
FOR EXAMINATION PURPOSES ONLY
AEROPLANE MANUAL
PRIVATE PILOT LICENCE
FLIGHT
AND
PERFORMANCE
PLANNING
SACAA-01
SOUTH AFRICAN
CIVIL AVIATION
AUTHORITY
PLEASE DO NOT MARK ON OR DAMAGE THIS MANUAL IN ANY WAY
OCTOBER 2008
CONTENTS
SECTION 1 - PERFORMANCE GRAPHS
Page 1-1 .........Figure 1-1..............Airspeed System CalibrationPage 1-2 .........Figure 1-2..............Stall SpeedsPage 1-3 .........Figure 1-3..............Flaps Up Take-off Ground RollPage 1-4 .........Figure 1-4..............Flaps Up Take-off PerformancePage 1-5 .........Figure 1-5..............25° Flaps Take-off Ground RollPage 1-6 .........Figure 1-6..............25° Flaps Take-off PerformancePage 1-7 .........Figure 1-7..............Climb PerformancePage 1-8 .........Figure 1-8..............Time, Distance and Fuel to ClimbPage 1-9 .........Figure 1-9..............Engine PerformancePage 1-10 .......Figure 1-10............Speed Power - Performance CruisePage 1-11 .......Figure 1-11............Speed Power - Economy CruisePage 1-12 .......Figure 1-12............Range - Performance CruisePage 1-13 .......Figure 1-13............Range - Economy CruisePage 1-14 .......Figure 1-14............EndurancePage 1-15 .......Figure 1-15............Time, Fuel and Distance to DescendPage 1-16 .......Figure 1-16............Glide RangePage 1-17 .......Figure 1-17............Landing PerformancePage 1-18 .......Figure 1-18............Landing Ground RollPage 1-19 .......Figure 1-19............Airspeed Calibration TablePage 1-20 .......Figure 1-20............Climb Performance TablePage 1-21 .......Figure 1-21............Stall Speeds TablePage 1-22 .......Figure 1-22............Take-off Performance TablePage 1-23 .......Figure 1-23............Cruise Performance TablePage 1-24 .......Figure 1-24............Landing Performance Table
SECTION 2 - MASS AND BALANCE
Page 2-1 .........Figure 2-1..............Mass and Balance Loading FormPage 2-2 .........Figure 2-2..............Loading GraphPage 2-3 .........Figure 2-3..............CG Range and Weight
PPL Flight Planning Manual- Aeroplane
CONTENTSPage (i)
AIRSPEED SYSTEM CALIBRATION
Figure 1-1: Airspeed System Calibration
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-1
50 70 90 110 130 150 170 190
INDICATED AIRSPEED - KNOTS
CA
LIB
RA
TE
DA
IRS
PE
ED
-K
NO
TS
170
150
130
110
90
70
50
0°FLAPS
40°FLAPS
AIRSPEED SYSTEM CALIBRATION
2500 LBS GROSS WEIGHT
SACAA-01
STALL SPEEDS
Figure 1-2: Stall Speeds
PPL Flight Planning Manual- Aeroplane
25
20
15
25
20
15
020
40
60
WE
IGH
T-
10
0L
BS
AN
GL
EO
FB
AN
K-
DE
GR
EE
S
CA
LIB
RA
TE
DA
IRS
PE
ED
IND
ICA
TE
DA
IRS
PE
ED
50
60
70
80
90
40
STA
LL
SP
EE
DS
PO
WE
RO
FF
0°
FL
AP
S
25°
FL
AP
S
40°
FL
AP
S
2500
LB
SG
RO
SS
WE
IGH
T
PERFORMANCE GRAPHSPage 1-2
SACAA-01
FLAPS UP TAKE-OFF GROUND ROLL
Figure 1-3: Flaps Up Take-off Ground Roll
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
2500
2300
2100
1900
010
20
500
1000
1500
2000
2500
TAKE-OFFGROUNDROLL-FEET
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°C
WE
IGH
T-
LB
SW
IND
-K
NO
TS
SEALE
VEL10
0020
00
3000
4000
5000
6000
7000
STD. TEMP
PRESSUREALT
-FT
REFERENCELINE-2500LBS
REFERENCELINE-WIND
HEA
DW
IND
TAILWIND
FL
AP
SU
PTA
KE
-OF
FG
RO
UN
DR
OL
LF
ULL
TH
RO
TT
LE
BE
FO
RE
BR
AK
ER
ELE
AS
E
PA
VE
D,LE
VE
L,D
RY
RU
NW
AY
TAK
E-O
FF
SP
EE
DS
-K
IAS
WT
-L
BS
LIF
TO
FF
2500
5324
0050
2300
4921
0047
PERFORMANCE GRAPHSPage 1-3
SACAA-01
FLAPS UP TAKE-OFF PERFORMANCE
Figure 1-4: Flaps Up Take-off Performance
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
2500
2300
2100
1900
010
20
1500
2000
2500
3000
3500
4000
TAKE-OFFDISTANCEOVER50FTBARRIER-FEET
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°C
WE
IGH
T-
LB
SW
IND
-K
NO
TS
SEALE
VEL
1000
2000
3000
40005000
6000
7000
STD. TEMP
PRESSUREALT-FT
REFERENCELINE-2500LBS
REFERENCELINE-WIND
HEA
DW
IND
TAILWIND
FL
AP
SU
PTA
KE
-OF
FP
ER
FO
RM
AN
CE
FU
LL
TH
RO
TT
LE
BE
FO
RE
BR
AK
ER
ELE
AS
E
PA
VE
D,LE
VE
L,D
RY
RU
NW
AY
1000
TAK
E-O
FF
SP
EE
DS
-K
IAS
WT
-L
BS
LIF
TO
FF
50F
T25
0053
6024
0050
5723
0049
5521
0047
53
PERFORMANCE GRAPHSPage 1-4
SACAA-01
25° FLAPS TAKE-OFF GROUND ROLL
Figure 1-5: 25° Flaps Take-off Ground Roll
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
2500
2300
2100
1900
010
20
500
1000
1500
2000
TAKE-OFFGROUNDROLL-FEET
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°C
WE
IGH
T-
LB
SW
IND
-K
NO
TS
SE
ALE
VE
L
1000
2000
300040
0050
00
6000
7000
STD. TEMP
PRESSUREALT
-FT
REFERENCELINE-2500LBS
REFERENCELINE-WIND
HEA
DW
IND
TAILWIND
25°
FL
AP
STA
KE
-OF
FG
RO
UN
DR
OL
LF
ULL
TH
RO
TT
LE
BE
FO
RE
BR
AK
ER
ELE
AS
E
PA
VE
D,LE
VE
L,D
RY
RU
NW
AY
TAK
E-O
FF
SP
EE
DS
-K
IAS
WT
-L
BS
LIF
TO
FF
2500
5024
0048
2300
4521
0043
2500
PERFORMANCE GRAPHSPage 1-5
SACAA-01
25° FLAPS TAKE-OFF PERFORMANCE
Figure 1-6: 25° Flaps Take-off Performance
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
2500
2300
2100
1900
010
20
1000
1500
2000
2500
3000
3500
TAKE-OFFDISTANCEOVER50FTBARRIER-FEET
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°C
WE
IGH
T-
LB
SW
IND
-K
NO
TS
SEALE
VEL
1000
200030
004000
5000
6000
7000
STD. TEMP
PRESSUREALT
-FT
REFERENCELINE-2500LBS
REFERENCELINE-WIND
HEADWIN
D
25°
FL
AP
STA
KE
-OF
FP
ER
FO
RM
AN
CE
FU
LL
TH
RO
TT
LE
BE
FO
RE
BR
AK
ER
ELE
AS
E
PA
VE
D,LE
VE
L,D
RY
RU
NW
AY
TAILWIND
TAK
E-O
FF
SP
EE
DS
-K
IAS
WT
-L
BS
LIF
TO
FF
50F
T25
0050
5524
0048
5323
0046
5121
0045
50
PERFORMANCE GRAPHSPage 1-6
SACAA-01
CLIMB PERFORMANCE
Figure 1-7: Climb Performance
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
0200
400
600
800
1000
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CR
AT
EO
FC
LIM
B-
FP
M
SEALEVEL
1000
2000
3000
4000
500060
0070
0080
00
9000
1000
0
1100
0
1200
0
1300
0
PRESSUREALTITUDE-FEET
STD TEMP
CL
IMB
PE
RF
OR
MA
NC
EF
UL
LT
HR
OT
TL
E,F
LA
PS
UP,
75
KIA
S
2500
LB
SG
RO
SS
WE
IGH
T
PERFORMANCE GRAPHSPage 1-7
SACAA-01
TIME, DISTANCE AND FUEL TO CLIMB
Figure 1-8: Time, Distance and Fuel to Climb
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
010
20
30
40
50
60
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CT
IME
,D
ISTA
NC
EA
ND
FU
EL
TO
CL
IMB
SE
AL
EV
EL
1000
2000
3000
4000
5000
6000
7000
8000
9000
1000
0
1100
0
1200
0PRESSURE
ALTIT
UDE-FEET
STD TEMP
FUEL-GAL
TIME
-MIN
DIS
TAN
CE
-NM
TIM
E,D
ISTA
NC
EA
ND
FU
EL
TO
CL
IMB
CL
IMB
AT
FU
LL
TH
RO
TT
LE
75K
IAS
, FL
AP
SU
P,25
00L
BS
GR
OS
SW
EIG
HT
GR
AP
HIN
CL
UD
ES
FU
EL
FO
RS
TAR
T,TA
XI A
ND
TAK
E-O
FF
PERFORMANCE GRAPHSPage 1-8
SACAA-01
ENGINE PERFORMANCE
Figure 1-9: Engine Performance
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
2000
2200
2400
2600
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CE
NG
INE
SP
EE
D-
RP
M
1000
2000
3000
4000
5000
6000
7000
80009000
10000
11000
12000
SEALEVEL
STD TEMPPRESSUREALT
ITUDE-FEET
PE
RC
EN
TP
OW
ER
5560
6570
75
EN
GIN
EP
ER
FO
RM
AN
CE
BE
ST
PO
WE
RM
IXT
UR
E
FU
EL
FL
OW
-G
AL
LO
NS
PE
RH
OU
RB
ES
TP
OW
ER
BE
ST
EC
ON
OM
Y7.
555
%6.
08.
565
%7.
010
.075
%8.
5
PERFORMANCE GRAPHSPage 1-9
SACAA-01
SPEED POWER - PERFORMANCE CRUISE
Figure 1-10: Speed Power - Performance Cruise
PPL Flight Planning Manual- Aeroplane
-40
-20
020
40
90
100
110
120
130
140
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CT
RU
EA
IRS
PE
ED
-K
NO
TS
1000
2000
3000
4000
5000
6000
7000
80009000
10000
11000
12000
SEALEVEL
STD TEMPPRESSUREALT
ITUDE-FEET
PE
RC
EN
TP
OW
ER
5565
75
SP
EE
DP
OW
ER
-P
ER
FO
RM
AN
CE
CR
UIS
E
BE
ST
PO
WE
RM
IXT
UR
E
2650 RPM OR FULL THROTTLE
2500
LB
SM
AX
GR
OS
SW
EIG
HT
PERFORMANCE GRAPHSPage 1-10
SACAA-01
SPEED POWER - ECONOMY CRUISE
Figure 1-11: Speed Power - Economy Cruise
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-11
-40
-20
020
40
90
100
110
120
130
140
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CT
RU
EA
IRS
PE
ED
-K
NO
TS
1000
2000
3000
4000
5000
6000
7000
80009000
10000
11000
12000
SEALEVEL
STD TEMPPRESSUREALT
ITUDE-FEET
PE
RC
EN
TP
OW
ER
5565
SP
EE
DP
OW
ER
-E
CO
NO
MY
CR
UIS
E
BE
ST
EC
ON
OM
YM
IXT
UR
E
2650 RPM OR FULL THROTTLE
2500
LB
SM
AX
GR
OS
SW
EIG
HT
SU
BT
RA
CT
5K
TS
IFW
HE
EL
FA
IRIN
GS
RE
MO
VE
D
SACAA-01
RANGE - PERFORMANCE CRUISE
Figure 1-12: Range - Performance Cruise
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-12
-40
-20
020
40
400
500
600
500
600
700
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CR
AN
GE
-N
AU
TIC
AL
MIL
ES
2000
4000
6000
800010000
12000
SEALEVEL
STD TEMPPRESSUREALTITUDE-FEET
RA
NG
E-
PE
RF
OR
MA
NC
EC
RU
ISE
BE
ST
PO
WE
RM
IXT
UR
E2500
LB
SM
AX
GR
OS
SW
EIG
HT
RA
NG
ER
ED
UC
ED
BY
5%
IF
WH
EE
LFA
IRIN
GS
RE
MO
VE
D
RA
NG
EW
ITH
45
MIN
RE
SE
RV
E
AT
55%
PO
WE
R
RA
NG
EW
ITH
NO
RE
SE
RV
E
55%
PO
WE
R
65%
75%
55%
65%
75%
SACAA-01
RANGE - ECONOMY CRUISE
Figure 1-13: Range - Economy Cruise
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-13
-40
-20
020
40
500
600
700
600
700
800
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CR
AN
GE
-N
AU
TIC
AL
MIL
ES
2000
4000
6000
800010000
12000
SEALEVEL
STD TEMPPRESSUREALTITUDE-FEETRA
NG
E-
EC
ON
OM
YC
RU
ISE
BE
ST
EC
ON
OM
YM
IXT
UR
E2500
LB
SM
AX
GR
OS
SW
EIG
HT
RA
NG
ER
ED
UC
ED
BY
5%
IF
WH
EE
LFA
IRIN
GS
RE
MO
VE
D
RA
NG
EW
ITH
45
MIN
RE
SE
RV
E
AT
55%
PO
WE
R
RA
NG
EW
ITH
NO
RE
SE
RV
E
55%
PO
WE
R
65%
75%
55%
65%
75%
SACAA-01
ENDURANCE
Figure 1-14: Endurance
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-14
EN
DU
RA
NC
E-
HO
UR
S
EN
DU
RA
NC
EB
ES
TE
CO
NO
MY
MIX
TU
RE
2500
LB
SM
AX
GR
OS
SW
EIG
HT
EN
DU
RA
NC
EW
ITH
45
MIN
RE
SE
RV
E
AT
55%
PO
WE
R
EN
DU
RA
NC
E
WIT
HN
O
RE
SE
RV
E65%
75%
75%
34
56
74
56
7S
L
2000
4000
6000
8000
10000
12000
55%
PO
WE
R55%
65%
PRESSUREALTITUDE-FT
SACAA-01
TIME, FUEL AND DISTANCE TO DESCEND
Figure 1-15: Time, Fuel and Distance to Descend
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-15
-40
-20
020
40
10
20
30
40
50
60
70
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°CT
IME
,D
ISTA
NC
EA
ND
FU
EL
1000
2000
3000
4000
5000
6000
7000
8000
9000
1000
0
1100
0
1200
0
SE
AL
EV
EL
STD TEMP
TIM
E,F
UE
LA
ND
DIS
TA
NC
ET
OD
ES
CE
ND
PR
ES
SU
RE
ALT
ITU
DE
-F
EE
T
FUEL-GAL
TIME
-MIN
DIS
TANCE
-NM
DE
SC
EN
DA
T115
KIA
S,
2400
RP
M
2500
LB
SG
RO
SS
WE
IGH
T
SACAA-01
GLIDE RANGE
Figure 1-16: Glide range
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-16
SACAA-01
010
20
30
40
GL
IDE
RA
NG
E-
NA
UT
ICA
LM
ILE
S
GL
IDE
RA
NG
E
0
2000
4000
6000
8000
10000
12000
PRESSUREALTITUDE-FEETP
OW
ER
OF
F,0°
FL
AP,
75
KIA
S
2500
LB
S,
ZE
RO
WIN
D
LANDING PERFORMANCE
Figure 1-17: Landing Performance
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-17
SACAA-01
-40
-20
020
40
2500
2300
2100
1900
010
20
1100
1200
1300
1400
1500
LANDINGDISTANCEOVER50FTBARRIER-FEET
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°C
WE
IGH
T-
LB
SW
IND
-K
NO
TS
SE
ALE
VE
L
2000
4000
STD. TEMP
PRESSUREALT
-FT
REFERENCELINE-2500LBS
REFERENCELINE-WIND
HEADWIN
D
TAILWIND
LA
ND
ING
PE
RF
OR
MA
NC
E
6000
8000
1000
PO
WE
RO
FF,
40
°F
LA
PS
,F
UL
LS
TA
LL
TO
UC
HD
OW
N
MA
XIM
UM
SA
FE
BR
AK
ING
PA
VE
D,
LE
VE
L,
DR
YR
UN
WA
Y
65
KIA
SA
PP
RO
AC
HS
PE
ED
LANDING GROUND ROLL
Figure 1-18: Landing Ground Roll
PPL Flight Planning Manual- Aeroplane
PERFORMANCE GRAPHSPage 1-18
SACAA-01
-40
-20
020
40
2500
2300
2100
1900
010
20
600
700
800
900
1000
LANDINGGROUNDROLL-FEET
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E-
°C
WE
IGH
T-
LB
SW
IND
-K
NO
TS
SE
ALE
VE
L
2000
4000
STD. TEMP
PRESSUREALT
-FT
REFERENCELINE-2500LBS
REFERENCELINE-WIND
HEADWIN
D
TAILWIND
LA
ND
ING
GR
OU
ND
RO
LL
6000
8000
500
PO
WE
RO
FF,
40
°F
LA
PS
,F
UL
LS
TA
LL
TO
UC
HD
OW
N
MA
XIM
UM
SA
FE
BR
AK
ING
PA
VE
D,
LE
VE
L,
DR
YR
UN
WA
Y
65
KIA
SA
PP
RO
AC
HS
PE
ED
AIRSPEED CALIBRATION TABLE
Figure 1-19: Airspeed Calibration Table
PPL Flight Planning Manual- Aeroplane
FLAPS UP
KIAS 40 50 60 70 80 90 100 110 120 130 140 150
KCAS
FLAPS 10°
KIAS
KCAS
FLAPS 40°
KIAS
KCAS
40 50 60 70 80 90 100 110 120 - - - - - - - - -
40 50 60 70 80 90 100 110 120 - - - - - - - - -
47 56 63 71 80 90 98 107 117 128 138 149
47 56 63 72 82 91 99 110 120 - - - - - - - - -
45 54 62 71 81 91 101 111 122 - - - - - - - - -
AIRSPEED CORRECTION TABLE
PERFORMANCE GRAPHSPage 1-19
SACAA-01
CLIMB PERFORMANCE TABLE
Figure 1-20: Climb Performance Table
PPL Flight Planning Manual- Aeroplane
WEIGHT
LBS
PRESS CLIMB
ALT SPEED
FT KIAS
RATE OF CLIMB - FPM
-20°C 0°C 20°C 40°C
2300 SL 75 750 690 625 560
2000 73 650 590 530 475
4000 71 550 495 435 375
6000 69 455 400 325 270
8000 67 360 305 250 195
10,000 65 260 210 160 - - -
12,000 63 170 120 - - - - - -
CLIMB PERFORMANCE
CONDITIONS: Full Power, Flaps retracted and mixture leaned
for maximum RPM during the climb
PERFORMANCE GRAPHSPage 1-20
SACAA-01
STALL SPEEDS TABLE
Figure 1-21: Stall Speeds Table
PPL Flight Planning Manual- Aeroplane
WEIGHT FLAP
(LBS) SETTING
ANGLE OF BANK
0° 30° 45° 60°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
2400
UP 48 54 52 58 58 64 68 76
10° 45 52 48 56 54 60 64 74
40° 42 48 46 52 50 56 60 68
UP 44 52 48 54 52 58 60 68
10° 42 48 46 52 50 56 56 64
40° 40 46 44 50 48 54 54 62
2200
STALL SPEEDS
CONDITIONS: Power Off.
NOTE: Indicated airspeed figures are approximate values
PERFORMANCE GRAPHSPage 1-21
SACAA-01
TAKE-OFF PERFORMANCE TABLE
Figure 1-22: Take-off Performance Table
PPL Flight Planning Manual- Aeroplane
WE
IGH
T
(LB
S)
TA
KE
-OF
F
SP
EE
D
(KIA
S)
PR
ES
SU
RE
ALT
ITU
DE
(FT
)
0°C
10
°C2
0°C
30
°C4
0°C
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
LIF
TA
T
OF
F5
0F
T
24
00
54
60
SE
ALE
VE
L7
85
14
20
84
51
51
59
05
16
15
97
01
72
51
04
01
83
5
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
10
00
86
01
55
09
25
16
55
99
01
76
51
06
01
90
51
13
52
01
0
20
00
94
01
69
01
01
01
81
01
08
51
93
51
16
52
07
01
24
52
21
0
30
00
10
30
19
55
11
10
19
85
11
90
21
25
12
80
22
75
13
70
23
35
40
00
11
35
20
40
12
20
21
85
13
10
23
45
14
05
25
15
15
05
26
95
50
00
12
45
22
50
13
40
24
15
14
40
25
95
15
50
27
90
16
60
30
00
60
00
13
75
24
90
14
80
26
80
15
90
28
90
17
10
31
10
----
----
70
00
15
15
27
70
16
35
30
35
17
60
32
30
18
80
33
30
----
----
80
00
16
75
31
05
18
10
33
60
19
35
35
60
----
----
----
----
TA
KE
-OF
FD
ISTA
NC
ER
EQ
UIR
ED
CO
ND
ITIO
NS
:
Fla
ps
up
,
Fu
llp
ow
er
befo
reb
rake
rele
ase,
Paved
,le
vel,
dry
run
way,
Zero
win
d
NO
TE
S:
Decre
ase
all
dis
tan
ces
by
10
%fo
reach
5kn
ots
head
win
d.
Incre
ase
all
dis
tan
ces
by
10
%fo
reach
2kn
ots
tailw
ind
.
Fo
ro
pera
tio
no
na
dry
,g
rass
run
way
incre
ase
all
dis
tan
ces
by
10
%
ofth
e"G
rou
nd
Ro
ll"fig
ure
.
PERFORMANCE GRAPHSPage 1-22
SACAA-01
CRUISE PERFORMANCE TABLE
Figure 1-23: Cruise Performance Table
PPL Flight Planning Manual- Aeroplane
CRUISE PERFORMANCE
Gross Weight 2300 Lbs, Mixture Leaned For Cruise, Zero Wind
RPM
2000 2600 85 124 9.6 4.7 650
2500 78 119 8.5 5.4 730
2400 71 113 7.7 6.0 750
2300 64 107 7.1 6.5 760
2200 58 101 6.6 7.0 785
4000 2600 81 124 8.9 5.1 690
2500 74 118 8.0 5.7 750
2400 67 112 7.3 6.2 780
2300 60 106 6.8 6.7 795
2200 53 98 6.4 7.2 795
6000 2600 77 123 8.3 5.5 745
2500 70 117 7.6 6.0 780
2400 63 111 7.0 6.5 790
2300 57 103 6.6 7.0 810
2200 51 95 6.1 7.5 800
8000 2600 69 119 7.5 6.1 800
2500 66 115 7.2 6.3 810
2400 60 108 6.8 6.8 820
2300 54 100 6.3 7.3 815
2200 48 90 5.9 7.8 790
10, 000 2600 62 113 6.9 6.6 830
2500 56 105 6.5 7.1 825
2400 50 95 6.1 7.6 805
Figures are based on 48 Gallons of usable fuel (No Reserve)
Endurance Range
(hours) (nm)PRESSURE
ALTITUDE % BHP KTAS GPH
PERFORMANCE GRAPHSPage 1-23
SACAA-01
LANDING PERFORMANCE TABLE
Figure 1-24: Landing Performance Table
PPL Flight Planning Manual- Aeroplane
WE
IGH
T
LB
S
PR
ES
SU
RE
ALT
ITU
DE
FE
ET
KIA
SA
T
50
FT
0°C
10
°C2
0°C
30
°C4
0°C
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
GN
D
RO
LL
TO
TA
L
TO
CLE
AR
50
FT
24
00
65
SE
ALE
VE
L5
00
12
20
51
51
25
05
35
12
80
55
01
31
05
70
13
45
10
00
51
51
25
05
35
12
80
55
51
31
55
70
13
45
59
01
38
0
20
00
53
51
28
05
55
13
15
57
51
35
05
95
13
85
61
51
42
0
30
00
55
51
31
55
75
13
50
59
51
38
56
15
14
20
63
51
45
5
40
00
57
51
35
05
95
13
85
62
01
42
56
40
14
60
66
01
49
5
50
00
59
51
38
56
20
14
40
64
01
46
56
60
15
00
68
51
54
0
60
00
62
01
44
06
45
14
70
70
51
50
56
90
15
50
71
01
62
5
70
00
64
51
48
06
65
15
10
73
01
55
07
15
15
90
73
51
67
0
80
00
67
01
52
56
95
15
55
75
51
59
57
40
16
35
76
51
72
0
CO
ND
ITIO
NS
:
Fla
ps
40
°
Po
wer
off
Maxim
um
bra
kin
g
Paved
,le
vel,
dry
run
way
Zero
win
d
NO
TE
S:
Decre
ase
all
dis
tan
ces
by
10
%fo
reach
10
kn
ots
ofh
ead
win
d.
Incre
ase
all
dis
tan
ces
by
10
%fo
reach
10
kn
ots
ofta
ilwin
d.
Fo
ro
pera
tio
no
na
dry
,g
rass
run
way
incre
ase
all
dis
tan
ces
by
25
%
ofth
e"G
rou
nd
Ro
ll"fig
ure
.
LA
ND
ING
DIS
TA
NC
ER
EQ
UIR
ED
PERFORMANCE GRAPHSPage 1-24
SACAA-01
MASS AND BALANCE LOADING FORM
Figure 2-1: Mass and Balance Loading Form
PPL Flight Planning Manual- Aeroplane
MASS AND BALANCEPage 2-1
Weight Arm Aft Datum Moment
Basic Empty Weight 1490 84.7 126203
Pilot and Passenger 77.8
Passengers (Aft) 116.6
Fuel 93.0
Baggage 140.5
Total Loaded Aeroplane
(lbs) (inches) (inch-pounds)
NOTE: The Maximum All Up Weight of this aeroplane is 2500 lb.
SACAA-01
LOADING GRAPH
Figure 2-2: Loading Graph
PPL Flight Planning Manual- Aeroplane
MASS AND BALANCEPage 2-2
0 10 20 30 40 50
500
400
300
200
100
0
MOMENT/1000 (POUNDS - INCHES)
LO
AD
WE
IGH
T(P
OU
ND
S)
PILO
TAND
FRO
NTPA
SSEN
GER
FUEL
(6LB
/USG) AFT
PASSENGERS
BAGGAGE
SACAA-01
CG RANGE AND WEIGHT
Figure 2-3: CG Range and Weight
PPL Flight Planning Manual- Aeroplane
MASS AND BALANCEPage 2-3
1100
1300
1500
1700
1900
2100
2300
2500
81 83 85 87 89 91 93
UTILITY CATEGORY
NORMAL CATEGORY
CG LOCATION - INCHES AFT OF DATUM
AE
RO
PL
AN
EW
EIG
HT
INP
OU
ND
S
SACAA-01
Recommended