flight performance and planning · 2020. 9. 30. · ppl flight planning manual- aeroplane weight...

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

-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


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


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


SACAA-01

FLAPS UP TAKE-OFF GROUND ROLL

Figure 1-3: Flaps Up Take-off Ground Roll


-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


SACAA-01

FLAPS UP TAKE-OFF PERFORMANCE

Figure 1-4: Flaps Up Take-off Performance


-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-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


SACAA-01

25° FLAPS TAKE-OFF GROUND ROLL

Figure 1-5: 25° Flaps Take-off Ground Roll


-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-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


SACAA-01

25° FLAPS TAKE-OFF PERFORMANCE

Figure 1-6: 25° Flaps Take-off Performance


-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-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


SACAA-01

CLIMB PERFORMANCE

Figure 1-7: Climb Performance


-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


SACAA-01

TIME, DISTANCE AND FUEL TO CLIMB

Figure 1-8: Time, Distance and Fuel to Climb


-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


SACAA-01

ENGINE PERFORMANCE

Figure 1-9: Engine Performance


-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


SACAA-01

SPEED POWER - PERFORMANCE CRUISE

Figure 1-10: Speed Power - Performance Cruise


-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


SACAA-01

SPEED POWER - ECONOMY CRUISE

Figure 1-11: Speed Power - Economy Cruise



-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



-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



-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



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



-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



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



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-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



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-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


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


SACAA-01

CLIMB PERFORMANCE TABLE

Figure 1-20: Climb Performance Table


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


SACAA-01

STALL SPEEDS TABLE

Figure 1-21: Stall Speeds Table


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


SACAA-01

TAKE-OFF PERFORMANCE TABLE

Figure 1-22: Take-off Performance Table


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

:

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ps

up

,

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llp

ow

er

befo

reb

rake

rele

ase,

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,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

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by

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reach

2kn

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tailw

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.

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ro

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incre

ase

all

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%

ofth

e"G

rou

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ll"fig

ure

.


SACAA-01

CRUISE PERFORMANCE TABLE

Figure 1-23: Cruise Performance Table


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


SACAA-01

LANDING PERFORMANCE TABLE

Figure 1-24: Landing Performance Table


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.

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ro

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rass

run

way

incre

ase

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tan

ces

by

25

%

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e"G

rou

nd

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ll"fig

ure

.

LA

ND

ING

DIS

TA

NC

ER

EQ

UIR

ED


SACAA-01

MASS AND BALANCE LOADING FORM

Figure 2-1: Mass and Balance Loading Form


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



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



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

flight performance and planning · 2020. 9. 30. · ppl flight planning manual- aeroplane weight...

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