LOADSHEET & Loadmessage -.+ - Walter Bislins

Fly awa,ykits considered in CG % calculations. Approved By ... kg kg kg. --, CORRECTEDINDEX1D .1. WEIGHT. INDEX. WEIGHT. INDEX. (kg). (kg). 1000. 1.5.
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LOADSHEET & Loadmessage ADDRESS :

TO:

FROM:

DISTRIBUTOR

-.

:

MaxWeightfor

Takeoff 0

1

WEIGHT :1:

Adjustments

TAKE OF FUEL

Operating

l'Trip Fuel

b

Max.Allowed Take off Weight: Lowestof a, b or e

Ccrreeted Dry Op Wt

rr:::: ..

-.+

Take off Fuel DRY OPERATING

DATE

CREW

FLiGHT

Weight

Allowed Traffie Load

OPERATINGWEIGHT TOTALS

DEST

5

B C M T Tr

2

3

4

5

2

3

4

5

2

3

4

B C M T Tr B C M

.

.

.

T

IL

TOTAL!

Allowed

+

Passenger Weight

Traffie Load

TOTAL TRAFFIC LOAD

.

DRY OPERATING WEIGHT

ZERO FUEL WEIGHT L M C

DEST

+ 1 - = TAKE OF FUEL

Passenger

Yes

Details

Weight M

TAKE OFWEIGHT

F

L M C + 1- =

C TOTAL LMC

TRIPFUEL

1 TOTAL Balance Condition

L M C + 1- = Prepared By

DOW includes the basic weight, crew members, fly away kits and pantry load. Fly awa,y kits considered in CG % calculations. Approved By

Ali Nets Fitted and Controlled.

.

~

.n.-

--

'r

JnURAIR AIRBUS INDUSTRIE

LOAD

and

VERSION: TO:

FROM:

.

OHY G . 040

TURKISH DGCAAPPROVAL 1055361

REG/STRATION:

FLT NO 1 DTE:

KILOGRAMS

kg kg

TOTAL TOTAL FUEL FUEL

kg kg

TOTAL WEIGHT

kg

Cabin Section

Version Pax

TC-OAA

Compartment

OA

OB

OC

46

175

94

47

171

97

49

163

99

1

2

3

4

5

9522

6348

2770

315

TC-OAB TC-OAG TC-OAH

ZONES

ZERO FUEL ZERO FUEL WEIGHT WEIGHT

APPROVED BY :

PREPARED BY :

ALL WEIGHT WEIGHT

.'

Registration

ALL WEIGHTIN

A300 - 600 R

TRIM

311

--,

9522

9522

CORRECTED INDEX1D

CARGO 1 CARGO 2

-

CARGO 3 CARGO 4 CARGO 5 CABIN

OA

CABIN

OB

CABIN°c TRANSFER TRIM TANK FUEL CORRECTION % MAC

FUEL INDEX CORRECTION WEIGHT (kg) 1000 2000 3000 4000 5000 6000 7000 8000 9.000 10000 11000 12000 13000 14000 15000 16000 17000 18000 19000 20000 21000 22000 23000 24000

INDEX WEIGHT INDEX (kg) 3.6 1.5 25000 3.1 26000 3.4 4.7 27000 3.2 6.5 28000 3.2 8.4 29000 3.2 30000 3.4 10.5 12.8 31000 3.8 13.0 32000 4.0 33000 4.5 12.2 11.6 34000 5.0 11,0 6.4 34721 10.3 36000 5.2 9.7 .36000 4.6 37000 3.7 9.1 8.4 2.7 38000 1.7 7.8 39000 7,2 40000 .7 6.7 41000 -.4 42000 -1.4 6,1 5,6 -2.4 43000 5,1 44000 -3.4 4.7 -4.4 45000 4.2 46000 -5.4 3,9 47000 -6.5

NOTE: FOR FUEL WEIGHT GREATER THAN 47.000 kg ( See table overleaf )

19

20

21

22

23

24

25

26

27

28

29

30

31

32

33

34

35

170 160 150

140 130

120 110

100

90

,

%MAC PITCH TRIM

3'0

20

INDEX

1 3

/

40

1

50

1 ./ """'-UP-

60

1-

80

7'0

'

DOWN-.

. /

g'o

100

1

1 Weight