ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYA Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMCMax allowed =

RTOW =

LMCPREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYB Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYC Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYD Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYE Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYF Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYG Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYH Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYI Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

ss

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYJ Rev0

CA

RG

O C

om

par

t. max.

741 kgmax.

2884 kgmax.

3382 kgmax.

763 kg

max.

48paxmax.

39pax

max.

16paxmax.

48pax

ZO

NE

S

PA

X C

AB

IN C

om

pt.

SE

RV

ICE

INDEX

100 KG

< - + >

35000 + 45

INDEX FORMULA :

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[D]

[D]

[C]

[E]

[ ı ]

[ ıı ]

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

[C]

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

500 kg

[A] Fwd Takeoff and Zero Fuel Check (No Auxiliary Fuel Loaded) [B] Fwd Zero Fuel Check (Auxiliary Fuel Loaded)

[C] Aft Takeoff Check

[D] Aft Zero Fuel Check

[E] Aft Takeoff Check (Auxiliary Fuel Loaded)

AUX Tank

max2923(d=0.8)

Wing+Center Tank FUEL ..............kg.

TOF(Wing+Center+Aux)

d=0.80 d=0.81 d=0.82 d=0.83

0A - FWD 4 Rows

max: 16 PAX

0B - MID 8 Rows

max: 48 PAX

0D - AFT 7 Rows

max: 39 PAX

LOAD and TRIM SHEET B737-900W_ER 1.Aug.2017 151 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 8 Rows

max: 48 PAX

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

L A S T M I N U T E C H A N G E S

WEIGHT INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

WEIGHT INDEX

3000 0.4 3500 0.6 4000 1.0 4500 1.5 5000 2.2 5500 3.0 6000 3.9 6500 5.1 7000 6.5 7500 8.1 8000 9.1 8500 8.4 9000 7.7 9500 6.9

10000 6.1 10500 5.3 11000 4.5 11500 3.8 12000 3.0 12500 2.3 13000 1.5 13500 0.8 14000 0.1 14500 -0.6 15000 -1.4 15500 -2.0 16000 -2.8 16500 -3.5 17000 -4.1 17500 -4.9 18000 -5.6 18500 -6.4 19000 -7.1 19500 -8.0 20000 -8.7 20500 -9.7 20897 -10.421079 -10.521339 -10.621560 -10.7

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYL Rev0

max.

2884 max.

4358 max.

667 kg

60max

33max

max.

675 kg

CA

RG

O C

om

par

t.

ZO

NE

S

PA

X C

AB

IN C

om

pt.

16max

60max

SE

RV

ICE

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[C]

[D]

[C]

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

INDEX

100 KG

< - + >

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

[D] Do not operate in this area during takeoff

[A] Fwd Takeoff and Zero Fuel Check [B] Aft Takeoff Check [C] Aft Zero Fuel Check

d=0.80

d=0.81

d=0.82

d=0.83

0A - FWD 4 Rows-max.16pax

0B - MID 10 Rows-max.60pax

0D - AFT 6 Rows-max33pax

LOAD and TRIM SHEET B737-900W ER 2.Aug.2017 169 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 10 Rows- max.60pax

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

WEIGHT

L A S T M I N U T E C H A N G E S

INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

FUEL INDEX

35000 + 45

W x (Harm-658.3)

INDEX FORMULA :

[ ı ]

[ ıı ]

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYM Rev0

max.

2884 max.

4358 max.

667 kg

60max

33max

max.

675 kg

CA

RG

O C

om

par

t.

ZO

NE

S

PA

X C

AB

IN C

om

pt.

16max

60max

SE

RV

ICE

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[C]

[D]

[C]

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

INDEX

100 KG

< - + >

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

[D] Do not operate in this area during takeoff

[A] Fwd Takeoff and Zero Fuel Check [B] Aft Takeoff Check [C] Aft Zero Fuel Check

d=0.80

d=0.81

d=0.82

d=0.83

0A - FWD 4 Rows-max.16pax

0B - MID 10 Rows-max.60pax

0D - AFT 6 Rows-max33pax

LOAD and TRIM SHEET B737-900W ER 2.Aug.2017 169 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 10 Rows- max.60pax

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

WEIGHT

L A S T M I N U T E C H A N G E S

INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

FUEL INDEX

35000 + 45

W x (Harm-658.3)

INDEX FORMULA :

[ ı ]

[ ıı ]

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYN Rev0

max.

2884 max.

4358 max.

667 kg

60max

33max

max.

675 kg

CA

RG

O C

om

par

t.

ZO

NE

S

PA

X C

AB

IN C

om

pt.

16max

60max

SE

RV

ICE

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[C]

[D]

[C]

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

INDEX

100 KG

< - + >

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

[D] Do not operate in this area during takeoff

[A] Fwd Takeoff and Zero Fuel Check [B] Aft Takeoff Check [C] Aft Zero Fuel Check

d=0.80

d=0.81

d=0.82

d=0.83

0A - FWD 4 Rows-max.16pax

0B - MID 10 Rows-max.60pax

0D - AFT 6 Rows-max33pax

LOAD and TRIM SHEET B737-900W ER 2.Aug.2017 169 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 10 Rows- max.60pax

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

WEIGHT

L A S T M I N U T E C H A N G E S

INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

FUEL INDEX

35000 + 45

W x (Harm-658.3)

INDEX FORMULA :

[ ı ]

[ ıı ]

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYO Rev0

max.

2884 max.

4358 max.

667 kg

60max

33max

max.

675 kg

CA

RG

O C

om

par

t.

ZO

NE

S

PA

X C

AB

IN C

om

pt.

16max

60max

SE

RV

ICE

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[C]

[D]

[C]

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

INDEX

100 KG

< - + >

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

[D] Do not operate in this area during takeoff

[A] Fwd Takeoff and Zero Fuel Check [B] Aft Takeoff Check [C] Aft Zero Fuel Check

d=0.80

d=0.81

d=0.82

d=0.83

0A - FWD 4 Rows-max.16pax

0B - MID 10 Rows-max.60pax

0D - AFT 6 Rows-max33pax

LOAD and TRIM SHEET B737-900W ER 2.Aug.2017 169 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 10 Rows- max.60pax

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMC Max allowed =

RTOW =

LMC PREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

WEIGHT

L A S T M I N U T E C H A N G E S

INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

FUEL INDEX

35000 + 45

W x (Harm-658.3)

INDEX FORMULA :

[ ı ]

[ ıı ]

BASIC INDEX :

F KG

G KG

DRY OP. INDEX :

0A PAX

0B PAX

0C PAX

0D PAX

1 KG

2 KG

3 KG

4 KG

This Load & Trim sheet is valid for; TC-JYP Rev0

max.

2884 max.

4358 max.

667 kg

60max

33max

max.

675 kg

CA

RG

O C

om

par

t.

ZO

NE

S

PA

X C

AB

IN C

om

pt.

16max

60max

SE

RV

ICE

40

45

50

55

60

65

70

75

80

85

90

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95

[C]

[D]

[C]

[ I ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 17% MAC [ II ] For Takeoff aft of this limit, AFM-DFI Alternate Fwd C.G. limit may be used with "ALTFWD C.G."input of 20% MAC

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32

INDEX

100 KG

< - + >

AIR

CR

AF

T W

EIG

HT

(to

ns

)

INDEX

AIRCRAFT % CG (% RC)

MTOW= 85139 KG

MLW=71350 KG

MZFW=67721 KG

[A]

[B]

MTaxi= 85366 KG

ZONE F ZONE G

100 KG

[D] Do not operate in this area during takeoff

[A] Fwd Takeoff and Zero Fuel Check [B] Aft Takeoff Check [C] Aft Zero Fuel Check

d=0.80

d=0.81

d=0.82

d=0.83

0A - FWD 4 Rows-max.16pax

0B - MID 10 Rows-max.60pax

0D - AFT 6 Rows-max33pax

LOAD and TRIM SHEET B737-900W ER2.Aug.2017 169 SEAT

5 PAX

10 PAX

200 kg

200 kg

200 kg

200 kg

10 PAX

5 PAX

0C - MID 10 Rows- max.60pax

Priority Address(es)

Originator Recharge Date/Time Initials

/ L D MFlight A/C Registration Version Crew Date:

BASIC WEIGHT ZERO FUEL LANDING

COCKPIT CREW BAG.

CABIN CREW BAG. TRIP

PANTRY FUEL1 2 3

DRY OPER. WEIGHT

OPERATING

WEIGHT

NO OF PAX CAB. DISTRIBUTION WEIGHT

M F CH INF BAG. TOTAL 1 2 3 4 0 cabin

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

Tr

B

C CY/ PAD/

M

EIC

T 1/ 2/ 3/ 4/

TOTAL:

SI RWY

OAT

Wind C.

LMC NOTES:

=

Max = DEST Specification

LMCMax allowed =

RTOW =

LMCPREPARED BY

APPROVED BY

Max allowed CHECKED BYTOTAL PASSENGERS

RLDW

WEIGHT

L A S T M I N U T E C H A N G E S

INDEX

ALLOWED WEIGHT FOR TAKE-OFF (Lowest of 1,2,3)

=

+

TAKE-OFF

ALLOWED TRAFFIC LOAD =

Dest

ALL WEIGHTS IN KILOS

TAKE-OFF FUEL

MAX.WEIGHT FOR

=

+

=++++

OPERATING WEIGHT

REMARKS

PAX PAD

C CY Y

=

ALLOWED TRAFFIC LOAD

UNDERLOAD BEFORE LMC =

LMC TOTAL +/-

SEATING BALANCE

Passenger Aircraft

Cl cpt

Check LMC Total with Underload

+

++

+

TAKE-OFF WEIGHT

ZERO FUEL WEIGHT

Take-Off Fuel

Trip Fuel

LANDING WEIGHT

TOTAL TRAFFIC LOAD

Dry-Operating Weight

±±

±±

±±

TAKE-OFFFUEL

TURKISH AIRLINES

FUEL INDEX

35000 + 45

W x (Harm-658.3)

INDEX FORMULA :

[ ı ]

[ ıı ]