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 ]