SHEET NO Dec18 61 Updated - List Of Effective Pages / Revision Highlights

Transcription

1 PAGE NO A Dec-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 61 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD" ISSUE DATE REV NO ATION FOR PAGES SHEET NO ontents Apr General Info Apr A1,A2 ontact Address. PAGE DESRIPTION Apr B1,B2 Passenger & baggage weights/ crew weights Apr DOW and DOI specifications / Special Information Apr Load&Trim Sheet Information Dec18 61 Updated - List Of Effective Pages / Revision Highlights Jul ,3 Basic and MA formula/ Stabilizer Trim Settings/A/ Registration., Wt Details Aug A/ Basic & Dry Operating Weight & Table 10.02A 26Dec18 61 Updated - Pantry odes Aug Aircraft Weight Limitations Jul Take-off G Limits for Loadsheet Purpose 10.04A 28Apr Zero Fuel G Limits for Loadsheet Purpose 10.04B 16Jul Landing G Limits for Loadsheet Purpose Apr Effect of Fuel / APU Taxi Fuel Weight 10.05A 03Aug Seperate Fuel Tank Table Jun , 7 rew seats loc. & distrib Jul Galley & Pantry Apr Pass. abin 10.08A 24May Pass. abin 10.08B 16Jul Pass. abin Jul lass / abin Sections Aug Seating Layout ode Letters Mar16 50 Deleted 11 Seat Plan Layout JLM,JLN 10.11A 26Mar15 45 Deleted 11 Seat Plan Layout JLO,JLP 10.11B 18Mar16 50 Deleted 11 Seat Plan Layout 10.11D 16Jul14 39 Deleted 11 Seat Plan Layout JUA, JUB, JUD 10.11E 26Jan Seat Plan Layout JLS,JLT,JLU,JLV,JLY,JLZ 10.11F 18Mar Seat Plan Layout Jul Details For ompartment Trim Jul Details For Bay/Section Trim Jul ,D1, D2,D3 Ballast, Ideal Trim Line, ULD / Special Load AHM560 Data for heck-in & Loadcontrol Page No:10.00

2 A Dec-2018 REVISION HIGHLIGHTS REV NO REVISION DESRIPTION 61 Pantry standart weight /ındex table for all Anadolu Jet Flights has been added and T-JLM, T- JLN, T-JLO, T-JLP, T-JUB, T-JUD left THY fleet. 60 T-JLY BW/BI changed due to weighing, 59 T-JLZ BW/BI changed due to weighing 58 T-JLU,-JLV BW/BI changed due to weighing 57 LM Limits are changed. 56 T-JUA left THY fleet. 56 T-JLR BW/BI changed due to weighing. 55 T-JLS BW/BI changed due to weighing 54 T-JLT BW/BI changed due to weighing 53 T-JLP BW/BI changed due to weighing. 52 T-JUB BW/BI changed due to weighing 51 T-JUD BW/BI changed due to weighing 50 T-JLM seatplan modified by addition of seat row T-JUA BW/BI changed due to weighing. 48 T-JLR BW/BI changed due to weighing. 47 T-JLV,-JLY and -JLZ BW/BI changed due to weighing. Domestic Flight pantry weight is updated. 46 T-JLU BW/BI changed due to weighing 45 T-JLT BW/BI changed due to weighing 45 T-JLN seatplan modified by addition of seat row T-JLO BW/BI changed due to weighing 43 T-JLS BW/BI changed due to weighing 42 JLU seatplan modified by addition of seat row JLO,JLP,JLY,JLZ seatplan modified by addition of seat row T-JLS,JLT seatplan modified by addition of seat row T-JUB cabin layout is converted from 132Y full E/ to 132 seat dual class passenger configuration 38 T-JLV seatplan modified by addition of seat row T-JUD cabin layout converted from 132Y full E/ to 132 seat dual class passenger configuration 36 T-JLR cabin layout converted from 138 to 132 seat dual class passenger configuration 36 T-JLM,JLN BW/BI changed due to weighing. 35 T-JUA cabin layout converted from 132Y full E/ to 132 seat dual class passenger configuration 34 T-JLO BW/BI changed due to weighing. 33 T-JLP BW/BI changed due to weighing. 33 LM values are updated 32 T-JUD BW/BI changed due to weighing. 31 T-JUB, JUD joined THY fleet. 30 T-JUA joined THY fleet. 30 T-JLR /Y configuration defined. 29 T-JLS,-JLT,-JLU,-JLV,-JLY,-JLZ emergency exit row changed. 28 T-JLR is modified to 138Y configuration. 27 T-JLR joined THY fleet. 26 All pantry codes are amended. New design of BW/BI page. ockpit index values updated. 25 BW/BI of JLT & JLU are changed due to modifications. 25 T-JLZ new aircraft 24 T-JLY new aircraft 23 BW/BI of JLT & JLU are changed due to modifications. 22 T-JLV new aircraft 21 T-JLU new aircraft 20 T-JLT new aircraft 20 onfiguration 8/120Y is deleted from JLS. 20 New stations are added to Pantry Standard Weight / table T-JLS entered THY fleet 19 New stations are added to Pantry Standard Weight / table Pantry codes are amended 18 abin rew Seats locations table is amended.pls refer to page T-JLR is subleased to Air Bosna.You may removed from your database. 17 T-JLR new aircraft AHM560 Data for heck-in & Loadcontrol Page No:10.00

3 A Dec OEB is not applicable anymore. Effected sections :FWD Take-off cg limits,fuel index (btw kg) 16 Passenger cabins are changed. 15 T-JLM &JLN are weighed. 14 Seat Planlayout of JLO & JLP is changed. 14 BW/BI of JLN & JLO is changed. 12 BW/BI index of JLP is updated. 11 T-JLP new aircraft 10 T-JLO new aircraft 10 Pantry codes for AUH,BAH,DXB are amended from M to N 09 T-JLM: pax cabin config changed to new 132 seat config 09 T-JLN: pax cabin config changed to new 132 seat config 08 Added stations in pantry table 07 Pantry codes are updated 06 Effect of OEB & FOT /06 05 A/ basic and DOW/DOI table is re-designed AHM560 Data for heck-in & Loadcontrol Page No:10.00

4 A Jul-2008 AIRRAFT DATA Sheet 2 abin onfiguration(s) A / TYPE arrier 2. BASI INDEX AND MA FORMULA 2.1. Examples and definitions % MA W (Station Ref.Sta.) K ( (I- K) Ref.Sta. LEMA W MA 100 W = Weight,actual [kg] Station = Station, Horizontal distance in inches or meters from station zero Ref.Station = Reference Station/axis. Selected station around which all index values are calculated K = onstant used as a plus value to avoid negative index figures = onstant used as a Denominator to convert moment values into index values I = value corresponding to respective weight MA = Length of Mean Aerodynamic hord in inches or meters LEMA = Horizontal Distance in inches or meters from the station zero to location of the leading EDGE of the MA formula Ref.Station. at =17.25 meters from zero K (onstant) = 50 (onstant) = MA Information Length of MA = meters LEMA at = meters/ from zero 2.4. Stabilizer Trim Setting MARange STABRange Nose up Nose up Linear variation between 18% MA and 41% MA 41-3 Nose down AIRRAFT DATA Sheet 3 abin onfiguration(s) A / TYPE arrier 3. AIRRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT X BASI WEIGHT X A list of weight and index values for each aircraft registration is given on next page. AHM560 Data for heck-in & Loadcontrol Page No:10.01

5 A Aug-2018 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE A/ Type MSN A/ Reg. Number of Seats Basic*(crew(0/0) Weight A T-JLR A T-JLS A T-JLT A T-JLU A T-JLV A T-JLY A T-JLZ How to calculate DOW/DOI? Basic Weight/ (Full potable water tank) + ockpit rew Total Weight/ + abin rew Total Weight/ + Pantry Weight/ = Dry Operating Weight/ If actual is different, then make necessary adjustments OKPIT REW TOTAL EFFET / ockpit rew No/Locations A/ Reg JLR (WV001) JLS,JLT,JLU,JLV, JLY,JLZ (WV005) A/ Limitations MTAXI KG MTOW KG MLDW MZFW MTAXI MTOW MLDW MZFW KG KG KG KG KG KG ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW (2 FrontSeat) OKPIT REW (2 FrontSeat +1 JumpSeat) ABIN REW TOTAL EFFET / abin rew No/Locations abin rew No/Locations WEIGHT INDEX 3 ABIN REW (1 Fwd+2 Aft) ABIN REW (2 Fwd+2 Aft) ABIN REW (2 Fwd+3 Aft) ABIN REW (2 Fwd+4 Aft) only for T-JLR,S,T,U,V,Y,Z PANTRY (ATERING) STANDARD W/I TABLE IS ON PAGE 10.02A BW/BI value in the above table already includes potable water with FULL tank (200 kg / 2.2 ).If potable water tanks are different; adjust DOW &DOI in proper ratios. %75 POTABLE WATER %50 POTABLE WATER %25 POTABLE WATER Subtract 50 KG / Subtract 0.6 Subtract 100 KG / Subract1.1 Subtract 150 KG / Subtract 1.7 *Basic Wt/ includes: ockpit & A/ Documents, Potable Water Tanks Full, Skylife Magazine, Tare empty Weight of all Trolleys & Galley Equipment (hotcup, hotjug, etc). If some items or Equipment are NOT carried make necessary adjustments. Dry Operating Weight/ does NOT include Toolkit Box and **B/ Passsenger IPAD bag. heck if they are carried in cargo compartment. It should be shown as Load in compartments (distribution) on loadsheet as Equipment in compartment. TOOLKIT BOX = 35 KG / 0,3 index **B IPAD Bag = 9.5kg / -0,1index **B Passenger IPAD Bag contains 16 IPAD ans these are used for connecting to wireless onboard IFE System on some Airfcrafts which have not Structural IFE system installed on backside of passenger seats. REW BAGGAGE (in BULK argo ompartment): For Long-haul flights and for flights that crew stays overnight at destination, additional REW BAGGAGE, standard bag weight of 10 kg per crew member is carried. This load is NOT included in above DOW/DOI, and it should be shown as 'LOAD IN OMPARTMENT - DISTRIBUTION" in Loadsheet. * Refer to DOW-DOI_Table-A file for several possible standard cockpit/cabin crew, pantry codes & potable water tanks fill ratio. DOI calculation remark: During alculations due to DS system rounding (or truncating), approximately +/- 0.3 index difference is acceptable. AHM560 Data for heck-in & Loadcontrol Page No:10.02

6 A Dec-2018 PANTRY STANDART WEIGHT/INDEX TABLE (ATERING) I- Valid for all A Aircrafts Pantry ode Galley weight TOTAL Fwd Aft WEIGHT INDEX Destination / Departure N ALL INTERNATIONAL FLIGHTS D DOMESTI FLIGHTS ONE WAY G DOMESTI FLIGHTS RETURN PANTRY REMARKS: 1- All weights are in kg. II- Valid for all Anadolu Jet Flights Pantry ode Galley weight TOTAL Fwd Aft WEIGHT INDEX Destination / Departure U ,4 DOMESTI FLIGHTS ONE WAY V ,7 DOMESTI FLIGHTS RETURN PANTRY W ,0 ALL INTERNATIONAL FLIGHTS AHM560 Data for heck-in & Loadcontrol Page No:10.02A

7 A Aug-2017 AIRRAFT DATA Sheet 4 abin onfiguration(s) A / TYPE arrier 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: Aircraft Design Takeoff Wet Dry Landing Design Take-off Design MSN Ramp/Taxi Zero Fuel Reg. T-JLR kg N/A kg kg kg T-JLS kg N/A kg kg kg T-JLT kg N/A kg kg kg T-JLU kg N/A kg kg kg T-JLV kg N/A kg kg kg T-JLY kg N/A kg kg kg T-JLZ kg N/A kg kg kg LM (Last Minute hanges) Information: Last Minute hanges (LM) to the mass and balance sheet are only permitted when the changes of the load (either minus or plus) in last minutes are within the following limits. A : 500 kg Total Weight (Passengers,argo,Mail or any combination) These changes must be shown as pax, cargo, mail, baggage etc. in the Load & Trim Sheet. The effect of LM in aircraft G must be checked. Aircraft G after LM must not exceed forward and aft operational G Limits. In Addition to LM Weight, LM influence should be shown on Load & Trim Sheet in a suitable space under LM title preferably next to LM weight. AHM560 Data for heck-in & Loadcontrol Page No:10.03

8 A Jul-2014 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier 4.2. G - Limits for Loadsheet Purpose TAKE-OFF G - Limits for Loadsheet Purpose Special condition if applicable Specify applicability T-JLR TAKE-OFF FWD Special condition if applicable Specify applicability T-JLS,-JLT,-JLU,-JLV, T-JLY,-JLZ TAKE-OFF FWD Special condition if applicable TAKE-OFF AFT Weight(kg) Specify applicability Weight(kg) Value Value T-JLR Special condition if applicable TAKE-OFF AFT Weight(kg) Specify applicability Weight(kg) Value Value T-JLS,-JLT,-JLU,-JLV, T-JLY,-JLZ AHM560 Data for heck-in & Loadcontrol Page No:10.04

9 A Apr-2014 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier 4.2. G - Limits for Loadsheet Purpose ZERO FUEL G - Limits for Loadsheet Purpose Special condition if applicable Specify applicability T-JLR T-JLS,-JLT,-JLU,-JLV, T-JLY,-JLZ ZERO FUEL FWD ZERO FUEL FWD Special condition if applicable ZERO FUEL AFT Weight(kg) Specify applicability Weight(kg) Value Value T-JLR ZERO FUEL AFT Specify applicability Weight(kg) Specify applicability Weight(kg) T-JLS,-JLT,-JLU,-JLV, T-JLY,-JLZ AHM560 Data for heck-in & Loadcontrol Page No:10.04A

10 A Jul-2014 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier A TK 4.2. G - Limits for Loadsheet Purpose Landing G - Limits for Loadsheet Purpose Special condition if applicable Specify applicability T-JLR LANDING FWD Special condition if applicable LANDING AFT Weight(kg) Specify applicability Weight(kg) Value Value T-JLR Specify applicability T-JLS,-JLT,-JLU,-JLV, T-JLY,-JLZ TAKE-OFF FWD TAKE-OFF AFT Weight(kg) Specify applicability Weight(kg) Value Value T-JLS,-JLT,-JLU,-JLV, T-JLY,-JLZ AHM560 Data for heck-in & Loadcontrol Page No:10.04B

11 A Aug-2018 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier 5. EFFET OF FUEL Fuel Wt. (kg) Fuel Density (Kg/lt) FULL (index) FULL (kg) REMARK: FUEL TANKS' TOTAL VOLUMETRI APAITY IS LT 5.1 APU / TAXI FUEL WEIGHT Due to local taxiing distances and local needs for APU running, total taxi Fuel may be different in your local station. It may be calculated by using the following fuel flow figures; Taxi Fuel Flow = 10 kg/minute APU Fuel Flow = 130 kg/hour AHM560 Data for heck-in & Loadcontrol Page No:10.05

12 A Aug-2018 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier 5.2 Separate Fuel Tank Table Inner Tank Left or Right Wing Outer Tank Left or Right Wing enter Tank Weight Weight Weight Fuel Density 0.8 lt/kg AHM560 Data for heck-in & Loadcontrol Page No:10.05

13 A Jun-2012 AIRRAFT DATA Sheet 7 abin onfiguration(s) A / TYPE arrier 6. REW 6.1. Number of cockpit crew seats and average location Maximum number of Length of arm from reference station influence cockpit seats +/- meter(s) +/- per 1 kg 4* *Max no of seats: 4 seats for only JLR 6.2. Number of cabin crew seats and location ABIN rew seats Max. Length of arm from reference station influence locations No. of seats +/- meter(s) +/- per 1 kg FWD AFT rew Distribution / rew ode rew ode ockpit rew Total No abin rew Total No Number of abin rews at Location FWD 2/ / / / / / AFT Location of rew Baggage BULK ARGO OMPT. 5 AHM560 Data for heck-in & Loadcontrol Page No:10.06

14 A Jul-2008 AIRRAFT DATA Sheet 8 abin onfiguration(s) A / TYPE arrier 7. GALLEY AND PANTRY 7.1. Galleys Galley locations Length of arm from reference station influence +/- meter(s) +/- per 1 kg G1 FWD GALLEY G5 AFT GALLEY Pantry Weight / Pantry ode Pantry Weight / Pantry ode table is given on page 10.02A 7.3 SEATING ONDITIONS LOADSHEET OUTPUT State below how the seating conditions should be shown in the respective loadsheet box. Give example. Enclose a passenger distribution table if used. AHM560 Data for heck-in & Loadcontrol Page No:10.07

15 A May-2012 AIRRAFT DATA Sheet 9 abin onfiguration(s) A / TYPE arrier T-JLR A TK 8. PASSENGER ABIN 8.1 Passenger Seats Passenger Seats (T-JLR) LASS ODES lass 1: lass 2 : Y lass 3 : Name of cabin section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section Name of cabin section NUMBER OF SEATS lass 1 lass 2 lass 3 ABIN ONFIGURATION 132Y ABIN ONFIGURATION 8 / 120Y OA OA OB OB O O Total per Total per 132 class class ABIN ONFIGURATION 16 / 108Y ABIN ONFIGURATION 28 / 90Y OA OA OB OB O O Total per Total per class class Total per cabin section Passenger Seats (T-JLS,-JLT,-JLU,-JLV,-JLY,-JLZ) Name of cabin section LASS ODES lass 1 : lass 2 : Y lass 3 : NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section Name of cabin section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section ABIN ONFIGURATION 132Y ABIN ONFIGURATION 12 / 114Y OA OA OB OB O O Total per Total per 132 class class ABIN ONFIGURATION 16 / 108Y ABIN ONFIGURATION 20 / 102Y OA OA OB OB O O Total per Total per class class ABIN ONFIGURATION 24 / 96Y ABIN ONFIGURATION 28 / 90Y OA OA OB OB O O Total per Total per class class AHM560 Data for heck-in & Loadcontrol Page No:10.08

16 A Jul-2014 AIRRAFT DATA Sheet 9 abin onfiguration(s) A / TYPE arrier 8.2 lass/abin Sections T- JLR lass/abin Section Length of arm from reference station influence +/- meter(s) +/- per 1 kg OA OB O T-JLS,-JLT,-JLU,-JLV,-JLY,-JLZ lass/abin Section Length of arm from reference station influence +/- meter(s) +/- per 1 kg OA OB O AHM560 Data for heck-in & Loadcontrol Page No:10.09

17 8.3 Seating Layout A Aug-2011 AIRRAFT DATA Sheet 10 A / TYPE arrier A TK Show the passenger seating layout for the configurations given in the box at the top by inserting the seat row numbers and letters in the following table. For special seats use the description codes listed below : B = Bassinet position = rew seat E = Emergency exit G = Groups H = Incapacitated passenger I = Infant preference rows/seats J = Rear facing seats K = Near galley L = Leg space seat M = Wheel chair N = No Smoking O = Over wing seat P = Stretcher location Q = Quiet zone S = Smoking T = Near toilet U = Unaccompanied minor V = Seat left vacant/offered last W = No Movie X = No facility seat (e.g. no distinction between smoking and non-smoking) Y = Not fitted Z = Buffer zone. = Aisle Alfa/haracters - A, D, F, R, Blank not used Note : Seat designators to be in accordance with Recommended Practice AHM560 Data for heck-in & Loadcontrol Page No:10.10

18 A Mar-2016 AIRRAFT DATA Sheet 11 abin onfiguration(s) A / TYPE arrier T-JLR A TK Seatplan Layout / Facilities and Row Influence SETION A B ROW NO Influence per Seat- Row per1kg Rows from-to: ABIN ONFIGURATION 132Y A B D E F Rows from-to A B D E F ABIN ONFIGURATION 8 / 120Y NI NB N N NBI N 1 NBI V N N V NBI N NI NM NM N NI 2 NI V NM NM V NI NE NE NE NE NE NE 3-8 N NI NM NM N NI N NI NM NM N NI 9 NE NE NE NE NE NE N NI NM NM N NI ABIN ONFIGURATION 16 / 108Y ABIN ONFIGURATION 28 / 90Y NBI V N N V NBI 1 NBI V N N V NBI NI V NM NM V NI 2-7 NI V NM NM V NI N NI NM NM N NI 8 N NI NM NM N NI NE NE NE NE NE NE 9 NE NE NE NE NE NE N NI NM NM N NI N NI NM NM N NI MOVEABLE ERTAIN LASS DIVIDER is shown as : AHM560 Data for heck-in & Loadcontrol Page No:10.11

19 A Jan-2015 AIRRAFT DATA Sheet 11 abin onfiguration(s) A / TYPE arrier T-JLS,-JLT,-JLU,-JLV,-JLY,-JLZ A TK Seatplan Layout / Facilities and Row Influence SETION A B ROW NO Influence per Seat- Row per1kg Rows from-to: ABIN ONFIGURATION 132Y A B D E F Rows from-to: A B D E F ABIN ONFIGURATION 12 / 114Y NI NB N. N NB NI 1 NBI V N. N V NBI NI N N. N N NI 2-3 NI V N. N V NI NE NE NE. NE NE NE 4-8 NI N N. N N NI NI N N. N N NI 9 NE NE NE. NE NE NE NI N N. N N NI NI N N. N N NI NI N N. N N NI ABIN ONFIGURATION 16 / 108Y ABIN ONFIGURATION 20 / 102Y NBI V N. N V NBI 1 NBI V N. N V NBI NI V N. N V NI 2-5 NI V N. N V NI NI N N. N N NI 6-8 NI N N. N N NI NE NE NE. NE NE NE 9 NE NE NE. NE NE NE NI N N. N N NI NI N N. N N NI NI N N. N N NI NI N N. N N NI ABIN ONFIGURATION 24 / 96Y ABIN ONFIGURATION 28 / 90Y NBI V N. N V NBI 1 NBI V N. N V NBI NI V N. N V NI 2-7 NI V N. N V NI NI N N. N N NI 8 NI N N. N N NI NE NE NE. NE NE NE 9 NE NE NE. NE NE NE NI N N. N N NI NI N N. N N NI NI N N. N N NI NI N N. N N NI MOVEABLE ERTAIN LASS DIVIDER is shown as : AHM560 Data for heck-in & Loadcontrol Page No:10.11E

20 A Jul-2008 AIRRAFT DATA Sheet 12 abin onfiguration(s) A / TYPE arrier 9. DETAILS FOR OMPARTMENT TRIM NUMBER OMPARTMENT MAXIMUM APAITY influence GROSS WEIGHT VOLUME* DESRIPTION (kg) (M 3 +/- per 1 kg ) 1 FWD ompartment Bulk Loading AFT ompartment Bulk Loading Rear (Bulk) argo ompartment REMARKS:ULD (ontainer & Pallet) loading is NOT possible. argo Loading System (LS) is NOT installed. 9.1 ombined Load Limitations: N/A AHM560 Data for heck-in & Loadcontrol Page No:10.13

21 A Jul-2008 AIRRAFT DATA Sheet 13 abin onfiguration(s) A / TYPE arrier 10. DETAILS FOR BAY / SETION TRIM MAX. APAITY influence BAY / SETION GROSS WEIGHT VOLUME (kg) (M 3 ) +/- per 1 kg 11 Bulk Loading Bulk Loading Bulk Loading Bulk Loading Rear Bulk argo Hold Section REMARKS:ULD (ontainer & Pallet) loading is NOT possible. argo Loading System (LS) is NOT installed. AHM560 Data for heck-in & Loadcontrol Page No:10.13

22 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS: BALLAST IS NOT REQUIRED A Jul-2008 AIRRAFT DATA Sheet 14 A / TYPE arrier A TK AIRRAFT DATA D Sheet 1 A / TYPE arrier A TK 1. G LIMITS 1.1. Planning Limits G-Limits for load planning purpose shall be agreed between carrier and system operator. 1.2 Ideal Trim Line at ZFW for Fuel Saving Purposes The IDEAL TRIM LINE shown in the balance graph below is a load planning limit only. In the interest of fuel economy the load in the compartments shall whenever possible, be distributed in such a way that the LIZFW is aft of this line. The respective breakpoints (weight / index) ofthe ideal trim line shall be entered in the table below. WEIGHT INDEX VALUE UNIT LOAD DEVIES DETAILS Type ode Tare weight Maximum apacity Gross VOLUME Weight (M 3 ) AIRRAFT DATA D Sheet 2 A / TYPE arrier A TK Remarks 2.1 UNIT LOAD DEVIES NOTES In ULD compartments (compartments other than bulk ompartment) cargo and bags should be loaded only in ULD. Do not load anything at the empty spaces around ULDs and between ULDs. D AIRRAFT DATA Sheet 3 A / TYPE arrier A TK 3. SPEIAL LOAD Turkish Airlines & IATA regulations apply. When necessary contact Turkish Airlines Station Manager. AHM560 Data for heck-in & Loadcontrol Page No:10.14