A F 8-Oct-2018 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 16

Transcription

1 A F 8-Oct-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 16 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_Pages_ pdf" ATION PAGE ISSUE SHEET REV NO FOR PAGE DESRIPTION NO DATE NO PAGES Title Page ontents Jan General Info Jan A1,A2 ontact Address Jan B1,B2 Passenger & baggage weights/ crew weights Jan DOW and DOI specifications / Special Information Jan Load&Trim Sheet Information Oct18 16 Updated - List Of Eff. Pages Mar ,3 Basic and MA formula/ Stabilizer Trim Settings/A/ Registration., Wt Details Oct18 16 Updated - A/ Basic & Dry Operating & Table Sep Aircraft Limitations Apr G Limits for Loadsheet Purpose 16.04A 25Jan G Limits for Loadsheet Purpose 16.04B 10Sep G Limits for Loadsheet Purpose Oct G Limits for Loadsheet Purpose Apr Effect of Fuel - Fuel Density 16.05A 10Sep Effect of Fuel - Fuel Density (JDO) Mar ockpit,abin rew Seats,rew Distr Mar Galley &odes Mar ,10 Passenger Seats Average Station (abin Areas) Mar Seating Layout ode Letters Mar Seat Plan Layout, Facilities & Row index Influence Oct18 16 Updated 12 Details For ompartment Trim Sep Details For Bay/Section Trim 16.12A 10Sep Details For Bay/Section Trim 16.12B 31Mar Details For Bay/Section Trim Mar Details For Bay/Section Trim 16.12D 14May Details For Bay/Section Trim 14,D1 BALLAST,G LIMITS / Ideal Trim Line, Unit Load Dec D2,D3 Devices / Special Load Mar Load&Trim Sheet A F (argo) front side 06.14A 31Mar Load&Trim Sheet A F (argo) reverse side Page No:16.00

2 REV NO A F 8-Oct-2018 REVISIONS Fuel index tabiosunu uçakların kapasitelerine göre ayır. REVISION DESRIPTION 16 JOO has been weighed. 15 New Aircraft (T-JOO) entered THY fleet, JDO has been weighed. 14 T-JDS and T-JOU have been weighed. Fuel tables added. 13 T-JI has been weighed and Ideal Trim Line added. 12 Modifications applied to Aircraft (T-JDS,T-JI) 11 New Aircraft (T-JOZ) entered THY fleet 10 New Aircraft (T-JOY) entered THY fleet, JDO, JDR, JOU BW/BI changed due to Eng.Order. 09 New Aircraft (T-JOV) entered THY fleet 08 T-JDP has been weighed 07 New Aircraft (T-JOU) entered THY fleet 06 T-JDO has been weighed 05 New Aircraft (T-JI) entered THY fleet 04 New Aircraft (T-JDS) entered THY fleet 03 New Aircraft (T-JDR) entered THY fleet 02 New Aircraft (T-JDP) entered THY fleet, pantry information amended 01 JDO ertified Limits Variant-01 added. 01 JDO Fuel Effect (cont.0.8) added. Page No:16.00

3 A F 31-Mar-2011 Sheet 2 abin onfiguration(s) A / TYPE arrier ALL A F TK 2. BASI INDEX AND MA FORMULA 2.1. Examples and definitions W (Station Ref.Sta.) K % MA W Station Ref.Station K I MA LEMA ( (I - K) Ref.Sta. LEMA W MA 100 =, actual [kg] = Station, Horizontal distance in inches or meters from station zero = Reference Station/axis. Selected station around which all index values are calculated = onstant used as a plus value to avoid negative index figures = onstant used as a Denominator to convert moment values into index values = value corresponding to respective weight = Length of Mean Aerodynamic hord in inches or meters = Horizontal Distance in inches or meters from the station zero to location of the leading EDGE of the MA formula Ref.Station. at = meters from zero K (onstant) = 100 (onstant) = MA Information Length of MA = 7.27 meters LEMA at = meters/ from zero 2.4. Stabilizer Trim Setting MA Range STAB Range 15 9 Up Up Linear variation between 15% MA and 38% MA Up Sheet 3 abin onfiguration(s) A / TYPE arrier ALL A TK 3. AIRRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT BASI WEIGHT X X A list of weight and index values for each aircraft registration is given on next page. Page No:16.01

4 A F 08-Oct-2018 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE A/ Type MSN A/ Reg. Basic*(rew 0/0) How to calculate DOW/DOI? Basic / (Full potable water) A F 1004 T-JDO A F 1092 T-JDP ockpit rew Total / A F 1344 T-JDR abin rew Total / A F 1418 T-JDS A F 1442 T-JI Pantry / A F 1164 T-JOO = A F 1550 T-JOU Dry Operating / A F 1722 T-JOV If actual is different, then make necessary A F 1750 T-JOY adjustments A F 1768 T-JOZ A/ Reg & WV TYPE A/ Limitations (Kg) ALL MTAXI WEIGHT MTOW VARIANT 00 MLDW (RANGE MODE) MZFW Min A/ G Design (Kg) Minimum for flight and landing < T-JDO,-JDP,-JDR,-JDS,- JI,-JOV,-JOY,-JOZ T-JOO T-JOU ALL WEIGHT VARIANT 01 (PAYLOAD MODE) WEIGHT VARIANT 02 (DYNAMI MODE) MTAXI MTOW MLDW MZFW MTAXI MTOW MLDW MZFW Linear variation OKPIT REW TOTAL EFFET / ockpit rew No / Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW OKPIT REW OKPIT REW LOADMASTER TOTAL EFFET / Loadmaster No / Locations WEIGHT INDEX 1 (Loadmaster or Technician) (Loadmaster or Technician) (Loadmaster or Technician) (Loadmaster or Technician) PANTRY EFFET / Pantry ode / lass, onfig, App. WEIGHT INDEX N (International Freighter Flight / Short-Mid Range) Galley@13.403m.(H.Arm) A (ER Freighter Flight / Long Range) INFLUENE OF POTABLE WATER ON DOW/DOI BW/BI value in the above table already includes potable water with FULL tank (100 kg / -0.4 ). If potable water tanks are different, adjust DOW &DOI in proper ratios. %75 POTABLE WATER %50 POTABLE WATER %25 POTABLE WATER Subtract 25 KG / Add 0.1 Subtract 50 KG / Add 0.2 Subtract 75 KG / Add 0.3 *Basic Wt/ includes: ockpit & A/ Documents, Potable Water Tanks Full, Skylife Magazine, Tare empty of all Trolleys & Galley Equipments (hotcup, hotjug, etc). If some items or Equipments are NOT carried make necessary adjustments Dry Operating / does NOT include Toolkit Box, Technician KIT, Loadmaster KIT. heck if they are carried, make necessary adjustments. Toolkit box and Technician KIT are loaded in argo comp5. Loadmaster KIT carried in pax.compt.. TOOLKIT BOX = 58,3kg / 0,4iu Technician Kit = 35kg / 0,2 iu Loadmaster KIT = 10kg / -0.1iu ONTAINERS AND PALLETS (ULD-Unit Load Devices) : - Tare weight of ontainers and Pallets (ULD) should NOT be included in Dry Operating weight/.tare weight of ULD should be shown within GROSS load in position (added to net cargo/bag weight in ULD position). GROSS load (sum of Net cargo/bag weight + pallet/container tare weight) should be shown in "LOAD IN OMPARTMENTS"in "DISTRIBUTION" column of LOADSHEET. REW BAGGAGE (in BULK argo ompartment) : For Longhoul flights and for flights that crew stays overnight at destination, additional REW BAGGAGE, standard bag weight of 15 kg per crew member is carried. This load is NOT included in above DOW/DOI, and it should be calculated in consideration of rew Baggage loading position. Spare Wheel&Tire Dry Operating / does not include nose/main gear Nose Gear(NG) (Qty1) in ompt spare wheel&tire.heck if they are carried in cargo compartment. It Main Gear(MG) (Qty1) in ompt should be shown as Load in compartments (distribution) on TOTAL in Bulk ompt.5 : loadsheet as Equipment in compartment Page No:16.02

5 A F 10-Sep-2018 Sheet 4 abin onfiguration(s) A / TYPE arrier ALL A F TK 4. LIMITATIONS 4.1. Aircraft Limitations Maximum weights for : Aircraft Design Takeoff Wet * Dry Landing Design Take-off Design MSN Ramp/Taxi Zero Fuel Reg. WEIGHT VARIANT 00: T-JDO kg N/A kg kg kg T-JDP kg N/A kg kg kg T-JDR kg N/A kg kg kg T-JDS kg N/A kg kg kg T-JI kg N/A kg kg kg T-JOV kg N/A kg kg kg T-JOY kg N/A kg kg kg T-JOZ kg N/A kg kg kg WEIGHT VARIANT 01: T-JDO kg N/A kg kg kg T-JDP kg N/A kg kg kg T-JDR kg N/A kg kg kg T-JDS kg N/A kg kg kg T-JI kg N/A kg kg kg T-JOV kg N/A kg kg kg T-JOY kg N/A kg kg kg T-JOZ kg N/A kg kg kg WEIGHT VARIANT 02: Dynamic Payload T-JOO kg N/A kg Function of kg ATOW** T-JOU kg N/A kg kg ** The MZFW is a function of the Actual Take-Off (ATOW) : For ATOW kg, MZFW = kg For ATOW > kg, MZFW (kg) = (ATOW (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. 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, LM influence should be shown on Load & Trim Sheet in a suitable space under LM title preferably next to LM weight. Page No:16.03

6 A F 27-Aug-2013 Sheet 5 abin onfiguration(s) A / TYPE arrier T-JDO A F TK 4.2. G - Limits for Loadsheet Purpose T-JDO T-JDO Variant01 TAKE-OFF FWD T-JDO T-JDO Variant01 TAKE-OFF AFT T-JDO T-JDO Variant01 ZERO FUEL FWD T-JDO T-JDO Variant01 ZERO FUEL AFT Page No:16.04

7 A F 25-Jan-2017 Sheet 5 abin onfiguration(s) A / TYPE arrier T-JDP,-JDR,-JDS,-JI,-JOV,-JOY,-JOZ A F TK 4.2. G - Limits for Loadsheet Purpose Variant0 TAKE-OFF FWD Variant0 TAKE-OFF AFT Variant Variant Variant0 Variant01 ZERO FUEL FWD Variant0 Variant01 ZERO FUEL AFT Page No:16.04A

8 A F 10-Sep-2018 Sheet 5 abin onfiguration(s) A / TYPE arrier T-JOO,T-JOU A F TK 4.2. G - Limits for Loadsheet Purpose Variant02 TAKE-OFF FWD Variant02 ZERO FUEL FWD Variant02 TAKE-OFF AFT Variant02 ZERO FUEL AFT Page No:16.04B

9 A F 25-Oct-2016 Sheet 5 abin onfiguration(s) A / TYPE arrier Empty Flights A F TK 4.2. G - Limits for Loadsheet Purpose Empty Flights TAKE-OFF FWD TAKE-OFF AFT ZERO FUEL FWD ZERO FUEL AFT Page No:16.04

10 A F 11-Apr-2011 Sheet 6 abin onfiguration(s) A / TYPE arrier T-JDO A F TK 5. EFFET OF FUEL 5.1 EFFET OF FUEL (FUEL DENSITY : 0.80 KG/L) Fuel (KG) Fuel (KG) FULL 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 = 25 kg/minute APU Fuel Flow = 200 kg/hour Page No:16.05

11 A F 10-Sep-2018 Sheet 6 abin onfiguration(s) A / TYPE arrier JDP,-JDR,-JDS,-JI,-JOV,-JOY,-JOZ,- JOO,-JOU A F TK 5. EFFET OF FUEL 5.1 EFFET OF FUEL (FUEL DENSITY : 0.80 KG/L) Fuel (KG) Fuel (KG) FULL 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 = 25 kg/minute APU Fuel Flow = 200 kg/hour Page No:16.05A

12 A F 31-Mar-2011 Sheet 7 abin onfiguration(s) A / TYPE arrier ALL A F TK 6. REW 6.1. Number of cockpit crew seats and average location Length of arm from reference Maximum number of cockpit seats station influence +/- meter(s) +/- per 1 kg 1.&2.Seats seats seats Number of cabin crew seats and location Loadmaster seat locations FWD of Safety Barrier Wall Max. No. of seats Length of arm from reference influence station +/- meter(s) +/- per 1 kg rew Distribution / rew ode rew ode ockpit rew Total No Number of abin rew at Location abin rew Total No FWD MID AFT 2/ / / / / / Location of rew Baggage BULK ARGO OMPT. 51 Page No:16.06

13 abin onfiguration(s) ALL 7. GALLEY AND PANTRY 7.1. Galleys A F 31-Mar-2011 Sheet 8 A / TYPE arrier A F TK Length of arm from reference station influence Galley locations +/- meter(s) +/- per 1 kg G Pantry / Pantry ode Pantry / Pantry ode is given on A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE. 7.3 SEATING ONDITIONS LOADSHEET OUTPUT STATE BELOW HOW THE SEATING ONDITIONS SHOULD BE SHOWN IN THE RESPETIVE LOADSHEET BOX. GIVE EXAMPLE. ENLOSE A PASSENGER DISTRIBUTION TABLE IF USED. A PERMANENT PASSENGER DISTRIBUTION TABLE IS NOT USED. Page No:16.07

14 abin onfiguration(s) ALL 8. PASSENGER ABIN 8.1 Passenger Seats lass 1 : LASS ODES lass 2 : Y lass 3 : - NUMBER OF SEATS Name of cabin section lass 1 lass 2 lass 3 Total per cabin section A F 31-Mar-2011 A / TYPE A F Sheet 9 arrier TK 8.2 lass/abin Sections lass/abin Section Length of arm from reference influence station +/- meter(s) +/- per 1 kg Page No:16.08

15 A F 31-Mar-2011 Sheet 10 A / TYPE arrier A F TK 8.3 Seating Layout 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 Pratice Page No:16.09

16 A F 31-Mar-2011 Sheet 11 abin onfiguration(s) A / TYPE arrier A F TK Seatplan Layout / Facilities and Row Influence SETION ROW NO abin onfig. A B D E F G J K Length of arm from reference station INDEX INFLUENE per SEAT- ROW per1kg Page No:16.10

17 A F 10-Sep-2018 Sheet 12 abin onfiguration(s) A / TYPE arrier ALL A F TK 9. DETAILS FOR OMPARTMENT TRIM For JDO only OMPARTMENT MAXIMUM APAITY influence NUMBER DESRIPTION GROSS WEIGHT VOLUME* (kg) (m 3 ) +/- per 1 kg 1 FWD ARGO HOLD 1+2 MAX.UM FWD ARGO HOLD AFT ARGO HOLD 3+4 MAX.UM AFT ARGO HOLD REAR / BULK argohold For T-JDP, -JDR, -JDS, -JI,-JOO,-JOU OMPARTMENT MAXIMUM APAITY influence NUMBER DESRIPTION GROSS WEIGHT VOLUME* (kg) (m 3 ) +/- per 1 kg 1 FWD ARGO HOLD 1+2 MAX.UM FWD ARGO HOLD AFT ARGO HOLD 3+4 MAX.UM AFT ARGO HOLD REAR / BULK argohold Remarks: * : Volume information is given only for Bulk compartments. 9.1 ombined Load Limitations : N/A Page No:16.11

18 A F 10-Sep-2018 Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A F TK 10. DETAILS FOR BAY / SETION TRIM T-JDO BAY / SETION DESRIPTION GROSS VOLUME influence WEIGHT (kg) (M 3 ) +/- per 1 kg 51 Bulk Bulk T-JDP, -JDR, -JDS, -JI,-JOO,-JOU BAY / SETION DESRIPTION GROSS VOLUME influence WEIGHT (kg) (M3) +/- per 1 kg 51 Bulk Bulk Bulk REMARKS: -PAG and PM pallet index influences are equalized by averaging original influences. This allowed to minimize the number of Hold versions. I. ONTAINER Lower Deck Maximum capacity Bay/Section Gross Volume * value per 1 kg ontainers (only for T-JDO,JOO) Page No:16.12

19 A F 10-Sep-2018 Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A F TK II. PALLET 88 x125 Lower Deck Maximum capacity Bay/Section Gross Volume * value per 1 kg PALLET 88 x P P P P P P P P (only for T-JDO,JOO) III. PALLET 96 x125 Lower Deck Maximum capacity Bay/Section Gross Volume * value per 1 kg PALLET 96 x P P P P P P P P (only for T-JDO,JOO) Page No:16.12a

20 A F 27-Aug-2013 Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A F TK 10. DETAILS FOR BAY / SETION TRIM Main Deck Bay/Section 88 x125 Single Row Maximum capacity Gross Volume * value per 1 kg A B D E F G H J K L M P R S T U Main Deck Bay/Section 96 x125 Single Row Maximum capacity Gross Volume * value per 1 kg AA BB DD EE FF GG HH JJ KK LL MM PP RR SS TT Page No:16.12b

21 A F 27-Aug-2013 Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A F TK Main Deck Bay/Section 125 x 96 Single Row Maximum capacity Gross Volume * value per 1 kg AB B E EF FH HJ JK KM MP * Volume information required for bulk compartments only. Main Deck Bay/Section 125 x 88 Side By side Maximum capacity Gross Volume * value per 1 kg AB B E EF FH HJ JK KM MP PR * Volume information required for bulk compartments only. Main Deck Bay/Section 125 x 96 Side By side Maximum capacity Gross Volume * value per 1 kg AB B E EF FH HJ JK KM MP Page No:16.12c

22 A F 14-May-2015 Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A F TK 10. DETAILS FOR BAY/SETION TRIM 16ft Pallets Main Deck Bay/Section 16ft PALLETS Maximum capacity Gross Volume * value per 1 kg FR FJR JLR LPR * Volume information required for bulk compartments only. Note 1: Attach a plan for each compartment configuration. Note 2: Use additional sheets as required DETAILS FOR BAY/SETION TRIM 20ft. Pallets Main Deck Bay/Section 20ft PALLETS Maximum capacity Gross Volume * value per 1 kg FG FJG JLG * Volume information required for bulk compartments only. Note 1: Attach a plan for each compartment configuration. Note 2: Use additional sheets as required. Page No:16.12d

23 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS : BALLAST IS NOT REQUIRED A F 19-Dec-2017 Sheet 14 A / TYPE arrier A F TK A / TYPE A F 1. G LIMITS 1.1. Planning Limits G-Limits for loadplanning purpose shall be agreed between carrier and system operator. D Sheet 1 arrier TK 1.2 Ideal Trim Line at ZFW for Fuel Saving Purposes The IDEAL TRIM LINE shown in the balance graph below is a loadplanning 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) of the ideal trim line shall be entered in the table below. WEIGHT INDEX VALUE UNIT LOAD DEVIES DETAILS A / TYPE A F Maximum apacity Type Tare Gross VOLUME ode weight (M 3 ) Remarks AVE x61.5 in.half-size container V3(LD3) AKE x61.5 in. half-size container V3(LD3) PLA x125 inch size pallet (W2) P9A x125 inch size pallet (W2) PAG x125 inch size pallet (A2) PM x125 inch size pallet (Q2) NOTES : - GROSS WEIGHT includes tare weight of pallets, containers, nets and igloo - GROSS WEIGHT is valid for only the aircraft type A UNIT LOAD DEVIES NOTES D Sheet 2 arrier TK 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. A / TYPE A F 3. SPEIAL LOAD Turkish Airlines & IATA regulations apply. When necessary contact Turkish Airlines Station Manager. D Sheet 3 arrier TK Page No:16.13