SUPPLIER'S CONTACTS AHM565 EDP SYSTEM SEMI PERMANENT DATA. Contact and Message Information Supplier Contacts. Sheet 1 Carrier

Transcription

1 Contact and Message Information Supplier Contacts A Sheet 1 1 SUPPLIER'S CONTACTS Completed sheets and changes of basic data and procedure must be forwarded to: MAILING ADDRESS: (INC. TEL & FA) Click Here To Add Another Row To Table TELETYPE ADDRESSES: Click Here To Add Another Row To Table ADDRESSES: Click Here To Add Another Row To Table DATA TRANSFER METHOD: Direct data transmitted E-Document Hard Copy Doc Other (Specify) Remarks: Completed by: SMA-DGK-HÇ Issue No: 34

2 Contact and Message Information Contacts A Sheet 2 2 CARRIER'S CONTACTS Database output and related material (e.g. test loadsheets) must be forwarded to: MAILING ADDRESS: (INC. TEL & FA) Turkish Airlines Inc. Cargo Addition Building, Yesilkoy Istanbul / Turkey Phone: / Fax: wabe@thy.com TELETYPE ADDRESSES: Click Here To Add Another Row To Table ADDRESSES: wabe@thy.com DATA TRANSFER METHOD: Direct data transmitted E-Document Hard Copy Doc Other (Specify) Remarks: Completed by: SMA-DGK-HÇ Issue No: 34

3 List of Revisions A Sheet 3 3 LIST OF REVISIONS The issue number and the date are mandatory. Document Issue Number Revision Number Related Date (YYYYMMDD) Completed by Reason* Changes Overview** SMA-DGK-H.Ç U * Short description of changes ** If issue number changes, "Update Complete Document", else"n/u/d section sheet paragraph". Completed by: SMA-DGK-HÇ Issue No: 34

4 List of Effective Sheets A Sheet 4 4 LIST OF EFFECTIVE SHEETS The issue number and the date are mandatory. Section Sheet Multiple Page Identifier Sheet Issue Number Date (YYYYMMDD) Section A Sheet Section A Sheet Section A Sheet Section A Sheet Section A Sheet Section B Sheet Section B Sheet Section B Sheet Section B Sheet Section C Sheet Section C Sheet Section C Sheet Section C Sheet Section C Sheet 5 C5,C5.1,C Section C Sheet Section C Sheet 8 C8,C8.1,C Section C Sheet 9 C9,C Section C Sheet 10 C10,C Section C Sheet Section C Sheet 12 C12,C Section D Sheet 2 D2,D Section D Sheet 5 D5,D5.1,D Section D Sheet Section D Sheet Section D Sheet 8 D8,D8.1,D8.2,D8.3,D Section D Sheet 9 D9,D9.1,D Section E Sheet Section E Sheet 2 E2,E Section E Sheet Section E Sheet 5 E5,E Section F Sheet 1 F1,F Section G Sheet Remarks: Section A:Datasheet references and high level carrier/supplier information Section B:General data Section C:Aircraft type specific data(units,fuel,cg limits,max Weights etc...) Section D:Aircraft type specific data(holds and Cabins) Section E:Dry Operating weight Build Up Section F: Limiting Weights Sections G:Cargo compartment Considerations Section H:Business rules Completed by: SMA-DGK-HÇ Issue No: 34

5 Documents and Messages A Sheet AUTOMATICALLY PRODUCED DOCUMENTS (tick as required) LOADSHEET LOADING INSTRUCTION/REPORT NOTOC PASSENGER INFO LIST SEATPLAN MESSAGE REQUIREMENTS (tick as required) ALI Abbreviated Load Information Message AHM 584 CPM Container/Pallet Distribution Message AHM 587 DIV Diversion Message AHM 781 FMM Fuel Monitoring Message AHM 782 IDM Industry Discount Message Recommended Practice 1714 LDM Load Message AHM 583 MVT Movement Message AHM 011 and 780 PFS Passenger Final Sales Message Recommended Practice 1719 (dispatch only) PNL/ADL Passenger Name List, and Additions and Deletions List (Recommended Practice 1708) (acceptance only) PSM Passenger Service Message Recommended Practice 1715 (dispatch only) PTM Passenger Transfer Message Recommended Practice 1718 RQL Request List Message Recommended Practice 1709 (dispatch only) RQM Request Information Message AHM 783 SAL Seats Available List Recommended Practice 1713 (acceptance only) SLS Statistical Load Summary AHM 588 SOM Seats Occupied Message Recommended Practice 1712 TPM Teletype Passenger Manifest Recommended Practice 1717 (dispatch only) UCM ULD Control Message AHM 388 (dispatch only) UWS ULD/Bulk Load Weight Signal AHM 581 (acceptance only) Other (Specify): MESSAGE ADDRESSES Contact Turkish Airlines Local Station Manager for message Addresses. MULTIPLE SHEETS NUMBERING In the event of the requirement to produce multiple copies of the same sheets (e.g. C5, C9 ) establish an additional sequence identifier while keeping the original sheet number. E.g. C5.1, C5.2, etc. Completed by: SMA-DGK-HÇ Issue No: 34

6 Standards Units and Codes B Sheet 1 1 1,1 STANDARD UNITS AND CODES Definition of Airline Units of Measure Unit Measurement (tick one for each unit) Weight: Kilogram Pound <<<Click applicable checkboxes Volume: Cubic Metre Cubic Feet 1,2 Definition of class codes The following class naming convention shall be used throughout the document. Class codes: (e.g. F, Y, C, M, etc.) Class Code Priority Code Description F 1 First Class C 2 Business Class U 3 Comfort Class Y 4 Eonomy Class Click Here To Add Another Row To Table 1,3 Airline Defined Information Load Codes Define airline unique load information codes here. BF BC BU BY BT TBF TBC TBU TBY SPB Airline Load Information Code Description First Class Baggage Bussines Class Baggage Comfort Class Baggage Economy Class Baggage Transfer Baggage Transit First Class Baggage Transit Bussines Class Baggage Transit Comfort Class Baggage Transit Economy Class Baggage Special Baggage Click Here To Add Another Row To Table Completed by: SMA-DGK-HÇ Issue No: 34

7 Standards Crew and Baggage Weights B Sheet 2 2 2,1 CREW AND CREW BAGGAGE WEIGHTS Crew weights Gender Flight Deck Crew Weights Cabin Crew Weights Description Crew Hand Baggage Crew Hand Baggage STANDARD M STANDARD F Click Here To Add Another Row To Table * Variations may include domestic, international, charter, route, etc. Hand baggage weight is included in the above mentioned crew weights. If No: Actual or standard hand baggage weight must be used. Remarks: Yes No 2,2 Crew baggage weights (other than hand baggage) Description* Flight Deck Crew Baggage Cabin Crew Baggage LONGHAUL STANDARD 0 0 * Variations may include domestic, international, charter, route, etc. Remarks: Completed by: SMA-DGK-HÇ Issue No: 34

8 Standards Passenger and Carry-on Weights B Sheet 3 3 PASSENGER AND BAGGAGE WEIGHTS 3,1 Standard / Default Passenger / Cabin Baggage Weights Enter standard passenger weights, followed by any variations. Description Adult Male Female All flight except holiday charters Holiday charters Child Infant Hand Baggage * Variations may include domestic, international, charter, route, etc. Hand baggage weight is included in the above mentioned passenger weights. If No: Actual or standard hand baggage weight must be used. Remarks (conditions for oversize, etc): Yes No Completed by: SMA-DGK-HÇ Issue No: 34

9 Standards Baggage Weights and Planning B Sheet 4 3,3 Checked baggage weight Enter standard baggage weights, followed by any variations. Description * Class Weight per Piece Weight per Passenger Domestic All International All ER-Longhaul All Charter All Click Here To Add Another Row To Table * Variations may include domestic, international, charter, route, etc. Enter actual if standard weight not permitted. Remarks (conditions for Oversize etc.): In case weighing platform is unusuable or actual weight of baggages is unknown, Standard baggage weights listed above table 3.3 should be used. Heavy Baggage which is higher than 23 kg is considered as Heavy Baggage. Completed by: SMA-DGK-HÇ Issue No: 34

10 Aircraft Information Units of Measurement Seat Config: Aircraft Type: B Load Config: ALL C Sheet 1 1 AIRCRAFT TYPE OR FLEET Manufacturer: BOEING Aircraft type: B Series or subtype: B ER Aircraft Name: B ER Aircraft Manufacturer IATA or ICAO aircraft type code Also referred to as suffix in the IATA SSIM manual Aircraft type as it appears on the loadsheet 1,1 Definitions of Aircraft Units of Measure Unit Measurement (tick one for each unit) # Weight Kilograms US Pounds è Centimeters Inches è Length Metres Feet è MM è Liquid Volume Litres US Gallons Volume Cubic Metres Cubic Feet Fuel Density KG / Litre KG / US Gallon LB / Litre LB / US Gallon Moments KG Inches ### LB Inches KG Centimeters KG Metres KG MM ### ### ### LB Centimeters LB Metres LB MM Tick as appropriate Remarks: Completed by: SMA-DGK-HÇ Issue No: 34

11 Aircraft Information Loadsheet Options Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet 2 2 BALANCE AND SPECIAL INFORMATION OUTPUT ON LOADSHEET 2,1 Balance output Copy Document Rules from EDP AHM517 to other columns Prelim Final Item EDP ACARS EDP ACARS AHM517 AHM518 AHM517 AHM518 Basic Index BI Y Y Dry Operating Index DOI Y Y Deadload Index DLI Deadload MAC MACDLW* Loaded Index at zero fuel weight LIZFW Y Y Loaded Index at take-off weight LITOW Y Y Loaded Index at landing weight LILAW Y Y MAC at zero fuel weight MACZFW* Y Y MAC at take-off weight MACTOW* Y Y MAC at landing weight MACLAW* Y Y Stabilizer trim setting at take-off STABTO Y Y Stabilizer trim setting at landing STABLA Remarks Fuel Density LW MAC with Fwd & Aft Limits TO MAC with Fwd & Aft Limits ZF MAC with Fwd & Aft Limits Stabiliser Setting Y Click Here To Add Another Row To Table * Indicate if RC (Reference Chord) to be printed on loadsheet in place of MAC 2,2 Passenger trim output Remarks* Class trim Cabin area trim Y Seat row trim Y *Remarks: Indicate any other terminology to be printed on the loadsheet (Ref AHM item 44). Completed by: SMA-DGK-HÇ Issue No: 34

12 Aircraft Information Loadsheet Options Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet 3 2,3 Supplementary Information Prelim Final Item EDP ACARS EDP ACARS Remarks AHM517 AHM518 AHM517 AHM518 Ballast Fuel Y Y In case of necessary. DOC* Basic Weight Y Y Centre of Gravity Limits - LAW Y Y Centre of Gravity Limits - TOW Y Y Centre of Gravity Limits - ZFW Y Y Crew Code Crew Index Deadload Breakdown Fuel Density LDM Y Y Pantry Code Y Y Pantry Index Y Y Service Weight Adjustments Y Y Transit Transit Zero Fuel Centre of Gravity Transit Zero Fuel Weight Trapped Fuel *Depends On Operational Conditions during Flight Preparation. Completed by: SMA-DGK-HÇ Issue No: 34

13 Aircraft Information Basic Index and MAC Formula Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet 4 3 3,1 BASIC INDE AND MAC / RC FORMULA Examples and definitions Index = W (Balance Arm Reference Arm.) C + K %MAC / RC = C (I K) W + Reference Arm - LEMAC or LERC MAC or RC 100 W = Weight, actual. Balance Arm = Station, horizontal distance in length units from reference datum to the location. Reference Arm = reference Station/axis. Selected Station around which all index values are calculated. K = Constant used as a plus value to avoid negative index figures C = Defined Weight Constant used as a denominator to convert moment values into index values. I = index value corresponding to respective weight. MAC / RC = length of Mean Aerodynamic Chord/reference Chord in length units LEMAC / LERC = horizontal distance in length units from the reference datum to location of the Leading Edge 3,2 Index formula Reference Arm at = K (constant) = C (constant) = 658, Length units from reference datum 3,3 MAC/RC information Length of MAC/RC = LEMAC/LERC = 155,8 627,1 (Chord type = MAC) length units length units reference datum. Completed by: SMA-DGK-HÇ Issue No: 34

14 Load Config: Registrations: Aircraft Information Centre of Gravity Limits Seat Config: Aircraft Type: B TC-JYA,JYB,JYC,JYD,-JYE,-JYF,-JYG,- JYH,-JYI,-JYJ C Sheet 5 4 4,1 CENTRE OF GRAVITY CHARTS CG limits for loadsheet Purposes Enter the forward and the aft balance limits in the boxes, commencing at the lowest possible operating weight and terminating at the highest possible operating weight to be checked. IMPORTANT: If limits are affected and/or determined by passenger/fuel/version or other conditions, specify each set of limits on a separate sheet, entering the special condition(s) in the box. Table Name: STANDARD Condition: From: To: Type: + Envelope is: Certified: Curtailed: FORWARD AFT Specify Specify Weight MAC Index applicability * applicability * ZERO FUEL ,13 32,7 Fuel Loaded in Aux Tank ,60 25, , , ,18 51,5 ZERO FUEL ,13 32,7 No Fuel Loaded in Aux Tank , ,84 19, ,32 24,8 Weight MAC Index ZERO FUEL ,81 50,9 ZERO FUEL ,53 56,4 ZERO FUEL ,71 70,6 ZERO FUEL ,97 72,5 ZERO FUEL ,31 71,2 ZERO FUEL ,49 64,5 TAKE OFF ,13 32,7 TAKE OFF ,27 40,7 TAKE OFF ,16 16 No Fuel Loaded in Aux Tank ,39 81,1 TAKE OFF ,84 19, ,76 83,3 TAKE OFF ,32 24, ,30 65 TAKE OFF ,11 26,2 TAKE OFF ,16 26,3 TAKE OFF ,27 40,7 TAKE OFF ,13 41,6 Fuel Loaded in Aux Tank ,39 81, ,41 81, ,98 60 Alternate forward Limits-1 Take off Check , , , ,7 Alternate forward Limits-2 Take off Check , , , ,1 ff LANDING LANDING LANDING LANDING LANDING Remarks: ,13 32,7 LANDING ,16 16 LANDING ,84 19,3 LANDING ,32 24,8 LANDING ,11 26,2 17,27 40,7 31,39 81,1 LANDING Click here to add a new CG limits table : Click here to add a registration specific CG limits sheet : NLT REG Completed by: SMA-DGK-HÇ Issue No: 34

15 Aircraft Information Centre of Gravity Limits Seat Config: Aircraft Type: B Load Config: Registrations: TC-JYL,JYM,JYN,JYO,JYP C Sheet ,1 CENTRE OF GRAVITY CHARTS CG limits for loadsheet Purposes Enter the forward and the aft balance limits in the boxes, commencing at the lowest possible operating weight and terminating at the highest possible operating weight to be checked. IMPORTANT: If limits are affected and/or determined by passenger/fuel/version or other conditions, specify each set of limits on a separate sheet, entering the special condition(s) in the box. Table Name: STANDARD Co From: To: Type: + Envelope is: Certified: Curtailed: FORWARD AFT Specify Specify Weight MAC Index applicability * applicability * ZERO FUEL ,77 33,7 ZERO FUEL ,54 17 ZERO FUEL ,20 20,3 ZERO FUEL ,66 25,8 Weight MAC Index ZERO FUEL ,17 49,9 ZERO FUEL ,96 55,4 ZERO FUEL ,33 69,6 ZERO FUEL ,61 71,5 ZERO FUEL ,95 70,2 ZERO FUEL ,16 63,5 TAKE OFF ,77 33,7 TAKE OFF ,62 39,7 TAKE OFF ,54 17 TAKE OFF ,08 80,1 TAKE OFF ,20 20,3 TAKE OFF ,45 82,3 TAKE OFF ,66 25,8 TAKE OFF ,04 64 TAKE OFF ,42 27,2 TAKE OFF ,47 27,3 TAKE OFF ,39 42,6 Alternate forward Limits-1 Take off Check ,81 48, ,42 42,7 Alternate forward Limits-2 Take off Check ,29 54, ,43 54,1 LANDING ,77 33,7 LANDING ,62 39,7 LANDING ,54 17 LANDING ,08 80,1 LANDING ,20 20,3 LANDING ,66 25,8 LANDING ,42 27,2 Click here to add a new CG limits table : NLT ff ff ff ff ff ff Remarks: Click here to add a registration specific CG limits sheet : REG Completed by: SMA-DGK-HÇ Issue No: 34

16 Aircraft Information Centre of Gravity Limits Seat Config: Aircraft Type: B737-9MA Load Config: Registrations: TC-LYA C Sheet ,1 CENTRE OF GRAVITY CHARTS CG limits for loadsheet Purposes Enter the forward and the aft balance limits in the boxes, commencing at the lowest possible operating weight and terminating at the highest possible operating weight to be checked. IMPORTANT: If limits are affected and/or determined by passenger/fuel/version or other conditions, specify each set of limits on a separate sheet, entering the special condition(s) in the box. Table Name: STANDARD Condition: LDW<=73345 From: To: Type: + Envelope is: Certified: Curtailed: FORWARD AFT Specify Specify Weight MAC Index applicability * applicability * Weight MAC Index ZERO FUEL ,54 28,9 ZERO FUEL ,34 41,8 ZERO FUEL ,64 17,2 ZERO FUEL ,23 45,4 ZERO FUEL ,47 27,9 ZERO FUEL ,36 49,9 ZERO FUEL ,03 29,2 ZERO FUEL ,15 83,3 TAKE OFF ,54 28,9 TAKE OFF ,34 41,8 TAKE OFF ,64 17,2 TAKE OFF ,23 45,4 TAKE OFF ,47 27,9 TAKE OFF ,51 78,9 TAKE OFF ,03 29,2 TAKE OFF ,42 54,4 TAKE OFF ,93 28,3 TAKE OFF ,05 37,4 TAKE OFF ,59 43,3 LANDING ,54 28,9 LANDING ,34 41,8 LANDING ,64 17,2 LANDING ,23 45,4 LANDING ,47 27,9 LANDING ,51 78,9 LANDING ,03 29,2 LANDING ,45 76,2 LANDING ,94 28,38 LANDING ,49 36,6

17 Table Name: STANDARD Condition: LDW>73345 From: To: Type: + Envelope is: Certified: Curtailed: FORWARD AFT Specify Specify Weight MAC Index applicability * applicability * Weight MAC Index ZERO FUEL ,54 28,90 ZERO FUEL ,15 83,3 ZERO FUEL ,46 23,30 ZERO FUEL ,36 49,9 ZERO FUEL ,30 55,0 ZERO FUEL ,23 45,4 ZERO FUEL ,58 53,7 ZERO FUEL ,34 41,8 ZERO FUEL ,12 50,3 ZERO FUEL ,67 46,7 ZERO FUEL ,37 43,2 ZERO FUEL ,11 39,5 ZERO FUEL ,96 35,9 ZERO FUEL ,73 38,1 ZERO FUEL ,48 40,3 ZERO FUEL ,99 41,8 ZERO FUEL ,32 42,8 ZERO FUEL ,42 43,1 TAKE OFF ,54 28,9 TAKE OFF ,34 41,8 TAKE OFF ,64 17,2 TAKE OFF ,23 45,4 TAKE OFF ,47 27,9 TAKE OFF ,51 78,9 TAKE OFF ,03 29,2 TAKE OFF ,42 54,4 TAKE OFF ,93 28,3 TAKE OFF ,05 37,4 TAKE OFF ,59 43,3 LANDING ,54 28,9 LANDING ,34 41,8 LANDING ,64 17,2 LANDING ,23 45,4 LANDING ,47 27,9 LANDING ,51 78,9 LANDING ,03 29,2 LANDING ,45 76,2 LANDING ,94 28,38 LANDING ,49 36,6 Completed by: SMA-DGK-HÇ Issue No: 34 (Signature) Date: 28 / 02 / 19

18 Aircraft Information Ideal Trim Line and Tipping Limits Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet 7 4,3 Ideal Trim Line / Area Specify Ideal Trim Line Table Name IDEAL TRIM LINE - NORMAL OPERATIONS Condition: ALL From: To: Type: Zero Fuel Weight Weight Ideal Trim Line Ideal Trim Area - Fwd Ideal Trim Area - Aft %MAC/RC Index %MAC/RC Index %MAC/RC Index , , , , , ,3 58 Remarks: The IDEAL TRIM LINE shown in the balance graph above 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 above. Completed by: SMA-DGK-HÇ Issue No: 34

19 Load Config: Registrations: Aircraft Information Fuel Seat Config: Aircraft Type: B TC-JYA,JYB,JYC,JYD,-JYE,-JYF,-JYG,- JYH,-JYI,-JYJ C Sheet 8 5 5,1 FUEL Use Seperate sheets for each tank or tank pair. Effect of fuel (for each tank) Enter fueling procedure or fuel tank(s) information. Table Name: STANDART FUEL TANKS TABLES Tank Available For Standard Distributions: Max Volume: 26024,6 Max Weight: Tank Available For Non-Std Distributions: Ballast/Trapped (Unusable) Fuel Allowed: Fuel Density: 0,785 Min: 0,76 Max: 0,82 Tank Names: Main Tanks Fuel Quantity Volume Weight () Balance Arm Index ,7-0, ,7-0, ,1-0, ,9-0, ,7 0, ,4 0, ,6 0, ,4 0, ,6 0, ,4 0, ,6 0, ,1 0, ,1 1, ,1 1, , ,4 2, ,8 2, ,1 3, ,9 4, , ,2 5, ,3 6, ,9 7, ,8 8, ,2 9,16

20 Tank Names: Center Tank Fuel Quantity Volume Weight () Balance Arm 610,2 609,8 608,3 607,1 606,3 605,5 605,1 605,1 604,7 604,7 604,7 604,7 604,7 604,7 605,1 605,1 605,1 Index -0,43-0,87-1,35-1,84-2,33-2,84-3,34-3,82-4,33-4,81-5,29-5,77-6,25-6,73-7,16-7, , ,5-8, ,5-9, ,5-9, ,9-9, ,9-10, ,9-10, ,3-11, ,3-11, ,3-12, ,3-12, ,7-12, ,7-13, ,7-13, ,7-14, ,7-14, , , ,28-15,74-16,20-16, , ,3 606,3-17, ,3-17, ,9-18, ,5-18, ,4-19,31 Tank Names: Auxilary Trim Tank Fuel Quantity Volume Weight () Balance Arm , , , , , , , , , , , , , , ,4 Remarks (Use free text to specify any non-standard procedures not covered by the table): REMARKS: FUEL LOADING PROCEDURE IS AS FOLLOWS; Index 0,7 1,4 2,1 2,7 3,4 4,1 4,8 5,5 6,2 6,8 7,5 8,2 8,9 9,6 10,0 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank until full. 3. Load additional fuel in the auxilary trim tank until full. Completed by: SMA-DGK-HÇ Issue No: 34

21 Aircraft Information Fuel Seat Config: Aircraft Type: B Load Config: Registrations: TC-JYL,JYM,JYN,JYO,JYP C Sheet ,1 FUEL Use Seperate sheets for each tank or tank pair. Effect of fuel (for each tank) Enter fueling procedure or fuel tank(s) information. Table Name: STANDART FUEL TANKS TABLES Tank Available For Standard Distributions: Max Volume: 26024,6 Max Weight: Tank Available For Non-Std Distributions: Ballast/Trapped (Unusable) Fuel Allowed: Fuel Density: 0,785 Min: 0,76 Max: 0,82 Tank Names: Main Tanks Fuel Quantity Volume Weight () Balance Arm Index ,7-0, ,7-0, ,1-0, ,9-0, ,7 0, ,4 0, ,6 0, ,4 0, ,6 0, ,4 0, ,6 0, ,1 0, ,1 1, ,1 1, , ,4 2, ,8 2, ,1 3, ,9 4, , ,2 5, ,3 6, ,9 7, ,8 8, ,2 9,16

22 Tank Names: Center Tank Fuel Quantity Volume Weight () Balance Arm Index ,2-0, ,8-0, ,3-1, ,1-1, ,3-2, ,5-2, ,1-3, ,1-3, ,7-4, ,7-4, ,7-5, ,7-5, ,7-6, ,7-6, ,1-7, ,1-7, ,1-8, ,5-8, ,5-9, ,5-9, ,9-9, ,9-10, ,9-10, ,3-11, ,3-11, ,3-12, ,3-12, ,7-12, ,7-13, ,7-13, ,7-14, ,7-14, ,7-15, ,7-15, ,7-16, ,3-16, ,3-17, ,3-17, ,9-18, ,5-18, ,4-19,31 Remarks (Use free text to specify any non-standard procedures not covered by the table): REMARKS: FUEL LOADING PROCEDURE IS AS FOLLOWS; 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank until full. Click here to add a new Fuel Tank : NLT Completed by: SMA-DGK-HÇ Issue No: 34

23 Aircraft Information Fuel Seat Config: Aircraft Type: B737-9 Load Config: Registrations: TC-LYA C Sheet ,1 FUEL Use Seperate sheets for each tank or tank pair. Effect of fuel (for each tank) Enter fueling procedure or fuel tank(s) information. Table Name: STANDART FUEL TANKS TABLES Tank Available For Standard Distributions: Max Volume: Max Weight: Tank Available For Non-Std Distributions: Ballast/Trapped (Unusable) Fuel Allowed: Fuel Density: 0,785 Min: 0,76 Max: 0,82 Tank Names: Main Tanks Fuel Quantity Volume Weight () Balance Arm Index ,9 0, ,6-0, , ,9 0, , , , , ,9 0, ,9 0, , ,4 0, , ,8 1, ,8 1, , ,2 2, ,7 3, ,4 4, ,3 4, ,3 5, ,6 6, ,1 7, ,9 8, ,2 8,84

24 Tank Names: Center Tank Fuel Quantity Volume Weight () Balance Arm Index ,7-0, ,9-0, ,3-1, ,8-1, ,1-2, ,4-2, ,1-3, ,9-3, ,8-4, ,7-4, ,8-5, ,8-5, ,9-6, , ,1-7, ,2-7, ,4-8, ,6-8, ,7-8, ,9-9, , ,2-10, ,3-10, ,4-11, ,5-11, ,6-12, ,7-12, ,8-12, ,8-13, ,9-13, ,9-14, , , ,9-15, ,8-16, ,7-16, ,5-17, ,3-17, , ,7-18, ,73 605,6-19,12 Remarks (Use free text to specify any non-standard procedures not covered by the table): REMARKS: FUEL LOADING PROCEDURE IS AS FOLLOWS; 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank until full. Click here to add a new Fuel Tank : NLT Completed by: SMA-DGK-HÇ Issue No: 34 (Signature) Date: 28 / 02 / 19

25 Aircraft Information Fuel Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet 9 5,2 Effect of Fuel - Cumulative FUEL LOADING PROCEDURE IS AS FOLLOWS; 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank until full. 3. Load additional fuel in the aft auxiliary fuel tank if required. * Procedure Name: STANDARD Tank Available For Standard Distributions: Max Volume: Tank Available For Non-Std Distributions: Max Weight: Fuel Density: 0,803 Min: Max: Fuel Quantity Volume Weight Balance Arm Index , ,3-0, ,7-0, ,7-0, ,3-0, ,3 0, ,3 0, ,3 0, ,3 0, ,3 0, ,3 0, ,3 0, ,3 0, ,3 1, ,3 1, ,3 1, ,3 2, ,3 2, ,3 3, ,3 4, ,3 4, ,3 5, ,3 6, ,3 7, ,3 8, ,3 9, ,3 8, ,3 8, , , ,3 8 7,49 6,99

26 VOLUMETRIC CAPACITY LITER KG (0.803kg/lt) MAIN TANKS LT 3915 KG MAIN TANKS LT 3915 KG CENTER TANK LT KG TOTAL LT KG AUILIARY FUEL TANK (0,803) 3641,6 LT 2923 KG TOTAL 29666,2 LT KG , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , ,7 6,47 5,96 5,47 4,95 4,45 3,96 3,47 2,98 2,49 2,05 1,56 1,07 0,65 0,17-0,32-0,72-1,21-1,69-2,08-2,56-3,03-3,51-3,89-4,36-4,83-5,31-5,78-6,25-6,73-7,2-7,81-8,28-8,76-9,38-10,01-10,38

27 Seat Config: Aircraft Type: B737-9 Load Config: Registrations: MA 5,2 Effect of Fuel - Cumulative FUEL LOADING PROCEDURE IS AS FOLLOWS; 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank until full. Aircraft Information Fuel C Sheet 9 Procedure Name: STANDARD Tank Available For Standard Distributions: Max Volume: Tank Available For Non-Std Distributions: Max Weight: Fuel Density: 0,8028 Min: Max: Fuel Quantity Volume Weight Balance Arm Index 0 658, , , , , , , , , , , ,2 7737¹ , ,2

28 9500 6, , , , , , , ² ¹ Main tanks 1&2 full at nominal density of kg/l.² Main tanks 1&2 and Center tank are full at nominal density of kg/l. 3 Main tanks 1&2 and Center tank are full at maximum density of kg/l. VOLUMETRIC CAPACITY(0,80507 density) MAIN TANKS ,8 LT 4099KG MAIN TANKS2 4818,8 LT 4099KG CENTER TANK 16178,8 LT KG TOTAL LT 21962KG (Signature) Date: 28 / 02 / 19

29 Aircraft Information Fuel Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet 10 5,3 Fuel Distribution Supply fueling sequence If individual tanks used. Distribution name: Automatic Refueling of Tanks Maximum Volume: Maximum Weight: Fuel Density: 0,785 Sequence Fuel range Quantity Tank Name(s) From To Vol or Wt Volume Weight Step ,2 Volume Main 9751,2 7654,692 Step , ,6 Volume Center 16273, ,62 Step , ,6 Volume Auxilary ,4 Ratio *Auxiliary Tank is installed only on TC-JYA,B,C,D,E,F,G,H,I,J Click here to add a new Fuel Distribution table : NLT If fuel burn sequence is not the reverse of the loading sequence complete additional table 5.2 for the fuel burn sequence Remarks (Use free text to specify any non-standard procedures not covered by the table.): Enter any comments here... 5,4 Taxi fuel Station or default Standard Taxi Fuel Weight Default burn order * Click Here To Add Another Row To Table * Indicate tanks from which taxi fuel is burned considering all fuel loading conditions Remarks: 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 = 15 kg/minute APU Fuel Flow = 105 kg/hour

30 Aircraft Information Fuel Seat Config: Aircraft Type: B737-9 Load Config: Registrations: MA C Sheet 10 5,3 Fuel Distribution Supply fueling sequence If individual tanks used. Distribution name: Automatic Refueling of Tanks Maximum Volume: Maximum Weight: Fuel Density: 0,785 Sequence Fuel range Quantity Tank Name(s) From To Vol or Wt Volume Weight Step ,6 Volume Main 9637,6 7565,516 Step , ,4 Volume Center 16178, ,36 Ratio Click here to add a new Fuel Distribution table : NLT If fuel burn sequence is not the reverse of the loading sequence complete additional table 5.2 for the fuel burn sequence Remarks (Use free text to specify any non-standard procedures not covered by the table.): Enter any comments here... 5,4 Taxi fuel Station or default Standard Taxi Fuel Weight Default burn order * Click Here To Add Another Row To Table * Indicate tanks from which taxi fuel is burned considering all fuel loading conditions Remarks: 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 = 15 kg/minute APU Fuel Flow = 105 kg/hour (Signature) Date: 28 / 02 / 19

31 Aircraft Information Stabilizer and Trim Setting Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet 11 Enter the %MAC/RC values used and for each weight the corresponding stabilizer trim settings. FLAPS 1 & 5 Take Off Weight %MAC / RC and corresponding STAB ,8 2,75 2,65 2, ,2 2,75 2,65 2, ,96 2, ,62 3, ,2 3, ,45 3,75 Click Here To Add Another Row To Table FLAPS 10, 15 & 25 Take Off Weight %MAC / RC and corresponding STAB , ,9 3,45 2,75 2,65 2, ,25 3,7 2,95 2,65 2, ,3 2,65 2, ,65 4,78 2,65 2, ,2 5,22 2,65 2, ,45 5,48 2,65 Click Here To Add Another Row To Table Remarks: Click here to add a new Stabiliser Trim table : NLT

32 Aircraft Information Identification Seat Config: Aircraft Type: B Load Config: Registrations: ALL C Sheet ,1 AIRCRAFT IDENTIFICATION Aircraft Identification Table Name Condition: From: To: Type: Aircraft Registration MSN Name Other Identifier TC-JYA SELCUK JYA TC-JYB DENIZLI JYB TC-JYC EREGLI JYC TC-JYD BAYBURT JYD TC-JYE TUZ GOLU JYE TC-JYF CIRAGAN JYF TC-JYG UNYE JYG TC-JYH OF JYH TC-JYI MUGLA JYI TC-JYJ EMIRDAG JYJ TC-JYL ORLU JYL TC-JYM INCEBURUN JYM TC-JYN KANLICA JYN TC-JYO ILICA JYO TC-JYP CATALCA JYP - Registration Group Remarks Remarks: Enter any comments here

33 Aircraft Information Identification Seat Config: Aircraft Type: B737-9 Load Config: Registrations: MA C Sheet ,1 AIRCRAFT IDENTIFICATION Aircraft Identification Table Name Condition: From: To: Type: Aircraft Registration MSN Name TC-LYA _ Other Identifier Registration Group Remarks Remarks: Enter any comments here (Signature) Date: 28 / 02 / 19

34 Configuration Information Holds Seat Config: Aircraft Type: B Load Config: Registrations: TC-JYA,JYB,JYC,JYD,-JYE,-JYF,-JYG,- JYH,-JYI,-JYJ D Sheet 2 2 2,1 HOLDS AND COMPARTMENTS Bulk Holds Deck Name: LOWER Hold / Cpt Name HOLD BULK Max Weight Volume CPT ,39 CPT ,11 CPT ,19 CPT ,85 Lateral Arm Centroid From To Centroid Balance Arm FWD AFT Index per wt unit 172, , , , , , , ,01319 Click Here To Add Another Row To Table

35 Configuration Information Holds Seat Config: Aircraft Type: B Load Config: Registrations: TC-JYL,JYM,JYN,JYO,JYP D Sheet ,1 HOLDS AND COMPARTMENTS Bulk Holds LOWER Hold / Cpt Name Max Weight Volume HOLD BULK CPT ,96 CPT ,11 CPT ,95 CPT ,85 Lateral Arm Balance Arm Index per Centroid From To Centroid FWD AFT wt unit 176, , , , , , , ,01319 Click Here To Add Another Row To Table

36 Seat Config: Aircraft Type: B737-9 Load Config: Registrations: MA Configuration Information Holds D Sheet ,1 HOLDS AND COMPARTMENTS Bulk Holds LOWER Hold / Cpt Name Max Weight Volume HOLD BULK CPT ,96 CPT ,11 CPT ,95 CPT ,85 Lateral Arm Balance Arm Index per Centroid From To Centroid FWD AFT wt unit 176, , , , , , , ,01309 Click Here To Add Another Row To Table (Signature) Date: 28 / 02 / 19

37 Configuration Information Cabin and Crew Locations Seat Config: Aircraft Type: B Load Config: Registrations: TC-JYA,JYB,JYC,JYD,-JYE,-JYF,-JYG,- JYH,-JYI,-JYJ D Sheet 5 5 5,1 CABIN AND EQUIPMENT Cabins, crew, galleys, lavatories, diplomatic (DIP) lockers Cabin Definitions Section Deck Rows Lateral Arm Balance ARM Index per From To From To Centroid FWD AFT Weight Unit 0A MAIN 253,5-0, B MAIN 515,1-0, C MAIN , D MAIN 1041,9 +0, ,2 0 Click Here To Add Another Row To Table Flight Deck Locations Location Deck Maximum Nbr of Seats Lateral Arm Centroid Balance Arm Centroid Index per Weight Unit Captain ,01967 First Officer ,01967 First Observer 1 5-0, ,3 3 Click Here To Add Another Row To Table Cabin Crew Locations Include cabin crew locations if particular to configuration Maximum Nbr of Location Deck Seats Lateral Arm Centroid Balance Arm Centroid Index per Weight Unit F01 (FWD) ,01727 F02 (FWD) ,01727 A01 (AFT) ,01585 A02 (AFT) ,01585 A03 (AFT) ,01585 A04 (AFT) ,01585 Remarks: Crew Location Weight Index 2 COCKPIT CREW (2 FrontSeat) 170-3,3 3 COCKPIT CREW (2 FrontSeat + 1JumpSeat) 255-4,9 3 CABIN CREW (2 Fwd + 1 Aft) 225 1,1 4 CABIN CREW (2 Fwd + 2 Aft) 300-0,2 5 CABIN CREW (2 Fwd + 3 Aft) CABIN CREW (2 Fwd + 4 Aft) 450 2,2

38 Configuration Information Cabin and Crew Locations Seat Config: 169 Aircraft Type: B Load Config: Registrations: TC-JYL,JYM,JYN,JYO,JYP D Sheet D ,1 CABIN AND EQUIPMENT Cabins, crew, galleys, lavatories, diplomatic (DIP) lockers Cabin Definitions Section Deck Rows Lateral Arm Balance ARM Index per From To From To Centroid FWD AFT Weight Unit 0A MAIN 224,5-0, B MAIN 488-0, C MAIN , D MAIN , ,2 2 5,3 Click Here To Add Another Row To Table Flight Deck Locations Location Deck Maximum Nbr of Seats Captain ,01967 First Officer ,01967 First Observer 1 5-0,01867 Cabin Crew Locations Include cabin crew locations if particular to configuration Maximum Nbr of Location Deck Seats Lateral Arm Centroid Lateral Arm Centroid Balance Arm Centroid Balance Arm Centroid Index per Weight Unit Index per Weight Unit F01 (FWD) ,01727 F02 (FWD) ,01727 A01 (AFT) ,01585 A02 (AFT) ,01585 A03 (AFT) ,01585 A04 (AFT) ,01585 Remarks: Crew Location Weight Index 2 COCKPIT CREW (2 FrontSeat) 170-3,3 3 COCKPIT CREW (2 FrontSeat + 1JumpSeat) 255-4,9 3 CABIN CREW (2 Fwd + 1 Aft) 225 1,1 4 CABIN CREW (2 Fwd + 2 Aft) 300-0,2 5 CABIN CREW (2 Fwd + 3 Aft) CABIN CREW (2 Fwd + 4 Aft) 450 2,2

39 Seat Config: 169 Aircraft Type: B737-9 Load Config: Registrations: MA Configuration Information Cabin and Crew Locations D Sheet D ,1 CABIN AND EQUIPMENT Cabins, crew, galleys, lavatories, diplomatic (DIP) lockers Cabin Definitions Section Deck Rows Lateral Arm Balance ARM Index per From To From To Centroid FWD AFT Weight Unit 0A MAIN 224,5-0, B MAIN 457,6-0, C MAIN 736,2 +0, D MAIN , ,2 0 Click Here To Add Another Row To Table Flight Deck Locations 2 Location Deck Maximum Nbr of Seats Lateral Arm Centroid Balance Arm Centroid Index per Weight Unit Captain ,01967 First Officer ,01967 First Observer 1 5-0, ,3 Cabin Crew Locations Include cabin crew locations if particular to configuration Location Deck Maximum Nbr of Lateral Arm Index per Balance Arm Centroid Seats Centroid Weight Unit F01 (FWD) ,01727 F02 (FWD) ,01727 A01 (AFT) ,01585 A02 (AFT) ,01585 A03 (AFT) ,01585 A04 (AFT) ,01585 Remarks: Crew Location Weight Index 2 COCKPIT CREW (2 FrontSeat) 170-3,3 3 COCKPIT CREW (2 FrontSeat + 1JumpSeat) 255-4,9 3 CABIN CREW (2 Fwd + 1 Aft) 225 1,1 4 CABIN CREW (2 Fwd + 2 Aft) 300-0,2 5 CABIN CREW (2 Fwd + 3 Aft) CABIN CREW (2 Fwd + 4 Aft) 450 2,2 (Signature) Date: 28 / 02 / 19

40 Configuration Information Galley and Other Locations Seat Config: ALL Aircraft Type: B Load Config: Registrations: D Sheet 6 5,4 Potable Water Locations Specify potable water tank locations Tank Name Max Weight (lt) Lateral Centroid Balance ARM (mt.) Centroid FWD AFT Potable Water Tank ,4 Index per Weight Unit +0, ,5 0 Galleys and Other Locations Include locations for galleys, lavs, dip lockers, etc. Location Max Weigh Lateral Arm Balance ARM Index per Type Description Centroid From To Centroid FWD AFT Weight Unit GALLEY FWD G1 21,9-0,01818 GALLEY FWD G7 95,8-0,01607 GALLEY GALLEY FWD G2 AFT G6a 101, , ,01419 GALLEY AFT G4b ,01719 Click Here To Add Another Row To Table Location Max Weigh Lateral Arm Balance ARM Index per Type Description Centroid From To Centroid FWD AFT Weight Unit GALLEY FWD 76,1-0,01663 GALLEY AFT 1251,8 +0,01696 Click Here To Add Another Row To Table B737-9 Max Aircrafts(TC-LYA) Location Max Weigh Lateral Arm Balance ARM Index per Type Description Centroid From To Centroid FWD AFT Weight Unit GALLEY FWD G1 27,4-0,01803 GALLEY FWD G2 101,5-0,01591 GALLEY FWD G7 95,8-0,01607 GALLEY AFT G6a 1152,5 +0,01412 GALLEY AFT G4c ,01708 Location Max Weigh Lateral Arm Balance ARM Index per Type Description Centroid From To Centroid FWD AFT Weight Unit GALLEY FWD 1234,3 +0,01646 GALLEY AFT 1236,7 +0,01653 Remarks: FWD, AFT average Galley locations can be used for simplicity (Signature) Date: 28 / 02 / 19

41 Seat Config: Aircraft Type: Load Config: Registrations: ALL Configuration Information Seating Layout B D Sheet 7 6 6,1 SEATING Seating Layout First letter indicates class (e.g. F, C, Y) 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. A B C E F G H I J K L M = Aisle N = No smoking = Bassinet position O = Over wing seat = Crew seat P = Stretcher location = Emergency exit Q = Quiet zone = Bulkhead seat S = Smoking = Groups T = Near toilet = Incapacitated passenger U = Unaccompanied minor = Infant preference row / seats V = Seat left vacant / offered last = Rear facing seats W = No movie = Near galley = Not available = Leg space seat Y = Not fitted = Wheel chair Z = Buffer zone Alpha / Characters - D, R, Blank, not used Example: FV = First class seat left vacant

42 Seat Config: 151Y Aircraft Type: B Load Config: Registrations: Configuration Information Seating Layout TC-JYA,JYB,JYC,JYD,-JYE,-JYF,-JYG,- JYH,-JYI,-JYJ D Sheet 8 6,2 Seat Plan Layout / Facilities and balance information Section Row Max Seat Identifier Balance Index per Wt Max Seats Arm weight unit A B C D E F 0A 1 NBI N Y - Y N NBI 4 167,95-0, A 2 NI N Y - Y N NI 4 228,85-0, A 3 NI N Y - Y N NI 4 282,05-0, A 4 NI N Y - Y N NI 4 334,9-0, B 5 NBI N N - N N NBI 6 396,85-0, B 6 NI N N - N N NI 6 430,1-0, B 7 NI N N - N N NI , B 8 NI N N - N N NI 6 495,9-0, B 9 NI N N - N N NI 6 529,15-0, B 10 NI N N - N N NI 6 562,05-0, B 11 NE NE NE - NE NE NE 6 601,95-0, B 12 NE NE NE - NE NE NE 6 641,85-0, C 13 NI N N - N N NI 6 676,15 0, C 14 NI N N - N N NI 6 710,1 0, C 15 NI N N - N N NI 6 744,05 0, C 16 NI N N - N N NI , C 17 NI N N - N N NI 6 811,95 0, C 18 NI N N - N N NI 6 845,9 0, C 19 NI N N - N N NI 6 879,85 0, C 20 NI N N - N N NI 6 914,15 0, D 21 NI N N - N N NI 6 948,1 0, D 22 NI N N - N N NI 6 982,05 0, D 23 NI N N - N N NI , D 24 NI N N - N N NI ,95 0, D 25 NI N N - N N NI ,9 0, D 26 NI N N - N N NI ,15 0, D 27 Y Y Y - N N NI ,05 0,01405

43 Configuration Information Seating Layout Seat Config: 16C 135Y Aircraft Type: B Load Config: Registrations: TC-JYA,JYB,JYC,JYD,-JYE,-JYF,-JYG,- JYH,-JYI,-JYJ D Sheet 8 6,2 Seat Plan Layout / Facilities and balance information Section Row Max Seat Identifier Balance Index per Wt Max Seats Arm weight unit A B C D E F 0A 1 NBI N Y - Y N NBI 4 167,95-0, A 2 NI N Y - Y N NI 4 228,85-0, A 3 NI N Y - Y N NI 4 282,05-0, A 4 NI N Y - Y N NI 4 334,9-0, B 5 NBI N N - N N NBI 6 396,85-0, B 6 NI N N - N N NI 6 430,1-0, B 7 NI N N - N N NI , B 8 NI N N - N N NI 6 495,9-0, B 9 NI N N - N N NI 6 529,15-0, B 10 NI N N - N N NI 6 562,05-0, B 11 NE NE NE - NE NE NE 6 601,95-0, B 12 NE NE NE - NE NE NE 6 641,85-0, C 13 NI N N - N N NI 6 676,15 0, C 14 NI N N - N N NI 6 710,1 0, C 15 NI N N - N N NI 6 744,05 0, C 16 NI N N - N N NI , C 17 NI N N - N N NI 6 811,95 0, C 18 NI N N - N N NI 6 845,9 0, C 19 NI N N - N N NI 6 879,85 0, C 20 NI N N - N N NI 6 914,15 0, D 21 NI N N - N N NI 6 948,1 0, D 22 NI N N - N N NI 6 982,05 0, D 23 NI N N - N N NI , D 24 NI N N - N N NI ,95 0, D 25 NI N N - N N NI ,9 0, D 26 NI N N - N N NI ,15 0, D 27 Y Y Y - N N NI ,05 0,01405

44 Configuration Information Seating Layout Seat Config: 169Y Aircraft Type: B Load Config: Registrations: TC-JYL,JYM,JYN,JYO,JYP D Sheet 8.1 6,2 Seat Plan Layout / Facilities and balance information Section Row Max Seat Identifier Balance Index per Wt Max Seats Arm weight unit A B C D E F 0A 1 N NBI Y Y NBI N 4 157,1-0, A 2 NI N Y Y N NI 4 201,9-0, A 3 NI N Y Y N NI 4 247,05-0, A 4 NI N Y Y N NI 4 291,85-0, B 5 N NBI N N NBI N 6 346,1-0, B 6 NI N N N N NI 6 376,9-0, B 7 NI N N N N NI 6 408,05-0, B 8 NI N N N N NI 6 438,85-0, B 9 NI N N N N NI , B 10 NI N N N N NI 6 501,15-0, B 11 NI N N N N NI 6 531,95-0, B 12 NI N N N N NI 6 563,1-0, B 13 NE NE NE NE NE NE 6 601,95-0, B 14 NE NE NE NE NE NE 6 641,85-0, C 15 NI N N N N NI 6 674,05 0, C 16 NI N N N N NI 6 705,9 0, C 17 NI N N N N NI 6 738,1 0, C 18 NI N N N N NI 6 769,95 0, C 19 NI N N N N NI 6 802,15 0, C 20 NI N N N N NI , C 21 NI N N N N NI 6 865,85 0, C 22 NI N N N N NI 6 898,05 0, C 23 NI N N N N NI 6 929,9 0, C 24 NI N N N N NI 6 962,1 0, D 25 NI N N N N NI 6 993,95 0, D 26 NI N N N N NI ,45 0, D 27 NI N N N N NI ,6 0, D 28 NI N N N N NI ,4 0, D 29 NI N N N N NI ,55 0, D 30 Y Y Y N N NI ,4 0,01406

45 Configuration Information Seating Layout Seat Config: 16C 153 Aircraft Type: B Load Config: Registrations: TC-JYL,JYM,JYN,JYO,JYP D Sheet 8.1 6,2 Seat Plan Layout / Facilities and balance information Section Row Max Seat Identifier Balance Index per Wt Max Seats Arm weight unit A B C D E F 0A 1 N NBI Y Y NBI N 4 157,1-0, A 2 NI N Y Y N NI 4 201,9-0, A 3 NI N Y Y N NI 4 247,05-0, A 4 NI N Y Y N NI 4 291,85-0, B 5 N NBI N N NBI N 6 346,1-0, B 6 NI N N N N NI 6 376,9-0, B 7 NI N N N N NI 6 408,05-0, B 8 NI N N N N NI 6 438,85-0, B 9 NI N N N N NI , B 10 NI N N N N NI 6 501,15-0, B 11 NI N N N N NI 6 531,95-0, B 12 NI N N N N NI 6 563,1-0, B 13 NE NE NE NE NE NE 6 601,95-0, B 14 NE NE NE NE NE NE 6 641,85-0, C 15 NI N N N N NI 6 674,05 0, C 16 NI N N N N NI 6 705,9 0, C 17 NI N N N N NI 6 738,1 0, C 18 NI N N N N NI 6 769,95 0, C 19 NI N N N N NI 6 802,15 0, C 20 NI N N N N NI , C 21 NI N N N N NI 6 865,85 0, C 22 NI N N N N NI 6 898,05 0, C 23 NI N N N N NI 6 929,9 0, C 24 NI N N N N NI 6 962,1 0, D 25 NI N N N N NI 6 993,95 0, D 26 NI N N N N NI ,45 0, D 27 NI N N N N NI ,6 0, D 28 NI N N N N NI ,4 0, D 29 NI N N N N NI ,55 0, D 30 Y Y Y N N NI ,4 0,01406

46 Seat Config: 16C 153 Aircraft Type: B737-9 Load Config: Registrations: TC-LYA Configuration Information Seating Layout D Sheet 8.1 6,2 Seat Plan Layout / Facilities and balance information Section Row Max Seat Identifier Balance Index per Wt Max Seats Arm weight unit A B C D E F 0A 1 NBI N Y Y N NBI 4 157,1-0, A 2 NI N Y Y N NI 4 201,9-0, A 3 NI N Y Y N NI 4 247,05-0, A 4 NI N Y Y N NI 4 291,85-0, B 5 N NBI N N NBI N , B 6 NI N N N N NI 6 382,15-0, B 7 NI N N N N NI 6 412,95-0, B 8 NI N N N N NI 6 443,05-0, B 9 NI N N N N NI 6 473,15-0, B 10 NI N N N N NI 6 502,9-0, B 11 NI N N N N NI , B 12 NI N N N N NI 6 563,1-0, C 13 NE NE NE NE NE NE 6 601,95-0, C 14 NE NE NE NE NE NE 6 641,15-0, C 15 NI N N N N NI , C 16 NI N N N N NI 6 704,85 0, C 17 NI N N N N NI 6 737,05 0, C 18 NI N N N N NI 6 768,9 0, C 19 NI N N N N NI 6 801,1 0, C 20 NI N N N N NI 6 832,95 0, C 21 NI N N N N NI 6 865,15 0, D 22 NI N N N N NI , D 23 NI N N N N NI 6 928,85 0, D 24 NI N N N N NI 6 961,05 0, D 25 NI N N N N NI 6 992,9 0, D 26 NI N N N N NI ,05 0, D 27 NI N N N N NI ,85 0, D 28 NI N N N N NI , D 29 NI N N N N NI ,15 0, D 30 N N NI ,95 0,01399 (Signature) Date: 28 / 02 / 19

47 Configuration Information Saleable Configurations Seat Config: Aircraft Type: A Load Config: Registrations: TC-JYA,JYB,JYC,JYD,-JYE,-JYF,-JYG,- JYH,-JYI,-JYJ D Sheet 9 6,3 Saleable Configurations Repeat 6.3 for each saleable configuration. Saleable Configuration: 151Y Saleable Configuration: 16C / 135Y Saleable Configuration: Saleable Configuration: Saleable Configuration: Saleable Configuration: Saleable Configuration: Code: Code: Code: Code: Code: Code: Code: Cabin Area Information Number of Seats per Cabin Name and Class Cabin Total Balance Arm Index per (specify classes below) Name Per Weight Unit C Y Cabin Centroid FWD AFT 0A , , B , , C , , D , , Total per class 151 Number of Seats per Cabin Name and Class Cabin Total Balance Arm Index per (specify classes below) Name Per Weight Unit C Y Cabin Centroid FWD AFT 0A , , B , , C , , D , , Total per class Class Information Class code First Row Last Row Number of Seats Lateral Arm Balance ARM From To Centroid FWD AFT Index per Weight Unit