FHYA321AHM560 Rev.5 03.04 · PRESENT A321-231 FLEET (ALL 202 Y) REGISTRATION MODEL TC – FBG...

FREEBIRD AIRLINES (FH/FHY)

AHM 560

PRESENT A321-231 FLEET

(ALL 202 Y)

REGISTRATION MODEL

TC – FBG A321-231 with MSN 771

TC – FBT A321-231 with MSN 855

Reason(s) for issue No 5: 1. Special Information/Notes to the Captain, note to the captain that the specific flight

has been loaded by the handling agent according to this Freebird Airlines A321 AHM560 Issue No.5, dated 03.04.2013.

2. DOW / DOI Tables are corrected. New weight reports. 3. Max take off weight reduced to 85000 kg (from WV00 to WV05).

Prepared by: Mrs. Zehra Ceren Aeronautical Engineer Flight Operations Engineer

Checked by: Capt. Auke van Ginkel Freebird Airlines

Antalya, 03.04.2013

AHM 560 GENERAL

COMMUNICATION

ADDRESSES A

Sheet 1

EDP-SYSTEM SEMI-PERMANENT-DATA

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Issue No: 5 Date: 03.04.2013

1. HANDLING AGENTS CONTACT ADDRESS Completed sheets and changes of basic data and procedures must be forwarded to: MAIN CONTACT : MAILING ADDRESS : PHONE : FAX : SITA :

2. CARRIERS CONTACT ADDRESS MAILING ADDRESS : FREEBIRD AIRLINES Capt. Auke van GINKEL Güzeloba Mah. Barınaklar Bulvarı No. 156/A 07230 GÜZELOBA – ANTALYA TURKEY PHONE : +90 – 242 – 349 3300 Ext 117 : +90 – 533 – 601 8917 (mobile) FAX : + 90 – 242 – 330 3405 SITA : ISTFBFH (General) AYTFOFH (OCC Antalya) E-MAIL : [email protected] & [email protected]

AHM 560 GENERAL

COMMUNICATION

ADDRESSES A

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Issue No: 5 Date: 03.04.2013

3. AUTOMATICALLY PRODUCED DOCUMENTS NOTOC SEATPLAN X LOADPLAN X PASSENGER INFO LIST X LOADSHEET X LOADING INSTRUCTION / REPORT

4. MESSAGE REQUIREMENTS LPM Load Planning Message AHM 580 X LDM Load Message AHM 583 ALI Abbreviated Load Information Message AHM 584 CPM Container/Pallet Message AHM 587 UCM ULD Control Message AHM 388 X MTV Movement Messages AHM 011 /AHM 780 X DIV Diversion Message AHM 781 X SOM Seats Occupied Message RP 1712 X PTM Passenger Transfer Message RP 1718 X PSM Passenger Service Message RP 1715 X TPM Teletype Passenger Manifest RP 1717 PFS Passenger Final Sales Message RP 1719 IDM Industry Discount Message RP 1714 RQL Request List Message RP 1709 X PNL Passenger Names List RP 1708 ADL Additions and Deletions List RP 1708 SAL Seats Available List RP 1713 SLS Statistical Load Summary AHM 588 FMM Fuel Monitoring Message AHM 782 RQM Request Information Message AHM 783 UWS ULD/Bulk Load Weight Signal AHM 781

5. MESSAGE ADDRESSES ISTFOFH-ISTFBFH-ISTGSXH

6. Definition of class codes All Freebird Airlines A321-200 fleet is configured class: Y

AHM 560 GENERAL

LIST OF REVISIONS A

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Issue No: 5 Date: 03.04.2013

List of Revisions: FHY A321 AHM560 Issue No.1 ….. FHY A321 AHM560 Issue No.2 ….. FHY A321 AHM560 Issue No.5 03.08.2006 FHY A321 AHM560 Issue No.6 09.07.2007 ----- Revision number correction ----- FHY A321 AHM560 Issue No.3 24.02.2012 FHY A321 AHM560 Issue No.4 10.05.2012 FHY A321 AHM560 Issue No.5 03.04.2013 Always update complete document.

AHM 560 GENERAL

LIST OF EFFECTIVE SHEETS A

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Issue No: 5 Date: 03.04.2013

List of Effective Sheets: A Sheet 1 Communication Addresses Issue No. 5 03.04.2013 A Sheet 2 Communication Addresses Issue No. 5 03.04.2013 A Sheet 3 List of Revisions Issue No. 5 03.04.2013 A Sheet 4 List of Effective Sheets Issue No. 5 03.04.2013 B Sheet 1 General Information Issue No. 5 03.04.2013 B Sheet 2 General Information Issue No. 5 03.04.2013 B Sheet 3 General Information Issue No. 5 03.04.2013 C Sheet 1 Aircraft Data Issue No. 5 03.04.2013 C Sheet 2 Aircraft Data Issue No. 5 03.04.2013 C Sheet 3 Aircraft Data Issue No. 5 03.04.2013 C Sheet 4 Aircraft Data Issue No. 5 03.04.2013 C Sheet 5 Aircraft Data Issue No. 5 03.04.2013 C Sheet 6 Aircraft Data Issue No. 5 03.04.2013 C Sheet 7 Aircraft Data Issue No. 5 03.04.2013 C Sheet 8 Aircraft Data Issue No. 5 03.04.2013 C Sheet 9 Aircraft Data Issue No. 5 03.04.2013 C Sheet 10 Aircraft Data Issue No. 5 03.04.2013 C Sheet 11 Aircraft Data Issue No. 5 03.04.2013 C Sheet 12 Aircraft Data Issue No. 5 03.04.2013 C Sheet 13 Aircraft Data Issue No. 5 03.04.2013 D Sheet 1 Load Planning data Issue No. 5 03.04.2013 D Sheet 2 Load Planning data Issue No. 5 03.04.2013 Attachment 1a DOW & DOI Tables –G Issue No. 5 03.04.2013 Attachment 1b DOW & DOI Tables –T Issue No. 5 03.04.2013 Attachment 2a Load & Trim Sheet Rev.3 Issue No. 5 03.04.2013 Attachment 2b Load & Trim Sheet Rev.3 Overleaf Issue No. 5 03.04.2013 Attachment 3a Ferry Flight Load & Trim Sheet Rev.1 Data Issue No. 5 03.04.2013 Attachment 3b Ferry Flight Load & Trim Sheet Rev.1 Issue No. 5 03.04.2013

AHM 560 GENERAL

GENERAL INFORMATION B

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Issue No: 5 Date: 03.04.2013

1. PASSENGER AND BAGGAGE WEIGHTS

1.1. Standard & Alternate Passenger Weights. EU-OPS 1 Subpart J (1.620.d.1) and the Turkish DGCA’s SHT J (17d.1) allow the use of two different values for pax weights, i.e. “Standard” and “Alternative” pax weights. When preparing the Load Sheet for FHY flights use the “Standard” pax weights and retain these values if the ZFW is within limits. If the ZFW is exceeded with the “Standard” pax weights then use the “Alternate” pax weights as listed below. Definitely should the ZFW never be exceeded! Figures below are i.a.w. EU-OPS 1 SUBPART J (1.620.d.1) and the Turkish DGCA’s SHT J (17d.1.).

Standard Pax Weights Pax Category Holiday Charter Flights Non-Holiday Charter Flights

Adult Male 83 kg 88 kg Adult Female 69 kg 70 kg

Child 35 kg 35 kg Infant 10 kg 10 kg

Alternative Pax Weights Pax Category Holiday Charter Flights Non-Holiday Charter Flights

All Adult 76 kg 84 kg Child 35 kg 35 kg Infant 10 kg 10 kg

Note : The trim section of the Weight & Balance Sheet contains two different scales for Holiday & Non-Holiday Charter Flights.

1.2. Cabin Baggage Weight Yes No

Cabin baggage weight is included in the above mentioned passenger weights.

1.3. Deviations from Standard & Alternate Passenger Weights. If the actual average adult pax weight is known to be higher than 84 kg, the actual average adult pax weight must be used to determine the ZFW. To calculate the ZFW CG, consider the flight as a Non-Holiday Charter flight and use the Index Influence of 1 Pax from the table provided in paragraph 8.2 on C Sheet 9. If the average known adult pax weight is lower than 76 kg, the flight must be considered as Holiday Charter flight, hence use 76 kg as the average adult pax weight. To calculate the ZFW CG, consider the flight as a Holiday Charter flight and use the Index Influence of 1 Pax from the table provided in paragraph 8.2 on C Sheet 9.

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1.4. Checked Baggage Weights

Route Weight Per Piece

Holiday Charter Flights Non-Holiday Charter Flights

All Use Actual Weight Use Actual Weight

13 kg (see note below!) 15 kg (see note below!) Important note: Freebird Airlines requires and uses actual baggage weights to determine Aircraft’s weights and CG. Weight per piece values must only be used if it is not possible to weigh the checked baggage.

2. CREW AND CREW BAGGAGE WEIGHTS

2.1. Crew Weights

Cockpit Crew 85 kg Cabin Crew 75 kg

Yes No Crew hand baggage weight is included in the above crew weights.

2.2. Crew Baggage Weights Short Haul: 15 kg per bag (layover bags) shall be loaded in cargo compartment 1 Long Haul: N/A

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3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS

DOW DOI Remarks

ITEM Included Excluded Included Excluded Basic Weight X X Cockpit Crew X X Cabin Crew X X Crew Hand Baggage X X

Pantry X X Containers X X Pallets X X Portable Water X X Fly-Away kit X X

Remarks: None.

AHM 560 GENERAL

AIRCRAFT DATA C

Sheet 1

EDP-SYSTEM SEMI-PERMANENT-DATA A/C TYPE : A321-231

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1. BALANCE AND SPECIAL INFORMATION-OUTPUT ON LOADSHEET

1.1. Balance Output

Remarks Basic Index BI X Dry Operating Index DOI X Dead-load Index DLI Dead-load MAC MACDLW Loaded Index at Zero Fuel Weight LIZFW X Loaded Index at Take-off Weight LITOW X Loaded Index at Landing Weight LILAW X MAC - at Zero Fuel weight MACZFW X MAC - at Take-off Weight MACTOW X MAC - at Landing Weight MACLAW X Stabilizer Trim setting at Take-off STABTO* X

1.1.1. Passenger Trim Output

Remarks Class trim not applicable Cabin Area Trim X 2nd Priority Seat Row Trim X 1st Priority

1.2 SPECIAL INFORMATION Special information and/or notes to be entered in the lower parts of the EDP Load sheet.

1.2.1 Special Information/Notes to the Captain Freebird Airlines requests the following information to be added in the section Information/ Notes to the Captain: “This A321 of Freebird Airlines is being loaded according the Freebird Airlines A321 AHM560 Issue No.5 dated 03.04.2013”.

AHM 560 GENERAL

AIRCRAFT DATA C

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2. BASIC INDEX AND MAC FORMULA

2.1. Examples and definitions

Index = W x ( Sta – Ref. Sta )

+ K C

% MAC =

C x ( I – K ) + Ref. Sta – LEMAC

W

MAC 100

W : Weight, actual. Sta : Station, horizontal distance in inches or meters from station zero to the location. Ref. Sta : 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 : Constant used as a denominator to convert moment values into index values. I : Index value corresponding to respective weight. MAC : Length of Mean Aerodynamic Chord in inches or meters. LEMAC : Horizontal distance in inches or meters from the station zero to location of the Leading Edge of the MAC.

2.2. Index formula

Ref. Sta. at 23.117 meters from zero K ( constant ) = + 50.0 C ( constant ) = 1000

2.3. MAC information

Length of MAC = 4.1935 meters LEMAC at 22.0687 meters from zero

2.4. Stabilizer trim setting MAC range STAB range

10 12 41 46

4.5 4.5 -3.5 -3.5

Up Up

Down Down

linear variation between 12% and 41%.

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No: 5 Date: 03.04.2013

3. AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT [ ] BASIC WEIGHT [ X ] Note : The standard fleet weight and index shown below should only be used for load

planning purposes and must never be used for the final load-sheet. The load-sheet must always show the actual Basic Weight/Index. If the actual is not shown below it can be obtained from the incoming load-message but must always be checked against the weight schedule on board.

Fleet Basic Empty Weight : 48500 KG (*) Fleet Index : 41.50

Registration Weight Adjustment Index Adjustment

TC-FBG 48501 41.68 TC-FBT 48305 41.25

(*): For the simplicity the BEWFLEET is rounded up to 485000 kg. Note : Notification for data changes at short notice may also be made by means of a data exchange message (AHM 562). ALL WEIGHTS IN KILOGRAM (KG)

AHM 560 GENERAL

AIRCRAFT DATA C

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4. LIMITATIONS

4.1. AIRCRAFT WEIGHT LIMITATIONS Operator defined maximum weights for:

Aircraft Reg./Tail Number Ramp/Taxi Take-off Zero Fuel Landing

TC-FBG 85400 85000 71500 75500 TC-FBT 85400 85000 71500 75500

AHM 560 GENERAL

AIRCRAFT DATA C

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4.2. CG - Limits for Loadsheet Purposes

4.2.1. Take-off Operational CG Limits

FORWARD (Take-off) AFT (Take-off) Applicability Weight Index Value Applicability Weight Index Value

45000 +34.81 47500 +33.19 45000 +42.74 50213 +31.43 47500 +46.13 71000 +20.09 79200 +89.12 83000 +32.69 81800 +92.64

MTOW 85000 +32.06 MTOW 85000 +91.19

4.2.2. ZFW Operational (Loading) CG Limits

FORWARD (Zero Fuel Weight) AFT (Zero Fuel Weight) Applicability Weight Index Value Applicability Weight Index Value

45000 +36.74 45000 +70.82 47500 +35.38 47500 +72.61 62202 +27.36 50287 +74.60 65260 +30.64 MZFW 71500 +88.83 65740 +31.06 66220 +31.35 66700 +31.54 67180 +22.08 70540 +20.25

MZFW 71500 +20.63

Note 1 : For check purposes, per AHM 519, the Load & Trimsheet is attached to the AHM 560. See attachment 1B & 1C.

Note 2: Ferry flight curtailments are provided in Attachement 3 a and the A321 Ferry

Flight Load & Trim sheet is attached as attachment 3 b.

AHM 560 GENERAL

AIRCRAFT DATA C

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5. EFFECT OF FUEL Fuel Loading : Standard Procedure Fuel Density : 0.785 kg/l.

Fuel Weight Index Index (rounded) Fuel Weight Index Index

(rounded) 3500 – 3.72 – 4 12500 – 3.222 – 3 4000 – 4.17 – 4 13000 – 3.879 – 4 4500 – 4.59 – 5 13500 – 4.587 – 5 5000 – 4.99 – 5 14000 – 5.351 – 5 5500 – 5.37 – 5 14500 – 6.137 – 6 6000 – 5.73 – 6 15000 – 6.975 – 7 6500 – 6.07 – 6 15500 – 7.697 – 8 7000 – 6.38 – 6 16000 – 8.481 – 8 7500 – 6.63 – 7 16500 – 9.246 – 9 8000 – 6.79 – 7 17000 – 10.036 – 10 8500 – 6.79 – 7 17500 – 10.805 – 11 9000 – 6.65 – 7 18000 – 11.583 – 12 9500 – 6.41 – 6 18500 – 12.439 – 12 10000 – 6.05 – 6 18605(**) – 12.610 – 13 10500 – 5.54 – 6 11000 – 4.92 – 5 11500 – 4.14 – 4 12000 – 3.18 – 3 12160(*) – 2.845 – 3

(*) : Wing tanks full (**) : all tanks full Remarks : 1. Fuel Weight is in kg with (0.785 Kg/l) 2. By company policy, take-off is not allowed when fuel is less than 3500 kg. Note 1 : Add Fuel index correction (+/–) to the ZFW Index to obtain the TOW Index. Note 2 : The index values in column 1 above is provided for computerized loadsheet systems like the DCS system, which perform precise computations. Since drawing of index values on the manual load and trimsheet lower than whole numbers is not possible, the fuel index table on the manual load and trimsheet contains index values which are mathematically rounded to whole numbers (column 2).

AHM 560 GENERAL

AIRCRAFT DATA C

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6. CREW

6.1. Cockpit Crew Seats and Average Locations

Cockpit Crew seats locations Number of seats

Length of Arm from Reference Station

(m)

Index Influence per kg

Captain & First Officer 2 – 18.032 – 0.018032

Third or fourth occupant(*) 2 – 17.323 – 0.017323 Note(*) : Since it is hard to predict where a third or fourth cockpit crew member may be seated average values are listed for the third and fourth cockpit crew member. Remarks : Crew Members Hand Baggage is included in the Dry Operating Weight (DOW) and in the Dry Operating Index (DOI).

6.2. Cabin Crew Seats and Locations

Cabin Crew seats locations Number of seats

Length of Arm from Reference

Station (m)

Index Influence

per kg

Rear wall of toilet La (pos 1) 2 –15.752 – 0.01575 Fwd of door Nr.2 area RH (pos 4) 1 – 7.415 – 0.00741

Fwd of door Nr.3 area RH (pos 5) 1 + 3.579 +0.00358

Side wall of toilet Le (pos 3) 1 + 15.359 +0.01536

Rear wall of toilet Ld (pos 2) 1 +15.694 +0.01569 Note : When 4 cabin crews on duty : 1 crew seated at Pos 1. 1 crew seated at Pos 2. 1 crew seated at Pos 3. 1 crew seated at Pos 4. When 5 cabin crews on duty : 1 crew seated at Pos 1. 1 crew seated at Pos 2. 1 crew seated at Pos 3. 1 crew seated at Pos 4. 1 crew seated at pos 5. When 6 cabin crews on duty : 2 crew seated at Pos 1. 1 crew seated at Pos 2. 1 crew seated at Pos 3. 1 crew seated at pos 4. 1 crew seated at pos 5.

AHM 560 GENERAL

AIRCRAFT DATA C

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7. GALLEY AND PANTRY

7.1. Galleys

Galley Locations

Length of Arm from Reference Station

(m)


G1 Fwd – 16.472 – 0.01647 G5 Aft +17.018 +0.01702

Remarks : Catering load stored in the galleys is included in the Dry Operating Weight (DOW) and in the Dry Operating Index (DOI)

7.2. Pantry Weight and Pantry Codes

Pantry Code

Pantry Weight (kg)

Total Index

Influence Location / kg

(A) 2-way international 800 + 3.569 G1 (Fwd) / 300 G5 (Aft) / 500 (B) 1-way international 560 + 2.498 G1 (Fwd) / 210 G5 (Aft) / 350 (C) 2-way domestic 450 + 2.133 G1 (Fwd) / 165 G5 (Aft) / 285 (D) 1-way domestic 370 + 2.614 G1 (Fwd) / 110 G5 (Aft) / 260 (E) Ferry Flight 300 + 1.422 G1 (Fwd) / 110 G5 (Aft) / 190

Remarks : Trolleys are included in the pantry weight.

AHM 560 GENERAL

AIRCRAFT DATA C

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8. PASSENGERS AND CABIN Class codes: Class 1 : ----- Class 2 : ----- Class 3 : Y

8.1. Passenger Seats

Cabin Section

Number of Seats Total per Cabin Section Row numbers Class 1 Class 2 Class 3

0A 01-09 53 53 0B 10-23 77 77 0C 24-35 72 72

Sub–Total = 202 Total per Class = 202

8.2. Class / Cabin Section

Cabin Section

Length of arm from reference station


Index Influence of 1 Pax

Holiday Charter Flights

Non-Holiday Charter Flights

OA –10.956 – 0.01096 – 0.83266 – 0.92030 OB –1.269 – 0.00127 – 0.09644 – 0.10660 OC +9.738 + 0.00974 + 0.74009 + 0.81799

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AIRCRAFT DATA C

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8.3. Cabin Seating Layout A = Aisle B = Bassinet Position C = Crew 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 Alpha Characters “D”, “F”, “R” are blank, not used.

AHM 560 GENERAL

AIRCRAFT DATA C

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8.3.1. TC-FBG & TC-FBT Seat Plan Layout / Facilities and Row Index Influence

Cabin Section

Row No.

Row Letter Index Influence per Seat Row

per 1kg A B C D E F

OA

01 NTL NTL NTLA NTLA NTL NTL –0.01412 02 NL NL NAL NAL NL NL –0.01331 03 NL NL NAL NAL NL NL –0.01249 04 NUIH N NA NA N NUH –0.01168 05 NUIH N NA NA N NUH –0.01087 06 NUIH N NA NA N NUH –0.01008 07 NUIH N NA NA N NUH –0.00929 08 NI N NA NA N N –0.00851 09 N N NA NA N CE –0.00772

OB

10 NLE NLE NLEA NLEA NLE NLE –0.00586 11 NI N NA NA N N –0.00508 12 NI N NA NA N N –0.00429 14 NI N NA NA N N –0.00350 15 NI N NA NA N N –0.00271 16 NI N NA NA N N –0.00195 17 NI N NA NA N N –0.00119 18 NI N NA NA N N –0.00043 19 NI N NA NA N N +0.00033 20 NI N NA NA N N +0.00110 21 NI N NA NA N N +0.00186 22 NI N NA NA N N +0.00262 23 N N NA NA N CE +0.00338

OC

24 NLE NLE NLEA NLEA NLE NLE +0.00544 25 NI N NA NA N N +0.00623 26 NI N NA NA N N +0.00701 27 NI N NA NA N N +0.00780 28 NI N NA NA N N +0.00859 29 NHI N NA NA N NH +0.00938 30 NHI N NA NA N NH +0.01016 31 NHI N NA NA N NH +0.01093 32 NHI N NA NA N NH +0.01169 33 NHI N NA NA N NH +0.0124534 NI N NA NA N N +0.01321 35 N N NA NA N N +0.01397

Note : Row number 13 does NOT exist on both TC-FBG and TC-FBT registered aircrafts. Restrictions: • WCHC Row 4, 5 A seat. • Only 1 PRM per row.

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AIRCRAFT DATA C

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9. DETAILS FOR COMPARTMENT TRIM

Compartment Number Description

Maximum Capacity Index value

per 1 kg Gross Weight (kg)

Volume (m3)

Max. Distributed

Load (kg/m2)

1 Forward Cargo Hold 5670

8.531 732 –0.01146

2 Forward Cargo Hold 13.585 732 –0.00755

3 Aft Cargo Hold 5670

14.147 732 +0.00588

4 Aft Cargo Hold 8.108 732 +0.01007

5 Rear (Bulk) Cargo Hold 1497 5.880 732 +0.01315

9.1. Combined Load limitations Not Applicable.

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AIRCRAFT DATA C

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10. DETAILS FOR BAY/SECTION TRIM

Maximum capacity

Bay/Section Gross Weight Volume * Index value per kg

BULK

11 1013 3.882 –0.01237

12 1189 4.649 –0.01068

21 1189 4.649 –0.00908

22 1189 4.649 –0.00748

23 1090 4.287 –0.00595

31 1289 5.094 +0.00430

32 1177 4.649 +0.00598

33 1121 4.404 +0.00758

41 919 3.489 +0.00918

42 1164 4.619 +0.01078

51 374 1.460 +0.01185

52 353 1.380 +0.01265

53 770 3.040 +0.01401 * Volume information required for bulk compartments only.

11. BALLAST Fixed provisions for carrying ballast. Not Applicable.

AHM 560 GENERAL

LOAD PLANNING DATA D

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1. CG LIMITS 1.1. Ideal Trim Line at ZFW for Fuel Saving purposes The DESIRED 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 desired trim line shall be entered in the table below. Freebird Airlines aim is to obtain a TOW CG within the 24 – 28 % MAC. 2. UNIT LOAD DEVICES DETAILS Not Applicable. 3. SPECIAL LOAD For Special Load handling, please consult FHY Ground Operations Manual.

AHM 560 GENERAL

LOAD PLANNING DATA D

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4. STANDARD PAX & LOAD DISTRIBUTION FOR LOAD PLANNING Freebird Airlines uses table below for standard load planning. The goal of this empirical data is to achieve an ideal stabilizer pitch trim setting, with the TO CG between 24 - 28 % MAC. Table is established using standard and alternate pax weights with 15 kg of checked-in baggage per pax for holiday charter flights and 25 kg for non-holiday charter flights. Other combinations of loading or pax seating may be acceptable provided that the warning below and the loading & off-loading instructions below are respected.

Warning : To avoid ground instability, DO NOT leave cargo compartments 1 or 2 empty when there are more than 30 pax on board! Notes : 1. LMC loading should be evenly distributed between the cargo compartments 1 and 2 on one side and 3 and 4 on the other side when it exceeds 250 kg. 2. "Free -Seating" is NOT allowed without approval of the Pilot in Command. 5. LOADING & OFF-LOADING With respect to aircraft’s ground stability, at all times forward cargo compartments 1 & 2 MUST be loaded first and off-loaded last!

AHM 560 GENERAL

DOW & DOI Table Attachment 1A


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Issue No: 5 Date: 03.04.2013

DOW & DOI table of TC-FBG.

TC - FBG

Pantry Code

Crew Composition

A B C D E

Cockpit Cabin DOW DOI DOW DOI DOW DOI DOW DOI DOW DOI

2 0 49471 42.18 49231 41.11 49121 40.75 49041 41.23 48971 40.04

2 1 49306 41.00 49306 39.93 49196 39.57 49116 40.05 49046 38.86

2 2 49621 39.82 49381 38.75 49271 38.39 49191 38.87 49121 37.67

2 3 49696 41.60 49456 40.53 49346 40.16 49266 40.64 49196 39.45

2 4 49771 41.87 49531 40.80 49421 40.43 49341 40.91 49271 39.72

2 5 49846 43.04 49606 41.97 49496 41.61 49416 42.09 49346 40.90

2 6 49921 41.86 49681 40.79 49571 40.43 49491 40.91 49421 39.72

3 0 49556 40.71 49316 39.64 49206 39.28 49126 39.76 49056 38.56

3 1 49631 39.53 49391 38.46 49281 38.09 49201 38.57 49131 37.38

3 2 49706 38.35 49466 37.28 49356 36.91 49276 37.39 49206 36.20

3 3 49781 40.13 49541 39.06 49431 38.69 49351 39.17 49281 37.98

3 4 49856 40.39 49616 39.32 49506 38.96 49426 39.44 49356 38.25

3 5 49931 41.57 49691 40.50 49581 40.14 49501 40.62 49431 39.42

3 6 50006 40.39 49766 39.32 49656 38.95 49576 39.43 49506 38.24

4 0 49641 39.24 49401 38.17 49291 37.80 49211 38.28 49141 37.09

4 1 49716 38.06 49476 36.99 49366 36.62 49286 37.10 49216 35.91

4 2 49791 36.88 49551 35.81 49441 35.44 49361 35.92 49291 34.73

4 3 49866 38.65 49626 37.58 49516 37.22 49436 37.70 49366 36.51

4 4 49941 38.92 49701 37.85 49591 37.49 49511 37.97 49441 36.78 4 5 50016 40.10 49776 38.66 49666 38.66 49586 39.14 49516 37.95 4 6 50091 38.92 49851 37.96 49741 37.48 49661 37.96 49591 36.77

Pantry Codes A : 2-Way International B : 1-Way International C : 2-Way Domestic D : 1-Way Domestic E : Ferry Flight

AHM 560 GENERAL

DOW & DOI Table Attachment 1B


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DOW & DOI table of TC-FBT.

TC - FBT

Pantry Code

Crew Composition A B C D E

Cockpit Cabin DOW DOI DOW DOI DOW DOI DOW DOI DOW DOI

2 0 49275 41.75 49035 40.68 48925 40.31 48845 40.79 48775 39.60

2 1 49350 40.57 49110 39.50 49000 39.13 48920 39.61 48850 38.42

2 2 49425 39.39 49185 38.32 49075 37.95 48995 38.43 48925 37.24

2 3 49500 41.16 49260 40.09 49150 39.73 49070 40.21 49000 39.02

2 4 49575 41.43 49335 40.36 49225 40.00 49145 40.48 49075 39.29

2 5 49650 42.61 49410 41.54 49300 41.17 49220 41.65 49150 40.46

2 6 49725 41.43 49485 40.36 49375 39.99 49295 40.47 49225 39.28

3 0 49360 40.28 49120 39.21 49010 38.84 48930 39.32 48860 38.13

3 1 49435 39.10 49195 38.02 49085 37.66 49005 38.14 48935 36.95

3 2 49510 37.91 49270 36.84 49160 36.48 49080 36.96 49010 35.77

3 3 49585 39.69 49345 38.62 49235 38.26 49155 38.74 49085 37.54

3 4 49660 39.96 49420 38.89 49310 38.52 49230 39.00 49160 37.81

3 5 49735 41.14 49495 40.07 49385 39.70 49305 40.18 49235 38.99

3 6 49810 39.96 49570 38.88 49460 38.52 49380 39.00 49310 37.81

4 0 49445 38.80 49205 37.73 49095 37.37 49015 37.85 48945 36.66

4 1 49520 37.62 49280 36.55 49170 36.19 49090 36.67 49020 35.48

4 2 49595 36.44 49355 35.37 49245 35.01 49165 35.49 49095 34.29

4 3 49670 38.22 49430 37.15 49320 36.78 49240 37.26 49170 36.07

4 4 49745 38.49 49505 37.42 49395 37.05 49315 37.53 49245 36.34 4 5 49820 39.66 49580 38.59 49470 38.23 49390 38.71 49320 37.52 4 6 49895 38.48 49655 37.41 49545 37.05 49465 37.53 49395 36.34

Pantry Codes A : 2-Way International B : 1-Way International C : 2-Way Domestic D : 1-Way Domestic E : Ferry Flight

AHM 560 GENERAL

LOAD & TRIM SHEET Attachment 2A


Carrier

FH/FHY

Signature:

Issue No: 5 Date: 03.04.2013

AHM 560 GENERAL

FERRY LOAD & TRIM SHEET Attachment 3A


Carrier

FH/FHY

Signature:

Issue No: 5 Date: 03.04.2013

IMPORTANT : Following limits apply for FERRY FLIGHTS ONLY! (For normal operational CG limits, see C Sheet 5)

1. Ferry Flight CG - Limits for Loadsheet Purposes.

1.1. Ferry Flight Take-off CG Limits.

FORWARD (Take-off) AFT (Take-off) Applicability Weight Index Value Applicability Weight Index Value

45000 + 27.07 45000 + 49.85 71000 + 12.90 79000 + 95.96 83000 + 25.50 81800 + 99.76

MTOW 85000 + 24.87 MTOW 85000 + 98.30

1.2. Ferry Flight ZFW (Loading) CG Limits.

FORWARD (Zero Fuel Weight) AFT (Zero Fuel Weight) Applicability Weight Index Value Applicability Weight Index Value

45000 29.48 45000 78.22 62202 20.10 MZFW 71500 96.00 65160 23.28 65640 23.73 66120 24.04 66600 24.25 67080 14.88 70920 12.78 71400 13.17

MZFW 71500 13.27 Note : For check purposes, per AHM 519, The Load & Trimsheet for Ferry Flights is attached to the AHM 560. See attachment 3B

AHM 560 GENERAL

FERRY LOAD & TRIM SHEET Attachment 3B


Carrier

FH/FHY

Signature:

Issue No: 5 Date: 03.04.2013

FHYA321AHM560 Rev.5 03.04 · PRESENT A321-231 FLEET (ALL 202 Y) REGISTRATION MODEL TC – FBG...

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