ahm 560 - freebird · pdf fileahm 560 . present a320-200 fleet (all 180 y) registration model...

FREEBIRD AIRLINES (FH/FHY)

AHM 560

PRESENT A320-200 FLEET

(ALL 180 Y)

REGISTRATION MODEL

TC – FBH A320-214 with MSN 4207

TC – FBJ A320-232 with MSN 0580

TC – FBO A320-214 with MSN 5096

TC – FBR A320-232 with MSN 2524

TC – FBV A320-214 with MSN 4658

TC – FHE A320-232 with MSN 2804

Reason(s) for issue No 10:

1. New aircraft, TC-FHE MSN 2804, joint Freebird Airlines A320 fleet. 2. Checked bagage weights corrected to EU-OPS standard weights. 3. 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 A320 AHM560 Issue No.10, dated 26.02.2013.

4. ZFW and Take-Off Operational CG limits 5. Fuel effect 6. Passengers and Cabin 7. DOW / DOI tables corrected of the A320 Freebird Airlines fleet.

Mrs. Zehra Ceren Flight Operations Engineer

& Capt. Auke van Ginkel Freebird Airlines Antalya, 26.02.2013

AHM 560 GENERAL

COMMUNICATION

ADDRESSES A

Sheet 1

EDP-SYSTEM SEMI-PERMANENT-DATA

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Issue No:10 Date: 26.02.2013

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 : CAPTAIN AUKE VAN GINKEL FREEBIRD AIRLINES GUZELOBA MAHALLESI BARNIKLAR BULVARI No: 156/A-B 07230 LARA – ANTALYA TURKEY PHONE : +90 – 242 – 330 3410 Ext 117 : +90 – 533 – 601 8917 (mobile) FAX : +90 – 242 – 330 3405 SITA : ISTFBFH (General) AYTFOFH (OCC Anyalya) E-MAIL : [email protected] [email protected]

AHM 560 GENERAL

COMMUNICATION

ADDRESSES A

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Issue No:10 Date: 26.02.2013

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 MVT 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 A320-200 fleet is configured class: Y

AHM 560 GENERAL

LIST OF REVISIONS A

Sheet 3

EDP-SYSTEM SEMI-PERMANENT-DATA A320-200 AHM560

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Issue No:10 Date: 26.02.2013

List of Revisions: FHY A320 AHM560 Issue No.1 ….. FHY A320 AHM560 Issue No.2 ….. FHY A320 AHM560 Issue No.3 03.08.2006 FHY A320 AHM560 Issue No.4 10.04.2009 FHY A320 AHM560 Issue No.5 05.07.2009 FHY A320 AHM560 Issue No.6 24.02.2010 FHY A320 AHM560 Issue No.7 14.03.2010 FHY A320 AHM560 Issue No.8 24.04.2011 FHY A320 AHM560 Issue No.9 30.04.2012 FHY A320 AHM560 Issue No.10 30.02.2013 Always update complete document!

AHM 560 GENERAL

LIST OF EFFECTIVE SHEETS A

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Issue No:10 Date: 26.02.2013

List of Effective Sheets: A Sheet 1 Communication Addresses Issue No. 10 26.02.2013 A Sheet 2 Communication Addresses Issue No. 10 26.02.2013 A Sheet 3 List of Revisions Issue No. 10 26.02.2013 A Sheet 4 List of Effective Sheets Issue No. 10 26.02.2013 B Sheet 1 General Information Issue No. 10 26.02.2013 B Sheet 2 General Information Issue No. 10 26.02.2013 B Sheet 3 General Information Issue No. 10 26.02.2013 C Sheet 1 Aircraft Data Issue No. 10 26.02.2013 C Sheet 2 Aircraft Data Issue No. 10 26.02.2013 C Sheet 3 Aircraft Data Issue No. 10 26.02.2013 C Sheet 4 Aircraft Data Issue No. 10 26.02.2013 C Sheet 5 Aircraft Data Issue No. 10 26.02.2013 C Sheet 6 Aircraft Data Issue No. 10 26.02.2013 C Sheet 7 Aircraft Data Issue No. 10 26.02.2013 C Sheet 8 Aircraft Data Issue No. 10 26.02.2013 C Sheet 9 Aircraft Data Issue No. 10 26.02.2013 C Sheet 10 Aircraft Data Issue No. 10 26.02.2013 C Sheet 11 Aircraft Data Issue No. 10 26.02.2013 C Sheet 12 Aircraft Data Issue No. 10 26.02.2013 C Sheet 13 Aircraft Data Issue No. 10 26.02.2013 D Sheet 1 Load Planning data Issue No. 10 26.02.2013 D Sheet 2 Load Planning data Issue No. 10 26.02.2013 Attachment 1A DOW & DOI Tables –H Issue No. 10 26.02.2013 Attachment 1B DOW & DOI Tables –J Issue No. 10 26.02.2013 Attachment 1C DOW & DOI Tables –O Issue No. 10 26.02.2013 Attachment 1D DOW & DOI Tables –R Issue No. 10 26.02.2013 Attachment 1E DOW & DOI Tables –V Issue No. 10 26.02.2013 Attachment 1F DOW & DOI Tables –HE Issue No. 10 26.02.2013 Attachment 2a Load & Trim Sheet Rev.6 Issue No. 10 26.02.2013 Attachment 2b Load & Trim Sheet Rev.6 Issue No. 10 26.02.2013

AHM 560 GENERAL

GENERAL INFORMATION B

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Issue No:10 Date: 26.02.2013

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.

AHM 560 GENERAL


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Issue No:10 Date: 26.02.2013

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 weight 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

AHM 560 GENERAL


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Issue No:10 Date: 26.02.2013

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 : A320-200

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Issue No:10 Date: 26.02.2013

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 A320 of Freebird Airlines is being loaded according the Freebird Airlines A320 AHM560 Issue No.10 dated 26.02.2013”.

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

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 18.850 meters from zero K ( constant ) = + 50.0 C ( constant ) = 1000

2.3. MAC information

Length of MAC = 4.1935 meters LEMAC at 17.8015 meters from zero

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

2.4. Stabilizer trim setting

MAC range STAB range

10.5 17 40 43

2.5 2.5 -2.5 -2.5

Up Up Down Down

Linear variation between 17% and 40%. Stabilizer change per 1% MAC, 0.217 degrees.

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 Empty 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 Weight : 42500 KG (*) Fleet Index: 53.82

Registration Weight Adjustment

Index Adjustment Registration Weight

Adjustment Index

Adjustment TC-FBH 42244 55.94 TC-FBV 42603 56.16 TC-FBJ 42365 52.77 TC-FHE 42755 51.01 TC-FBO 42528 56.36 TC-FBR 42428 50.67

(*): For the simplicity the OEWFLEET = 42487 kg is rounded up to 42500 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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Issue No:10 Date: 26.02.2013

4. LIMITATIONS

4.1. AIRCRAFT WEIGHT LIMITATIONS Operator defined maximum weights for:

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

4207 / TC-FBH 77400 77000 61000 64500 0580 / TC-FBJ 77400 77000 61000 64500 5096 / TC-FBO 77400 77000 62500 66000 2524 / TC-FBR 77400 77000 62500 66000 4568 / TC-FBV 77400 77000 62500 66000 2804 / TC-FHE 77400 77000 62500 66000

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

4.2. CG - Limits for Loadsheet Purposes

4.2.1. ZFW Operational CG Limits

FORWARD (ZFW) AFT (ZFW) Applicability Weight Index Value Applicability Weight Index Value

37230 46.27 37230 68.48

40000 44.90 40000 70.46

47880 40.90 57900 80.77

53400 41.37 TC-FB… -H/-J 61000 82.85

55300 40.79 TC-FB…

-O/-R/-V TC-FHE

62500 83.52

60120 41.08 TC-FB… -H/-J 61000 40.76

TC-FB… -O/-R/-V TC-FHE

62500 40.28

4.2.2. Take-Off Operational CG Limits

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

37230 44.63 37230 60.63 40000 43.31 40000 62.71 53000 37.10 47500 65.79 63000 38.10 57900 80.77 72000 35.09 72100 90.30 73500 40.44 MTOW 77000 82.25

MTOW 77000 68.93

Note : For check purposes, per AHM 519, the Load & Trimsheet is attached to the AHM 560. See attachment 2A & 2B.

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

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 + 1.09 + 1 12500 - 1.59 - 2 4000 + 0.58 + 1 13000 - 2.12 - 2 4500 + 0.10 0 13500 - 2.77 - 3 5000 - 0.37 0 14000 - 3.49 - 4 5500 - 0.81 - 1 14500 - 4.26 - 4 6000 - 1.23 - 1 15000 - 5.04 - 5 6500 - 1.63 - 2 15500 - 5.82 - 6 7000 - 2.00 - 2 16000 - 6.59 - 7 7500 - 2.36 - 2 16500 - 7.37 - 7 8000 - 2.68 - 3 17000 - 8.15 - 8 8500 - 2.99 - 3 17500 - 8.92 - 9 9000 - 3.23 - 3 18000 - 9.70 - 10 9500 - 3.33 - 3 18500 - 10.50 - 11 10000 - 3.31 - 3 18730(**) - 11.14 - 11 10500 - 3.15 - 3 19000 – 11.09 - 11 11000 - 2.86 - 3 FULL(***) – 11.09 - 11 11500 - 2.44 - 2 12000 - 1.92 - 2 12254(*) – 1.75 - 2

(*) : Wing tanks full (**) : all tanks full, TC-FB…-J/-R, TC-FHE (***) : all tanks full, TC-FB…-H/-O/-V Remarks : 1. Fuel Weight is in kg. with ( 0.785 kg./l ) 2. By company policy, take-off is not allowed when Take-off 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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Issue No:10 Date: 26.02.2013

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 – 13.765 – 0.013765

Third or fourth occupant(*) 2 – 13.055 – 0.013055 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 Baggage and Navigation Bags are 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


(m)


Rear wall of toilet La (pos 1) 2 – 11.4643 – 0.01146 Rear wall of toilet Ld (pos 2) 1 + 13.0168 + 0.01302 Rear wall of toilet Le (pos 3) 2 + 12.9916 + 0.01299 Side wall of toilet Le (pos 4) 1 + 12.7376 + 0.01274

Note : When 4 cabin crews on duty : 2 crews seated at Pos 1. 1 crew seated at Pos 2. 1 crew seated at Pos 3. When 5 cabin crews on duty : 2 crews seated at Pos 1. 1 crew seated at Pos 2. 2 crews seated at Pos 3. When 6 cabin crews on duty : 2 crews seated at Pos 1. 1 crew seated at Pos 2. 2 crews seated at Pos 3. 1 crew seated at pos 4.

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

7. GALLEY AND PANTRY

7.1. Galleys

Galley Locations


(m)


G1 Fwd – 12.172 – 0.01217 G5 Aft + 14.282 + 0.01428

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 3.489 G1 (Fwd) / 300 G5 (Aft) / 500 (B) 1-way international 560 2.442 G1 (Fwd) / 210 G5 (Aft) / 350 (C) 2-way domestic 450 2.062 G1 (Fwd) / 165 G5 (Aft) / 285 (D) 1-way domestic 370 2.374 G1 (Fwd) / 110 G5 (Aft) / 260 (E) Ferry Flight 300 1.375 G1 (Fwd) / 110 G5 (Aft) / 190

Remarks : Trolleys are included in the pantry weight.

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

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 01-10 60 60 0B 11-20 60 60 0C 21-30 60 60

Sub–Total = 180 Total per Class = 180

8.2. Class / Cabin Section

Cabin section


(m)


Index Influence of 1 Pax

Holiday Charter Flights

Non-Holiday Charter Flights

0A – 6.56983 – 0.006568 – 0.49919 – 0.55174 0B + 1.01867 + 0.001017 + 0.07727 + 0.08540 0C + 8.21233 + 0.008213 + 0.62421 + 0.68992

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

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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Issue No:10 Date: 26.02.2013

8.3.1. FHY A320 Fleet Seat Plan Layout / Facilities and Row Index Influence TC-FBH, TC-FBJ, TC-FBR, TC-FBV, TC-FBO and TC-FHE.

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 -0.00988 02 N N NA NA N N -0.00914 03 N N NA NA N N -0.00840 04 NHIU N NA NA N NHIU -0.00767 05 NHIU N NA NA N NHIU -0.00693 06 NHIU N NA NA N NHIU -0.00620 07 NHIU N NA NA N NHIU -0.00547 08 NI N NA NA N NI -0.00473 09 NI N NA NA N NI -0.00400 10 NI N NA NA N NI -0.00328

OB

11 N N NA NA N N -0.00251 12 NE NE NEA NEA NE NE -0.00163 13 NE NE NEA NEA NE NE -0.00073 14 N N NA NA N N 0.00000 15 NI N NA NA N NI 0.00073 16 NI N NA NA N NI 0.00145 17 NI N NA NA N NI 0.00216 18 NI N NA NA N NI 0.00287 19 NI N NA NA N NI 0.00358 20 NI N NA NA N NI 0.00429

OC

21 NI N NA NA N NI 0.00500 22 NI N NA NA N NI 0.00571 23 NI N NA NA N NI 0.00642 24 NHI N NA NA N NHI 0.00713 25 NHI N NA NA N NHI 0.00785 26 NHI N NA NA N NHI 0.00856 27 NHI N NA NA N NHI 0.00928 28 N N NA NA N N 0.01000 29 N N NA NA N N 0.01072 30 NT NT NTA NTA NT NT 0.01145

Restrictions:

• WCHC Row 4, 5 A seat. • Only 1 PRM per row

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

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 FWD 3402 13.28 732 – 0.00642 3 ALF 2426 9.76 732 + 0.00401 4 ALA 2110 8.50 732 + 0.00741 5 BLK 1497 5.88 732 + 0.01048

Security Locker (DIP)

9.1. Combined Load limitations Not Applicable.

AHM 560 GENERAL

AIRCRAFT DATA C

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Issue No:10 Date: 26.02.2013

10. DETAILS FOR BAY/SECTION TRIM

Maximum capacity

Bay/Section Gross Weight (kg)

Volume (m3 )* Index value per 1 kg

Bulk 3.882

FWD / 11 1045

13.28 – 0.00811

FWD / 12 1225 – 0.00642

FWD / 13 1132 – 0.00488

ALF / 31 1301 9.76.380 + 0.00324

ALF / 32 1125 + 0.00491

ALA / 41 928 8.50 + 0.00651

ALA / 42 1182 + 0.00811

BLK / 51 374

5.88 + 0.00918

BLK / 52 353 + 0.00998

BLK / 53 770 + 0.01133

* Volume information required for bulk compartments only.

11. BALLAST Not Applicable.

AHM 560 GENERAL

LOAD PLANNING DATA D

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Issue No:10 Date: 26.02.2013

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 is 29% MAC TO CG shall is entered in the table below.

Weight Index Value 40000 56.75 47500 58.00 61000 64.00 62500 65.00

2. UNIT LOAD DEVICES DETAILS Not Applicable. 3. SPECIAL LOAD For Special Load handling, please consult FHY Ground Operations Manual. Only TC-FBO and TC-FBV are available for live animal transportation in cargo compartments 3 and 4.

AHM 560 GENERAL

LOAD PLANNING DATA D

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Issue No:10 Date: 26.02.2013

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 around 29% MAC. The aim of Freebird is to have a Take-Off CG between 27 – 31% MAC. Table is established using standard and alternate pax weights with 15 kg of checked-in baggage per pax for holiday charter flights and 20 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.

Total Number of Pax to Seat

Pax Seating in Cabin Section Load Distribution In Compartment

(% of Total Load)

OA OB OC 1 3 4

Up to 25 -- 0 - 25 -- 40% 30% 30%

26 - 40 -- 25 1 - 15 40% 30% 30%

41 - 50 1 - 10 25 15 40% 30% 30%

51 - 75 20 16 - 40 15 40% 30% 30%

76 - 100 25 36 - 60 15 40% 30% 30%

101 - 125 35 36 -60 30 40% 30% 30%

126 - 150 45 36 - 60 45 40% 30% 30%

151 - 180 60 31 - 60 60 40% 30% 30%

Max. Capacity = 60 Pax 60 Pax 60 Pax 3402 kg 2426 kg 2110 kg Note 1 : Free seating is not allowed without pre-confirmation and approval of the Pilot in Command. Note 2 : Fill Cargo Compartment 5 (capacity = 1497 kg) when other Compartments are full. 5. LOADING & OFF-LOADING With respect to aircraft’s ground stability, at all times forward cargo compartment 1 MUST be loaded first and off-loaded last!

AHM 560 GENERAL

DOW & DOI Table Attachment 1A


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Issue No:10 Date: 26.02.2013

DOW & DOI table of TC-FBH. Basic Weight = 42244 kg Basic Index = 55.94

42244 55.94 TC - FBH

Pantry Code

Crew Composition

A 2-way Int.

B 1-way Int.

C 2-way Dom.

D 1-way Dom.

E Ferry

Cockpit Cabin DOW DOI DOW DOI DOW DOI DOW DOI DOW DOI 2 0 43214 57.09 42974 56.04 42864 55.66 42784 55.97 42714 54.97 2 1 43289 56.22 43049 55.18 42939 54.80 42859 55.11 42789 54.11 2 2 43364 57.20 43124 56.15 43014 55.77 42934 56.08 42864 55.08 2 3 43439 58.18 43199 57.13 43089 56.75 43009 57.06 42939 56.06 2 4 43514 57.31 43274 56.27 43164 55.88 43084 56.20 43014 55.20 2 5 43589 58.29 43349 57.24 43239 56.86 43159 57.17 43089 56.17 2 6 43664 59.24 43424 58.19 43314 57.81 43234 58.13 43164 57.13 3 0 43299 55.98 43059 54.93 42949 54.55 42869 54.86 42799 53.86 3 1 43374 55.12 43134 54.07 43024 53.69 42944 54.00 42874 53.00 3 2 43449 56.09 43209 55.04 43099 54.66 43019 54.97 42949 53.98 3 3 43524 57.07 43284 56.02 43174 55.64 43094 55.95 43024 54.95 3 4 43599 56.20 43359 55.16 43249 54.77 43169 55.09 43099 54.09 3 5 43674 57.18 43434 56.13 43324 55.75 43244 56.06 43174 55.06 3 6 43749 58.13 43509 57.09 43399 56.70 43319 57.02 43249 56.02 4 0 43384 54.87 43144 53.82 43034 53.44 42954 53.75 42884 52.76 4 1 43459 54.01 43219 52.96 43109 52.58 43029 52.89 42959 51.89 4 2 43534 54.98 43294 53.93 43184 53.55 43104 53.86 43034 52.87 4 3 43609 55.96 43369 54.91 43259 54.53 43179 54.84 43109 53.84 4 4 43684 55.09 43444 54.05 43334 53.67 43254 53.98 43184 52.98 4 5 43759 56.07 43519 55.02 43409 54.64 43329 54.95 43259 53.95 4 6 43834 57.02 43594 55.98 43484 55.59 43404 55.91 43334 54.91

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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Issue No:10 Date: 26.02.2013

DOW & DOI table of TC-FBJ. Basic Weight = 42365 kg Basic Index = 52.77

42365 52.77 TC - FBJ

Pantry Code

Crew Composition

A 2-way Int.

B 1-way Int.

C 2-way Dom.

D 1-way Dom.

E Ferry



AHM 560 GENERAL

DOW & DOI Table Attachment

1C


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Issue No:10 Date: 26.02.2013

DOW & DOI table of TC-FBO. Basic Weight = 42528 kg Basic Index = 56.36

42527 56.36 TC - FBO

Pantry Code

Crew Composition

A 2-way Int.

B 1-way Int.

C 2-way Dom.

D 1-way Dom.

E Ferry



AHM 560 GENERAL

DOW & DOI Table Attachment 1D


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Issue No:10 Date: 26.02.2013

DOW & DOI table of TC-FBR. Basic Weight = 42428 kg Basic Index = 50.67

42428 50.67 TC - FBR

Pantry Code

Crew Composition

A 2-way Int.

B 1-way Int.

C 2-way Dom.

D 1-way Dom.

E Ferry

Cockpit Cabin DOW DOI DOW DOI DOW DOI DOW DOI DOW DOI 2 0 43398 51.82 43158 50.77 43048 50.39 42968 50.70 42898 49.70 2 1 43473 50.95 43233 49.91 43123 49.53 43043 49.84 42973 48.84 2 2 43548 51.93 43308 50.88 43198 50.50 43118 50.81 43048 49.81 2 3 43623 52.91 43383 51.86 43273 51.48 43193 51.79 43123 50.79 2 4 43698 52.04 43458 51.00 43348 50.61 43268 50.93 43198 49.93 2 5 43773 53.02 43533 51.97 43423 51.59 43343 51.90 43273 50.90 2 6 43848 53.97 43608 52.92 43498 52.54 43418 52.86 43348 51.86 3 0 43483 50.71 43243 49.66 43133 49.28 43053 49.59 42983 48.59 3 1 43558 49.85 43318 48.80 43208 48.42 43128 48.73 43058 47.73 3 2 43633 50.82 43393 49.77 43283 49.39 43203 49.70 43133 48.71 3 3 43708 51.80 43468 50.75 43358 50.37 43278 50.68 43208 49.68 3 4 43783 50.93 43543 49.89 43433 49.50 43353 49.82 43283 48.82 3 5 43858 51.91 43618 50.86 43508 50.48 43428 50.79 43358 49.79 3 6 43933 52.86 43693 51.82 43583 51.43 43503 51.75 43433 50.75 4 0 43568 49.60 43328 48.55 43218 48.17 43138 48.48 43068 47.49 4 1 43643 48.74 43403 47.69 43293 47.31 43213 47.62 43143 46.62 4 2 43718 49.71 43478 48.66 43368 48.28 43288 48.59 43218 47.60 4 3 43793 50.69 43553 49.64 43443 49.26 43363 49.57 43293 48.57 4 4 43868 49.82 43628 48.78 43518 48.40 43438 48.71 43368 47.71 4 5 43943 50.80 43703 49.75 43593 49.37 43513 49.68 43443 48.68 4 6 44018 51.75 43778 50.71 43668 50.32 43588 50.64 43518 49.64 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 1E


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Issue No:10 Date: 26.02.2013

DOW & DOI table of TC-FBV. Basic Weight = 42603 kg Basic Index = 56.16

42603 56.16 TC - FBV

Pantry Code

Crew Composition

A 2-way Int.

B 1-way Int.

C 2-way Dom.

D 1-way Dom.

E Ferry



AHM 560 GENERAL

DOW & DOI Table Attachment 1F


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Issue No:10 Date: 26.02.2013

DOW & DOI table of TC-FHE. Basic Weight = 42755 kg Basic Index = 51.01

TC - FHE

Pantry Code

Crew Composition

A 2-way Int.

B 1-way Int.

C 2-way Dom.

D 1-way Dom.

E Ferry



AHM 560 GENERAL

LOAD & TRIM SHEET Attachment 2A


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Issue No:10 Date: 26.02.2013

AHM 560 GENERAL

FHY EFB LOAD & TRIM SHEET Attachment 2C


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Issue No:10 Date: 26.02.2013

ahm 560 - freebird · pdf fileahm 560 . present a320-200 fleet (all 180 y) registration model...

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