ahm 560 - Aircraft Weight & Balance F100.pdf · AHM 560 IATA AHM DATA F100 Issue No. 6-1 ... PSM Passenger Service Message > Recommended Practice 1715 ... DOW / DOI / Balance Table

AHM 560IATA AHM DATA F100

Issue No. 6-1

14-Jun-17

Ground ServicesAircraft Handling Policies

Montenegro Airlines

AHM 560

A Sheet 1

CarrierYM

1.

REMARKS:

2.

REMARKS:

deleted

www.aircraftweightbalance.comIWB ™ V.Zivkovic DEM 0MGX Vladimir Novosel / Ground Ops Mgr. UFN14-Jun-17

See LIST OF REVISIONS page A3

Balance Table:

Completed sheets and changes of basic data and procedure must be forwarded to:

Verified by:

Main Changes:

Legend : ∆ - changed □ - added

Issue No. 6-1Completed by:

Amended C10 page - NOTE: Emergency EXIT rows

CARRIER's CONTACT ADDRESS

TGDOWYM

Airport Podgorica, ME, Montenegro

EDP-SYSTEM SEMI-PERMANENT DATA

COMMUNICATION ADDRESSES

SUPPLIER's CONTACT ADDRESS

MAILING ADDRESS:

E-MAIL ADDRESS:

TELETYPE ADDRESS:

MAILING ADDRESS:Flight Operation Department

TELETYPE ADDRESS:

E-MAIL ADDRESS:

[email protected]

AHM 560

A Sheet 2Carrier

YM

3.√ (tick as required)

4.√

LOADSHEET



PRL Passenger Reconcile List

PSM Passenger Service Message > Recommended Practice 1715 (dispatch only)

MESSAGE REQUIREMENTS (tick as required )

LIR LOADING INSTRUCTION REPORT

LPM Load Planning Message AHM 580

ALI Abbreviated Load Information Message AHM 584CPM Container / Pallet Distribution Message AHM587

IDM Industry Discount Message > Recommended Practice 1714

AUTOMATICALLY PRODUCED DOCUMENTS

PIL PASSENGER INFO LISTLOAD PLANSEAT PLAN

PNL/ADL Passenger Name List Additions and Deletions List > RP 1708 (dispatch only)

PFS Passenger Final Sales Message > Recommended Practice 1719 (dispatch only)

PTM Passenger Transfer Message > Recommended Practice 1718

MVT Movement Message AHM 730 and 780DIV Diversion Message AHM 781SOM Seats Occupied Message > Recommended Practice 1712

UCM ULD Control Message AHM 424 (dispatch only)

TPM Teletype Passenger Manifest > Recommended Practice 1717 (dispatch only)

NOTOC

LDM Load Message AHM 583

□

5.

6.

Class 1 CClass 2 YClass 3Class 4Class 5

7. √▼ ▼

Weight Kg LbsLength mm InchesVolume Cu. Mtr Cu. Ft

Liquid Vol. Ltr US Gallon8.

IWB ™ V.Zivkovic Issue No. 6 DEM 0MGX Vladimir Novosel / Ground Ops Mgr. 1-Nov-16 UFN

In the event of the requirements to produce multiple copies of the same sheets(e.g. C5. C9) establish an additional sequence identifier while keeping the original number. E.g. C5A, C9A.

Completed by: Verified by:

FMM Fuel Monitoring Message AHM 782RQM Request Information Message AHM 783

MULTIPLE SHEETS NUMBERING

DEFINITIONS OF UNITS OF MEASURE (tick as appropriate)

NTM Notoc EDP Message AHM 384

PNL/ADL Passenger Name List, Additions and Deletions List > RP 1708 (dispatch only) SAL Seat Available List > Recommended Practice 1713 (acceptance only)SLS Statistical Load Summary AHM 588

MESSAGE ADDRESSES

DEFINITIONS OF CLASS CODESAttach a complete address list for all messages under paragraph 4 above. Attachment C sheet 2A.

The following class naming convention shall be used throughout the doc. Class Codes: (e.g. F C Y..)

AHM560

A Sheet 2 ACarrier

YM

∆

NTM - TGDAPYM mandatory effective 1.JAN 2014

SOM - TGDXXYMFTL - TGDXXYM

ETL - TGDXXYMTPM - TGDXXYM

FMM - TGDXXYM

FWB - TGDXXYM TGDFFYM

PFS - MUCPNYM TGDXXYM

ASL - TGDXXYM

SLS - TGDXXYM

PSM - TGDXXYM TGDAPXH

LDM - TGDXXYM TGDAPXH TGDLLYM TGDAPYMMVT - MUCRM1A TGDXXYM TGDOWYM TGDAPYM TGDAPXHDIV - TGDXXYM TGDOWYM TGDAPYM TGDAPXH

Message Addresses

FFM - TGDXXYM TGDAPXH TGDFFYM TGDFFXH



PTM - TGDXXYM TGDAPXHPRL - TGDXXYMBTM - TGDXXYM

IWB ™ V.Zivkovic Issue No. 6 DEM 0MGX Vladimir Novosel / Ground Ops Mgr. 1-Nov-16 UFNVerified by:

Completed by: www.aircraftweightbalance.com/aero.php

AHM 560

A Sheet 3Carrier

A/C type F100 YM

Section Sheet Issue No ▪ Rev No Date

C 10 6 ▪ 1 14.06.17

C 3A 6 1.11.16C 3A 6 1.11.16C 3A 5 29.03.15C 3A 5 29.03.15C 8 5 29.03.15C 9 5 29.03.15A A2 5 29.03.15B 1 4 ▪ 2 05.11.14A 2A 4 ▪ 2 01.10.14D 1 4 ▪ 1 20.08.14C 6 4 ▪ 0 26.05.14

C 3A 4 ▪ 0 26.05.14 New BT issue 19, uniform rounding CPTs index

IWB ™MGXVerified by: Vladimir Novosel / Ground Ops Mgr. 14-Jun-17

Completed by: V.Zivkovic Issue No. 6-1www.aircraftweightbalance.com

Remarks only : FUEL AS BALAST - Spec. Procedure is NOT mandatory . . for EDP loadsheet

EDP-SYSTEM SEMI-PERMANENT DATA LIST OF REVISIONS

D E S C R I P T I O N** NOTE: Emergency EXIT rows

Remarks only : Holiday charter means . .

NEW DOW / DOI due to change pantry CODE B / C / D

PREVIOUS REVISIONS

added ITL GRAPHIC DIAGRAM

FFM address added TGDFFXH

DEM1 message INCLUDED, changed MVT message

RMKS: Handling Advisory - Reminder - Uniform PAX distribution

NO s e a t i n g in emergency exit rows PRM PAX

Valid BT Issue 20Consult separate Pantry Code list published by MGX Ground Ops

NEW DOW / DOI due to A/C weighingValid BT Issue 21

AHM 560

A Sheet 4Carrier

A/C type F100 YM

Section Sheet Issue No ▪ Rev No

Date Action for Pages

0 6 ▪ 1 14.06.17A 1 6 ▪ 1 14.06.17A 2 6 1.11.16A 2A 6 1.11.16A 3 6 ▪ 1 14.06.17A 4 6 ▪ 1 14.06.17B 1 6 1.11.16B 2 6 1.11.16B 3 6 1.11.16C 1 6 1.11.16C 2 6 1.11.16C 3 6 1.11.16C 3A 6 1.11.16C 4 6 1.11.16C 5 6 1.11.16C 6 6 1.11.16C 7 6 1.11.16

C 8 6 1.11.16C 8A 6 1.11.16

C 9 6 1.11.16C 9A 6 1.11.16

C 10 6 ▪ 1 14.06.17 ∆C 11 6 1.11.16C 11A 6 1.11.16

C 12 6 1.11.16C 13 6 1.11.16C 14 6 1.11.16D 1 6 1.11.16D 2 6 1.11.16D 3 6 1.11.16

IWB ™MGX

www.aircraftweightbalance.comCompleted by: V.Zivkovic Issue No. 6-1

Special Load

Verified by: Vladimir Novosel / Ground Ops Mgr 14-Jun-17

Details BAY trim Ballast

Seat plan facilities and row index influence

OPTIMAL TRIM at ZFW for Fuel Saving PurposesULD details

Cabin configurations / Sections

Seating layout

Cabin configurations / Sections

Seat plan facilities and row index influence

Compartment trim

Contacts

Communication > Message addressesList of revisionsList of effective pagesGeneral information - PAX & BAG weightsGeneral information - CREW & BAG weights

DOW / DOI / Balance Table forms / Pantry codesMax Design Weights

Galley / Pantry

CG limitsFuel indexCrew index influence

Galley / Pantry

EDP-SYSTEM SEMI-PERMANENT DATA LIST OF EFFECTIVE

SHEETS

P A G E D E S C R I P T I O N

COVER PAGE

Communication

DOW / DOI specificationBalance and Special Info outputBASIC INDEX AND MAC/RC FORMULAA/C registrations DOW / DOI STD crew

AHM 560

B Sheet 1Carrier

YM

11.1 Standard / default passenger weights in kgs

Standard Alternate *n.a 84 7688 n.a n.a70 n.a n.a35 35 35

0 0 0(tick as appropriate √ )

Cabin baggage weight is included in the above mentioned passengers weights. YES NOIf NO: Actual cabin baggage weight must be used.Remarks:

□

1.2 If passenger weights include cabin baggage and vary by class, use the following table:

Class 1 Class 2 Class 3 Class 4 Class 5

N/AInfant

PASSENGER AND BAGGAGE WEIGHT

MaleFemaleChild

Holiday charter means a charter flight that is part of a holiday travel package

Average AdultMaleFemale


Child

Infant

Average Adult

other than a HOLIDAY CHARTER flight.

Holiday Charter 3rd

GENERAL INFORMATION

Para 1.1 STD or ALT passengers weights also applies to any AD-HOC charter flight . .

Standard / variations *

Class as appropriate

RMKS:AHM561 APPROVAL - TEST LOADSHEETLDS example to be sent with all ADT or Male PAX only.

Para 1.1 3rd option Holiday Charter

N/ARemarks:

1.3 CHECKED BAGGAGE WEIGHT

Standard EU Standard IC * * *13kg n/a

* Variations may include Domestic, Charter, etc.Enter "actual" if standard weight not permitted.

Remarks:

IWB ™ V.Zivkovic DEM 0MGX Vladimir Novosel / Ground Ops Mgr. 1-Nov-16 UFN

Not applicable for MGX.

2nd priority standard weight per piece.

Verified by:

Standard / variations *

Completed by:

Weight per piece

Issue No. 6

1st priority use ACTUAL BAG weight.

Weight per passenger

AHM 560

B Sheet 2

CarrierYM

2 CREW AND CREW BAGGAGE WEIGHTS2.1 Crew Weights

Standard Male FemaleCockpit 85Cabin 75

Remarks:

2.2 Crew Baggage Weights Included in Crew WeightCockpit Cabin

* Specify conditions as appropriate.Remarks:

Shorthaul

Others *


GENERAL INFORMATION

Longhaul


Completed by:

AHM 560

B Sheet 3

CarrierYM

3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS

(tick as appropriate) √

Incl. Excl. Incl. Excl.

DOI

GENERAL INFORMATION

ITEM

Basic Weight

Cabin Crew

Crew Baggage


DOW

Pantry

Containers

Pallets

Potable Water

Remarks

n/a



Remarks:

AHM 560

C Sheet 1Carrier

A/C type F100 YM

1. BALANCE AND SPECIAL INFORMATION - OUTPUT ON LOADSHEET1.1 Balance output (Reference AHM 517)

Please mark your requirements in respective box. √Basic index BIDry Operating Index DOIDeadload index DLI

Deadload MAC MACDLWLoaded Index at zero fuel weight LIZFWLoaded Index at take-off weight LITOWLoaded Index at landing LILAWMAC % at zero fuel weight MACZFWMAC % at take-off weight MACTOWMAC % at landing weight MACLAWStabilizer trim setting at take-off STABTO *

* Specify ANU or AND as appropriate.

1.1.1 Passenger trim output√

Please mark your requirements in respective box.

* Remarks: Indicate any other terminology to be printed on the loadsheet ( Ref. AHM 517, 6.2, item44).

Remarks *Class trimCabin area trimSeat row trim

Not allowed2nd PRIORITY1ST PRIORITY

AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA

Remarks

only for TEST LOADSHEET, approval of DCS.

Remarks: Indicate any other terminology to be printed on the loadsheet ( Ref. AHM 517, 6.2, item44).

1.2 SPECIAL INFORMATION

Specify the information to be entered in the lower parts of the EDP Loadsheet.

1.2.1 Captain`s information/notes, Center of Gravity limits, ramp weight, etc. (give examples). Ref. AHM 517, 6.2, item 45.

1.2.2 Loadmessage before LMC, if required, to be shown. Ref. AHM 517, 6.2, item46.

Completed by: IWB ™ V.Zivkovic Issue No. 6 DEM 0Verified by: MGX Vladimir Novosel / Ground Ops Mgr. 1-Nov-16 UFN

AHM 560

C Sheet 2

Carrier

A/C type F100 YM

2 BASIC INDEX AND MAC/RC FORMULA

INDEX =

C*(I-K)%MAC / RC = W

MAC100

W Weight actual.Sta.Ref.Sta

calculated.KCIMAC/RCLEMAC

2.2

Ref.Sta at : 17332K = 400

C = 100,000

2.3

Length of MAC/RC = 3832 length unit.

LEMAC at : 15779

2.4

Minimum 7 Maximum 35

STAB Range Minimum Maximum

►



AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA

+Ref.Sta -LEMAC

C

W * (Sta - Ref.Sta.) + K

Station, horizontal distance in length units from station zero to the location.Reference station/axis. Selected station around which all index values are

Constant used as a plus value to avoid negative index figures.Constant used as a denominator to convert moment values into index values.Index value corresponding to respective weight.

MAC/RC information

Index formula

Stabilizator change item per 1 % MAC/RC

(Attach a table or diagram if item changing at different weights.)

length unit from zero.

Stabilizer trim setting

Length of Mean Aerodynamic Chord / Reference Chord in length units.Horizontal distance in length unit from the station zero to location of the Leading Edge of the MAC/RC.

length unit from zero.

MAC/RC Range

AHM 560

C Sheet 3

CarrierCabin Conf. * A/C type F100 YM

3.

BASIC WEIGHT

FLEET WEIGHT FLEET INDEX

A/C Registration/tail

number

Weight Adjustment

Index Adjustment

Cabin Configuration

(s)DOW DOI

4O - AOM 109CY 26265 323

4O - AOP 109CY 26053 349

EDP-SYSTEM SEMI-PERMANENT DATA AIRCRAFT DATA

AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS

DRY OPERATING WEIGHT

Provide full list of registrations/tail numbers and adjustments to fleet weight/index:

▼Reference DATA Includes standard Crew 2/3 Pantry

Code A

Tick as appropriate Tick as appropriate

Note: Notifications for data changes at short notice may also be made by means of data exchange

Rmks:


SUMMARY TABLE of DOW / DOI, see below C sheet 3A.

message- DEM (AHM 562).

Reference DOW & DOI includes crew 2/3 Pantry Code A.

Completed by:

Tick as appropriate Tick as appropriate

SUMMARY F102 MZFW 36742 Ref.AHM560 C sheet 3A

2 / 0 2 / 1 2 / 2 2 /3 2 /4 3 / 3 3 / 426040 26115 26190 26265 26340 26350 26425337 328 333 323 329 311 317

26105 26180 26255 26330 26405 26415 26490330 320 326 316 321 304 309

26185 26260 26335 26410 26485 26495 26570320 310 316 306 312 294 299

26285 26360 26435 26510 26585 26595 26670311 302 307 297 303 285 291

25905 25980 26055 26130 26205 26215 26290352 342 348 338 343 326 331

∆2 / 0 2 / 1 2 / 2 2 /3 2 /4 3 / 3 3 / 425828 25903 25978 26053 26128 26138 26213363 354 359 349 355 337 343

25893 25968 26043 26118 26193 26203 26278356 346 351 342 347 330 335

25973 26048 26123 26198 26273 26283 26358346 336 341 331 337 319 325

26073 26148 26223 26298 26373 26383 26458336 327 332 322 328 310 316

25693 25768 25843 25918 25993 26003 26078378 368 374 364 370 352 358

A

B

C

D

V lid BT F 1009 P I 21 ∆

4O - AOP

ZValid BT Form. 1009 M Issue 20

A

B

C

Z

D

PANTRY Code

DRY OPERATING WEIGHT (DOW) and DRY OPERATING INDEX (DOI) DOW / DOI Total number of crew

DOW / DOI Total number of crew 4O - AOM PANTRY Code

DRY OPERATING WEIGHT (DOW) and DRY OPERATING INDEX (DOI)

Sheet 3A

C

MTOW 44452 MLW 39917

PANTRY Z

Montenegro AirlinesGround Services Issue No. 6Aircraft Handling Policies

eqv. less than 0.1 mac% is neglectable as having no effect on the performance calculations within a/c limits. Due to DCS SYS rounding method (integer or truncating), approximately +/- 0.6 IU index unit difference is acceptable,

► For use of appropriate PANTRY CODE consult separate Pantry Code list published by MGX Ground Ops

Ferry flights

RMKS - DOI tolerance calculation:

Valid BT Form. 1009 P Issue 21 ∆

1-Nov-16

AHM 560

C Sheet 4

Carrier

A/C type F100 YM

4. LIMITATIONS4.1 Aircraft Weight Limitations

Operator defined maximum weights for :

4O - AOM 44680 44450 36740 39915

4O - AOP 44680 44450 36740 39915

IWB ™ V.Zivkovic DEM 0MGX Vladimir Novosel / Ground Ops Mgr. UFN

Zero Fuel Landing

Issue No. 61-Nov-16



AIRCRAFT DATA

Aircraft REG. / Tail Ramp/Taxi Take-off

AHM 560

C Sheet 5

Carrier A/C type F100 YM

4.2 CG - LIMITS OF LOADSHEET PURPOSES

Enter the forward and the aft balance limits in the boxes, commencing at the lowest possibleoperating 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.

Weight (kg) Index value Weight (kg) Index value

24000 95 24000 35235950 -55 35950 33036740 -55 36740 325

27600 50 27600 34535950 -55 35950 33042000 -55 42000 32044450 0 44450 275

27600 50 27600 34535950 -55 35950 33039915 -55 39915 320

*Zero fuel, taxi, take-off, inflight, landing.Note: A balance chart/trim sheet must be attached for check purposes as per AHM 519. State trimmethod (i.e. cabin area trim, cpt trim etc.)

Remarks:


Zero

fuel

lim

its

Operational Limits Specify applicability*

Zero

fuel

lim

itsTa

ke-o

ff lim

its

FORWARD AFTOperational Limits



Specify applicability*

Land

ing

Lim

its

AIRCRAFT DATA

Take

-off

limits

La

ndin

g Li

mits

AHM 560

C Sheet 6

Carrier A/C type F100 YM

5. EFFECT OF FUEL

tick

FUEL AS BALLAST - Special Procedure

Fuel weight + - Index Fuel weight + - Index Fuel density: 0.800100 -1.0 100 -0.8500 -5.2 200 -1.8

1000 -10.9 400 -4.21500 -17.0 600 -6.72000 -19.3 800 -9.42500 -21.5 1000 -12.23000 -23.2 1200 -14.93500 -24.5 1400 -17.64000 -25.5 1600 -20.34500 -26.2 1800 -23.05000 -26.7 2000 -25.75500 -26.6 2200 -28.46000 -26.2 2400 -31.16500 -25 1 2512 KG -32 2

It is not mandatory for EDP - LOADSHEET, manual LDS could be issued too.

TOF index is sum of Main wings & Center tanks IDX.

Note: Fuel amount in center tank is considered as DEADLOAD. Adjust DOW and DOI.Note: Non-standard porocedure - fuel as ballast in Center Tank, on CMD request only

Non-standard procedure

Remarks / Procedure Name


AIRCRAFT DATA

Main wings Center tank

Standard procedure

6500 -25.1 2512 KG -32.27000 -23.57500 -21.47744 KG -20.4

Note 1:

Note 2: 10256 KG

Note 3:


Completed by:

Use additional sheets for other fuel densities or state correction factors.

Use additional sheets for each fuel conditions/procedure.

Specify maximum capacity ►

Standard Fuel Procedure

STD FUELING - Main Wings tanks full first than rest in Center Tank.

AHM 560

C Sheet 7Carrier

A/C type F100 YM

6 CREW6.1

mm mm

2452 -14880 -0.14880 -12.63060 -14272 -0.14272 -12.1

6.2

mm mm

2 4283 -13049 - 0.13049 -9.8

2 24637 7305 + 0.07305 5.5

Rmks:

6.3

Note:

Crew Code Cockpit Crew Cabin Crew

Remarks:


Index influence per weight unit & 1 person

per kg 1CP - Sum index

Number of cockpit crew seats and average location


AIRCRAFT DATA

Location * Location of crew baggage

1st / 3rd FWD facing fwd

2nd / 4th AFT

Crew Distribution / Crew Code

The column "Location" is to be filled in only if Basic Weight is specified under paragraph 3.

Completed by:

* Use the locations as under paragraph 6.2

Not applicable for MGX, included in DOW/DOI, see C3.

Verified by:

Not applicable for MGX, included in DOW/DOI, see C3.

Index influence per weight unit & 1 person

per 1 kg 1 CA -Sum index

Crew seat locationMaximum number of

seats

Balance Arm ▪ Sta.

Length of arm from Ref.STA

Number of cabin crew seats and location

2 pilots1 observer

Registrations +

Maximum number of cockpit seats

Valid for REG 4O-AOM and 4O-AOP



AHM 560

C Sheet 8

CarrierAll A/C type F100 YM

40-AOM

7. GALLEY and PANTRY7.1 Galleys

mm mm

G1 3609 -13723 - 0.13723 0.0G2 5140 -12192 - 0.12192 0.0G3 5247 -12085 - 0.12085 0.0G4 23159 5827 + 0.05827 0.0

Total 0 0.0

Remarks:

7.2 Pantry Weight / Pantry Code

Pantry Code Pantry Weight

Pantry Index

* Use location as under paragraph 7.1

Remarks:PANTRY Z Ferry flights


Index influence per weight unitLength of arm from Ref.STA

Consult separate Pantry Code list published by MGX Ground Ops

Verified by: 1-Nov-16Issue No. 6


Location *

(normally used for above mentioned cabin configuration, IF NOT included in DOW).

http://www.aircraftweightbalance.com/aero.php

Galley Locations

index per 1kg

Not applicable for MGX, included in DOW / DOI

Sum Index


Cabin Configuration

AIRCRAFT DATA

Completed by:

Weight kg

Registrations +

`

AHM 560

C Sheet 8 A


4O - AOP

7. A GALLEY and PANTRY7.1 Galleys

mm mm

G1 3287 -14045 -0.14045 0.0G2 4731 -12601 -0.12601 0.0G3 4826 -12506 -0.12506 0.0

23040 5708 0.05708 0.0

Total 0 0.0

Remarks:

7.2 Pantry Weight / Pantry Code

Pantry Code Pantry Weight

Pantry Index

* Use location as under paragraph 7.1

Remarks:


Location *

RH & LH trolley

Consult separate Pantry Code list published by MGX Ground Ops

(normally used for above mentioned cabin configuration, IF NOT included in DOW).

Index influence per weight unitBalance Arm ▪ Sta.


Cabin Configuration

Verified by:

Weight kg index per 1kg

1-Nov-16

Sum Index

Issue No. 6Completed by:

AIRCRAFT DATA

http://www.aircraftweightbalance.com/aero.php

Not applicable for MGX, included in DOW / DOI

Galley Locations

Registrations +


AHM 560

C Sheet 9

Carrier109CY A/C type F100 YM

4O-AOM

8. PASSENGER CABIN8.1 Passenger Seats

Note:

Class 1 Class 2 Section A Section B Section C Section D

CCV C Y * * * * Row seats C/Y

90A 0 109 25Y 25Y 30Y 29Y - 10990B 5 104 5C/20Y 25Y 30Y 29Y 1/2 109

90C 10 99 10C/15Y 25Y 30Y 29Y 2/3 109

90D 15 94 15C/10Y 25Y 30Y 29Y 3/4 109

90E 20 89 20C/5Y 25Y 30Y 29Y 4/5 109

90F 25 84 25C 25Y 30Y 29Y 5/6 10990G 30 79 25C 5C/20Y 30Y 29Y 6/7 109

0

8.2

Balance Length of arm Index

TotalName of cabin

Class / Cabin Sections

Fill in one table for each cabin configuration code.

Curtain position

Valid Registration

Number of seats


AIRCRAFT DATA

Cabin Configuration

VER 109CY



Index influence

mm mm + / - per 1kg

7808 -9524 -0.0952411667 -5665 -0.0566515944 -1388 -0.0138820548 3216 0.03216

Completed by: IWB ™ V.Zivkovic Issue No. 6Verified by: MGX Vladimir Novosel / Ground Ops Mgr. 1-Nov-16

PAX should be uniformly distibuted too, but it is NOT mandatory

1-Nov-16DEM 0

Cabin Section

Section 0C ( rows11-17)

Section 0D ( rows 18-23)

Section 0A ( rows 1-5)

PAX MUST BE UNIFORMLY DISTRIBUTED WITHIN EACH CABIN SECTION.

Handling Advisory for SEAT ROW TRIM

Section 0B ( rows 6-10)

REMARKS:Handling Advisory for CABIN AREA TRIM

AHM 560

C Sheet 9A

Carrier109CY A/C type F100 YM

8.A PASSENGER CABIN8.1

Note:

Class 1 Class 2 Section A Section B Section C Section DCCV C Y * * * * Row seats C/Y90A 0 109 25Y 25Y 30Y 29Y - 109

90B 5 104 5C/20Y 25Y 30Y 29Y 1/2 109

90C 10 99 10C/15Y 25Y 30Y 29Y 2/3 109

90D 15 94 15C/10Y 25Y 30Y 29Y 3/4 109

90E 20 89 20C/5Y 25Y 30Y 29Y 4/5 10990F 25 84 25C 25Y 30Y 29Y 5/6 10990G 30 79 25C 5C/20Y 30Y 29Y 6/7 109

8.2



Index influence

mm mm

Class / Cabin Sections

Cabin Section

Passenger Seats

Valid RegistrationVER 109CY *

Curtain position

AIRCRAFT DATA

Name of cabin

Number of seats

4O - AOP


Cabin Configuration

Fill in one table for each cabin configuration code.

Total

mm mm+ / - per 1 kg

7650 -9682 -0.0968211650 -5682 -0.05682

16072 -1260 -0.01260

20813 3481 0.03481

Completed by: IWB ™ V.Zivkovic Issue No. 6Verified by: MGX Vladimir Novosel / Ground Ops Mgr. 1-Nov-16

Handling Advisory for CABIN AREA TRIMPAX MUST BE UNIFORMLY DISTRIBUTED WITHIN EACH CABIN SECTION.

Handling Advisory for SEAT ROW TRIMPAX should be uniformly distibuted too, but it is NOT mandatory

REMARKS:

Section 0A ( rows 1-5)

DEM 0

Section 0C ( rows11-17)

Section 0B ( rows 6-10)

UFN

Section 0D ( rows 18-23)

W = No movie

V = Seat left vacant / offered last

U

K = Near galley

L = Leg space seat

M = Wheelchair Y = Not fitted

X = No facility seat, e.g. no disctinction betweensmoking and non-smoking

H

I = Infant preferance rows / seats

J = Rear facing seat

∆

MGX 14-Jun-17

emergency situation ref. IATA COS procedures - COS Cabin Operations Safety

² - denotes IATA PRMs

N = No smoking

O = Over wing seat A = Aisle

Z = Buffer zone

Vladimir Novosel / Ground Ops Mgr.Verified by:

AHM 560


AIRCRAFT DATA C Sheet 10

CarrierCabin Configuration All A/C type F100 YMCabin Configuration +

8.3 Seating layout

Show the passenger seating layout for the configuration given in the box at the top by inserting the seatrow numbers and letters in the following table. For special seats use the description codes listed below.

B = Bassinet position P = Stretcher location

C = Crew seat Q = Quit zone

∆ E = Emergency exit ** S = Smoking zone

G = Groups T = Near toilet

= Incapaciatated passenger = Unaccompanied minor

** NOTE: Emergency EXIT rows ** REMINDERS **Check-in agents need to be aware of COS Cabin Operations Safety policies******************************************************************************************************************

CKIN NO s e a t i n g in emergency exit rows following PRM PAX on PNL >SSR / OSI items :BSCT INF CHD TCP family GPST*BLND DEAF ²DEPA DEPU INADEXST - overweight passenger - heavy PAXMEDA LEGR LEGL LEGB PRMs DPNA ²PETCUMNRWCHC WCHR WCHS ²******************************************************************************************************************APST * Apportion Seat in exit rows to be set by APTs / DCS during CKIN preparation, e.g. DHC XCR orfit Adult PAX*, who are physically capable of using the exit and might be an ABP if deems necessary;ABPs - Able Bodied Passengers are selected by crew members to assist in managing an

http://www.aircraftweightbalance.com/aero.php Completed by: IWB ™ V.Zivkovic Issue No. 6-1

AHM 560

C Sheet 11

CarrierYM

8.3.1 Seat plan Layout / Facilities and row index influence



Index influence per weight unit

A C D E F mm mm + / - 1kg

1 N NA NA N N 6168 -11165 -0.11165

2 N NAI NAI N N 6993 -10339 -0.10339

3 N NAI NAI N N 7808 -9524 -0.09524

4 N NAI NAI N N 8602 -8730 -0.08730

5 N NAI NAIU NU N 9397 -7935 -0.07935

6 NU NAIM NAI NU NU 10167 -7166 -0.07166

7 NU NAI NAI NU NU 10926 -6406 -0.06406

8 N NAI NAI N N 11667 -5665 -0.05665

9 N NAI NAI N N 12407 -4925 -0.04925

10 N NAI NAI N N 13175 -4157 -0.04157

11 N NAI NAI N N 13918 -3414 -0.03414

12 N NA NA N N 14683 -2649 -0.02649

14 NE NEA NEA NE NE 15504 -1828 -0.01828

15 NE NEA NEA NE NE 16383 -949 -0.00949

16 N NA NA N N 17166 -166 -0.00166

17 N NAI NAI N N 17949 617 0.00617

0A

0B

OC

Cabin Section


Cabin Configuration 109CY A/C type

Only REG. 4O-AOM

F100Valid for REG.

Seat identifier

Row

17 N NAI NAI N N 17949 617 0.00617

18 N NAI NAI N N 18701 1369 0.01369

19 N NAMH NAMH N N 19454 2122 0.02122

20 N NAMH NAMH N N 20223 2891 0.02891

21 N NAI NAI N N 21008 3676 0.03676

22 N NAI NAI N N 21776 4443 0.04443

23 N NAI Y N N 22521 5189 0.05189

Completed by: IWB ™ V.Zivkovic Issue No. 6 DEM 0Verified by: MGX 1-Nov-16 UFN

0D

Vladimir Novosel / Ground Ops Mgr.

AHM 560

C Sheet 11A

CarrierYM

Only REG. 4O - AOP

8.3.1A Seat plan Layout / Facilities and row index influence

Balance

Arm ▪ Sta. Length of arm from Ref.STA

Index influence per weight unit

A C D E F mm mm + / - 1kg

1 N NA NA N N 6050 -11282 -0.11282

2 N NAI NA N N 6848 -10484 -0.10484

3 N NAI NA N N 7650 -9682 -0.09682

4 N NAI NA N N 8450 -8882 -0.08882

5 N NAI NAU NAU N 9250 -8082 -0.08082

6 NU NAIM NA NU NU 10050 -7282 -0.07282

7 NU NAI NA NU NU 10850 -6482 -0.06482

8 N NAI NA N N 11650 -5682 -0.05682

9 N NAI NA N N 12451 -4881 -0.04881

10 N NAI NA N N 13251 -4081 -0.04081

11 N NAI NA N N 14051 -3281 -0.03281

12 N NA NA N N 14864 -2468 -0.02468

14 NE NEA NEA NE NE 15676 -1656 -0.01656

15 NE NEA NEA NE NE 16514 -818 -0.00818

16 N NA NA N N 17270 -62 -0.00062

17 N NAI NA N N 18057 725 0.00725

OC

0B


Cabin Configuration 109CY A/C type F100Cabin Configuration +

Row

Seat identifier Cabin Section

0A

17 N NAI NA N N 18057 725 0.00725

18 N NAI NA N N 18844 1512 0.01512

19 N NAMH NAMH N N 19632 2300 0.02300

20 N NAMH NAMH N N 20419 3087 0.03087

21 N NAI NA N N 21207 3875 0.03875

22 N NAI NA N N 21994 4662 0.04662

23 N NAI C N N 22782 5450 0.05450

IWB ™ V.Zivkovic Issue No. 6 DEM 0MGX 1-Nov-16 UFNVladimir Novosel / Ground Ops Mgr.Verified by:

Completed by:

0D

AHM 560

C Sheet 12


4O-AOM

9. DETAILS FOR COMPARTMENT TRIM

*1 2806 9.48 10729 -6603 -0.06603*23 ALC/ALF 1387 5.31 20637 3305 0.033054 ALA 982 1.93 23330 5998 0.05998

Security locker (DIP)

* Volume information required for bulk compartments only.

Remarks:

9.1 Combined Load limitationsYES N/A

Configurations

Registrations +

AIRCRAFT DATA

Maximum Capacity

Volume *Index value

+ / - per weight unit

(1 k )

Length of arm from Ref.Sta.


mm


*FWD

Compartment Number Description Max Gross

weight

*1 Loads in FWD HOLD are considered to be equally distributed around the FWD HOLD centroid POINT

YES N/AAppropriate data shown or attached?

NIL

9.2 Cumulative Load LimitationsYES N/A

Appropriate data shown or attached?

IWB ™ V.Zivkovic DEM 0MGX UFNVladimir Novosel / Ground Ops Mgr.


NIL

Issue No. 61-Nov-16

AHM 560

C Sheet 12A


4O - AOP

9. A DETAILS FOR COMPARTMENT TRIM

*1 2680 8.49 10527 -6805 -0.06805*23 ALC/ALF 1387 5.43 20637 3305 0.033054 ALA 982 1.93 23792 6460 0.06460



Remarks:

9.1 Combined Load limitationsYES N/A

*FWD

Compartment Number


Description Max Gross weight Volume *


mm

Index value + / - per

weight unit (1 k )


AIRCRAFT DATA

Configurations

Registrations +

Maximum Capacity

*1 Loads in FWD HOLD are considered to be equally distributed around the FWD HOLD centroid POINT

YES N/AAppropriate data shown or attached?

NIL

9.2 Cumulative Load LimitationsYES N/A


IWB ™ V.Zivkovic DEM 0MGX UFNVladimir Novosel / Ground Ops Mgr.Verified by:

NIL

Completed by: Issue No. 61-Nov-16

AHM 560

C Sheet 13


N/A10.

AB CD EFGH


Bay / Section

Index value + / - per

weight unit (1 kg).

AIRCRAFT DATA

Tick if NOT applicable


Volume *

Cabin Configuration +

Cabin Configuration

* V l i f ti i d f b lk t t l


Max Gross weight

DETAILS FOR BAY/SECTION TRIM

Maximum Capacity

Note1:Note2:

10.1YES N/A


N/A

Use additional sheets as required.

Unsymmetrical Load Limitations


Completed by:

Attach a plan for each compartments only.

N/A


AHM 560

C Sheet 14Carrier

All A/C type F100 YM

11. BALLAST

YES NO

Remarks:

Note:Above special loading procedure for empty flights is applied in order to carry minimum BAL

AIRCRAFT DATA

index + / --10

FIXED PROVISIONS FOR CARRYING BALLAST?

If YES, specify below:

In the case of positioning and training flights where the empty aircraft will be tail heavy, minimum ballast

100KG200KG -20

400KG -40-50

-30far FLF

far FLF


Configuration

Location Weight

will be required to operates within certified limits.

far FLF

BAL must be loaded AS FAR FORWARD in FORWARD HOLD as it will go.Above BAL index table may be applied under special loading instruction only:

far FLF *

far FLF 300KG

500KG * FL F- Forward Lower Forward

Above special loading procedure for empty flights is applied in order to carry minimum BAL


Centroid index on BT-Balance Table is not used in this case.

Completed by:

AHM 560

D Sheet 1


1.

1.1

25500 310

36740 200

Rmks:

gives us optimal LIZFW. MANDATORY for MGX flights

AIRCRAFT DATA

Index + / -Weights at ZFW

Ideal Trim Line at ZFW for Fuel Saving Purposes. *

CG - LIMITS

ITL REALISTIC GRAPHIC DIAGRAM

For manual planning, intersection of EZFW and RED ITL LINE


Cabin Configuration

Mandatory

IWB ™ V.Zivkovic DEM 0MGX Vladimir Novosel / Ground Ops Mgr. 1-Nov-16 UFN

Issue No. 6

Ground Stability

OPTIMAL TRIM TO BE SUBMITTED FOR TEST LOADSHEET too, ref. AHM561 LDS approval.


* Attach Balance chart.

Aircraft is tail heavy, load the aircraft according following loading sequence: - ON DEPARTURE - Loading forward compartments first.- UPON ARRIVAL - Off-loading AFT compartments first.

AHM 560

D Sheet 2Carrier


2. N/A

Type Code Tare Weight Gross Weight Volume * RemarksPosition of height

restriction


ULD Configuration

AIRCRAFT DATA

U L D - UNIT LOAD DEVICES DETAILS

*Containers / Igloos only

Note: For Pallets specify height.



AHM 560

D Sheet 3Carrier


3. SPECIAL LOAD N/AAttach relevant company regulations for special load (AVI, Dangerous Goods, etc.).

ref.

Configuration

AVI/1 Live animals loadable in compartment 1. NOTOC is required.

Exceptionally loading of HUM up to 149 kg is allowed in FWD hold, in order toHEA not allowed on F100, loading of heavy items up to 100 kg, only.

AIRCRAFT DATA

BED - installation of stretcher not possible.

Imposed Cargo embargo of DG transportations of CLASS 1 to CLASS 5 on F100

secure min. ground time.


EXCEPTIONS for DG clas 6 - 9 consult

. . . Cargo Operations Manual . . . 10-1 . . . section 3.2

http://manuals.mgx.me/


Issue No. 61-Nov-16


www.aircraftweightbalance.com/LDI.php

Documents

ahm 560 - Aircraft Weight & Balance F100.pdf · AHM 560 IATA AHM DATA F100 Issue No. 6-1 ... PSM Passenger Service Message > Recommended Practice 1715 ... DOW / DOI / Balance Table