ahm560 f100

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Issue No. 5 29-Mar-15 Ground Services Aircraft Handling Policies Montenegro Airlines AHM 560 IATA AHM DATA F100

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AHM560 F100

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Page 1: AHM560 F100

Issue No. 5

29-Mar-15

Ground Services

Aircraft Handling Policies

Montenegro Airlines

AHM 560IATA AHM DATA F100

Page 2: AHM560 F100

AHM 560

A Sheet 1

Carrier

YM

1.

REMARKS:

2.

REMARKS:

V deleted

www.aircraftweightbalance.comIWB ™ V.Zivkovic DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. UFN

E-MAIL ADDRESS:

TELETYPE ADDRESS:

MAILING ADDRESS:

Flight Operation Department

TELETYPE ADDRESS:

E-MAIL ADDRESS:

[email protected]

CARRIER's CONTACT ADDRESS

TGDOWYM

Airport Podgorica, ME, Montenegro

EDP-SYSTEM SEMI-PERMANENT

DATA

COMMUNICATION

ADDRESSES

SUPPLIER's CONTACT ADDRESS

MAILING ADDRESS:

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

Verified by:

Main Changes:

Legend : ∆ - changed □ - added

Issue No. 5

New BT issue 20

Completed by:

New DOW / DOI table

29-Mar-15

See LIST OF REVISIONS page A3

Balance Table:

Page 3: AHM560 F100

AHM 560

A Sheet 2

Carrier

YM

3.

√ (tick as required)

4.

5.

6.

Class 1 C

Class 2 Y

Class 3

Class 4

Class 5

7. √

▼ ▼

Weight Kg Lbs

Length mm Inches

Volume Cu. Mtr Cu. Ft

Liquid Vol. Ltr US Gallon

8.

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

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

NOTOC

LDM Load Message AHM 583

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

MVT Movement Message AHM 730 and 780

DIV Diversion Message AHM 781

SOM Seats Occupied Message > Recommended Practice 1712

UCM ULD Control Message AHM 424 (dispatch only)

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

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

SAL Seat Available List > Recommended Practice 1713 (acceptance only)

SLS Statistical Load Summary AHM 588

MESSAGE ADDRESSES

DEFINITIONS OF CLASS CODES

Attach a complete address list for all messages under paragraph 4 above. Attachment C sheet 2A.

PTM Passenger Transfer Message > Recommended Practice 1718

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 782

RQM Request Information Message AHM 783

MULTIPLE SHEETS NUMBERING

DEFINITIONS OF UNITS OF MEASURE (tick as appropriate)

NTM Notoc EDP Message AHM 384

IDM Industry Discount Message > Recommended Practice 1714

AUTOMATICALLY PRODUCED DOCUMENTS

PIL PASSENGER INFO LIST

LOAD PLAN

SEAT PLAN

MESSAGE REQUIREMENTS (tick as required )

LIR LOADING INSTRUCTION REPORT

LPM Load Planning Message AHM 580

ALI Abbreviated Load Information Message AHM 584

CPM Container / Pallet Distribution Message AHM587

LOADSHEET

COMMUNICATION

ADDRESSESEDP-SYSTEM SEMI-PERMANENT DATA

PRL Passenger Reconcile List

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

Page 4: AHM560 F100

AHM560

A Sheet 2 A

Carrier

YM

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

PTM - TGDXXYM TGDAPXH

PRL - TGDXXYM

BTM - TGDXXYM

www.aircraftweightbalance.com/aero.php

EDP-SYSTEM SEMI-PERMANENT

DATA

COMMUNICATION

ADDRESSES

Completed by:

FFM - TGDXXYM TGDAPXH TGDFFYM TGDFFXH

Verified by:

PSM - TGDXXYM TGDAPXH

LDM - TGDXXYM TGDAPXH TGDLLYM TGDAPYM

MVT - MUCRM1A TGDXXYM TGDOWYM TGDAPYM TGDAPXH

DIV - TGDXXYM TGDOWYM TGDAPYM TGDAPXH

Message Addresses

ASL - TGDXXYM

SLS - TGDXXYM

FWB - TGDXXYM TGDFFYM

PFS - MUCPNYM TGDXXYM

NTM - TGDAPYM mandatory effective 1.JAN 2014

SOM - TGDXXYM

FTL - TGDXXYM

ETL - TGDXXYM

TPM - TGDXXYM

FMM - TGDXXYM

Page 5: AHM560 F100

AHM 560

A Sheet 3

Carrier

A/C type F100 YM

Section SheetIssue No

▪ Rev No Date

C 3A 5 29.03.15

C 3A 5 29.03.15

C 8 5 29.03.15

C 9 5 29.03.15

A A2 5 29.03.15

B 1 4 ▪ 2 05.11.14

A 2A 4 ▪ 2 01.10.14

D 1 4 ▪ 1 20.08.14

C 6 4 ▪ 0 26.05.14

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

IWB ™

MGX

added ITL GRAPHIC DIAGRAM

FFM address added TGDFFXH

DEM1 message INCLUDED, changed MVT message

PREVIOUS REVISIONS

RMKS: Handling Advisory - Reminder - Uniform PAX distribution

Valid BT Issue 20

Consult separate Pantry Code list published by MGX Ground Ops

EDP-SYSTEM SEMI-PERMANENT DATA LIST OF REVISIONS

D E S C R I P T I O N

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

Remarks only : Holiday charter means . .

Remarks only : FUEL AS BALAST - Spec. Procedure

is NOT mandatory . . for EDP loadsheet

Completed by: V.Zivkovic Issue No. 5

www.aircraftweightbalance.com

Verified by: Dejan Bojanic / Ground Ops Mgr. 29-Mar-15

Page 6: AHM560 F100

AHM 560

A Sheet 4

Carrier

A/C type F100 YM

Section SheetIssue No ▪

Rev No Date

Action for

Pages

0 5 29.03.15

A 1 5 29.03.15

A 2 5 29.03.15

A 2A 5 29.03.15

A 3 5 29.03.15

A 4 5 29.03.15

B 1 5 29.03.15

B 2 5 29.03.15

B 3 5 29.03.15

C 1 5 29.03.15

C 2 5 29.03.15

C 3 5 29.03.15

C 3A 5 29.03.15 ∆

C 4 5 29.03.15

C 5 5 29.03.15

C 6 5 29.03.15

C 7 5 29.03.15

C 8 5 29.03.15

C 8A 5 29.03.15

C 9 5 29.03.15

C 9A 5 29.03.15

C 10 5 29.03.15

C 11 5 29.03.15

C 11A 5 29.03.15

C 12 5 29.03.15

C 13 5 29.03.15

C 14 5 29.03.15

D 1 5 29.03.15

D 2 5 29.03.15

D 3 5 29.03.15

IWB ™

MGX

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 specification

Balance and Special Info output

BASIC INDEX AND MAC/RC FORMULA

A/C registrations DOW / DOI STD crew

DOW / DOI / Balance Table forms / Pantry codes

Max Design Weights

Galley / Pantry

CG limits

Fuel index

Crew index influence

Galley / Pantry

Contacts

Communication > Message addresses

List of revisions

List of effective pages

General information - PAX & BAG weights

General information - CREW & BAG weights

Cabin configurations / Sections

Seating layout

Cabin configurations / Sections

Seat plan facilities and row index influence

Compartment trim

Details BAY trim

Ballast

Seat plan facilities and row index influence

OPTIMAL TRIM at ZFW for Fuel Saving Purposes

ULD details

Special Load

Verified by: Dejan Bojanic / Ground Ops Mgr. 29-Mar-15

www.aircraftweightbalance.comCompleted by: V.Zivkovic Issue No. 5

Page 7: AHM560 F100

AHM 560

B Sheet 1

Carrier

YM

1

1.1 Standard / default passenger weights in kgs

Standard Alternate *

n.a 84 76

88 n.a n.a

70 n.a n.a

35 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/A

Remarks:

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 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

2nd priority standard weight per piece.

Verified by:

Standard / variations *

Completed by:

Weight per piece

Issue No. 5

1st priority use ACTUAL BAG weight.

Weight per passenger

Class as appropriate

RMKS:

AHM561 APPROVAL - TEST LOADSHEET

LDS example to be sent with all ADT or Male PAX only.

Para 1.1 3rd option Holiday Charter

EDP-SYSTEM SEMI-PERMANENT

DATA

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 *

Infant

Not applicable for MGX.

PASSENGER AND BAGGAGE WEIGHT

Male

Female

Child

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

Average Adult

Male

Female

Page 8: AHM560 F100

AHM 560

B Sheet 2

Carrier

YM

2 CREW AND CREW BAGGAGE WEIGHTS

2.1 Crew Weights

Standard Male Female

Cockpit 85

Cabin 75

Remarks:

2.2 Crew Baggage Weights Included in Crew Weight

Cockpit Cabin

* Specify conditions as appropriate.

Remarks:

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

GENERAL

INFORMATION

Longhaul

Completed by:

Verified by:

Shorthaul

Others *

EDP-SYSTEM SEMI-PERMANENT

DATA

Page 9: AHM560 F100

AHM 560

B Sheet 3

Carrier

YM

3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS

(tick as appropriate) √

Incl. Excl. Incl. Excl.

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

Remarks

n/a

Pantry

Containers

Pallets

Potable Water

DOW

Completed by:

Verified by:

Remarks:

DOI

GENERAL

INFORMATION

ITEM

Basic Weight

Cabin Crew

Crew Baggage

EDP-SYSTEM SEMI-

PERMANENT DATA

Page 10: AHM560 F100

AHM 560

C Sheet 1

Carrier

A/C type F100 YM

1. BALANCE AND SPECIAL INFORMATION - OUTPUT ON LOADSHEET

1.1 Balance output (Reference AHM 517)

Please mark your requirements in respective box. √

Basic index BI

Dry Operating Index DOI

Deadload index DLI

Deadload MAC MACDLW

Loaded Index at zero fuel weight LIZFW

Loaded Index at take-off weight LITOW

Loaded Index at landing LILAW

MAC % at zero fuel weight MACZFW

MAC % at take-off weight MACTOW

MAC % at landing weight MACLAW

Stabilizer 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).

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. 5 DEM 0

Verified by: MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

EDP-SYSTEM SEMI-PERMANENT

DATA

Remarks

only for TEST LOADSHEET, approval of DCS.

AIRCRAFT DATA

Remarks *

Class trim

Cabin area trim

Seat row trim

Not allowed

2nd PRIORITY

1ST

PRIORITY

Page 11: AHM560 F100

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

MAC

100

W Weight actual.

Sta.

Ref.Sta

calculated.

K

C

I

MAC/RC

LEMAC

2.2

Ref.Sta at : 17332

K = 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

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

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

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

Completed by:

Verified by:

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.

Page 12: AHM560 F100

AHM 560

C Sheet 3

Carrier

Cabin Conf. * A/C type F100 YM

3.

BASIC WEIGHT

FLEET

WEIGHTFLEET INDEX

A/C

Registration/tail

number

Weight

Adjustment

Index

Adjustment

Cabin

Configuration

(s)DOW DOI

4O - AOM 109CY 26265 323

4O - AOP 109CY 26072 347

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

Rmks:

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

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

message- DEM (AHM 562).

▼Reference DATA Includes

standard Crew 2/3 Pantry

Code A

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

Completed by:

EDP-SYSTEM SEMI-PERMANENT DATA AIRCRAFT DATA

AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS

DRY OPERATING WEIGHT

Verified by:

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

Tick as appropriate Tick as appropriate

Page 13: AHM560 F100

SUMMARY F100 MZFW 36740 Ref.AHM560 C sheet 3A

2 / 0 2 / 1 2 / 2 2 /3 2 /4 3 / 3 3 / 4

26040 26115 26190 26265 26340 26350 26425

337 328 333 323 329 311 317

26105 26180 26255 26330 26405 26415 26490

330 320 326 316 321 304 309

26185 26260 26335 26410 26485 26495 26570

320 310 316 306 312 294 299

26285 26360 26435 26510 26585 26595 26670

311 302 307 297 303 285 291

25905 25980 26055 26130 26205 26215 26290

352 342 348 338 343 326 331

2 / 0 2 / 1 2 / 2 2 /3 2 /4 3 / 3 3 / 4

25847 25922 25997 26072 26147 26157 26232

362 352 357 347 353 335 341

25912 25987 26062 26137 26212 26222 26297

354 344 350 340 345 328 333

25992 26067 26142 26217 26292 26302 26377

344 334 339 330 335 318 323

26092 26167 26242 26317 26392 26402 26477

335 325 330 320 326 308 314

25712 25787 25862 25937 26012 26022 26097

376 367 372 362 368 350 356

PANTRY Z

Montenegro Airlines

Ground Services Issue No. 5

Aircraft Handling Policies 29-Mar-15

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

MTOW 44450

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

DOW / DOI Total number of crew

MLW 39915

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

Z

Valid BT Form. 1009 M Issue 20

A

B

C

Z

D

PANTRY Code

A

B

C

D

Valid BT Form. 1009 P Issue 20

4O - AOP

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

Q Ferry flights

RMKS - DOI tolerance calculation:

Page 14: AHM560 F100

AHM 560

C Sheet 4

Carrier

A/C type F100 YM

4. LIMITATIONS

4.1 Aircraft Weight Limitations

Operator defined maximum weights for :

4O - AOM 44680 44450 36740 39915

4O - AOP 44680 44450 36740 39915

IWB ™ V.Zivkovic DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. UFN

EDP-SYSTEM SEMI-PERMANENT

DATA

AIRCRAFT DATA

Aircraft

REG. / Tail Ramp/Taxi Take-off Zero Fuel Landing

Issue No. 5

29-Mar-15

Completed by:

Verified by:

Page 15: AHM560 F100

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 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.

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

24000 95 24000 352

35950 -55 35950 330

36740 -55 36740 325

27600 50 27600 345

35950 -55 35950 330

42000 -55 42000 320

44450 0 44450 275

27600 50 27600 345

35950 -55 35950 330

39915 -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 trim

method (i.e. cabin area trim, cpt trim etc.)

Remarks:

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

Completed by:

Verified by:

EDP-SYSTEM SEMI-PERMANENT

DATA

Specify

applicability*

La

nd

ing

Lim

its

AIRCRAFT DATA

Ta

ke

-off lim

its

La

nd

ing

Lim

its

Ze

ro fu

el

limits

Operational Limits Specify

applicability*

Ze

ro fu

el

limits

Ta

ke

-off

limits

FORWARD AFT

Operational Limits

Page 16: AHM560 F100

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: 0.800

100 -1.0 100 -0.8

500 -5.2 200 -1.8

1000 -10.9 400 -4.2

1500 -17.0 600 -6.7

2000 -19.3 800 -9.4

2500 -21.5 1000 -12.2

3000 -23.2 1200 -14.9

3500 -24.5 1400 -17.6

4000 -25.5 1600 -20.3

4500 -26.2 1800 -23.0

5000 -26.7 2000 -25.7

5500 -26.6 2200 -28.4

6000 -26.2 2400 -31.1

6500 -25.1 2512 KG -32.2

7000 -23.5

7500 -21.4

7744 KG -20.4

Note 1:

Note 2: 10256 KG

Note 3:

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

EDP-SYSTEM SEMI-PERMANENT

DATA

AIRCRAFT DATA

Main wings Center tank

STD FUELING - Main Wings tanks full first than rest

in Center Tank.

Standard procedure

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

Note: Non-standard porocedure - fuel as ballast in Center Tank, on CMD request only

Verified by:

Completed by:

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

Use additional sheets for each fuel conditions/procedure.

Non-standard procedure

Specify maximum capacity ►

Remarks / Procedure Name

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

Note: Fuel amount in center tank is considered as DEADLOAD. Adjust DOW and DOI.

Standard Fuel Procedure

Page 17: AHM560 F100

AHM 560

C Sheet 7

Carrier

A/C type F100 YM

6 CREW

6.1

mm mm

2452 -14880 -0.14880 -12.6

3060 -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:

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

Length of arm

from Ref.STA

Number of cabin crew seats and location

2 pilots

1 observer

Registrations +

Maximum number of

cockpit seats

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

Balance

Arm ▪ Sta.

Length of arm

from Ref.STA

Verified by:

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

Index influence per

weight unit & 1 person

per 1 kg1 CA -Sum

index

Crew seat location

Maximum

number of

seats

Balance

Arm ▪ Sta.

Completed by:

* Use the locations as under paragraph 6.2

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

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.

Index influence per

weight unit & 1 person

per kg1CP - Sum

index

Number of cockpit crew seats and average location

EDP-SYSTEM SEMI-PERMANENT

DATA

AIRCRAFT DATA

Page 18: AHM560 F100

AHM 560

C Sheet 8

Carrier

All A/C type F100 YM

40-AOM

7. GALLEY and PANTRY

7.1 Galleys

mm mm

G1 3609 -13723 - 0.13723 0.0

G2 5140 -12192 - 0.12192 0.0

G3 5247 -12085 - 0.12085 0.0

G4 23159 5827 + 0.05827 0.0

Total 0 0.0

Remarks:

7.2 Pantry Weight / Pantry Code

Pantry CodePantry

Weight

Pantry

Index

* Use location as under paragraph 7.1

Remarks:

PANTRY Z Ferry flights

IWB ™ V.Zivkovic DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. UFN

Galley Locations

EDP-SYSTEM SEMI-PERMANENT

DATA

Cabin Configuration

AIRCRAFT DATA

Location *

Registrations +

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

Completed by:

Weight kg Sum Indexindex per

1kg

Not applicable for MGX, included in DOW / DOI

Issue No. 5

Balance

Arm ▪ Sta.

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

Index influence per weight unitLength of

arm from

Ref.STA

Consult separate Pantry Code list published by MGX Ground Ops

Verified by: 29-Mar-15

Page 19: AHM560 F100

`

AHM 560

C Sheet 8 A

Carrier

All A/C type F100 YM

4O - AOP

7. A GALLEY and PANTRY

7.1 Galleys

mm mm

G1 3287 -14045 -0.14045 0.0

G2 4731 -12601 -0.12601 0.0

G3 4826 -12506 -0.12506 0.0

23040 5708 0.05708 0.0

Total 0 0.0

Remarks:

7.2 Pantry Weight / Pantry Code

Pantry CodePantry

Weight

Pantry

Index

* Use location as under paragraph 7.1

Remarks:

IWB ™ V.Zivkovic DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. UFN

Galley Locations

Completed by:

AIRCRAFT DATA

Not applicable for MGX, included in DOW / DOI

Registrations +

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

Verified by:

Weight kgindex per

1kg

Issue No. 5

29-Mar-15

Sum Index

EDP-SYSTEM SEMI-PERMANENT

DATA

Length of

arm from

Ref.STA

Consult separate Pantry Code list published by MGX Ground Ops

Cabin Configuration

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

Index influence per weight unitBalance

Arm ▪ Sta.

RH & LH trolley

Location *

Page 20: AHM560 F100

AHM 560

C Sheet 9

Carrier

109CY A/C type F100 YM

4O-AOM

8. PASSENGER CABIN

8.1 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 - 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 4/5 109

90F 25 84 25C 25Y 30Y 29Y 5/6 109

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

0

8.2

Balance

Arm ▪ Sta.

Length of arm

from Ref.STA

Index

influence

mm mm + / - per 1kg

7808 -9524 -0.09524

11667 -5665 -0.05665

15944 -1388 -0.01388

20548 3216 0.03216

Completed by: IWB ™ V.Zivkovic Issue No. 5

Verified by: MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15

REMARKS:

Handling Advisory for CABIN AREA TRIM

EDP-SYSTEM SEMI-PERMANENT

DATA

AIRCRAFT DATA

Cabin Configuration

VER 109CY

Section 0B ( rows 6-10)

Section 0C ( rows11-17)

Curtain

position

Section 0D ( rows 18-23)

Section 0A ( rows 1-5)

Valid Registration

Number of seats

PAX MUST BE UNIFORMLY DISTRIBUTED WITHIN EACH CABIN SECTION.

Handling Advisory for SEAT ROW TRIM

TotalName of

cabin

Class / Cabin Sections

Cabin Section

Fill in one table for each cabin configuration code.

29-Mar-15

DEM 0

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

Page 21: AHM560 F100

AHM 560

C Sheet 9A

Carrier

109CY A/C type F100 YM

8.A PASSENGER CABIN

8.1

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 - 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 4/5 109

90F 25 84 25C 25Y 30Y 29Y 5/6 109

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

8.2

Balance

Arm ▪ Sta.

Length of arm

from Ref.STA

Index

influence

mm mm

+ / - per 1 kg

7650 -9682 -0.09682

11650 -5682 -0.05682

16072 -1260 -0.01260

20813 3481 0.03481

Completed by: IWB ™ V.Zivkovic Issue No. 5

Verified by: MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15

Section 0B ( rows 6-10)

UFN

Section 0D ( rows 18-23)

Fill in one table for each cabin configuration code.

Total

DEM 0

Section 0C ( rows11-17)

Cabin Configuration

EDP-SYSTEM SEMI-PERMANENT

DATA

Section 0A ( rows 1-5)

Valid RegistrationVER 109CY *

Curtain

position

AIRCRAFT DATA

Name of

cabin

Number of seats

4O - AOP

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

Class / Cabin Sections

Cabin Section

Passenger Seats

REMARKS:

Page 22: AHM560 F100

AHM 560

C Sheet 10

Carrier

All A/C type F100 YM

8.3 Seating layout

P = Stretcher location

IWB ™ V.Zivkovic Issue No. 5

MGX 29-Mar-15

W = No movie

Q = Quit zone

V = Seat left vacant / offered last

U = Unaccompanied minor

T = Near toilet

S = Smoking zone

K = Near galley

L = Leg space seat

M = Wheelchair

N = No smoking

O = Over wing seat A = Aisle

Z = Buffer zone

Y = Not fitted

X = No facility seat, e.g. no disctinction between

smoking and non-smoking

C = Crew seat

E = Emergency exit

G = Groups

H = Incapaciatated passenger

I = Infant preferance rows / seats

J = Rear facing seat

Dejan Bojanic / Ground Ops Mgr.

AIRCRAFT DATA

Completed by:

Verified by:

EDP-SYSTEM SEMI-PERMANENT

DATA

Cabin Configuration

Cabin Configuration +

Show the passenger seating layout for the configuration given in the box at the top by inserting the seat

row numbers and letters in the following table. For special seats use the description codes listed below.

B = Bassinet position

Page 23: AHM560 F100

AHM 560

C Sheet 11

Carrier

YM

8.3.1 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 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

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. 5 DEM 0

Verified by: MGX 29-Mar-15 UFN

Seat identifier

Row

EDP-SYSTEM SEMI-PERMANENT DATA AIRCRAFT DATA

Cabin Configuration 109CY A/C type

Only REG. 4O-AOM

F100

Valid for REG.

Cabin

Section

0A

0B

0D

Dejan Bojanic / Ground Ops Mgr.

OC

Page 24: AHM560 F100

AHM 560

C Sheet 11A

Carrier

YM

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

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. 5 DEM 0

MGX 29-Mar-15 UFN

0A

0D

Cabin

Section

Cabin Configuration +

Row

Seat identifier

EDP-SYSTEM SEMI-PERMANENT DATA AIRCRAFT DATA

Cabin Configuration 109CY A/C type F100

Verified by:

Completed by:

Dejan Bojanic / Ground Ops Mgr.

OC

0B

Page 25: AHM560 F100

AHM 560

C Sheet 12

Carrier

All A/C type F100 YM

4O-AOM

9. DETAILS FOR COMPARTMENT TRIM

*1 2806 9.48 10729 -6603 -0.06603

*2

3 ALC/ALF 1387 5.31 20637 3305 0.03305

4 ALA 982 1.93 23330 5998 0.05998

Security

locker (DIP)

* Volume information required for bulk compartments only.

Remarks:

9.1 Combined Load limitations

YES N/A

Appropriate data shown or attached?

NIL

9.2 Cumulative Load Limitations

YES N/A

Appropriate data shown or attached?

IWB ™ V.Zivkovic DEM 0

MGX UFN

*FWD

Issue No. 5

29-Mar-15

Compartment

NumberDescription

Max Gross

weight

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

Completed by:

Verified by:

AIRCRAFT DATA

NIL

Maximum Capacity

Volume *

Index value

+ / - per

weight unit

(1 kg).

Length of arm

from Ref.Sta.

Balance

Arm ▪ Sta.

mm

EDP-SYSTEM SEMI-PERMANENT

DATA

Configurations

Registrations +

Dejan Bojanic / Ground Ops Mgr.

Page 26: AHM560 F100

AHM 560

C Sheet 12A

Carrier

All A/C type F100 YM

4O - AOP

9. A DETAILS FOR COMPARTMENT TRIM

*1 2680 8.49 10527 -6805 -0.06805

*2

3 ALC/ALF 1387 5.43 20637 3305 0.03305

4 ALA 982 1.93 23792 6460 0.06460

Security

locker (DIP)

* Volume information required for bulk compartments only.

Remarks:

9.1 Combined Load limitations

YES N/A

Appropriate data shown or attached?

NIL

9.2 Cumulative Load Limitations

YES N/A

Appropriate data shown or attached?

IWB ™ V.Zivkovic DEM 0

MGX UFN

Issue No. 5

29-Mar-15

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

Index value

+ / - per

weight unit

(1 kg).

NIL

Completed by:

EDP-SYSTEM SEMI-PERMANENT

DATA

AIRCRAFT DATA

Configurations

Registrations +

Maximum Capacity

*FWD

Dejan Bojanic / Ground Ops Mgr.Verified by:

Compartment

Number

Length of

arm from

Ref.Sta.

DescriptionMax Gross

weightVolume *

Balance

Arm ▪ Sta.

mm

Page 27: AHM560 F100

AHM 560

C Sheet 13

Carrier

All A/C type F100 YM

N/A

10.

A

B

C

D

E

F

G

H

Security

locker (DIP)

Note1:

Note2:

10.1

YES N/A

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

AIRCRAFT DATA

Tick if NOT applicable

EDP-SYSTEM SEMI-PERMANENT

DATA

Volume *

Cabin Configuration +

DETAILS FOR BAY/SECTION TRIM

Verified by:

Bay / Section

N/A

Index value

+ / - per

weight unit

(1 kg).

Use additional sheets as required.

Completed by:

Cabin Configuration

Unsymmetrical Load Limitations

Attach a plan for each compartments only.

N/A

Appropriate data shown or attached?

Maximum Capacity

* Volume information required for bulk compartments only.

Length of

arm from

Ref.Sta.

Max Gross

weight

Page 28: AHM560 F100

AHM 560

C Sheet 14

Carrier

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

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

500KG -50

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

Verified by:

EDP-SYSTEM SEMI-PERMANENT

DATA

Configuration

Location Weight

will be required to operates within certified limits.

far FLF 400KG -40

Completed by:

far FLF * 100KG

far FLF 200KG

AIRCRAFT DATA

index + / -

-10

FIXED PROVISIONS FOR CARRYING BALLAST?

If YES, specify below:

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

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:

* FL F- Forward Lower Forward

-20

far FLF 300KG -30

far FLF

Page 29: AHM560 F100

AHM 560

D Sheet 1

Carrier

All A/C type F100 YM

1.

1.1

25500 310

36740 200

Rmks:

Mandatory

IWB ™ V.Zivkovic DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

For manual planning, intersection of EZFW and RED ITL LINE

Completed by:

Verified by:

EDP-SYSTEM SEMI-PERMANENT

DATA

Cabin Configuration

* 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.

AIRCRAFT DATA

Index + / -Weights at

ZFW

Ideal Trim Line at ZFW for Fuel Saving Purposes. *

CG - LIMITS

ITL REALISTIC GRAPHIC DIAGRAM

Issue No. 5

gives us optimal LIZFW. MANDATORY for MGX flights

Ground Stability

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

Page 30: AHM560 F100

AHM 560

D Sheet 2

Carrier

All A/C type F100 YM

2. N/A

Type Code Tare WeightGross

WeightVolume *

*Containers / Igloos only

Note: For Pallets specify height.

IWB ™ V.Zivkovic Issue No. 5 DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. 29-Mar-15 UFN

EDP-SYSTEM SEMI-PERMANENT

DATA

ULD Configuration

AIRCRAFT DATA

U L D - UNIT LOAD DEVICES DETAILS

Verified by:

Completed by:

RemarksPosition of height

restriction

Page 31: AHM560 F100

AHM 560

D Sheet 3

Carrier

All A/C type F100 YM

3. SPECIAL LOAD N/A

Attach relevant company regulations for special load (AVI, Dangerous Goods, etc.).

ref.

IWB ™ V.Zivkovic DEM 0

MGX Dejan Bojanic / Ground Ops Mgr. UFN

http://manuals.mgx.me/

EXCEPTIONS for DG clas 6 - 9 consult

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

www.aircraftweightbalance.com/LDI.php

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.

EDP-SYSTEM SEMI-PERMANENT

DATA

Issue No. 5

29-Mar-15

Completed by:

Verified by:

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 to

HEA not allowed on F100, loading of heavy items up to 100 kg, only.