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AHM560 F100
Citation preview
Issue No. 5
29-Mar-15
Ground Services
Aircraft Handling Policies
Montenegro Airlines
AHM 560IATA AHM DATA 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:
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:
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)
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
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
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
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
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
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
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
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.
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
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:
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:
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
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
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
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
`
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 *
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
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:
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
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
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
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.
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
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
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
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.
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
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.