AHM 560

EDP EXCHANGE FOR SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL

RECOMMENDED that, Carriers and Handling Compagnies shall exchange information to establish
and update the data base for the Departure Control Systems as follows:

1. INFORMATION TO BE EXCHANGED BETWEEN HEAD OFFICES

Contacts - there shall be only one official responsible for compiling/sending data to the handling
agent and for receiving/distributing data within his organisation.

If any items on the attachments are irrelevant to a particular EDP (Electronic Data Process)
system, such items shall not be omitted from the forms but shall be marked "NOT APPLICABLE".

Updates without specified effective date should be implemented in the system within two weeks
after receipt.

Use standardized data sheets, in accordance with the attached specimens.

Exchange of data for notice authorisation to semi-permanent data for use on the handling
carriers/compagnies line system, using AHM 052 procedures which is to be redeveloped into
machine readable format.

2. INFORMATION TO BE OBTAINED AT STATION LEVEL ACCORDING TO HANDLING

AGENT'S LOCAL PROCEDURES

For each sector:

taxi fuel information;

estimated take-off fuel;
estimated trip fuel;
estimated payload;
changes to basic weight/basic index;
changes to dry operating weight/dry operating index;
crew — number and where seated;
pantry — weight and location;
equipment not included in basic weight;
load plan information;
passenger handling information, e.g. seat selection procedures.

Commentary

Several Members have automated or intend to automated their check-in and load control system.
When these systems are intended to include the flights of other carriers, the carriers are required to
provide the data necessary for EDP handling.
A carrier may be preparing data for more than one handling agent. It helps to use data sheets of
uniform design and content.
In the interest of speed and convenience, data of a seasonal nature should be obtained at station
level.
AHM 560 (continued)
EDP-SYSTEM COMMUNICATION A
SEMI-PERMANENT DATA
ADDRESSES Sheet 1

Carrier

FLI
1. HANDLING AGENTS'S CONTACT ADDRESS

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

MAILING ADDRESS: sgs.dcs@sas.dk

TELETYPE ADDRESS: CPHKMSK

REMARKS: OY-RCL

2. CARRIER'S CONTACT ADDRESS

MAILING:
ATLANTIC AIRWAYS
Vagar Airport
FO-380 Soervag
Faroe Islands
Phone : +298 341000 – Fax : +298 341001
E-mail : samal@atlantic.fo

TELETYPE ADDRESS: SITA: FAEADRC

REMARKS: OY-RCL

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
COMMUNICATION A
EDP-SYSTEM
SEMI-PERMANENT DATA ADDRESSES Sheet 2

Carrier

FLI
3. AUTOMATICALLY PRODUCED DOCUMENTS
(tick as required)

NOTOC
SEATPLAN
LOADPLAN
PASSENGER INFO LIST
LOADSHEET
LOADING INSTRUCTION/REPORT

4. MESSAGE REQUIREMENTS
(tick as required)

LPM Load Planing message AHM 580

LDM Load Message AHM 583
ALI Abbreviated Load Information Message AHM 587
CPM ULD Control Message AHM 388 (dispatch only)
MVT Movement Message AHM 011 and 780
DIV Diversion Message AHM 781
SOM Seats Occupied Message Recommended Practice 1712
PTM Passenger Transfer Message Recommended Practice 1718
PSM Passenger Service Message Recommended Practice 1715 (dispatch only)
TPM Teletype Passenger Manifest Recommended Practice 1717 (dispatch only)
PFS Passenger Final Sales Message Recommended Practice 1719 (dispatch only)
IDM Industry Discount Message Recommended Practice 1714
RQL Request List Message Recommended Practice 1709 (dispatch only)
PNL/ADL Passenger Name List, and Additions and Deletions List
(Recommended Practice 1708) (acceptance only)
SAL Seats Available List Recommended Practice 1713 (acceptance only)
SLS Statistical Load Summary AHM 588
FMM Fuel Monitoring Message AHM 782
RQM Request Information Message AHM 783
UWS ULD/Bulk Load Weight Signal AHM 581 (acceptance only)

5. MESSAGE ADDRESSES

Attach a complete address list for all messages mentioned under paragraph 4 above.
Company note: “Atlantic Airways REV 20”

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)

GENERAL B
EDP-SYSTEM
SEMI-PERMANENT DATA INFORMATION Sheet 1

A/C Type Carrier

A320-251N FLI
ALL WEIGHTS IN KILOGRAM (kg)

1. PASSENGER AND BAGGAGE WEIGHTS

1.1 Passenger weights

ALL FLIGHTS
EXCEPT HOLIDAY
HOLIDAY CHARTERS
CHARTERS

Standard Adult 84 76
Adult Male 88 83
Adult Female 70 69
Child 35 35
Infant 00 00

Remarks: NIL for infant carried by an adult on one passenger seat

1.2 Cabin Baggage Weight

Yes No
Cabin baggage weight is included in the above mentioned passenger weights.

If No: Actual cabin baggage weight must be used.

Remarks:

1.3 Checked Baggage Weight

Weight per piece ACTUAL

Weight per passenger 13

Enter "actual" if standard weight not permited.

Remarks:

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM GENERAL B
SEMI-PERMANENT DATA
INFORMATION Sheet 2

A/C Type Carrier

A320-251N FLI
2. CREW AND CREW BAGGAGE WEIGHTS

2.1 Crew weights

Cockpit crew 85

Cabin crew 75

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

If No: Crew baggage weights must be specified in 2.2.

Remarks:

2.2 Crew Baggage Weights

For check purposes add list of valid weights and indices.

Cockpit Cabin

Shorthaul

Longhaul

Others*

*Specify conditions as appropriate.

Remarks:

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM GENERAL B
SEMI-PERMANENT DATA
INFORMATION Sheet 3

A/C Type Carrier

A320-251N FLI
3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS
(tick as appropriate)

Remarks
DOW DOI

Item incl. Excl. incl. Excl.

Basic weight  

Crew  

Crew baggage  

Pantry  

Containers

Pallets

Remarks:

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 1

A/C Type Carrier

A320-251N FLI
1. BALANCE AND SPECIAL INFORMATION - OUTPUT ON LOADSHEET

1.1 Balance output

Please mark your requirements in respective box. Remarks

Basic Index BI

Dry Operating Index DOI X

Deadload Index DLI

Deadload MAC MACDLW

Loaded Index at zero fuel weight LIZFW X

Loaded Index at take-off weight LITOW X

Loaded Index at landing weight LILAW X

MAC - at zero fuel weight MACZFW X

MAC - at take-off weight MACTOW X

MAC - at landing weight MACLAW

Stabilizer trim setting at take-off STABTO* X

*Specify ANU or AND as appropriate.

1.2 Special information

The following information must be entered in the lower part of the EDP-Loadsheet, e.g.
Loadmessage before LMC, Baggage, Cargo and Mail specifications, etc.

- LDM before LMC

- PTM with PNL
- BAG
- CARGO and MAIL SPECIFICATIONS

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 2

A/C Type Carrier

A320-251N FLI
ALL WEIGHTS IN KILOGRAM (kg)

1.3 Seating Conditions

State below the seating conditions are to be shown on the loadsheet in the respective box (give
example).

1.4 Special Information

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

Captain's information/notes, Center of Gravity limits, ramp weight, etc… (give examples).

Loadmessage before LMC, if required, to be shown.

2 AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS

DRY OPERATING WEIGHT BASIC WEIGHT (tick as appropriate)

For check purposes add list of valid weights and indices.

Fleet Weigt and Index

Registration Weight Index Registration Weight Index

OY-RCL 43681 kg 53,5

Note: Notification for data changes at short notice may also be made by means of a data exchange
message (AHM 052).

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 3

A/C Type Carrier

A320-251N FLI
3. BASIC INDEX AND MAC FORMULA

3.1 Examples and definitions

W . (Sta. – Ref. Sta.)

Index = + K
C

%MAC =
( C . (I – K)
W
) + Ref. Sta. – LEMAC

MAC
100

W = Weight, actual
Sta. = Station, horizontal distance in meters from station zero to location.
Ref. Sta. = Reference station/axis. Selected station around which all index values are
calculated.
K = Constant used as a plus value to avoid negative index figures.
C = Constant used as a denominator to convert moment values into index values.
I = Index value corresponding to respective weight.
MAC = Lenght of the Mean Aerodynamic Chord in meters.
LEMAC = Horizontal distance in meters from the station zero to location of the Leading
Edge of the MAC.

3.2 Index formula

Ref. Sta. at = 18.850 meters from zero.

K (constant) = 50
C (constant) = 1000

3.3 MAC information

Lenght of MAC = 4.1935 meters

LEMAC at = 17.8015 meters from zero

3.4 Stabilizer trim setting

MAC STAB
range range
15 3.8 Up
17 3.8 Up linear variation between 17% and 40%
40 -2.5 Down
%RC 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29
Trim 3,8 3,8 3,8 3,5 3,3 3,0 2,7 2,4 2,2 1,9 1,6 1,3 1,1 0,8 0,5

30 31 32 33 34 35 36 37 38 39 40
0,2 0,0 -0,3 -0,6 -0,9 -1,1 -1,4 -1,7 -2,0 -2,2 -2,5

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 4

A/C Type Carrier

4 EFFECT OF FUEL/INJECTION WATER
Fuel Loading A320-251N FLI
Fuel Usage
Standard Procedure (tick as appropriate)
Non-standard Procedure FUEL DENSITY: 0.803

Fuel Weight Index Value Fuel Weight Index Value

1500 -1,70 14500 -4,07

2000 -2,25 15000 -4,85
2500 -2,77 15500 -5,63
3000 +1.50 16000 -6.41
3500 +1.07 16500 -7.19
4000 +0.55 17000 -7.97
4500 +0.06 17500 -8.75
5000 -0.40 18000 -9.53
5500 -0.85 18500 -10.32
6000 -1.26 19000 -11.23
6500 -1.64 19050 (Full) -11.33
7000 -2.00
7500 -2.35
8000 -2.67
8500 -2.96
9000 -3.19
9500 -3.28
10000 -3.21
10500 -3.01
11000 -2.70
11500 -2.28
12000 -1.77
12500 -1.31
13000 -1.88
13500 -2.56
14000 -3.29

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)

EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 5

A/C Type Carrier

A320-251N FLI
5. COCKPIT

5.1 Number of seats and average station

Length of arm from

reference station Index influence
Pilot, number of seats
per 1 kg
meters

2 -13.765 -0.013765

Length of arm from Index influence

Third cockpit seat
reference station per 1 kg

1 -13.128 -0.013128

Length of arm from Index influence

Fourth cockpit seat
reference station per 1 kg

1 -12.983 -0.012983

Remarks:

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)

EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 6

A/C Type Carrier

6 LIMITATIONS

6.1 Aircraft Weight Limitations

A320-251N FLI
Maximum weights for:
Aircraft Reg. Design take-off Design take-off
Ramp/Taxi Zero fuel Design landing
or Subtype No. wet* dry
OY-RCL
79400 79000 64300 67400
(MSN 10006)

*Valid for take-off with injection water.

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
 AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 7

A/C Type Carrier

6.2 CG - Limits for Loadsheet Purposes

A320-251N FLI
Enter the forward and the aft balance limits in the boxes, commencing at the lowest weight and terminating
at the highest to checked.

IMPORTANT: If the limits are affected and/or determined by passenger/fuel/version or other

conditions, specify each set of limits on a seperate sheet, entering the special condition(s) in the
box.

FORWARD AFT

Special condition if applicable Special condition if applicable

Specify Specify
Weight Index Value Weight Index Value
applicability * applicability *

ZFW 40600 +43.26 ZFW 40600 +57.20

43283 +41.91 42022 +57.80
48601 +39.68 42496 +58.30
53398 +40.20 42970 +58.67
53872 +40.18 44392 +59.26
54346 +40.05 44866 +60.39
55562 +39.64 45340 +59.86
60111 +40.13 46930 +64.08
64300 +38.73 49132 +66.95
49606 +68.68
50080 +68.15
64300 +82.24

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
 AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 7

A/C Type Carrier

6.2 CG - Limits for Loadsheet Purposes

A320-251N FLI
Enter the forward and the aft balance limits in the boxes, commencing at the lowest weight and terminating
at the highest to checked.

IMPORTANT: If the limits are affected and/or determined by passenger/fuel/version or other

conditions, specify each set of limits on a seperate sheet, entering the special condition(s) in the
box.

FORWARD AFT

Special condition if applicable Special condition if applicable

Specify Specify
Weight Index Value Weight Index Value
applicability * applicability *

TAKEOFF 40600 +41.56 TAKEOFF 40600 +55.46

44587 +39.55 42904 +58.64
53000 +36.02 45249 +59.62
63000 +37.11 46917 +64.05
72000 +34.09 50000 +68.06
73500 +39.76 51000 +69.05
79000 +64.87 67400 +85.29
73326 +89.02
74708 +86.74
79000 +79.67

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)

EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 8

Cabin-Configuration(s) A/C Type Carrier

174 YC A320-251N FLI

7. PASSENGER SEATS

Class codes: Class 1 YC Class 4

(e.g. F, Y, C, M, etc…) Class 2 Class 5

Class 3

Note: Fill in one table for each cabin configuration code.

Number of seats

Name of Class Class Class Class Class Total per

cabin section 1 2 3 4 5 cabin section

OA 60 60

OB 54 54
OC
60 60
(Strecher)

Subtotal

Total per class 174

Remarks: When strecher installed (row 27, 28 and 29), OC is reduced by 7 PAX

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)

EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 9

Cabin-Configuration(s) A/C Type Carrier

174 YC A320-251N FLI

8. AVERAGE STATION

8.1 Class/Cabin sections

Lenght of arm from

Index influence
Class/Cabin Section reference station

meters per 1kg

OA -6.1449 -0.0061449
OB +1.4565 +0.0014565
OC +8.6125 +0.0086125
Strecher (35kg) +11.1931 +0.3917592

8.2 Seating layout

Show the passenger seating layout for the configurations 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
code listed below.

B= Bassinet position P= Stretcher location

C= Crew seat Q= Quiet zone
E= Emergency exit S= Smoking
G= Groups T= Near toilet
H= Incapacitated passenger U= Unaccompagnied minor
I = Infant preference rows/seats V= Seat left vacant/offered last
J= Rear facing seats W= No movie
K= Near galley X= No facility seat (e.g. no distinction
L= Leg space seat between smoking and non-smoking)
M= Wheel chair Y= Not fitted
N= No smoking Z= Buffer zone
O= Over wing seat A= Aisle
Alpha/Characters - D, F, R, Blank, not used.

Note: Seat designators to be in accordancewith Recommended Practice 1711.

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 10

Cabin-Configuration(s) A/C Type Carrier

174 YC A320-251N FLI

8.2.1 Seatplan Layout/Facilities and Row Index Influence

Index influence
ROW LETTER
Sectio Row per seat row
n No.
A B C D E F per 1 kg

OA 1 XL XLV XL XL XLV XL -0,0097873

2 XHU XUV XU XU XUV XHU -0,0089745
3 XH XV X X XV XH -0,0081617
4 XH XV X X XV XH -0,0073489
5 XH XV X X XV XH -0,0065361
6 XH XV X X XV XH -0,0057233
7 XH XV X X XV XH -0,0049105
8 XHI X X X X XHI -0,0041231
9 XHI X X X X XHI -0,0033357
10 XHIO XO XO XO XO XHIO -0,0025483
OB 11 XEO XEO XEO XEO XEO XEO -0,0016593
12 XEO XEO XEO XEO XEO XEO -0,0008211
13 XHOI XO XO XO XO XHOI -0,0000591
14 XHOI XO XO XO XO XHOI 0,0007029
15 XHOI XO XO XO XO XHOI 0,0014649
16 XHOI XO XO XO XO XHOI 0,0022269
17 XHOI XO XO XO XO XHOI 0,0029889
18 XHI X X X X XHI 0,0037509
19 XHI X X X X XHI 0,0045129
OC 20 XHIU X X X X XHIU 0,0052749
21 XHIU X X X X XHIU 0,0060369
22 XHIU X X X X XHIU 0,0067735
23 XHIU X X X X XHIU 0,0075101

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 10

Cabin-Configuration(s) A/C Type Carrier

174 YC A320-251N FLI

8.2.1 Seatplan Layout/Facilities and Row Index Influence

Index influence
ROW LETTER
Sectio Row per seat row
n No.
A B C D E F per 1 kg

24 XHIU X X X X XHIU 0,0082467

25 XHIU X X X X XHIU 0,0089833
26 XHIU X X X X XHIU 0,0097199
27 XHPIU XP XP XP XP XHPIU 0,0104565
28 XPHIU XPU XPU XPU XPU XPHIU 0,0111931
29 XP XP XP XP XP XP 0,0119297

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 11

Cabin-Configuration(s) A/C Type Carrier

174 YC A320-251N FLI

8.3 Cabin Crew Seats

Lenght of arm from

Maximum Index influence
Crew seats locations reference station
No. of seats
meters per 1 kg
Front 2 -11.520 -0.0115200
Aft side 1 +12.911 +0.0129910
Aft mid 1 +13.665 +0.0136650
Remarks:

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 11

Cabin-Configuration(s) A/C Type Carrier

174 YC A320-251N FLI

8.4 Galleys

Lenght of arm from

Index influence
Galley locations reference station

meters per 1 kg
G1 -12.160 -0.012160
G4B +14.267 +0.014267
Remarks:

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 12

Cabin-Configuration(s) A/C Type Carrier

174 YC A320-251N FLI

8.5 Pantry Weight/Pantry Code (normally used for above mentioned cabin configurations).

Pantry Pantry Index

Code Weight change

Outbound 810 kg +1,2

Inbound 506 kg +0,9 Note: The columns "Pantry Weight" and

"Location" must be filled in only if Basic
Charter 830 kg +1,2 Weight is specified under paragraph 2.

SAS 806 kg +1,5

Total

Remarks:

8.6 Crew distribution/Crew Code (normally used for above mentioned cabin configurations).

Note: The column "Location" is to be filled in only if Basic Weight is specified under paragraph
2.

Crew Location of
Cockpit Crew Cabin Crew Location *
Code crew baggage

*Use the locations as under paragraph 8.3

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 13

A/C Type Carrier

A320-251N FLI
9. DETAILS FOR COMPARTMENT TRIM

Maximum capacity

Compartment Index value

Description Gross Weight Volume *
Number per 1 kg
Forward cargo hold
1 3402 -0.006423
(section 11, 12 and 13)
3 Aft cargo hold (section 31) 1301 +0.003235
Aft cargo hold (section 32
4 3235 +0.006540
and 41 and 42)
Rear (Bulk) cargo hold
5 1497 +0.010475
(section 51, 52 and 53)

DIP-Locker
*Volume information required for bulk compartments only.

LOADING INSTRUCTION:
Compartment 1, 3 and 4 is filled up equally, and as last use compartment 5.

9.1 Combined Load Limitations

FWD, AFT and REAR cargo compartments:

The floor structure is capable of supporting a max distributed load of 732 kg/m2.
Each floor pannel is capable of supporting a load of 906 kg on 0,093m2 and a point load of
6,6kg/cm2

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)

EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 14

A/C Type Carrier

A320-251N FLI
10. DETAILS FOR BAY/SECTION TRIM

Maximum capacity

Index value
Bay/Section Gross Weight Volume *
per 1 kg

Bulk

* Volume information required for bulk compartments only.

Note 1: Attach a plan for each compartment configuration.

Note 2: Use additional sheets as required.

10.1 Unsymmetrical Load Limitations

Attach relevant compagny regulations.

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)

EDP-SYSTEM
SEMI-PERMANENT DATA AIRCRAFT DATA C
Sheet 15

A/C Type Carrier

A320-251N FLI
11. BALLAST

FIXED PROVISIONS FOR CARRYING BALLAST.

Specify or attach a table.

Remarks:

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA
LOADPLANNING - D
DATA Sheet 1

A/C Type Carrier

1. CG — LIMITS A320-251N FLI

ALL WEIGHTS IN KILOGRAM (kg)

1.1 Planning Limits

CG-limits for loadplanning purposes shall be agreed between carrier and system operator.

1.2 Desired Trim Line at ZFW for fuel Saving Purposes

The DESIRED TRIM LINE shown in the balance graph below is a loadplanning limit only. In the
interest of fuel economy the load in the compartments shall, whenever possible, be distributed in
such a way that the LIZFW is aft of this line. The respective breakpoints (weight/index) of the
desired trim line shall be entered in the table below.

Index value
Weight

0.01
100

0.1
10
±

Example

85
ine

80
im L
l Tr

75
Id e a

70

65
35 40 45 50 55 60 65 70 75 80 85 90

PLANNED LOADED INDEX ZERO FUEL WEIGHT

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA
LOADPLANNING - D
DATA Sheet 2

A/C Type Carrier

A320-251N FLI
2. UNIT LOAD DEVICES DETAILS

Maximum capacity
Gross
Type Code Tare Weight Volume * Remarks
Weight

* Containers/Igloos only

Note: For pallets, specify Lower Deck or Main Deck.

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021
AHM 560 (continued)
EDP-SYSTEM
SEMI-PERMANENT DATA
LOADPLANNING - D
DATA Sheet 3

A/C Type Carrier

A320-251N FLI
3. SPECIAL LOAD

AVIH 2-5 in compartment 1 and 3 and 4 and 5

DGR 1-4 is allowed.

Strecher :
When Strecher in Cabin add 35kg and placed in OC (OC is reduced by 7 PAX), index change
+0.3917592 for the stretcher.

LOADING INSTRUCTION:
Compartment 1, 3 and 4 is filled up equally, and as last use compartment 5.

Completed by: JEV Issue No.: MSN10006 OY-RCL REV05

(Signature) Date: 06/10/2021