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5
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1 Table of Contents

5
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1 Table of Contents
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2 Loading Procedure
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Loading Procedure Airbus A320-200
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Loading Procedure Airbus A321-231
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3 Load & Trim Sheet
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Passenger and Baggage Weights
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1 Passenger Weights
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2 Crew Member’s Weights
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3 Baggage weight and Baggage loading procedure
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4 Definitions
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Manual Load & Trim sheet for A320-200 and A321-231
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1 Load & Trim sheet Airbus A320-200 (F – FO – 003)
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2 Load & Trim sheet Airbus A321-231 (F – FO – 004)
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Codes for Load requiring Special Attention
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4 Last Minute Change (LMC)
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12
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LOAD CONTROL
GOM

5
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12
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LOAD CONTROL
GOM

5
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2 Loading Procedure
The purpose of load planning is to have a safe operation, to achieve the most economical utilization of
aircraft capacity and smooth Handling of the aircraft and load at all stations
...
In critical cases load planning has to be arranged with cockpit crew
...


Exception:

The number of pieces of luggage and / or volume of luggage does not allow segregation per
destination
...


The cockpit crew will prepare the Trip Information Sheet (Please see GOM Appendix) and hand it over to the
Operations agent
...


Upon closing of the check-in, all data is transferred to the operation’s office and collected by the Operations
agent in order to realize the loading instruction
...


The Loading Supervisor is responsible to verify that the actual load manifest is identical with the final version
of load distribution on the loading instruction
...


After the accomplishment of the loading, the Loading Supervisor shall sign the final loading instruction report
and relay it to the Operations agent
...


Aircraft mass and Centre of Gravity shall be calculated using a "Load and Trim sheet form" or a
"computerized Load and Trim sheet"
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01
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LOAD CONTROL
GOM

5
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For example in regards of the A320 Freebird aim is to obtain a
Take-off CG position of 27-31% (29 +/- 2%) and for the A321 24-28% (26% +/-2%)
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If the deviation or error is beyond the
tolerated limits, a new load sheet shall be prepared
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4
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The cockpit crew is responsible for checking the correctness of Load & Trim sheet
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Note1:

All weight and balance calculations shall be based on current aircraft weight and balance
data which is provided in last revision of AHM560 by suitable and qualified personnel
according to AHM590
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Engineering & Support department
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Engineering & Support department
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Once approval has been given, and prior to any further changes
advised by Freebird Airlines, responsibility for the data shall rest with the DCS/ Load control
system supplier and handling agents
...
625 paragraph b: there for after approving
the different systems it might occur that Freebird requests new test load sheets within the 6
months after the approval
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and
dissemination of dangerous goods with NOTOC to the Pilot in Command before the
departure of the concerned flight
...
g
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In the case of acceptance, OCC should
give an immediate notification to Pilot in Command before the departure
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01
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4

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2 Loading Procedure

1
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The goal of this empirical data is to achieve an
ideal stabilizer pitch trim setting, with the TO CG around 29% MAC
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Table is established using standard and alternate pax weights with 13
kg of checked-in baggage per pax for holiday charter flights and 15 kg for non-holiday charter flights
...


With respect to aircraft’s ground stability, at all times forward cargo compartment 1 MUST be loaded first and
off-loaded last!

Total Number of
Pax to Seat

Load Distibution
In compartment
(% of Total Load)

Pax seat in Cabin Section
OA
(Row 1-10)

OB
(Row 11-20)

OC
(Row 21-30)

1

3

4

Up to 25

--

0 - 25

--

40%

30%

30%

26 - 40

--

25

1 - 15

40%

30%

30%

41 - 50

1 - 10

25

15

40%

30%

30%

51 - 75

20

16 - 40

15

40%

30%

30%

76 - 100

25

36 - 60

15

40%

30%

30%

101 - 125

35

36 - 60

30

40%

30%

30%

126 - 150

45

36 - 60

45

40%

30%

30%

151 - 180

60

31 - 60

60

40%

30%

30%

Max
...
Please always check with last revision of
AHM560 which has been distributed to handling companies via e-mail
...
In order to confirm that the baggage in cargo compartments has been loaded in
respect with 6 cm Maximum Loading Height Regulation
...


Note4 :

Fill Cargo Compartment 5 (capacity = 1497 kg) when other Compartments are full
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09
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LOAD CONTROL
GOM

5
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Loading Procedure Airbus A321-231
Freebird Airlines uses table below for standard load planning
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Table is established using
standard and alternate pax weights with 13 kg of checked-in baggage per pax for holiday charter flights and
15 kg for non-holiday charter flights
...


With respect to aircraft’s ground stability, at all times forward cargo compartments 1 & 2 MUST be loaded
first and off-loaded last!

Total Number
of Pax to Seat

Load Distibution
In compartment
(% of Total Load)

Pax seat in Cabin Section
OA

OB

OC

1

2

3

4

5

--

--

--

50%

50%

--

1 - 30

20

--

50%

50%

--

--

10

21 -40

30

--

50%

50%

--

--

81 -100

20

26 - 45

35

10%

20%

30%

30%

10%

101 - 120

25

36 - 55

40

10%

20%

30%

30%

10%

121 - 140

30

41 - 60

50

10%

20%

30%

30%

10%

141 - 160

35

46 - 65

60

10%

20%

30%

30%

10%

161 -180

40

51 - 70

70

10%

20%

30%

30%

10%

180 - 202

32 - 53

77

72

10%

20%

30%

30%

10%

Max
...
Please always check with last revision of
AHM560 which has been distributed to handling companies via e-mail
...
In order to confirm that the baggage in cargo compartments has been loaded in
respect with 6 cm Maximum Loading Height Regulation,

Note3:

LMC loading should be evenly distributed between the cargo compartments 1 and 2 on one
side and 3 and 4 on the other side when it exceeds 250 kg
...


Rev10 / 18
...
2013

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6

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3 Load & Trim Sheet

1
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1 Passenger Weights
Figures below are i
...
w
...
620
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1) and the Turkish DGCA’s SHT J (17d
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Standard Pax Weights
Pax Category
Adult Male
Adult Female
Child
Infant
Pax Category
All Adult
Child
Infant

Holiday Charter Flights
Non-Holiday Charter Flights
83 kg
88 kg
69 kg
70 kg
35 kg
35 kg
10 kg
10 kg
Alternative Pax Weights
Holiday Charter Flights
Non-Holiday Charter Flights
76 kg
84 kg
35 kg
35 kg
10 kg
10 kg

Note : The trim section of the Weight & Balance Sheet contains two different scales for Holiday & Non-Holiday Charter Flights
...
Please always check with last revision of
AHM560 which has been distributed to handling companies via e-mail
...
2 Crew Member’s Weights
Cockpit crew (including crew hand baggage) = 85 kg
Cabin crew (including crew hand baggage) = 75 kg
Weights of operating crew are included in Dry Operating Weight (DOW)
...


Rev08 / 10
...
2012

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7

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3 Load & Trim Sheet

1
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If -for any reason- weighing is not
possible (for instance LMC´s) a minimum of 15 kg per piece shall be taken
...
This average baggage weight per piece
shall be multiplied with the number of pieces loaded in each compartment to get the total weight of baggage
of each compartment
...

While getting the final figures, the information to Load control before establishing final figures includes
communication about hold baggage, individual or cumulative masses, that exceed normal allowances, also
gate delivery items, including individual or cumulative weights that exceed normal allowances, and lastly
about other non-normal items that must be considered in the load control process
...

The cargo agent shall register the number of pieces and the total weight per destination, and transmit the
type of freight and the number of pieces to mass and balance staff in order to ensure proper load planning
...


Note1:

All compartment loads for an Airbus A320/ 321 shall ensure a space limit of 6cm between
load and compartment ceiling
...


Note3:

Do not add the Gate / Ramp Delivery Baggage to the total Baggage Weight when loaded
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1
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This average baggage weight shall be multiplied with the number of pieces
loaded in each compartment
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Estimated max: baggage load means: the baggage has to be sorted out and be weight once again before
loading into the compartments
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09
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LOAD CONTROL
GOM

5
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This procedure applies only for migrantworker charter flights and for charter flights with higher baggage free allowance up to 30 kg
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Rev10 / 18
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2013

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current prior to use

9

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3 Load & Trim Sheet

2
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3
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1 and 5
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2
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The cockpit crew will prepare the Trip Information Sheet (Please see GOM Appendix) and hand it over to the
handling agent
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The cockpit crew is responsible for checking the correctness of Load & Trim sheet
...


However, if the handling agent is not able to provide the load control service, the load & trim sheet should be
filled out by the cockpit crew according to given loading instructions
...
) should be
kept in the departure station at least for satisfactory completion of the flight
...
6
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Rev10 / 18
...
2013

Uncontrolled copy when downloaded
Check Quality Management Software to verify this version is
current prior to use

10

5
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3 Load & Trim Sheet

Table of Format
Ref
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Printed Heading

Description

1

Address

SITA Address for Load MSG

2

Originator

SITA Address of originator

Always to be shown

3

Flight

Flight number identifier

Entered by cockpit crew

4

A/C Reg
...
of transit PAX incl
...
in standard

agent

passenger weight
Total no
...

11

Number of PAX

PAD and weight of cabin

Entered by Load sheet

BAG; not incl
...
of outgoing PAX
incl
...
in

Used for LDM

standard passenger weight
(incl
...
09
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LOAD CONTROL
GOM

Ref
...


5
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EIC and Comail

16

Total M

Weight of joining mail

17

Total T

18

19

20

Sum
...
no
...
LMC)

15 and 16
...
LMC)
PAX

Seat(s) occupied by transit
passenger, including PAD(s)
Seat(s) occupied by joining

21

22

Total weight of dead load

passenger, including PAD(s)
PAD

Seat(s) occupied by transit
PAD(s)
Seat(s) occupied by joining

23

PAD(s)
Total seat(s) occupied by

24


...

PAD(s) and LMC

25


...
LMC

Sum of ref
...

Used for LDM
Sum of ref
...
22 and
23
...
of PAX and weight
26

Total no
...
in
standard passenger weight

27

Total weight of dead load
Total weight of dead load

28

per hold
Total number of seat(s)

29

Sum of ref
...
no
...


Rev05 / 09
...
2009

Sum of ref
...
22 and 23

Actual Pax Figure for Cabin

As

per

passenger

Zone 0A, 0B and 0C

seating onboard

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12

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No
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3 Load & Trim Sheet

Printed Heading

Notes:

Si:

Description
Information not transmitted
with LDM
Supplementary Information
Free format

Dry Operating

Weight of A/C excluding

Weight

traffic load and Fuel

35

ZERO FUEL

36

TAKE-OFF

37

LANDING

Allowed max
...
weight for A/C
for take-off
Allowed max
...
no
...
no
...

Entered by cockpit crew

39

Take-off fuel

Amount of fuel on board
before start take-off roll

Entered by cockpit crew
shall never be higher

Actual take-off weight - sum

than the max take-off

of ref
...
38 and ref
...
39

40

weight (ref
...
36)
...


than the max landing

no
...
no
...
no
...

Entered by cockpit crew

43

Balance

44

Approved by

45

Rev05 / 09
...
2009

Balance conditions (MAC
Takeoff etc
...
LOAD CONTROL
GOM

Ref
...


5
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s

Entered by cockpit crew

QNH:
EFP:

Rev05 / 09
...
2009

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14

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3 Load & Trim Sheet

2
...
Please always check with AHM560 for
last revision
...
09
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LOAD CONTROL
GOM

5
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2 Load & Trim sheet Airbus A321-231 (F – FO – 004)

Note:

This is just a sample of concerned document
...
09
...

Uncontrolled copy when downloaded
Check Quality Management Software to verify this version is
current prior to use

16

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3 Load & Trim Sheet

3
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AVI/2

flwd
...
loading pos
...
by 2-3 numeric for weight

Crew positioning to / from duty, not

1 numeric for seats occ
...


per class

Equipment in Compartment e
...


1 numeric to ind
...
/

spare parts (un-manifested)

flwd
...
in

1 numeric to ind
...
flwd
...
loading pos
...


by 2-3 numeric for weight

other than Crew perf
...



...
COM/4/123


...
EIC/2/75


...
HEA/2/200

by 2-3 numeric for weight
1 numeric to ind
...
flwd
...
AOG/1

1 numeric to ind
...
/

HEA

MOS

1 numeric to ind
...

1 numeric to ind
...


AOG Spare Parts required for A/C on

Example

1 numeric for seats occ
...
HUM/2/170


...
NIL

PAX not entitled to a firm booking
PAD

who may be off loaded to

1 numeric for seats occ
...
PAD/0/0/6

priority

SEC

Item removed from passenger for
security reason

incl
...
PAX figures

Rev09 / 28
...
2012

by 1-3 numeric to ind
...
of


...
PAX-seat(s)
XCR

1 numeric to ind
...
flwd
...
seats occ
...
XCR/0/0/1

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17

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4 Last Minute Change (LMC)

5
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2
...
2
...


A320:

A321:

Rev09 / 28
...
2012

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current prior to use

18



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