Weight and Balance is also
known as Load Control and it is part of each airlines operational
responsibility. The primary function of Load Control within
aircraft handling is to provide the Load Manifest or Load Sheet,
which shows the number of “souls” onboard and baggage/cargo/mail
figures. This document also shows that the center of gravity
of the aircraft is within balance limits and that the maximum
aircraft weights are also within their limits. There are many
significant documents that must be produced by the weight and
balance department including the Loading Instruction, Balance
Table and Load Sheet. An explanation of these documents is available
in the Airline Departure Process Document. There are also many
terms used within Weight and Balance that are also explained
in the Airline Departure Process Document.
Prior to the flight, the agent
produces a loading instruction for the Loadmaster. This is an
automated process within the AS system whereby based on booked
figures and aircraft information, the agent will produce a plan
for loading positions. The AS system produces a Ramp check list,
unloading information for inbound aircraft and loading instruction
for departure flight on the same document thus producing the
plan and a quality control document for ramp staff on one document.
The ramp checklist section begins
with the aircraft registration, scheduled time for arrival/departure,
destination, airline operator, aircraft type, version and crew
information. The actual checklist itself contains numerous areas,
which need to be filled in including time of fueling, cleaning
and catering. The checklist also contains any information regarding
inbound passengers (e.g. WCHR), which may slow down the departure
of the aircraft. This data is entered into the computer post-departure
for historical and quality control information.
The unloading instruction to
the ramp staff comes in the form of the inbound load message
advising where and what is loaded onboard. It will also advise
of any load staying on board i.e. transit load.
The Loading instruction section
contains an account of each hold or compartment number and will
usually be manually filled out to advise where expected outbound
load is to be positioned. Transit load is also accounted for
here.
As soon as the check-in and boarding
process is complete the weight and balance department are notified.
This notification comes in the form of a traffic light system
within the module of each flight. When the light is red the
agents are aware that the aircraft weights etc. can still change,
as the aircraft is still open for check-in or boarding. When
the light changes to green this is called the hand-over to weight
and balance stage as the agent can now see that check-in and
boarding are completed with this aircraft so it is now safe
to prepare final data.
The aircraft information (maximum
weights, schedule information, balance etc.) is already contained
within the CDB (as explained in CDB). The agent must now layer
all the other information required to prepare the final paperwork.
The agent receives the actual fuel figures from the fuel company
and adds it to the Loadsheet and Loadmessage screen. Once these
figures are added, immediately the agent will see figures starting
to change within the screen. Then the agent activates the function
to bring over passenger and baggage data to the same screen
and once again all figures will change. The agent must then
get final cargo and mail figures from cargo department (explained
later) and as before all data will change. The last item required
is the actual positions and weights for cargo, baggage and mail
(called deadload) received from the Load master based on the
original loading instruction.
At this stage the agent can see
if all weights and balance (trim) are within limits. In the
AS system this trim sheet including The Center of Gravity Position,
is represented in the form of a diagram for simplicity. The
trim sheet will also show “the ideal trim line”
advising the user how close they are to ideal trim. Ideal trim
is used for fuel efficiency and saves the airlines money. This
Ideal trim line can be checked at any stage prior to or during
load planning so the agent can see where baggage, cargo, mail
etc. needs to be moved to in order to achieve this ideal trim
line.
Once the agent is satisfied with
the weight and balance of the aircraft the Load and Trim sheets
may be printed. They can be printed in the IATA standard form,
in a graphical diagram or both.
Although the Weight and Balance
module is vast, AS have managed to make the whole process as
simple and safe as possible. Once again the AS system will prompt
the user with warnings when mistakes are made. The AS system
also prompts the user if there are any problems or possible
problems with weight or balance at an early stage to avoid incorrect
loading instructions or last minute changes to the loading which
often cause delays.
Another important addition is
the information list on all Weight and Balance staff. The AS
system holds an information list on all these staff members,
which aircrafts they can handle and when their license renewal
examination is due.
Within the Weight and Balance
module, depending on the type of user sign in, many changes
can be made. This includes changes to aircraft information,
which will affect the CDB permanently or semi-permanently. Also
alterations may be made after any aircraft departure. It is
possible for the load controller to add any last minute changes
(e.g. late passenger, late offload of cargo etc.) to the final
Load Message and Load sheet after the departure.
With regard to departure, arrival,
delay or load messages, the AS system is fully automated in
the creation of these messages using the details already input
for the particular flight e.g. For the Load message (LDM) an
automatic process is used whereby the user activates a function
post-departure to bring all passenger, baggage, cargo etc. figures
directly into LDM mask and all the user has to do is press “send”.
For the delay messages, within the mask there is a drop down
list with delay codes, sub delay codes and explanations to choose
from. The message mask contains the SITA addresses required
and also a drop down list of all other SITA addresses that possibly
may be required.
It is also possible for an agent
to create an aircraft not already in the CDB, in a very short
space of time by taking an aircraft type similar and changing
or adding information. The agent may save this aircraft type
as a new aircraft if it is to become a permanent fixture or
just undo changes back to the initial aircraft information if
it is an uncommon flight.
Within the AS system it is also
possible to complete a loadsheet without a trim sheet. This
would only be used for smaller aircraft or airlines where the
captain usually completes the aircraft trim.
The AS system incorporates an
Airport Parking Module based on software written by the owners
called Geo Data. This module can advise usable and unusable
parking places for all the different types of aircraft. It is
used as a plan for gate selection of aircraft. The module can,
through the use of colour coding, advise the user at which stage
of the ground operation that the aircraft is at e.g. engines
started ready to go, boarding or arriving on blocks etc.
At present the AS system does
not include any information on Standard Turnaround Times. This
is something they are hoping to incorporate in the future, as
it is invaluable for weight and balance staff and also makes
the production of correct delay codes for departure messages
more accurate. It could also be used as a form of Quality Control
for the airlines.