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six hours to build using Word now take just
minutes to complete,” says Yagaloff.
Since adopting FrameMaker+SGML in 1999,
Gables has increased the quality of its documentation
while dramatically improving
workflow. For example, instead of eight
weeks, the company now produces its largest,
300-page manuals in no more than two.
Moreover, says Yagaloff, “The Gables tech
pubs team now really understands structured
authoring and uses FrameMaker+SGML
very skillfully and effectively. In fact, Gables
is way ahead of its peers on delivering SGML
documents to customers.”
The Structure View and element definitions within FrameMaker+SGML automate the complexities of SGML
and keep authors focused on writing rather than technicalities, while preset styles improve document
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A320 system guide
OVERHEAD GENERAL
A320 Overhead and ECAM Software for Microsoft Flight simulator 2002
By
Copyright and Development
Holger Johannsen and Steffen Herberg
A320 System guide
GENERAL OVERHEAD HANDLING
The first thing to do after all systems in your cockpit are running is to select
the OHL RUN / PAUSE button.
Set it to RUN! The RUN light must illuminate.
This function is implemented because of that the OHL software goes in and
hides systems like PFD and ND displays from Project Magenta. So if you want
check all system running well you must set the OHL to PAUSE.
PAUSE is the default start status of the OHL software.
Now we are ready to work with the overhead.
DARK OVERHEAD IS GOOD!
If no lights are illuminating, everything is OK! That’s the logic of airbus.
So you can take these words in mind:
Light on, something wrong!
An on light is not a fault in every case, but it’s not the way it should be!
ALL WHITE LIGHTS OUT!
This is one of the major key functions in the airbus. A white light tells the
pilot that a system is set to off. In the normal procedure all white lights
should be off.
The on or off light on the button tells only the state of the button, not the
state of the system!
That’s not completely true, if the button is off, the system is off too. If the
button set to on, the system is able to connect the system if its avail. So the
aircraft system self connect system busses and power to the system.
ON LIGHT IS BLUE!
2-3
A320 System guide
GENERAL OVERHEAD HANDLING
All ON lights are in a blue color. So if a blue light is illuminating on the
overhead, is it been selected manual to this status.
Electric pumps, apu, gpu and other system will show a blue on light when
selected.
TEMPORARY SYSTEMS ARE GREEN!
All systems that only run temporary will illuminate with a green AVAIL light.
FAULT LIGHTS ARE AMBER
All fault lights are shown in an amber color. Only smoke or fire lights are red.
3-3
Gillfab™ 3072 Profile June 2002
Description
Woven glass reinforced phenolic "h" profile.
Applications
Used for the installation of replacement decompression panels in the lower cargo hold of Airbus
Industrie A300, A310, A300-600, A319, A320 and A321 aircraft.
Features
• Airbus Industrie 2550 M1M 0004 00.
• FAR Part 25, Appendix F, Parts I and III (burn through)
• M.C. Gill Report AIM 2001 - Airline Instruction Manual for Cargo Liner Laminates and Panels.
• Service temperature to 158°F (70° C)
Availability
Length: Up to 70" (1778 mm) + 1.0” (25.4mm) /-0
Nominal Thickness and Width Dimensions of Sandwich Panels and Corresponding h-Profiles
Sandwich Panel Corresponding h-Profile
Airbus
Type
Nominal
Thickness, mm
(in.)
M.C. Gill Panel
Identification
Airbus
Type
Nominal Width
of Channel mm
(in.)
M.C. Gill h-Profile
Identification
A 7.5 (0.295) Gillfab 4422-295 A 8.2 (0.323) Gillfab 3072A
C 8.0 (0.315 Gillfab 4422-315 A 8.2 (0.323) Gillfab 3072A
D 9.3 (0.366) Gillfab 4422-366 B 10.0 (0.394) Gillfab 3072B
E 9.8 (0.386) Gillfab 4422-386 B 10.0 (0.394 Gillfab 3072B
G 12.9 (0.508) Gillfab 4422-508 C 13.1 (0.516) Gillfab 3072C
H 15.5 (0.610) Gillfab 4422-610 D 16.0 (0.630) Gillfab 3072D
To ensure correct functioning of the decompression panel assembly, the corresponding sandwich panel
and h-profile must be used together. Failure to follow this procedure can cause a change in the geometry
of the assembly, resulting in possible malfunctioning during a decompression event.
　
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