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Required Field
Design
Engineering Requirements
The following
items are required for engineering design. Please advise if these
items are available:
A. Digital
photos, pictorial or descriptive layout of the current EGPWS/TAWS Computer
installation in the E/E bay compartment, Fwd/Aft Pedestal, Circuit Breaker & Instrument Panels and Current location of the existing EGPWS switches and annunciators. Pictures of available space for mounting new equipment will be necessary unless a survey of the aircraft by ASM is required.
Yes
No
B. Chapters 21-91 of:
Wire Diagrams
Yes
No
Maintenance Manual
Yes
No
IPC
Yes
No
Wire/Hook up list
Yes
No
Production Illustration Drawings (STC Cert.)
Yes
No
DFDR/DFDAU interface/operational function options:
Number of new parameters needed to record?
Number of existing parameters recorded?
Is the aircraft EFIS or an Analog aircraft?
If a B737, does the aircraft have Boeing Thrust Reverser SB 737-1059?
Are the Thrust Reverser inputs (if existing) digital or analog?:
If a B737, does the aircraft have Boeing Sensor & Wiring Installation SB 737-1099:
How many possible effectivity groups of aircraft?
Electrical Load and Weight & Balance Data for equipment to be removed?
Location for the installation to be performed?
Is the installation to be a special visit or scheduled for down time? Dates?
Equipment Part Numbers
Need Make, Model, Part Number, Location and Quantity of all major avionics equipment on the aircraft that the DFDR/DFDAU may interface with:
Notes or Questions:
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