* Required Field

Customer Name/Contact Name:
Company Name:
Email*:
Phone:
Aircraft Model, Registration and Serial Number(s):

Design Engineering Requirements

The following items are required for engineering design. Please advise if these items are available:

Digital photos, pictorial or descriptive layout of the current Air Data Computer installation in the E/E bay and altimeters/altitude alerter in the Forward Instrument Panel(s) Yes No

Air Data MM Section Yes No

Air Data, Altitude Alert & Reporting and Transponder System Wiring Diagrams
Yes No

Equipment Part Numbers

Make, Model and Part numbers of the following equipment:

If no air data computer is installed identify what provisions are installed (if any):

If only one air data computer is installed identify what provisions are installed (if any) for the 2nd Air Data Computer:

Does the Captain's pitot/static plumbing exist in the E/E bay and if so on what shelf is the plumbing located?

Does the F/O's pitot/static plumbing exist in the E/E bay and if so on what shelf is the plumbing located?

Is there a mounting tray installed in the E/E bay for the No. 1 Air Data Computer? If so
on what shelf is it located?

Is there a mounting tray installed in the E/E bay for the No. 2 Air Data Computer? If so
on what shelf is it located?

Does wiring exist for the No. 2 Air Data Computer (No. 2 Air Data wiring diagram)?
Yes No

If so then a copy or description of this wiring needs to be provided to ASM Engineering.

NOTES:

ASM offers two (2) RVSM compliant STC configurations for the B737 series aircraft. One configuration utilizes a single DADC with a repeater altimeter in the Captain’s instrument panel, an ADDU (Air Data Display Unit) for the F/O’s altimeter and an altitude alerter. The second configuration utilizes dual DADCs with repeater altimeters for the Captain’s and F/O’s altitude indicators and an altitude alerter. Both configurations require that a standby pressure altimeter be available in the P1 or P2 instrument panel.

There are two (2) variants of Pitot/Static installations on the B737 series aircraft:

1. Captain’s pitot/static plumbing to the E/E bay, for most SP-77 series B737-200s. This configuration can use the ASM “single DADC and ADDU configuration”.

2. Captain’s and F/O’s pitot/static plumbing to the E/E bay for B737-200s. This configuration can use the ASM “dual DADC configuration”. Some of these aircraft are equipped with complete provisions for a second air data computer installation.