AD 80-09-02

Historical

Airworthiness directive · Model Electric Pitch Trim Computers · British Aerospace and Societe Nationale Industrielle Aerospatiale Concorde Type I

Effective
April 14, 1980
Published
April 14, 1980
Issued
April 14, 1980
Model
Concorde Type I
Data sheet
TCDSA45EU
Product
Aircraft · Large airplane
Amendment
39-3755

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed November 21, 2025.

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The airworthiness directive

80-09-02 BRITISH AEROSPACE/SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE: Amendment 39-3755. Applies to all Concorde Type I airplanes, certificated in any category.

To prevent unwanted deviation from the flight path, accomplish the following:

(a) Prior to the next flight after the effective date of this AD, unless already accomplished, remove electrical pitch trim computers 1C151 or 2C151 and install in their place modified electrical pitch trim computers, P/N 49-004.071C51 or P/N 49-004.072C151, as appropriate, in accordance with Concorde Campaign Wire 22CW019, issue 2, dated March 27, 1979, or an equivalent approved by the Chief, Aircraft Certification Staff, Federal Aviation Administration, Europe, Africa, and Middle East Region, c/o American Embassy, Brussels, Belgium.

NOTE: Concorde service bulletin 22A019 (Mod. 1669) also concerns the installation of the modified electrical pitch trim computers.

This supersedes telegraphic airworthiness directive datedApril 6, 1979.

This amendment becomes effective April 14, 1980.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft

No registered aircraft matched this AD’s modelsForeign aircraft aren’t included, and ADs on propellers and appliances aren’t matched by model.