AD 90-08-11

Airworthiness directive · Wing Flap Electric Control Unit · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A

Effective
May 14, 1990
Models
BAe 146-100A, BAe 146-200A, BAe 146-300A
Data sheet
TCDSA49EU
Registered aircraft
8 matched by model
Product
Aircraft · Large airplane
Amendment
39-6568
Docket
89-NM-234-AD

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 May 30, 2024.

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The airworthiness directive

90-08-11 BRITISH AEROSPACE: Amendment 39-6568. Docket No. 89-NM-234-AD.

Applicability: Model BAe 146-100A, Serial Numbers E1002 and subsequent; Model BAe 146-200A, Serial Numbers E2012 and subsequent; and Model BAe 146-300A, Serial Numbers E3118 and subsequent; certificated in any category.

Compliance: Required within 180 days after the effective date of this AD, unless previously accomplished.

To prevent loss of wing flap asymmetry protection and reduced airplane controllability, accomplish the following:

A. Install an improved wing flap electronic control unit (ECU) in accordance with British Aerospace Service Bulletin 27-95-70420A, dated April 27, 1989.

NOTE: The British Aerospace Service Bulletin references Dowty Rotol Service Bulletin 146-27-75 for additional instructions.

B. Install a warning placard on the front face of the ECU, in accordance with British Aerospace Service Bulletin 27-95-70420A, dated April 27, 1989. The warning placard states:

"WARNING - This equipment must not be removed or re-racked in flight."

C. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6568, AD 90-08-11) becomes effective on May 14, 1990.

Affected TCDS · 1

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

Registered aircraft · 8

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • British Aerospace8 aircraft
By year built
19851989
Registered aircraft by year built: 6 aircraft
19851
19861
19871
19881
19892

2 with no year recorded

By model

Aircraft