AD 89-21-04 R1

Airworthiness directive · Engine Control Wiring · Boeing 767-200 Series, 767-300 Series and 767-300F Series

Effective
March 29, 1990
Models
767-200 Series, 767-300 Series, 767-300F Series
Data sheet
TCDSA1NM
Registered aircraft
402 matched by model
Product
Aircraft · Large airplane
Amendment
39-6549
Docket
88-NM-201-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.

On this page

The airworthiness directive

89-21-04 R1 BOEING: Amendment 39-6349 as corrected by Amendment 39-6549. Docket No. 88-NM-201-AD.

Applicability: Model 767 series airplanes, equipped with Pratt and Whitney JT9D series engines or General Electric CF6-80A series engines, specified in Boeing Service Bulletin 767- 71-0041, dated September 22, 1988, certificated in any category.

Compliance: Required within 15 months after the effective date of this AD, unless previously accomplished.

To minimize the potential for a thrust loss greater than the loss of one engine due to a lightning strike, accomplish the following:

A. Modify the engine electrical and electronic engine control wiring in accordance with Boeing Service Bulletin 767-71-0041, dated September 22, 1988; Revision 1, dated April 6, 1989; or Revision 2, dated June 29, 1989.

B. 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, Seattle Aircraft Certification Office, 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, Seattle Aircraft Certification Office.

C. 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 Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or at the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

The effective date for the requirements of this amendment remains November 8, 1989, as specified in Amendment 39-6349, AD 89-21-04.

This AD revises AD 89-21-04, Amendment 39-6349. This amendment (39-6549, AD 89-21-04 R1) becomes effective on March 29, 1990.

Affected TCDS · 1

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

Registered aircraft · 402

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
  • Boeing402 aircraft
By year built
19822026
Registered aircraft by year built: 363 aircraft
19824
19837
19849
19854
19861
19871
19884
19895
19909
199115
199221
199313
19946
199511
19969
199712
199819
199915
20009
20019
20022
20031
20042
20051
20064
20081
20105
20111
20124
20166
201710
201817
201920
202020
202118
202216
202317
202410
202515
202610

39 with no year recorded

By model

See all 35 models

Aircraft

See all 402 aircraft