AD 88-15-04

Airworthiness directive · Main Landing Gear Actuators · Boeing 767-200 Series, 767-300 Series and 767-300F Series

Effective
August 3, 1988
Models
767-200 Series, 767-300 Series, 767-300F Series
Data sheet
TCDSA1NM
Registered aircraft
402 matched by model
Product
Aircraft · Large airplane
Amendment
39-5979

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

88-15-04 BOEING: Amendment 39-5979. Applies to Model 767 series airplanes, as listed in Boeing Alert Service Bulletin 767-32A0071, dated June 2, 1988, certificated in any category. Compliance required as indicated, unless previously accomplished.

To preclude failure of the main landing gear to fully extend and lock due to faulty actuator piston seals or obsolete configuration rod seals, accomplish the following:

A. Within the next 300 hours time-in-service after the effective date of this AD, inspect the main landing gear drag brace actuators in accordance with Boeing Alert Service Bulletin 767-32A0071, dated June 2, 1988.

B. If any actuator has accumulated less than 200 hours total time-in-service at the time of inspection, repeat the inspection required by paragraph A., above, at intervals not to exceed 100 hours time-in-service until the actuator has accumulated more than 200 hours time- in-service, at which time the inspections may be terminated.

C. If anyactuator is found to have swollen seals or obsolete configuration seals, before further flight, replace or modify the actuator, in accordance with Boeing Service Bulletin 767-32A0071, dated June 2, 1988.

D. Accomplishing the piston seal replacement, and the rod seal inspection and replacement, if necessary, in accordance with Boeing Service Bulletin 767-32A0071, dated June 2, 1988, constitutes terminating action for the initial and repetitive inspections required by paragraphs A. and B., above.

E. 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 may add any comments and then send it to the Manager, Seattle Aircraft Certification Office.

F. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the inspections required by this AD.

All persons affected by this directive who have not already received copies of the appropriate service bulletin cited herein may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment, 39-5979, becomes effective August 3, 1988.

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

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Aircraft

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