AD 88-24-12

Airworthiness directive · Self-Locking Nut · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more

Effective
December 23, 1988
Models
727-100 Series, 727-100C Series, 727-200 Series, 727-200F Series, 727 Series, 727C Series
Data sheet
TCDSA3WE
Registered aircraft
25 matched by model
Product
Aircraft · Large airplane
Amendment
39-6068

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

88-24-12 BOEING: Amendment 39-6068. Applies to all Model 727 series airplanes, prior to line number 1620, not equipped with the safety bar modification described in Boeing Service Bulletin 727-32-275, Revision 2, dated March 30, 1984, certificated in any category. Compliance required within the next 3,500 flight cycles after the effective date of this AD, unless previously accomplished.

To prevent failure of the main landing gear (MLG) to extend as a result of loosening of the self-locking nut at the attachment of the downlock forward pushrod assembly to the downlock torque shaft, accomplish the following:

A. Modify airplanes listed in Boeing Service Bulletin 727-32-0237, Revision 5, dated July 7, 1988, by installing the bolt, washer, nut, and cotter pin called out in item 5 of Figure 5 of that service bulletin.

B. Modify airplanes listed in Boeing Service Bulletin 727-32-0353, Revision 1, dated July 7, 1988, by installing the bolt, washer, nut, and cotter pin in accordance with that service bulletin.

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, 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.

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 Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents 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, 39-6068, becomes effective December 23, 1988.

Affected TCDS · 1

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

Registered aircraft · 25

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
  • Boeing25 aircraft
By year built
19711982
Registered aircraft by year built: 18 aircraft
19711
19731
19752
19763
19772
19782
19791
19815
19821

7 with no year recorded

By model

Aircraft

See all 25 aircraft