AD 90-20-14

Airworthiness directive · Cargo Compartment Frames · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more

Effective
October 23, 1990
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
39-6730
Docket
90-NM-25-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

90-20-14 BOEING: Amendment 39-6730. Docket No. 90-NM-25-AD.

Applicability: Model 727 series airplanes, listed in Boeing Service Bulletin 727-53- 0068, Revision 4, dated September 14, 1989, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To detect cracks in the forward cargo compartment sidewall frames, accomplish the following:

A. Except as provided in paragraph B., below, within the next 2,000 flight cycles after the effective date of this AD, or prior to accumulating 15,600 total flight cycles, whichever occurs later, conduct a visual inspection of the forward cargo compartment sidewall frames for cracks, in accordance with the Accomplishment Instructions of Boeing Service Bulletin 727-53- 0068, Revision 4, dated September 14, 1989. Repeat the inspections at intervals not to exceed 9,000 flight cycles.

B. Repair cracked structure prior to further flight, in accordance with the Accomplishment Instructions of the Boeing Service Bulletin, 727-53-0068, Revision 4, dated September 14, 1989, or earlier FAA-approved revisions.

C. Modification of the affected structure in accordance with the Accomplishment Instructions of Boeing Service Bulletin 727-53-0068, Revision 4, dated September 14, 1989, or earlier FAA-approved revisions, terminates the inspection requirements of paragraph A. of this AD.

D. 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 (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

E. 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 Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

Airworthiness Directive 90-20-14 supersedes AD 83-02-08, Amendment 39-4548. Amendment 39-6730, AD 90-20-14, becomes effective on October 23, 1990.

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