AD 92-10-01

Airworthiness directive · Inboard Spoilers · Boeing 767-200 Series, 767-300 Series and 767-300F Series

Effective
June 11, 1992
Models
767-200 Series, 767-300 Series, 767-300F Series
Data sheet
TCDSA1NM
Registered aircraft
402 matched by model
Product
Aircraft · Large airplane
Amendment
39-8234
Docket
91-NM-240-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

92-10-01 BOEING: Amendment 39-8234. Docket No. 91-NM-240-AD. Supersedes AD 91-15-13, Amendment 39-7077.

Applicability: Model 767 series airplanes, as listed in Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991; certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent the overwing escape slide from being damaged by sharp edges of the rub strip on the inboard spoilers, accomplish the following:

(a) Except as provided by paragraph (b) of this AD, within the next 9 months after August 29, 1991 (the effective date of amendment 39-7077), modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, dated November 15, 1990, or Revision 1, dated May 30, 1991.

(b) For airplanes equipped with inboard spoiler assemblies, part numbers 113T4100-37, -38, -41, -42, -45, and -46: Within the next 9 months after the effective date of this AD, modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991.

(c) An alternative method 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. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO.

(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.

(e) The modification shall be done in accordance with Boeing Service Bulletin 767-27-0104, dated November 15, 1990; or Revision 1, dated May 30, 1991; or Revision 2, dated September 12, 1991; as applicable. This incorporation by reference was approved by theDirector of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. (The incorporation by reference of Boeing Service Bulletin 767-27-0104, dated November 15, 1990, and Revision 1, dated May 30, 1991, was previously approved by the Director of the Federal Register as of August 29, 1991 (56 FR 34019, July 25, 1991).) Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC.

(f) This amendment becomes effective on June 11, 1992.

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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