AD 92-07-10

Airworthiness directive · Wire Bundles · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 6 more

Effective
May 4, 1992
Models
737-100 Series, 737-200 Series, 737-200C Series, 737-300 Series, 737-400 Series, 737-500 Series and 3 more
Data sheet
TCDSA16WE
Registered aircraft
823 matched by model
Product
Aircraft · Large airplane
Amendment
39-8206
Docket
91-NM-93-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

92-07-10 BOEING: Amendment 39-8206. Docket No. 91-NM-93-AD.

Applicability: Model 737 airplanes, as listed in Boeing Service Bulletin 737-24-1077, Revision 2, dated July 25, 1991, and Boeing Service Bulletin 737-24-1084, Revision 1, dated March 21, 1991; certificated in any category.

Compliance: Required within 6 months after the effective date of this AD, unless accomplished previously.

To prevent chafing of wires and electrical overload of wires, and to remove the potential for a fire in the cockpit, accomplish the following:

(a) For airplanes listed in Boeing Service Bulletin 737-24-1077, Revision 2, dated July 25, 1991: Modify the wire bundles and install a capped quick release receptacle and nutplate, in accordance with Boeing Service Bulletin 737-24-1077, dated August 17, 1989; or Revision 1, dated August 16, 1990; or Revision 2, dated July 25, 1991.

(b) For airplanes listed in Boeing Service Bulletin 737-24-1084, Revision 1, dated March 21, 1991:Replace the undersized wire with a 12 gauge wire in the P6-2 circuit breaker panel, in accordance with Boeing Service Bulletin 737-24-1084, dated October 11, 1990; or Revision 1, dated March 21, 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 the airplane to a location where the requirements of this AD can be accomplished.

(e) The modifications shall be done in accordance with Boeing Service Bulletin 737- 24-1077, dated August 17, 1989, or Revision 1, dated August 16, 1990, or Revision 2, dated July 25, 1991; and in accordancewith Boeing Service Bulletin 737-24-1084, dated October 11, 1990, or Revision 1, dated March 21, 1991. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Northwest Mountain Region, 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 May 4, 1992.

Affected TCDS · 1

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

Registered aircraft · 823

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
  • Boeing823 aircraft
By year built
19692025
Registered aircraft by year built: 785 aircraft
19691
19751
19791
19811
19863
19874
19892
19901
19915
19924
19934
19941
19953
19972
199840
199987
200072
200173
200210
20037
200413
200514
200621
200721
200826
200938
201062
201121
201230
201331
201423
201520
201642
201772
201827
20252

38 with no year recorded

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