AD 90-26-51

Airworthiness directive · Outboard Leading Edge Slat · Boeing 767-200 Series, 767-300 Series and 767-300F Series

Effective
February 19, 1991
Models
767-200 Series, 767-300 Series, 767-300F Series
Data sheet
TCDSA1NM
Registered aircraft
402 matched by model
Product
Aircraft · Large airplane
Amendment
39-6881
Docket
90-NM-278-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

90-26-51 BOEING: Amendment 39-6881. Docket No. 90-NM-278-AD. Final Rule of Telegraphic AD.

Applicability: Model 767 series airplanes, line number 001 through 340, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To detect defective torque tube fittings in the leading edge slat drive system, accomplish the following:

A. Within the next 20 days after the effective date of this AD, inspect the outboard leading edge slat torque tube fittings in accordance with Boeing Alert Service Bulletin 767- 27A0110, dated December 13, 1990.

1. If a defective torque tube fitting is found, prior to further flight, replace the fitting or install a new torque tube assembly in accordance with Boeing Alert Service Bulletin 767-27A0110, dated December 13, 1990.

2. No further action is required if the torque tube fitting is found to have the correct dimensions.

B. Within 10 days after completion of the inspection required by paragraph A. of this AD, submit a report of findings of discrepancies to the Manager, Seattle Manufacturing Inspection District Office, FAA, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington 98055-4056; Rapid fax: (206) 227-1181.

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 (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.

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 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.

This amendment (39-6881, AD 90-26-51) becomes effective on February 19, 1991, as to all persons, except those persons to whom it was made immediately effective by telegraphic AD T90-26-51, issued on December 13, 1990, which contained this amendment.

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

By model

See all 35 models

Aircraft

See all 402 aircraft