AD 89-08-09

Airworthiness directive · Pulley Bracket · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 9 more

Effective
April 24, 1989
Models
747-100 Series, 747-100B Series, 747-100B SUD Series, 747-200B Series, 747-200C Series, 747-200F Series and 6 more
Data sheet
TCDSA20WE
Registered aircraft
63 matched by model
Product
Aircraft · Large airplane
Amendment
39-6188

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

89-08-09 BOEING: Amendment 39-6188. Applicability: Model 747 series airplanes, as listed in Boeing Alert Service Bulletin 747- 76A2074 dated January 19, 1989, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To eliminate the potential for uncommanded thrust operation due to engine control cable rupture, accomplish the following:

A. Within the next 30 days after the effective date of this AD, inspect control cable pulley bracket assemblies of the outboard engines located at Inboard Leading Edge Station (ILES) 1116 for proper installation and wear, and attach decals, in accordance with the accomplishment instructions of Boeing Alert Service Bulletin 747-76A2074, dated January 19, 1989.

B. If the installation is incorrect, prior to further flight, remove and install the pulley bracket in the correct position; and/or if parts are found to be worn, prior to further flight, replace worn parts; in accordance with theaccomplishment instructions of Boeing Service Bulletin 747-76A2074.

C. Report any incorrect pulley bracket installations detected during the inspections required by paragraph A., above, to the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, within seven days after the completion of the inspection.

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, 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.

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 information from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at 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 (39-6188, AD 89-08-09) becomes effective on April 24, 1989.

Affected TCDS · 1

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

Registered aircraft · 63

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
  • Boeing63 aircraft
By year built
19692007
Registered aircraft by year built: 49 aircraft
19691
19702
19711
19752
19761
19892
19904
19916
19922
19932
19943
19951
19974
19981
19994
20001
20011
20023
20031
20041
20053
20073

14 with no year recorded

By model

See all 24 models

Aircraft

See all 63 aircraft