AD 90-20-20

Airworthiness directive · Nacelle Thrust Inspection · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 9 more

Effective
October 23, 1990
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
39-6725
Docket
90-NM-79-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

90-20-20 BOEING: Amendment 39-6725. Docket No. 90-NM-79-AD.

Applicability: Model 747 series airplanes, line numbers 1 through 783, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent engine separation, accomplish the following:

A. Prior to the accumulation of 10,000 total flight cycles or within the next 1,000 flight cycles after the effective date of this AD, whichever occurs later, perform either a detailed visual inspection or an ultrasonic inspection of the nacelle strut diagonal braces for cracks in accordance with Boeing Service Bulletin 747-54-2123, dated March 1, 1990.

Repeat these inspections as follows:

1. If the immediately preceding inspection was accomplished visually, the next inspection must be conducted within 1,000 flight cycles.

2. If the immediately preceding inspection was accomplished ultrasonically, the next inspection must be conducted within 3,000 flight cycles.B. If cracking is found, replace the nacelle strut diagonal brace with a serviceable brace prior to further flight.

C. Replacement of the nacelle strut diagonal brace with a new production diagonal brace, which has revised internal and external surface finish, in accordance with the method described in Boeing Service Bulletin 747-54-2123, dated March 1, 1990, constitutes terminating action for the inspections required by paragraph A. of this AD.

D. For the purposes of compliance with this rule, two "touch-and-go" training flights may be considered equivalent to one flight cycle.

E. 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.

F. 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 (39-6725, AD 90-20-20) 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 · 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