AD 83-02-10

Airworthiness directive · Icing Prevention · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 9 more

Effective
March 31, 1983
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
39-4550

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

83-02-10 BOEING: Amendment 39-4550. Applies to Boeing Model 747 series aircraft certificated in all categories. Serial numbers as indicated in the following service bulletins.

Within the next 3000 hours time in service after the effective date of this AD, unless previously accomplished, modify the affected aircraft as noted below in accordance with the following service bulletins or later FAA approved revisions:

1. Applies to aircraft listed in Boeing 747 Service Bulletin 27-2065 dated February 22, 1971. To prevent icing of the aileron control cables in the right wing gear wheel well, modify the aircraft in accordance with the Accomplishment Instructions of Boeing 747 Service Bulletin 27- 2065 dated February 22, 1971.

2. Applies to aircraft listed in Boeing 747 Service Bulletin 27-2095 dated June 5, 1972. To prevent icing of the aileron control cables in the left wing gear wheel well, modify the aircraft in accordance with the Accomplishment Instructions of Boeing747 Service Bulletin 27-2095 dated June 5, 1972.

3. Applies to aircraft listed in Boeing 747 Service Bulletin 27-2161 dated March 4, 1977. To prevent icing of the aileron control cables in the left wing gear wheel well, modify the aircraft in accordance with the Accomplishment Instructions of Boeing 747 Service Bulletin 27- 2161 dated March 4, 1977.

4. Applies to aircraft listed in Boeing 747 Service Bulletin 51-2032 dated November 20, 1981. To prevent icing of the aileron control cables in the left wing gear wheel well, modify the aircraft by installation of an MS28778-8 "O" ring or replace the knurled nut with an AN818L- 10 nut in accordance with Boeing 747 Service Bulletin 51-2032 dated November 20, 1981.

5. Alternate means of compliance with this AD which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, Northwest Mountain Region.

6. Aircraft may be ferried to a base for maintenance in accordance with Section 21.197 and 21.199 of the Federal Aviation Regulations.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. These documents may also be examined at FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective March 31, 1983.

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