AD 83-02-10

Active

Icing Prevention

Key Information
83-02-10
Active
March 31, 1983
Not specified
Unknown
39-4550
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
747-100 Series 747-100B Series 747-100B SUD Series 747-200B Series 747-200C Series 747-200F Series 747-300 Series 747-400 Series 747-400D Series 747-400F Series 747SP Series 747SR Series
Regulatory Text

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. \n\n\tWithin 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: \n\n\t1.\tApplies 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. \n\n\t2.\tApplies 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. \n\n\t3.\tApplies 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. \n\n\t4.\tApplies 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. \n\n\t5.\tAlternate 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. \n\n\t6.\tAircraft may be ferried to a base for maintenance in accordance with Section 21.197 and 21.199 of the Federal Aviation Regulations. \n\n\tThe 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). \n\n\tAll 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. \n\n\tThis amendment becomes effective March 31, 1983.

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References
This information is not available.
--- - Part 39
FAA Documents