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AD 81-06-02 ACTIVE

Emergency Descent Devices
Key Information
AD Number 81-06-02 Status Active
Effective Date March 19, 1981 Issue Date Not specified
Docket Number Unknown Amendment 39-4059
Product Type ["Appliance"] Product Subtype Not specified
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Airbus The Boeing Company Frost Engineering Lockheed Martin Corporation
Model(s) A300 B2-1A A300 B2-1C A300 B2-203 A300 B2K-3C A300 B4-103 A300 B4-203 A300 B4-2C A300 B4-601 A300 B4-603 A300 B4-605R A300 B4-620 A300 B4-622 A300 B4-622R A300 C4-605R Variant F A300 F4-605R A300 F4-622R 747-100 Series 747-100B Series 747-200B Series 747-200C Series 747-200F Series 747SP Series 747SR Series Emergency Descent Devices L-1011-385-1 L-1011-385-1-14 L-1011-385-1-15 L-1011-385-3
Regulatory Text

81-06-02 FROST ENGINEERING DEVELOPMENT CORPORATION: Amendment 39-4059. Applies to emergency descent devices installed on Boeing 747, Lockheed L-1011, and Airbus Industrie A-300 airplanes. \n\n\tCompliance required as indicated. To prevent failure of emergency descent devices accomplish the following: \n\n\tA.\tWithin 30 days from the effective date of this AD, unless already accomplished, inspect Frost Engineering descent devices for broken handle straps in accordance with paragraph 2, steps (1), (2), and (4) of Frost Engineering Development Corporation Service Bulletin 379103-25-002 dated September 29, 1980, or in a manner approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region. \n\n\tB.\tDescent devices found to have a broken handle strap must be modified in accordance with paragraph 2, steps (6) through (9) of Frost Engineering Development Corporation Service Bulletin 379103-25-002 dated September 29, 1980, or in a manner approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region. \n\n\tC.\tWithin 120 days from the effective date of this AD, unless already accomplished, modify the descent devices found to have a magnetic handle strap in accordance with paragraph 2, steps (5) through (9) of Frost Engineering Development Corporation Service Bulletin 379103-25-002 dated September 29, 1980, or in a manner approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region. \n\n\tD.\tWithin 120 days from the effective date of this AD, replace descent devices P/N 379103-1, serial numbers 1 through 0134, with other FAA approved descent devices. \n\n\tE.\tUpon the request of the operator, and subject to prior approval by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region, an FAA Aviation Safety Inspector may adjust the compliance times if the request contains substantiating data to justify the change. \n\n\tThe manufacturer's specification 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 Frost Engineering Development Corporation, P.O. Box 1294, Englewood, Colorado 80150. These documents may also be examined at FAA Northwest Region, 9010 East Marginal Way South, Seattle, Washington 98108. \n\n\tThis amendment becomes effective March 19, 1981.