AD 87-17-11

Active

Nose Dome Assembly

Key Information
87-17-11
Active
September 24, 1987
Not specified
Unknown
39-5716
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
DC-8-62 DC-8-62F DC-8-63 DC-8-63F
Regulatory Text

87-17-11 MCDONNELL DOUGLAS: Amendment 39-5716. Applies to McDonnell Douglas Model DC-8-62, -62F, -63, and -63F series airplanes, modified in accordance with Aeronautic Development Corporation Supplemental Type Certificate (STC) SA2494NM, certificated in any category. Compliance required as indicated, unless previously accomplished. \n\n\tTo prevent the loss of engine inlet extended nose dome assembly due to metal fatigue failure of the aft attachment ring flanges and possible damage to the engine, accomplish the following: \n\n\tA.\tWithin 250 flight-hours after the effective date of this AD, unless already accomplished within last 250 flight-hours, visually inspect nose dome extension aft attachment ring flanges, Rohr Industries, Inc., Part Numbers 236-0002, in accordance with paragraph 2.A. of Rohr Industries, Inc., Alert Service Bulletin QDC8-A71-10, dated October 21, 1986, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tNOTE: Removal of the nose dome and extension requires disconnecting the PT2 sense line extension. Care must be taken to ensure proper connection when re-installing to prevent erroneous EPR indication. \n\n\tB.\tIf no cracks are found, repeat the visual inspections of the flanges in accordance with paragraph A. of this AD, at intervals not to exceed 500 flight-hours, until such time as the modification is accomplished in accordance with paragraph D. of this AD. \n\n\tC.\tIf cracks are found on flanges with attachments, prior to further flight, accomplish either of the following: \n\n\t\t1.\tAccomplish the modification in accordance with paragraph D. of this AD, or \n\n\t\t2.\tAccomplish repair and repetitive inspections as follows: \n\n\t\t\ta.\tFor extended nose dome with five alternate blank flanges: \n\n\t\t\t\t(1)\tRelocate the five attachments in accordance with paragraph 2.A.(3) through (13) of the Rohr Industries, Inc., Alert Service Bulletin QDC8-A71-10, dated October 21, 1986,or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\t\t\t\t(2)\tRepeat visual inspections of the flanges at the relocated attachments in accordance with paragraph A. of this AD, at intervals not to exceed 500 flight-hours. \n\n\t\t\tb.\tFor extended nose dome without the five alternate blank flanges: \n\n\t\t\t\t(1)\tRemove and replace the aft attachment ring of the extended nose dome in accordance with FAA-approved data. \n\n\t\t\t\t(2)\tRepeat visual inspections of the flanges of the newly installed attachment rings in accordance with paragraph A. of this AD, at intervals not to exceed 500 flight-hours. \n\n\tD.\tAccomplishment of the modification to replace existing spacers, captive nuts, and retainers on aft nose dome extension ring with support fittings and to add support fittings on forward nose dome extension ring in accordance with paragraph 2.A.(1) through (56) of the Rohr Industries, Inc., Service Bulletin QDC8-71-10, dated March 2, 1987, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region, constitutes terminating action for the requirements of this AD. \n\n\tE.\tAlternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tF.\tSpecial 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. \n\n\tAll persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Rohr Industries, Inc., Post Office Box 878, Chula Vista, California 92012-0878; Attention: Robert Dickenson. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at 4344 Donald Douglas Drive, Long Beach, California. \n\n\tThis amendment becomes effective September 24, 1987.

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References
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--- - Part 39
FAA Documents