AD 76-01-04

Active

Longitudinal Porpoising

Key Information
76-01-04
Active
January 15, 1976
Not specified
Unknown
39-2489
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
DC-9-31 DC-9-32 DC-9-32 (VC-9C) DC-9-32F DC-9-32F (C-9A) DC-9-32F (C-9B) DC-9-33F DC-9-34 DC-9-34F DC-9-51
Regulatory Text

76-01-04 MCDONNELL DOUGLAS: Amendment 39-2489. Applies to Model DC-9-30 and -50 Series Airplanes Fuselage Numbers 757, 763, 780 through 795, 797 and 798, certificated in all categories. \n\n\tCompliance required within the next 50 hours' time in service or 5 days whichever comes first after the effective date of this AD, unless already accomplished. \n\n\tTo prevent manually induced longitudinal proposing aggravated by the elevator boost system accomplish the following: \n\n\tRemove the hydraulic bleed stop assembly, P/N 4934616-1, per Douglas Alert Service Bulletin A27-176, dated December 13, 1975, or later FAA-approved revisions, or an equivalent procedure approved by the Chief, Aircraft Engineering Division, FAA Western Region. \n\n\tThis amendment becomes effective on January 15, 1976.

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