AD 71-08-02

Active

Control Of Speed Brake

Key Information
71-08-02
Active
November 30, 1971
Not specified
Unknown
39-1346
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
DC-9-11 DC-9-12 DC-9-13 DC-9-14 DC-9-15 DC-9-15F DC-9-21 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-9-41 DC-9-51 DC-9-81 (MD-81) DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87)
Regulatory Text

71-08-02 MCDONNELL DOUGLAS: Amend 39-1189 as amended by amendment 39-1346. Applies to DC-9 airplanes certificated in all categories. \n\n\tCompliance required within the next 50 hours' time in service after effective date of this AD, unless already accomplished. \n\n\tTo ensure pilot control of speed brake retraction and to prevent inflight deployment of ground spoilers, accomplish one of the following: \n\n\t1.\tAffix a placard(s) in the cockpit in plain view of both crew members stating: \n\n\t\tDO NOT EXTEND GEAR WITH SPEED BRAKES DEPLOYED \n\n\t\tDO NOT ARM GROUND SPOILERS PRIOR TO GEAR EXTENSION \n\n\t2.\ta. Install the interlock switch per McDonnell Douglas DC-9 Service Bulletin No. 32-128, dated November 17, 1971, or later FAA approved revisions, or an equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region and \n\n\t\tb.\tAmend the Limitations Section, FAA Approved Airplane Flight Manual, to include the statements: \n\n\t\t\tDo not extend gear withspeed brakes deployed. \n\n\t\t\tDo not arm ground spoilers prior to gear extension. \n\n\tNOTE: Placards previously installed per Step 1. may be removed if step 2 is accomplished. \n\n\tAmendment 39-1189 became effective April 13, 1971. \n\n\tThis amendment 39-1346 becomes effective November 30, 1971.

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