AD 91-11-10

Active

Cargo Door

Key Information
91-11-10
Active
July 01, 1991
Not specified
90-NM-249-AD
39-7008
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
DC-9-15F DC-9-32F DC-9-32F (C-9A) DC-9-32F (C-9B) DC-9-33F DC-9-34F
Regulatory Text

91-11-10 MCDONNELL DOUGLAS: Amendment 39-7008. Docket No. 90-NM-249-AD. \n\n\tApplicability: Model DC-9-15F, -32F, -33F, and -34F series airplanes, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo prevent loss of control following the opening of the main deck cargo door, accomplish the following: \n\n\tA.\tWithin 30 days after the effective date of this AD, add the following procedure to the FAA-approved Airplane Flight Manual (AFM) Emergency Procedures. This may be accomplished by inserting a copy of this AD in the AFM. \n\nCARGO DOOR OPENS DURING FLIGHT \n\nMAIN CARGO DOOR OPENS AFTER TAKEOFF: \n\n\n\nSeries 15F\t\nSeries 32F, 33F, 34F \n\n\n\nDirectional Control.........................\nMaintain\nMaintain\n Landing Gear.................................\nUp\t\nUp \nFlaps..................................................\nTakeoff\t\n--- \nFlaps/Slats.......................................\n ---\t\nTakeoff\n Land as soon aspractical. \n\n\n\t \n\tNOTE: The airplane yaw to the right may require almost full left rudder and aileron inputs to correct. Left turns may be more controllable than right turns. Return to the runway should be accomplished with coordinated turns using very little bank (less than 20 degrees), and with speed appropriate to the flap/slat position. Loss of communication may result if the cargo door strikes the upper VHF antenna (try another radio). Do not change configuration until lined up for straight-in landing. \n\n\nMAIN CARGO DOOR OPENS DURING CLIMB, CRUISE, DESCENT, OR APPROACH: \n\n\nDirectional control:\nMaintain \t\nMaintain \t\n\n\nRapid decompression/emergency descent: \n\n\nAccomplish\n(if required)\nAccomplish \n(if required) \n\n\tNOTE: Do not exceed recommended structural damage airspeed during descent. \n\tAfter level-off, slow to minimum maneuvering speed. \n\tLand as soon as practical. Accomplish "on final approach" items. \n\nMAIN CARGO DOOR OPENS ON FINAL APPROACH: \n\n\nLanding Gear\nDown\nDown\nFlaps\n30°\n --- \nFlaps/Slats\n---\n25°/Ext \nIAS\nEstablish*\nEstablish* \n\n \t*Reduce to normal approach speed using normal wind additives. \n\n\tNOTE: There may be indicated airspeed and altitude variations due to disturbed airflow across the static ports. \n\n\tB.\tAn alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. \n\n\tNOTE: The request should be forwarded through an FAA Principal Operations Inspector who may concur or comment then send it to the Manager, Los Angeles ACO. \n\n\tC.\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 information from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Business Unit Manager, Technical Publications, C1-HCW (34-60). This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington, or the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California. \n\n\tThis amendment (39-7008, AD 91-11-10) becomes effective on July 1, 1991.

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