AD 89-08-04

Airworthiness directive · Spoiler Position System · Boeing DC-9-11, DC-9-12, DC-9-13 and 19 more

Effective
May 4, 1989
Models
DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F and 16 more
Data sheet
TCDSA6WE
Registered aircraft
99 matched by model
Product
Aircraft · Large airplane
Amendment
39-6179

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

89-08-04 McDONNELL DOUGLAS: Amendment 39-6179.

Applicability: Model DC-9, DC-9-80, and C-9 (Military) series airplanes, certificated in any category, as listed in McDonnell Douglas Model DC-9 Service Bulletin 27-173, Revision 1, dated May 20, 1982, and Service Bulletin 27-257, Revision 1, dated June 20, 1988.

Compliance: Required within 12 months after the effective date of this airworthiness directive (AD), unless previously accomplished.

To eliminate lateral control difficulties after liftoff during takeoff, accomplish the following:

A. For McDonnell Douglas Model DC-9 and C-9 (Military) series airplanes, identified in McDonnell Douglas Model DC-9 Service Bulletin 27-173, Revision 1, dated May 20, 1982, and Service Bulletin 27-257, Revision 1, dated June 20, 1988: Install the Spoiler Position Sensing and Indication System and "spoiler deployed" annunciation takeoff inhibit feature in accordance with the accomplishment instructions of those service bulletins.B. For McDonnell Douglas Model DC-9-81, and DC-9-82, and DC-9-83 series airplanes identified in McDonnell Douglas Model DC-9 Service Bulletin 27-257, Revision 1, dated June 20, 1988: Install the spoiler deployed annunciation takeoff inhibit feature in accordance with the accomplishment instructions of that service bulletin.

C. For all McDonnell Douglas Model DC-9-81, DC-9-82, and DC-9-83 airplanes with the production equivalent of McDonnell Douglas Model DC-9 Service Bulletin, 27-257, Revision, dated June 20, 1988, incorporated but presently de-activated: Re-activate the spoiler deployed annunciation takeoff inhibit feature in accordance with the airplane type design configuration.

D. An alternate means 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 Certification Office, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who may add any comments and then send it to the Manager, Los Angeles Aircraft Certification Office.

E. Special flight permits may be used 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.

All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to the McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director of Publications, C1-LOO (54-60). These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at 3229 East Spring Street, Long Beach, California.

This amendment (39-6179, AD 89-08-04) becomes effective on May 4, 1989.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 99

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Mcdonnell Douglas93 aircraft
  • Douglas6 aircraft
By year built
19661999
Registered aircraft by year built: 84 aircraft
19661
19674
19692
19701
19821
19861
19875
19884
19893
19903
199123
19925
19931
19941
19961
19976
19986
199916

15 with no year recorded

By model

Aircraft

See all 99 aircraft