AD 90-04-05

Airworthiness directive · Takeoff Warning System · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more

Effective
March 8, 1990
Models
DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88
Data sheet
TCDSA6WE
Registered aircraft
100 matched by model
Product
Aircraft · Large airplane
Amendment
39-6504
Docket
89-NM-143-AD

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

90-04-05 MCDONNELL DOUGLAS: Amendment 39-6504. Docket No. 89-NM-143-AD.

Applicability: Model DC-9-80 and MD-88 series airplanes, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent takeoff of an airplane while in an unsafe configuration for takeoff, due to deactivation of the takeoff warning system by the flight crew to eliminate nuisance warnings of the takeoff warning system during single-engine taxi operation, accomplish the following:

A. Within 12 months after the effective date of this AD, rewire the takeoff warning system throttle lever switches to place them in series, rather than in parallel, in a manner approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region, or in accordance with the Accomplishment Instructions of McDonnell Douglas Service Bulletin 31-34, dated December 20, 1989.

B. An alternate means of compliance or adjustment of the compliancetime, which provides an acceptable level of safety, may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

NOTE: This request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

C. Special 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.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director of Publications, C1-L00 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California 90806.

This amendment (39-6504, AD 90-04-05) becomes effective on March 8, 1990.

Affected TCDS · 1

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

Registered aircraft · 100

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 Douglas99 aircraft
  • Douglas1 aircraft
By year built
19821999
Registered aircraft by year built: 87 aircraft
19821
19861
19875
19884
19893
19905
199129
19927
19932
19941
19961
19976
19986
199916

13 with no year recorded

By model

Aircraft

See all 100 aircraft