- 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.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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On this page
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.
| 1982 | 1 |
|---|---|
| 1986 | 1 |
| 1987 | 5 |
| 1988 | 4 |
| 1989 | 3 |
| 1990 | 5 |
| 1991 | 29 |
| 1992 | 7 |
| 1993 | 2 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 6 |
| 1998 | 6 |
| 1999 | 16 |
13 with no year recorded