AD 88-03-09

Airworthiness directive · Digital Flight Guidance Computer · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82) and DC-9-83 (MD-83)

Effective
March 11, 1988
Models
DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83)
Data sheet
TCDSA6WE
Registered aircraft
72 matched by model
Product
Aircraft · Large airplane
Amendment
39-5839

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

88-03-09 MCDONNELL DOUGLAS: Amendment 39-5839. Applies to McDonnell Douglas Model DC-9-81, -82, and -83 series airplanes, as listed in McDonnell Douglas Service Bulletin 34-177, dated April 28, 1987, certificated in any category. Compliance required as indicated, unless previously accomplished.

To prevent erroneous information from being transmitted to the Digital Flight Guidance Computer (DFGC) from the Digital Air Data computer (DADC) in the event of an electrical transient, accomplish the following:

A. Within 12 months after the effective date of this airworthiness directive (AD), inspect Honeywell P/N HG280D80 DADC in affected airplanes to determine if Modification 8 has been installed, in accordance with Part 2 of the Accomplishment Instructions of McDonnell Douglas Service Bulletin 34-177, dated April 28, 1987, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

1. If Modification 8 has been installed and identified, no further action is necessary.

2. If Modification 8 has been installed but not identified, identify the DADC in accordance with the service bulletin.

3. If Modification 8 has not been installed, modify and identify the DADC in accordance with the service bulletin.

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by 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 information 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); or Honeywell, Incorporated, Commercial Aviation Division Technical Services, Mail Station MN23-6345, P.O. Box 889, Minneapolis, Minnesota 55440. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Los Angeles Aircraft certification Office, 4344 Donald Douglas Drive, Long Beach, California.

This Amendment becomes effective March 11, 1988.

Affected TCDS · 1

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

Registered aircraft · 72

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 Douglas71 aircraft
  • Douglas1 aircraft
By year built
19821999
Registered aircraft by year built: 64 aircraft
19821
19861
19874
19883
19891
19903
199115
19925
19931
19941
19961
19976
19986
199916

8 with no year recorded

By model

Aircraft

See all 72 aircraft