AD 89-26-02

Airworthiness directive · Inspect Rudder Control · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more

Effective
January 13, 1990
Models
DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F and 17 more
Data sheet
TCDSA6WE
Registered aircraft
113 matched by model
Product
Aircraft · Large airplane
Amendment
39-6418
Docket
89-NM-73-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

89-26-02 MCDONNELL DOUGLAS: Amendment 39-6418. Docket No. 89-NM-73-AD.

Applicability: Model DC-9-10 through -80, Model MD88, and C-9 (Military) series airplanes, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To preclude failure of the rudder control sector, accomplish the following:

A. Within 60 days after the effective date of this airworthiness directive (AD), visually inspect the rudder control sector for cracks and acceptable wall thickness, in accordance with Figure 2 of McDonnell Douglas Alert Service Bulletin A27-302, dated February 17, 1989.

1. If no cracks are found and the wall thickness is more than .020 inch, no further action is required.

2. If cracks are found or if a wall thickness of .020 inch or less is found, prior to further flight, perform either a permanent or temporary repair or replace the rudder control sector, in accordance with the accomplishment instructions of McDonnellDouglas Service Bulletin A27-302, dated February 17, 1989.

3. If a temporary repair is performed, replace or permanently repair the rudder control sector within 6 months or 1,000 landings, whichever occurs earlier, in accordance with McDonnell Douglas Service Bulletin A27-302, dated February 17, 1989.

B. Within 15 days after the inspection required by paragraph A., above, submit a report of findings, positive or negative, to the Los Angeles Aircraft Certification Office, Attention: ANM-108L, FAA, Northwest Mountain Region, 3229 East Spring Street, Long Beach, California 90806-2425.

C. An alternate means of compliance or adjustment of the compliance times, 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: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to theManager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

D. 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, C2-165 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California.

This amendment (39-6418, AD 89-26-02) becomes effective January 13, 1990.

Affected TCDS · 1

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

Registered aircraft · 113

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 Douglas107 aircraft
  • Douglas6 aircraft
By year built
19661999
Registered aircraft by year built: 95 aircraft
19661
19674
19692
19701
19821
19861
19875
19884
19893
19905
199129
19927
19932
19941
19961
19976
19986
199916

18 with no year recorded

By model

Aircraft

See all 113 aircraft