- Effective
- March 13, 1987
- Models
- DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40, DC-10-40F
- Data sheet
- TCDSA22WE
- Registered aircraft
- 26 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-5545
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
87-04-17 MCDONNELL DOUGLAS: Amendment 39-5545. Applies to McDonnell Douglas Model DC-10-10, -15, -30, -40, and KC-10A (Military) series airplanes, certificated in any category. To prevent loss of fuel shutoff and fire extinguishing capabilities, accomplish the following within the next eighteen (18) months after the effective date of this AD, unless already accomplished:
A. Modify and reidentify engine No. 2 aft fuselage mounted fuel fire shutoff valve in accordance with the Accomplishment Instructions of McDonnell Douglas DC-10/KC-10A Service Bulletin 28-168, dated April 16, 1986, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.
B. Modify, reidentify, and rotate engine No. 1 and engine No. 2 wing spar mounted fuel fire shutoff valves, and modify and reidentify engine No. 3 wing spar mounted fuel fire shutoff valves, in accordance with the Accomplishment Instructions of McDonnell Douglas DC-10 ServiceBulletin 28-55, Revision 3, dated December 19, 1980, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.
C. An alternate means of compliance with this AD which provides an acceptable level of safety may be used when approved by the Manager, 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 the airplane to a base for accomplishment of 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, Publications and Training, C1-750 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, orthe Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California.
This supersedes AD 86-09-10, Amendment 39-5305, and AD 86-16-08, Amendment 39-5375.
This Amendment, 39-5545, becomes effective March 13, 1987.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 26
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1975 | 1 |
|---|---|
| 1976 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 1 |
| 1988 | 1 |
20 with no year recorded