AD 84-02-06

Airworthiness directive · Fuel Tank Pump Conduits · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more

Effective
March 2, 1984
Models
DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-30F (KC-10A, KDC-10) and 3 more
Data sheet
TCDSA22WE
Registered aircraft
26 matched by model
Product
Aircraft · Large airplane
Amendment
39-4799

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

84-02-06 McDONNELL DOUGLAS: Amendment 39-4799. Applies to McDonnell Douglas Model DC-10 and KC-10A (Military) series airplanes, certificated in all categories. Compliance required as indicated, unless previously accomplished.

To prevent chafing and electrical arcing in fuel tank pump electrical conduits, accomplish the following:

A. Prior to the accumulation of 20,000 hours time in service, or within the next 4000 hours time in service, or one year after the effective date of this AD, whichever occurs later, install teflon tubing in all aft fuel tank pump harness conduits (main tank aft pumps and center wing tank pumps) in accordance with the Accomplishment Instructions in McDonnell Douglas DC-10 Service Bulletin 24-123, Revision 1, dated November 22, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

B. Prior to the accumulation of 30,000 hours time in service, or within the next 4000 hourstime in service, or one year after the effective date of this AD, whichever occurs later, install teflon tubing in all remaining fuel tank pump harness conduits in accordance with the Accomplishment Instructions in McDonnell Douglas DC-10 Service Bulletin 24-123, Revision 1, dated November 22, 1983, or later revisions 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.

D. Alternate means of compliance providing an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

All persons affected by this amendment who have not already received these documents from the manufacturer may obtain copies upon request to the McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or at 4344 Donald Douglas Drive, Long Beach, California.

This amendment becomes effective March 2, 1984.

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.

By aircraft maker
  • Mcdonnell Douglas13 aircraft
  • Douglas8 aircraft
  • Mcdonnell-Douglas5 aircraft
By year built
19751988
Registered aircraft by year built: 6 aircraft
19751
19761
19781
19791
19801
19881

20 with no year recorded

By model

Aircraft

See all 26 aircraft