AD 96-14-04

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes

AD Number
96-14-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-254-AD
FR Citation
(Federal Register: July 09, 1996 (Volume 61, Number 132))

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-10-10 Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company DC-10-10F Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company DC-10-15 Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company DC-10-30 Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company DC-10-30F (KC-10A, KDC-10) Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company DC-10-40 Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company DC-10-40F Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company MD-11 Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes
aircraft The Boeing Company MD-11F Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10A (Military) Airplanes

Unsafe Condition

Failure of the nose landing gear (NLG) lock link bolts due to improper heat-treatment during manufacturing, which reduces their fatigue life and could result in NLG collapse.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Conduct a one-time visual inspection or records search to identify suspect lock link bolts and replace any suspect bolts with serviceable bolts. The replacement must be completed within 24 months after the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within 24 months after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

McDonnell Douglas Model DC-10-10, -15, -30, -40 series airplanes, KC-10A airplanes listed in Service Bulletin DC10-32-242, and MD-11 series airplanes listed in Service Bulletin MD11-32-060.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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