AD 96-19-03

final rule
Data completeness: 70%

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

AD Number
96-19-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-212-AD
FR Citation
(Federal Register: September 11, 1996 (Volume 61, Number 177))

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

Stress corrosion cracking in the steel Hi-Lok fasteners at the inboard flap inboard track could result in binding of the flap and inability of the flap to extend or retract.

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

Required Actions

Perform a visual inspection to detect corrosion or failure of the steel Hi-Lok fasteners. Replace corroded/failed steel Hi-Lok fasteners with either inconel or same material steel Hi-Lok fasteners. Repeat inspections every 18 months until all fasteners are replaced with inconel.

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

Compliance Time

Within 18 months after the effective date of this AD (October 16, 1996).

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

Affected Aircraft

McDonnell Douglas Model DC-10 and MD-11 series airplanes and KC-10A (military) airplanes, certificated in any category.

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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