AD 92-22-10

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes

AD Number
92-22-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-NM-222-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-10-10 Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-10F Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-15 Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-30 Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-30F (KC-10A, KDC-10) Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-40 Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-40F Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes

Unsafe Condition

Failure of the horizontal stabilizer rear upper spar cap and/or upper rear skin panel due to fatigue cracking.

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

Required Actions

Conduct dye penetrant or eddy current inspection of the horizontal stabilizer upper outer section rear spar cap and visual inspection of the upper outer rear skin panel per McDonnell Douglas Alert Service Bulletin A55-18 revisions. Repeat inspections at intervals based on flight hours/landings, with specific actions if cracks are found within or exceeding specified limits. Include eddy current inspection of the vertical tang and stress coin attachment holes as required.

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

Compliance Time

Prior to the accumulation of 30,000 flight hours or 7,500 landings, whichever occurs earlier, or within 15 days after August 14, 1987, whichever occurs later, unless already accomplished within the last 120 days since August 14, 1987.

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

Affected Aircraft

Model DC-10 and KC-10A (military) series 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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