AD 2010-13-06

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Corporation Model DC-10-10, DC-10-10F, and MD-10-10F Airplanes

AD Number
2010-13-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-0043
FR Citation
75 FR 35611

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas Corporation Model DC-10-10 Airworthiness Directives; McDonnell Douglas Corporation Model DC-10-10, DC-10-10F, and MD-10-10F Airplanes

Unsafe Condition

Cracking in the spar cap at station Xors=345, which could lead to cracking of the lower wing skin, fuel leaks, and the inability of the structure to sustain limit load.

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

Required Actions

Perform a one-time high frequency eddy current inspection for cracking of fastener holes at the left and right side wing rear spar lower cap at station Xors=345. If no cracking is found, cold work open holes and install new second oversize fasteners and nut assemblies. If any cracking is found, repair the spar cap using an approved method.

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

Compliance Time

Within 3,000 flight cycles 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 Corporation Model DC-10-10, DC-10-10F, and MD-10-10F airplanes, certificated in any category, as specified in Boeing Alert Service Bulletin DC10-57A157, dated May 12, 2009.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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View Official Source ↗ Find More ADs for McDonnell Douglas Corporation Model DC-10-10

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