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AD 75-09-11

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Airworthiness directive · Collar Assembly · Boeing DC-10-10 and DC-10-10F

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AboutSource files 1
Effective
April 28, 1975
Models
DC-10-10, DC-10-10F
Data sheet
TCDSA22WE
Product
Aircraft · Large airplane
Amendment
39-2184

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

75-09-11 MCDONNELL DOUGLAS: Amendment 39-2184. Applies to Model DC-10-10 and DC-10-10F airplanes, certificated in all categories, with P/N ACG 7008-1, collar assembly - lower steering support installed.

To insure continued airworthiness of these assemblies, prior to the accumulation of 44,500 landings, remove from service collar assembly - lower steering support, P/N ACG 7008-1, and mark it permanently and conspicuously to prevent its inadvertent return to service. Replace it with a serviceable assembly having less than 44,500 landings.

The previously established service life of 231,666 landings is no longer applicable.

This amendment becomes effective April 28, 1975.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

TCDS A22WEThe Boeing CompanyNames 2 of 11 models: DC-10-10F and DC-10-10

Registered aircraft

No registered aircraft matched this AD’s modelsForeign aircraft aren’t included, and ADs on propellers and appliances aren’t matched by model.