AD 76-16-07

final rule
Data completeness: 70%

Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes

AD Number
76-16-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 401 Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes
aircraft Cessna Aircraft Company 401A Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes
aircraft Cessna Aircraft Company 401B Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes
aircraft Cessna Aircraft Company 402 Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes
aircraft Cessna Aircraft Company 402A Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes
aircraft Cessna Aircraft Company 402B Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes
aircraft Cessna Aircraft Company 402C Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes
aircraft Cessna Aircraft Company 414 Airworthiness Directives; CESSNA AVIATION Models 401, 402 Series and 414 Airplanes

Unsafe Condition

Possible failures of the engine attachment tangs of engine mount PN5002.

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

Required Actions

Within 10 hours' time in service after the effective date, loosen engine attach bolts, compress rubber mounts with steel shims to reduce gap between forward tang and AN970 washer to no greater than 0.005 inches, and retorque bolts to 160-190 inch pounds. Visually inspect forward and aft tangs of all three engine attachment points with 8-power glass for cracks within 10 hours' time in service after effective date, and thereafter at intervals per specified time limits. Replace engine mount P/N 5002 if cracks detected before further flight.

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

Compliance Time

Within 10 hours' time in service after the effective date of this AD

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

Affected Aircraft

Cessna models 401 and 402 series airplanes and model 414 airplanes certificated in all categories, modified with Supplemental Type Certificate SA2424WE or SA117NW incorporating Allison turboprop engines.

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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