AD 72-14-08 R1

final rule
Data completeness: 70%

Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes

AD Number
72-14-08 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 310 Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310A Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310B Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310C Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310D Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310E Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310F Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310G Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310H Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes
aircraft Cessna Aircraft Company 310I Airworthiness Directives; CESSNA Models 310, 320, 401, 402, 411 and 421 Series Airplanes

Unsafe Condition

Flexible fuel and oil hose assemblies in the engine compartment may exhibit leakage, deterioration, or damage such as cracks, cuts, bulges, discoloration, hardness, chafing, and excessive wear due to time-in-service.

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

Required Actions

Inspect flexible fuel and oil hose assemblies in the engine compartment visually or by FAA-approved methods for leakage and deterioration/damage. Replace any deteriorated or damaged hose assemblies prior to further flight. Exclude airplanes with improved hose assemblies as specified.

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

Compliance Time

On airplanes having 200 hours or more time-in-service and thereafter at intervals not to exceed 60 hours time-in-service.

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

Affected Aircraft

Cessna Models 310, 320, 401, 402, 411, and 421 series airplanes except those with improved hose assemblies (Model 310R serial 310R0001+, 402C0001+, 421C0001+) or those upgraded per Cessna Service Information Letter ME81-17.

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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