AD Amdt-39-13406

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Airplanes

AD Number
Amdt-39-13406
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-CE-18-AD
FR Citation
69 FR 1657

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company Models 441 and F406 Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Airplanes

Unsafe Condition

Chafing and/or arcing of the fuel boost pump wiring could result in arcing within the wing fuel storage system, leading to ignition of explosive vapor within the fuel storage system.

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

Required Actions

Inspect the fuel boost pump wiring inside and outside the boost pump reservoir. Repair or replace the wiring as necessary. Install an improved design wire harness and fuel boost pump as a terminating action. Optionally, install protective sleeving modification for boost pump lead wires.

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

Compliance Time

Within 50 flight hours 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 Aircraft Company Models 441 and F406 airplanes, as specified in the original AD 2003-09-09.

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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