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2003-09-09 R1

final rule

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.

Effective: Jan 22, 2004 Category: aircraft Compliance: Initially within the next 25 hours time-in-service or 60 days after May 31, 2002, whichever occur...

Why matched: Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

98-04-28

final rule

Airworthiness Directives; Cessna Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414, 414A, 421B, 421C, 425, and 441 Airplanes.

Unsafe Condition: Flight in freezing rain, freezing drizzle, or mixed icing conditions may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in ice for...

Effective: Mar 13, 1998 Category: aircraft Compliance: Within 30 days after the effective date of this AD (March 13, 1998).

Why matched: Airworthiness Directives; Cessna Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414, 414A, 421B, 421C, 425, and 441 Airplanes.

97-01-13

final rule

Airworthiness Directives; Cessna 100, 200, 300, and 400 Series Airplanes

Unsafe Condition: Fuel, Oil and Hydraulic Hoses

Effective: Feb 3, 1997 Category: aircraft

Why matched: Airworthiness Directives; Cessna 100, 200, 300, and 400 Series Airplanes

92-16-18

final rule

Airworthiness Directives; CESSNA Models 401, 402, 402A, 402B, 402C, 404, F406, 421, 421A, 421B, 421C, and 441 Airplanes

Unsafe Condition: Passenger injury caused by commuter seat failure.

Effective: Sep 10, 1992 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD, unless already acc...

Why matched: Airworthiness Directives; CESSNA Models 401, 402, 402A, 402B, 402C, 404, F406, 421, 421A, 421B, 421C, and 441 Airplanes

83-22-06

final rule

Airworthiness Directives; Cessna Model 152, A152, 172N, 172P, 172Q, 172RG, R172K 180K 182Q, 182R, T182, R182, TR182, A185F, F152, FA152, F172N, F172P, FR172K, F182Q, and FR182 Airplanes

Unsafe Condition: Possible loss of an aileron hinge pin due to incorrect location of the cotter pin holes in the aileron hinges.

Effective: Nov 8, 1983 Category: aircraft Compliance: within the next 100 hours time in service, after the effective date of this AD

Why matched: Airworthiness Directives; Cessna Model 152, A152, 172N, 172P, 172Q, 172RG, R172K 180K 182Q, 182R, T182, R182, TR182, A185F, F152, FA152, F172N, F172P, FR172K, F182Q, and FR182 Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls