Rust, Robert E. Airworthiness Directives

8 ADs indexed for Rust, Robert E. aircraft.

Models

Recent ADs

2022-03-15

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...

Effective: Mar 21, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2014-24-01 Recurring

final rule

Airworthiness Directives; Various de Havilland Airplanes

Unsafe Condition: Structural failure of the attachment of the wing to the fuselage that resulted from failed lateral fuselage tie rods.

Effective: Jan 6, 2015 Category: aircraft Compliance: Within the compliance times specified in the AD, unless already done.

Why matched: Airworthiness Directives; Various de Havilland Airplanes

2014-17-09

final rule

Airworthiness Directives; Various de Havilland Airplanes

Unsafe Condition: Structural failure of the attachment of the wing to the fuselage resulting from failed lateral fuselage tie rods.

Effective: Sep 18, 2014 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various de Havilland Airplanes

2010-18-12

final rule

Airworthiness Directives; Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A Airplanes

Unsafe Condition: Unapproved latch plate design installation in the flap operating system.

Effective: Oct 7, 2010 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A Airplanes

2010-18-01

final rule

Airworthiness Directives; Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A Airplanes

Unsafe Condition: Latch plate supplied under part number (P/N) C1-CF-1489 failing in service, not manufactured to the applicable de Havilland drawing. The unapproved latch plate can become separated or bent, resulti...

Effective: Oct 7, 2010 Category: aircraft Compliance: Within 50 hours time-in-service (TIS) after October 7, 2010, or within 90 days after October 7, 2...

Why matched: Airworthiness Directives; Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A Airplanes

2003-17-16 Recurring

final rule

Airworthiness Directives; Robert E. Rust Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A Airplanes

Unsafe Condition: Stress corrosion cracking on the tailplane attachment brackets and fatigue cracking/chaffing on the engine mount frame.

Effective: Oct 10, 2003 Category: engine Compliance: Within 90 days after the effective date of this AD.

Why matched: Airworthiness Directives; Robert E. Rust Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2003-05-06

final rule

Airworthiness Directives; Robert E. Rust Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A Airplanes

Unsafe Condition: Reduced structural integrity in the primary structure of the airplane, which could result in failure of the rudder torque tube, elevator fasteners, and the vertical fin rear spar, or jamming or dam...

Effective: Apr 25, 2003 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Robert E. Rust Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A Airplanes

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

2003-05-05

final rule

Airworthiness Directives; Robert E. Rust Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A Airplanes

Unsafe Condition: Reports indicate that certain replacement steel fuselage center-section tie bars installed on the affected airplanes could fail before the originally published safe life limit, potentially leading ...

Effective: Apr 25, 2003 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Robert E. Rust Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A Airplanes

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