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2022-03-23

final rule

Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Raytheon Aircraft Company, Hawker Beechcraft Corporation, and Beechcraft Corporation) Airplanes

Unsafe Condition: A timing issue in the yaw servo software can generate a motor position fault when the pilot applies rudder input at the same time the rudder boost system is activated, which disables the rudder boo...

Effective: Feb 22, 2022 Category: aircraft Compliance: Within 100 flight hours or 3 months, whichever occurs first after the effective date of this AD.

Why matched: Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Raytheon Aircraft Company, Hawker Beechcraft Corporation, and Beechcraft Corporation) Airplanes

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

2020-25-01

final rule

Airworthiness Directives; Textron Aviation, Inc. Airplanes (Type Certificate Previously Held by Beechcraft Corporation)

Unsafe Condition: Fatigue cracks in the lower forward wing fitting due to premature torque indication caused by washer P/N 90-380058-1 on the wing bolt.

Effective: Jan 11, 2021 Category: aircraft Compliance: Within the next 200 flight hours or 12 months, whichever occurs later.

Why matched: Airworthiness Directives; Textron Aviation, Inc. Airplanes (Type Certificate Previously Held by Beechcraft Corporation)

2019-23-10

final rule

Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Beechcraft Corporation) Airplanes

Unsafe Condition: Failure of the right aileron flight control cable end fittings, un-commanded right roll of the airplane, and loss of roll control in the left direction, which may lead to loss of control of the air...

Effective: Nov 22, 2019 Category: aircraft Compliance: Within 30 days

Why matched: Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Beechcraft Corporation) Airplanes

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

2019-21-08

final rule

Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Beechcraft Corporation) Airplanes

Unsafe Condition: Reports of cracked and fractured right aileron flight control cable end fittings have occurred at the swaged cable end fittings that thread into the turnbuckle, creating an environment where corros...

Effective: Nov 22, 2019 Category: aircraft Compliance: Within 30 days

Why matched: Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Beechcraft Corporation) Airplanes

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

2016-13-13

final rule

Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) Airplanes

Unsafe Condition: Inadvertent stowage of the thrust reversers, which can result in high forward engine thrust even though the throttle is commanding reverse thrust.

Effective: Aug 12, 2016 Category: aircraft Compliance: Within 12 months of the effective date (August 12, 2016).

Why matched: Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) Airplanes

2014-26-05

final rule

Airworthiness Directives; Beechcraft Corporation Airplanes

Unsafe Condition: Fuel leaks due to fuel cells that did not properly fit; improper installation of fuel components causing loads on fuel cells and breach; improper installation of fuel hoses and clamps causing fuel ...

Effective: Feb 9, 2015 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Beechcraft Corporation Airplanes

2014-21-06 Recurring

final rule

Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes

Unsafe Condition: Failure of the Acme nut threads in a pitch trim actuator (PTA).

Effective: Nov 28, 2014 Category: aircraft Compliance: Within 200 flight hours or 6 months after the effective date, whichever occurs first.

Why matched: Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes

2014-15-08

final rule

Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) Airplanes

Unsafe Condition: Missing sealant on structural components in the fuel tank during the winglet installation process, which could result in a potential source of ignition in a fuel tank during a lightning strike, lea...

Effective: Sep 5, 2014 Category: aircraft Compliance: Within 600 flight hours or 12 months after the effective date of this AD, whichever occurs first.

Why matched: Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) Airplanes

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

2014-15-15 Recurring

final rule

Airworthiness Directives; Beechcraft Corporation Airplanes

Unsafe Condition: Fatigue cracking in the horizontal stabilizer ribs, which could result in the failure of the horizontal stabilizer and loss of pitch control of the airplane.

Effective: Sep 5, 2014 Category: aircraft Compliance: Before the accumulation of 7,400 total flight hours or within 6 months after the effective date o...

Why matched: Airworthiness Directives; Beechcraft Corporation Airplanes

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

2014-02-03

final rule

Airworthiness Directives; Beechcraft Corporation Airplanes

Unsafe Condition: Elevator bob-weight (stabilizer weight) traveling past its stop bolt may allow the attaching linkage to move over-center and lead to reduced nose down elevator control.

Effective: Mar 7, 2014 Category: aircraft Compliance: Within 600 flight hours time-in-service (TIS) from the effective date of this AD.

Why matched: Airworthiness Directives; Beechcraft Corporation Airplanes

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

2013-24-03

final rule

Airworthiness Directives; Beechcraft Corporation Airplanes

Unsafe Condition: Cracking in the front spar cap angles and hat section structure of the vertical stabilizer.

Effective: Jan 13, 2014 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Beechcraft Corporation Airplanes

2013-16-01

final rule

Airworthiness Directives; Beechcraft Corporation and Hawker Beechcraft Corporation

Unsafe Condition: Elevator balance weights becoming loose or failing because the balance weight material was under strength and did not meet material specifications.

Effective: Sep 24, 2013 Category: aircraft Compliance: Before further flight after September 24, 2013, for Model 58 airplanes, serial numbers TH-1768 th...

Why matched: Airworthiness Directives; Beechcraft Corporation and Hawker Beechcraft Corporation

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

2013-11-16

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Airplanes

Unsafe Condition: Reports of several instances of severe vibration and wing/aileron oscillation due to lack of sufficient flutter margin with winglets installed.

Effective: Jul 2, 2013 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Airplanes

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

2013-03-07

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes

Unsafe Condition: The wiring for the 5-volt direct current (DC) system is undersized and does not have adequate circuit protection for the smaller gauge wire.

Effective: Mar 19, 2013 Category: aircraft Compliance: Within 400 flight hours or 12 months after the effective date of this AD, whichever occurs first.

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes

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

2012-21-06

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Airplanes

Unsafe Condition: Incorrect gauge wires used in wiring bundles for cockpit electrical power for backlighting and instrument panel components could cause failure of the wiring, leading to smoke in the cockpit, loss o...

Effective: Nov 27, 2012 Category: aircraft Compliance: Within 50 hours time-in-service or within 6 calendar months after November 27, 2012, whichever oc...

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Airplanes

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

2012-21-05

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Airplanes

Unsafe Condition: Certain aircraft were produced with the incorrect gauge wiring installed.

Effective: Nov 27, 2012 Category: aircraft Compliance: Within the next 50 hours time-in-service (TIS) after November 27, 2012, or within the next 6 cale...

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Airplanes

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

2012-10-02

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Airplanes

Unsafe Condition: Installation of oversized clamps on fuel vapor return and/or fuel vent lines in the outboard sections of the left and right wings.

Effective: Jun 21, 2012 Category: aircraft Compliance: Within 50 hours time-in-service or within 6 calendar months after June 21, 2012, whichever occurs...

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Airplanes

2011-27-04

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Airplanes Equipped With a Certain Supplemental Type Certificate (STC)

Unsafe Condition: Incorrect minimum control speed (V<INF>MC</INF>) markings on airspeed indicator(s) and/or airspeed limitations placard(s).

Effective: Mar 5, 2012 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Airplanes Equipped With a Certain Supplemental Type Certificate (STC)

2011-27-51

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Models 1900, 1900C, and 1900D Airplanes

Unsafe Condition: Elevator bob-weight traveling past its stop bolt, allowing the attaching linkage to move over-center, resulting in reduced nose down elevator control and potential loss of control of the airplane.

Effective: Jan 18, 2012 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Models 1900, 1900C, and 1900D Airplanes

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

2011-15-05

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Models B300 and B300C (C-12W) Airplanes

Unsafe Condition: An error in the take-off speeds and field lengths published in the FAA-approved flight manual could result in taking off from shorter runways than required by the airplane if the airplane loses an ...

Effective: Aug 19, 2011 Category: engine Compliance: Within 14 days after the effective date of this AD.

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Models B300 and B300C (C-12W) Airplanes

2011-03-12

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400A and 400T Airplanes

Unsafe Condition: Missing sealant on the left and right pylon firewall structures, which could result in flames penetrating the seams in the firewall between the engine and the aft fuselage, and a subsequent uncontr...

Effective: Mar 14, 2011 Category: aircraft Compliance: Within 200 flight hours or 12 months after the effective date of this AD, whichever occurs first.

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400A and 400T Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2010-26-03

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes

Unsafe Condition: Collapses of the pneumatic supply tube for the tail deice system, which could result in failure of the tail deice boots to operate. This failure could lead to loss of control in icing conditions.

Effective: Dec 20, 2010 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes

2010-17-15

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes

Unsafe Condition: Starter generators with deficient armature insulating materials may have been installed, potentially leading to the loss of operation of one or both starter generators and consequent loss of all no...

Effective: Sep 29, 2010 Category: aircraft Compliance: Within the next 25 hours time-in-service (TIS) after September 29, 2010.

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes

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

2010-10-10

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes

Unsafe Condition: Improper installation of the metal oxide varistor (MOV) and spark gap wiring of the essential bus lightning strike protection, which could result in overload of the MOV in a lightning strike and al...

Effective: Jun 21, 2010 Category: aircraft Compliance: Within the next 200 hours time-in-service after June 21, 2010, or within the next 12 months after...

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes

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

2010-06-02

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Model G58 Airplanes

Unsafe Condition: Inadequate clearance of the brake reservoir tubing and the heater fuel pump wiring, which could result in chafing and shorting out of the electrical wiring and chafing of the tubing carrying flamma...

Effective: Apr 15, 2010 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Model G58 Airplanes