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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
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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

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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

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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
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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
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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
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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
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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
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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
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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

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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)

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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
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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

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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
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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

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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
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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
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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

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2010-05-10

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Models B300 and B300C Airplanes

Unsafe Condition: Installation of an incorrect bus bar on the terminal board of the circuit card rack assembly could result in failure of the pitot heat annunciators to illuminate, leading to the pilot being unaware...

Effective: Apr 8, 2010 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Models B300 and B300C Airplanes

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2009-25-01

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A, A36, A36TC, B36TC, E55, E55A, F33A, and V35B Airplanes

Unsafe Condition: Incorrect washers installed in the pilot and copilot shoulder harnesses could result in a malfunctioning shoulder harness, leading to occupant injury.

Effective: Jan 8, 2010 Category: aircraft Compliance: Within the next 100 hours time-in-service for Group 1 airplanes; compliance time for Group 2 airp...

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A, A36, A36TC, B36TC, E55, E55A, F33A, and V35B Airplanes

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2009-23-03 Recurring

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Models 1900, 1900C, and 1900D Airplanes

Unsafe Condition: Fatigue cracks in the wing rear spar lower caps, which could result in fatigue failure of the wing rear spar lower caps. A rear spar failure could result in complete wing failure and the wing separ...

Effective: Dec 14, 2009 Category: aircraft Compliance: Within 12 months of the effective date (December 14, 2009).

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Models 1900, 1900C, and 1900D Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure
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2009-23-01 Recurring

final rule

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

Unsafe Condition: Leaking and/or cracks in the left and right main landing gear (MLG) actuators could result in loss of hydraulic fluid, leading to an inability to extend or lock down the landing gear, which could r...

Effective: Dec 8, 2009 Category: aircraft Compliance: Within 12 months of the effective date of the AD.

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

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear
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2009-15-01

final rule

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Model G36 Airplanes

Unsafe Condition: Chafing between the wire harness/connector(s) and fuel line, which could lead to fuel leaking into the cockpit and fire in the cockpit if wiring arcs through the fuel line.

Effective: Jul 27, 2009 Category: aircraft Compliance: Within 10 hours time-in-service (TIS) after July 27, 2009, or 6 calendar months after July 27, 20...

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Model G36 Airplanes

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2009-08-04

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Model BH.125 Series 600A Airplanes and Model HS.125 Series 700A Airplanes Modified in Accordance With Supplemental Type Certificate (STC) SA2271SW

Unsafe Condition: A blower motor of the cockpit ventilation and avionics cooling system seized up and gave off smoke, indicating a potential for smoke and fumes in the cockpit due to excessive current draw.

Effective: May 14, 2009 Category: aircraft Compliance: Within 600 flight hours or 6 months after the effective date of this AD, whichever occurs first.

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Model BH.125 Series 600A Airplanes and Model HS.125 Series 700A Airplanes Modified in Accordance With Supplemental Type Certificate (STC) SA2271SW

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2009-07-02

final rule

Airworthiness Directives; Hawker Beechcraft Corporation Model MU-300-10 Airplanes and Model 400 and 400A Series Airplanes; and Raytheon (Mitsubishi) Model MU-300 Airplanes

Unsafe Condition: Incomplete latching of the existing adjustment mechanism and cracked reinforcement assemblies, which could result in sudden shifting of a flightcrew seat.

Effective: Apr 30, 2009 Category: aircraft Compliance: Within 200 hours time-in-service after March 13, 1996, for Hawker Beechcraft Model MU-300-10, Mod...

Why matched: Airworthiness Directives; Hawker Beechcraft Corporation Model MU- 300-10 Airplanes and Model 400 and 400A Series Airplanes; and Raytheon (Mitsubishi) Model MU-300 Airplanes

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