Beechcraft Beechjet 400A airworthiness directives

• AD 2014-21-06

  Effective 2014-11-28

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

  This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) airplanes identified in paragraphs (c)(1)(i), (c)(1)...

• AD 2014-15-15

  Effective 2014-09-05

  Beechcraft Corporation Airplanes

  This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(5) of this AD. (1) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Mitsubishi Heavy Industries, Inc. Ltd.) Model MU-300 airplanes, serial numb...

• AD 2013-03-07

  Effective 2013-03-19

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

  This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Hawker Beechcraft Corporation (Type Certificate previously held by Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400A airplanes having serial numbers RK-45 and RK-49 through RK-353 in...

• AD 2011-03-12

  Effective 2011-03-14

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

  This AD applies to Hawker Beechcraft Corporation (Type Certificate previously held by Raytheon Aircraft Company; Beech Aircraft Corporation) airplanes, certificated in any category; as identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model 400A airplanes having serial numbers RK-337 through RK-484, RK-486 thr...

• AD 2009-07-02

  Effective 2009-04-30

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

  We are issuing this AD to prevent sudden shifting of a flightcrew seat, which could impair the flightcrew's ability to control the airplane.

  This AD applies to the airplanes specified in Table 1 of this AD, certificated in any category. Table 1--Applicability Manufacturer Model Serial Nos. Hawker Beechcraft Model 400 series RJ-1 through RJ-65 Corporation. airplanes. inclusive. Hawker Beechcraft Model 400A series RK-1 through RK-93 Corporation. airplanes. in...

• AD 2008-24-10

  Effective 2009-01-02

  Pratt & Whitney Canada Corp. JT15D-5; -5B; -5F; and -5R Turbofan Engines

  We are issuing this AD to prevent engine flameouts of one or both engines caused by excessive moisture and freezing in the P3 servo during certain flight conditions.

  This AD applies to the following Pratt & Whitney Canada Corp. (P&WC) turbofan engines with compressor air to HMU delivery tube, part number (P/N) 3119150-01 installed: (1) JT15D-5 turbofan engines, serial numbers (SNs) below and including SN PCE-100411. (2) JT15D-5 turbofan engines, SNs below and including SN PCE- JA08...

• AD 2007-24-01

  Effective 2008-01-02

  Hawker Beechcraft Model 400A Series Airplanes

  We are issuing this AD to prevent overheating of wire insulation and consequent fire or smoke in the airplane cabin.

  This AD applies to Hawker Beechcraft Model 400A series airplanes, certificated in any category; as identified in Raytheon Service Bulletin SB 25-3758, dated June 2006.

• AD 2007-19-05

  Effective 2007-10-23

  Hawker Beechcraft Model 400, 400A, and 400T Series Airplanes

  We are issuing this AD to prevent failure of the attachment fasteners on the engine cowling panels, which could result in separation of a panel from the airplane, and consequent damage to airplane structure.

  This AD applies to Hawker Beechcraft Model 400, 400A, and 400T series airplanes, certificated in any category; as identified in Raytheon Service Bulletin SB 54-3788, dated December 2006.

• AD 2006-21-02

  Effective 2006-10-25

  Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi) Model MU-300 Airplanes

  This AD applies to all Raytheon (Beech) Model 400, 400A, and 400T series airplanes; and Raytheon (Mitsubishi) Model MU-300 airplanes; certificated in any category.

• AD 2006-15-16

  Effective 2006-09-05

  Raytheon (Beech) Model 400 and 400A Series Airplanes

  We are issuing this AD to prevent over- voltage conditions of the DC starter generator due to the incompatibility between certain generator control units (GCUs), which could result in the loss of normal electrical power, damage to some electrical components, or blown fuses during flight, and consequent unrecoverable loss of some or all essential equipment.

  This AD applies to the airplanes identified in Table 1 of this AD, certificated in any category. Table 1.--Applicability Raytheon (Beech) model-- Serials-- On which-- (1) 400 series airplanes: RJ-1 through RJ- Kit part number (P/N) 65 inclusive. 128-3004-1 P or 128- 3004-3 P has been incorporated (Lucas Aerospace/Goodr...

• AD 2004-22-02

  Effective 2004-12-01

  Raytheon (Beech) Model MU-300-10, 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi) Model Beech MU-300 Airplanes

  This AD was prompted by a report of fuel leaking from components in the spoiler mixer bay of several Raytheon (Beech) Model 400A series airplanes.

  This AD applies to Raytheon (Beech) Model MU-300-10, 400, 400A, and 400T series airplanes; and Raytheon (Mitsubishi) Model Beech MU-300 airplanes; certificated in any category; as listed in Raytheon Service Bulletin SB 53-3486, dated June, 2003.

• AD 2004-08-15

  Effective 2004-06-07

  Goodrich Avionics Systems, Inc. TAWS8000 Terrain Awareness Warning System

  This AD affects all airplane models and serial numbers, certificated in any category, that incorporate a Goodrich TAWS8000 terrain awareness warning system (TAWS), part number (P/N) 805- 18000-001, with "Mod None", "Mod A", or "Mod B" hardware installed. This list of airplanes that have the TAWS8000 TWAS installed incl...

• AD 2004-03-35

  Effective 2004-03-24

  Raytheon Model Beech 400A and 400T Series Airplanes

  To prevent intermittent sticking of the relays on the roll trim printed circuit board (PCB) in either the open or closed position, which could result in an out-of-trim condition that could require using considerable control wheel force to keep the wings level, and consequent reduced controllability of the airplane.

  Model Beech 400A series airplanes having serial numbers RK-45, and RK-49 through RK-322 inclusive; and Model 400T series airplanes having serial numbers TT-1 through TT-180 inclusive, and TX-1 through TX-12 inclusive; certificated in any category.

• AD 2003-10-13

  Effective 2003-07-01

  Raytheon Model Beech 400A and 400T Series Airplanes

  To prevent leakage of oxygen from scored low-pressure oxygen tubing, which could result in lack of available oxygen for the flightcrew, possible explosion, or fire.

  Model Beech 400A series airplanes, serial numbers RK-232 through RK-265 inclusive; and Model Beech 400T series airplane having serial number TX-10; certificated in any category.

• AD 2002-01-23

  Effective 2002-02-14 · recurring

  Raytheon Model Beech 400, 400A, and 400T Series Airplanes; Model Beech MU-300-10 Airplanes; and Model Mitsubishi MU-300 Airplanes

  To prevent failure of the engine mount and possible loss of the engine, and consequent loss of control of the airplane.

  The following airplanes, certificated in any category: Table 1.--Applicability Model Serial Numbers Beech 400 series airplanes: RJ-1 through RJ-65 inclusive. Beech 400A series airplanes: RK-1 and subsequent. Beech 400T series airplanes: TT-1 through TT-180 inclusive. Beech 400T-1 airplanes: TX-1 through TX-11 inclusive...

• AD 2001-24-11

  Effective 2001-12-11

  Raytheon Model Beech 400, 400A, and 400T Series Airplanes, Model Mitsubishi MU-300 Airplanes, and Model Beech MU-300-10 Airplanes

  To prevent reduced controllability of the airplane due to loss of airspeed indication by ensuring that the flightcrew is advised of in-flight procedures in the event of loss of airspeed indication.

  All Model Beech 400, 400A, and 400T series airplanes, Model Mitsubishi MU-300 airplanes, and Model Beech MU- 300-10 airplanes; certificated in any category.

• AD 2001-20-07

  Effective 2001-11-15

  Raytheon Model Beech 400A Series Airplanes

  To prevent electrical arcing or overheating of the ground connection in the aft fuselage area, which could result in a fire hazard due to ignition of fuel fumes during an engine start sequence.

  Model 400A series airplanes, serial numbers RK- 78, RK-87 through RK-207 inclusive, certificated in any category.

• AD 2001-03-06

  Effective 2001-03-22 · recurring

  Raytheon (Beech) Model MU-300, MU-300-10, 400, and 400A Series Airplanes

  All Model MU-300, MU-300-10, 400, and 400A series airplanes, certificated in any category.

• AD 2000-25-04

  Effective 2001-01-17

  Raytheon (Beech) Model MU-300, MU-300-10, 400, 400A, and 400T Series Airplanes

  To prevent an asymmetric braking condition and a longer stopping distance due to sudden loss of normal braking to the left wheel, which could result in the airplane overrunning the runway surface.

  Model MU-300, MU-300-10, 400, 400A, and 400T series airplanes; as listed in Raytheon Aircraft Service Bulletin SB 32-3300, dated December 1999; certificated in any category.

• AD 2000-09-12

  Effective 2000-06-16

  Raytheon (Beech) Model 400A and 400T Series Airplanes

  To prevent detachment or breakage of wires in the temperature switch assemblies of the wing ice protection system, which could result in the flightcrew not being advised of an over-temperature situation on the leading edge of the wing, and consequent structural damage to the wing.

  Model 400A series airplanes, having serial numbers RK-01 through RK-188 inclusive; Model 400T (T-1A) series airplanes, having serial numbers TT-01 through TT-180 inclusive; and Model 400T (TX) series airplanes, having serial numbers TX-01 through TX-09 inclusive; certificated in any category.

• AD 2000-05-06

  Effective 2000-04-12

  Raytheon (Beech) Model 400A and 400T Series Airplanes

  To prevent failure of the engine fire extinguisher bottle to discharge, or discharge of the wrong engine fire extinguisher bottle.

  Model 400A series airplanes, serial numbers RK-45 and RK-49 through RK-209 inclusive; Model 400T series airplanes (T- 1A), serial numbers TT-01 through TT-180 inclusive; and Model 400T series airplanes (TX), serial numbers TX-01 through TX-09 inclusive; certificated in any category.

• AD 99-21-26

  Effective 1999-11-22

  Raytheon (Beech) Model 400, 400A, 400T, and MU-300-10 Airplanes

  To prevent uncommanded nose-down pitch at certain flap settings during icing conditions.

  All Model 400, 400T, and MU-300-10 airplanes; and Model 400A airplanes having serial numbers RK-1 through RK-107 inclusive; certificated in any category.

• AD 99-21-08

  Effective 1999-11-12

  Raytheon (Beech) Model 400A Airplanes

  To prevent chafing of the fuel drain tube assembly, which could result in fuel leakage from the fuel drain tube assembly and consequent risk of fire.

  Model 400A airplanes, serial numbers RK-1 through RK-92 inclusive, certificated in any category.

• AD 98-06-30

  Effective 1998-04-24

  Raytheon (Beech) Model 400, 400A, 400T, MU-300, and MU-300-10 Airplanes

  To prevent cracking and consequent failure of the outflow/safety valves, which could result in rapid decompression of the airplane.

  The following models and series of airplanes, certificated in any category, equipped with AlliedSignal outflow/ safety valves, as identified in AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1, dated May 30, 1995: Model of airplane Serial Nos. 400: RJ-1 through RJ-65 inclusive. 400A: RK-1 through RK-4...

• AD 96-25-03

  Effective 1997-01-24

  Raytheon (Beech) Model 400A, 400T (Military T-1A), and 400T (Military TX) Series Airplanes

  To prevent loss of roller attach nuts and the flap roller, which could result in the loss of a flap when the airplane is subject to load limit conditions, and consequently lead to reduced controllability of the airplane.

  Model 400A and 400T series airplanes; as listed in Beech Service Bulletin No. 2522, dated January 1994, and Raytheon Service Bulletin No. 2522, Revision 1, dated May 1996; certificated in any category.

• AD 96-17-10

  Effective 1996-09-24 · superseded or removed

  Beech Model 400, 400A, MU-300-10, and 2000 Airplanes, and Model 200, B200, 300, and B300 Series Airplanes

  To prevent cracking and subsequent failure of the outflow/safety valves, which could result in rapid decompression of the airplane.

  Model 400, 400A, MU-300-10, and 2000 airplanes, Model 200 and B200 series airplanes having a maximum altitude capability of greater than 31,000 feet, and Model 300 and B300 series airplanes; equipped with AlliedSignal outflow/safety valves, as identified in AlliedSignal Aerospace Service Bulletins 103570-21- 4012 and 1...

• AD 96-03-07

  Effective 1996-03-13 · superseded or removed

  Beech Model 400, 400A, and MU-300-10 Airplanes

  To prevent reduced controllability of the airplane due to a shifting of the flightcrew seat during flight.

  Model 400 airplanes, serial numbers RJ-1 through RJ-65 inclusive; Model 400A airplanes, serial numbers RK-1 through RK-93 inclusive; and Model MU-300-10 airplanes, serial numbers A1001SA through A1011SA inclusive; certificated in any category.

• AD 95-25-06

  Effective 1996-01-16

  Beech Model 400, 400A, and 400T (Military T-1A) Airplanes

  To ensure that the standby instrument lighting system adequately illuminates the standby instrument, if normal electrical power is lost or is turned off as a result of a fire or smoke in the cockpit.

  Model 400 airplanes, serial number RJ-61; 400A airplanes, serial numbers RK-1 through RK-80 inclusive; and 400T (military T-1A) airplanes, serial numbers TT-1 through TT-108 inclusive; certificated in any category.

• AD 95-25-05

  Effective 1996-01-16

  Beech Model 400A Airplanes

  To prevent reduced controllability of the airplane after takeoff.

  Model 400A airplanes, serial numbers RK-1 through RK-96 inclusive, certificated in any category.

• AD 95-18-04

  Effective 1995-10-10

  Beech Model 400 and 400A Airplanes

  To prevent reduced controllability of the airplane.

  Model 400 airplanes, serial RJ-61; and Model 400A airplanes, serials RK-1 through RK-77 inclusive, and RK-79 through RK-92 inclusive; certificated in any category.

• AD 94-01-06

  Airworthiness Directives: Rockwell International, Collins Air Transport Division, Traffic Alert and Collision Avoidance System II Processors

  To prevent collisions or near misses caused by incompatibility between the traffic alert and collision avoidance system (TCAS) II processors and the current air traffic control system.

  Traffic Alert and Collision Avoidance System II processors that are installed on, but not limited to the following airplanes (all serial numbers), certificated in any category: General Aviation Airplanes Astra Model 1125 airplanes BAC Model 1-11 airplanes British Aerospace Model 125-800 airplanes Beech Models C90A, B20...

Beechcraft Beechjet 400A: price, specs and every tail

AD data from the Federal Register and the FAA. Data: Radar, FAA aircraft registry file of 2026-10-09.