Hawker 1000 / BAe125 Series1000 (certified family) airworthiness directives

• AD 2016-13-13

  Effective 2016-08-12

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

  This AD was prompted by reports of inadvertent stowage of the thrust reversers, which can result in high forward engine thrust even though the throttle is commanding reverse thrust.

  This AD applies to Beechcraft Corporation (type certificate previously held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model BAe.125 series 1000A and 1000B airplanes, serial numbers 258151, 258159, a...

• AD 2010-24-05

  Effective 2011-01-03

  Pratt & Whitney Canada Corp. (P&WC) PW305A and PW305B Turboprop Engines

  We are issuing this AD to prevent failure of the impeller, which could result in an uncontained event and possible damage to the airplane.

  This AD applies to Pratt & Whitney Canada Corp. (P&WC) PW305A and PW305B turboprop engines with certain impellers, part numbers (P/Ns) 30B2185, 30B2486, 30B2858-01, or 30B4565-01 installed. These engines are installed on, but not limited to, Hawker-Beech Corporation BAe.125 series 1000A, 1000B, and Hawker 1000 airplane...

• AD 2010-07-02

  Effective 2010-05-03

  Various Aircraft Equipped With Honeywell Primus II RNZ-850( )/-851( ) Integrated Navigation Units

  This AD applies to various aircraft, certificated in any category, equipped with any Honeywell Primus II RNZ-850( )/-851( ) integrated navigation units (INUs) identified in a service bulletin identified in Table 1 of this AD. The aircraft include, but are not limited to, BAE Systems (Operations) Limited (Jetstream) Mod...

• AD 2009-08-01

  Effective 2009-05-14

  Honeywell Flight Management Systems (FMSs) Equipped With Honeywell NZ-2000 Navigation Computers and Honeywell IC-800 or IC-800E Integrated Avionics Computers; as Installed on Various Transport Category Airplanes

  We are issuing this AD to prevent a shift in the FMS computed position, which could result in uncommanded deviations from the intended flight path of the airplane and, if those deviations are undetected by the flight crew, compromised terrain/traffic avoidance.

  This AD applies to all Honeywell NZ-2000 navigation computers and Honeywell IC-800 or IC-800E integrated avionics computers; as installed on transport category airplanes, certificated in any category, including but not limited to the airplanes identified in Table 1 of this AD. Table 1--Known Affected Airplanes Manufact...

• AD 2007-07-12

  Effective 2007-04-18 · superseded or removed

  Honeywell Flight Management Systems (FMSs) Served by Honeywell NZ-2000 Navigation Computers Approved Under Technical Standard Order (TSO) TSO-C115a, and IC-800 Integrated Avionics Computers Approved Under TSOs C9c, C52a, and C115a; as Installed on Various Transport Category Airplanes

  We are issuing this AD to prevent a shift in the FMS computed position, which could result in uncommanded deviations from the intended flight path of the airplane and, if those deviations are undetected by the flight crew, compromised terrain/traffic avoidance.

  This AD applies to all Honeywell NZ-2000 navigation computers approved under Technical Standard Order (TSO) TSO-C115a, and IC-800 integrated avionics computers approved under TSOs C9c, C52a, and C115a; as installed on transport category airplanes, certificated in any category, including but not limited to the airplanes...

• AD 2006-22-05

  Effective 2006-12-01 · superseded or removed

  Various Aircraft Equipped With Honeywell Primus II RNZ-850( )/-851( ) Integrated Navigation Units

  This AD applies to aircraft, certificated in any category, equipped with a Honeywell Primus II RNZ-850( )/-851( ) integrated navigation unit (INU) having a part number identified in Table 1 of this AD; including, but not limited to, BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes; Bombardier Model BD-...

• AD 2006-19-04

  Effective 2006-10-17

  Honeywell RCZ-833J/K, -851J/K, and -854J Communication (COM) Units, Equipped with XS-852E/F Mode S Transponders; and Honeywell XS-856A/B and -857A Mode S Transponders; Installed on But Not Limited to Certain Transport Category Airplanes

  We are issuing this AD to prevent the transponder of the COM unit from going into standby mode, which could increase the workload on the flightcrew and result in improper functioning of the traffic alert and collision avoidance system.

  This AD applies to the Honeywell parts identified in paragraphs (c)(1) and (c)(2) of this AD, approved under Technical Standard Order TSO-C112, installed on but not limited to Bombardier Model BD-700-1A10 and BD-700-1A11 airplanes; Cessna Model 550 and 560 airplanes; Cessna Model 650 airplanes; Dassault Model Falcon 90...

• AD 2006-12-20

  Effective 2006-07-03

  Raytheon Model HS.125 Series 700A and 700B Airplanes; Model BAe.125 Series 800A (Including Variants C-29A and U-125), 800B, 1000A, and 1000B Airplanes; and Hawker 800 (Including Variant U-125A), 800XP, and 1000 Airplanes

  We are issuing this AD to prevent loss of all primary electrical power, which could result in the airplane operating only under emergency power.

  This AD applies to the Raytheon airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category. (1) Model HS.125 series 700A and 700B airplanes, on which Raytheon Modification 252885 has been incorporated or British Aerospace 125 Service Bulletin SB 24-239-2885 has been accomplis...

• AD 2006-01-04

  Effective 2006-02-22

  Raytheon Model DH.125, HS.125, and BH.125 Series Airplanes; Model BAe.125 Series 800A (C-29A and U-125), 800B, 1000A, and 1000B Airplanes; and Model Hawker 800 (including variant U-125A), and 1000 Airplanes

  We are issuing this AD to prevent heat and fire damage to equipment adjacent to the fan venturi, which could result in smoke in the cabin and/or burning equipment.

  This AD applies to Raytheon Model DH.125, HS.125, and BH.125 series airplanes; Model BAe.125 Series 800A (C-29A and U-125), 800B, 1000A, and 1000B airplanes; and Model Hawker 800 (including variant U-125A), and 1000 airplanes, certificated in any category; as identified in Raytheon Service Bulletin SB 21-3669, dated De...

• AD 2005-11-05

  Effective 2005-07-18

  Precise Flight, Inc. Models SVS I and SVS IA Standby Vacuum Systems

  This AD affects Models SVS I and SVS IA standby vacuum systems (SVS), installed on, but not limited to, the following aircraft that are certificated in any category. These systems can be installed under the applicable supplemental type certificate (STC) or through field approval: Affected STC Make and model/series airc...

• AD 2003-04-20

  Effective 2003-04-04

  Raytheon Model DH.125, HS.125, and BH.125 Series Airplanes; Model BAe.125 Series 800A, 800A (C-29A), 800A (U-125), 800B, 1000A, and 1000B Airplanes; and Model Hawker 800, 800 (including variant U-125A), 1000, and 800XP Airplanes

  To prevent separation of the cylinder head lugs, which could prevent the main landing gear (MLG) from extending and result in a partial gear-up landing.

  Model DH.125, HS.125, and BH.125 series airplanes; Model BAe.125 series 800A, 800A (C-29A), 800A (U-125), 800B, 1000A, and 1000B airplanes; and Model Hawker 800, 800 (including variant U-125A), 1000, and 800XP airplanes; as listed in Raytheon Service Bulletin 32-3391, dated August 2000; certificated in any category.

• AD 2003-04-06

  Effective 2003-03-11 · superseded or removed

  Various Aircraft Equipped With Honeywell Primus II RNZ-850/-851 Integrated Navigation Units

  To ensure that the flightcrew has an accurate glideslope deviation indication.

  Aircraft, certificated in any category, equipped with a Honeywell Primus II RNZ-850/-851 Integrated Navigation Unit having a part number identified in Table 1 of this AD; including, but not limited to BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes; Bombardier BD-700-1A10 series airplanes; Bombardier ...

• AD 2001-17-26

  Effective 2001-10-03 · superseded or removed

  Raytheon Model DH.125, HS.125, BH.125, and BAe. 125 (U-125 and C-29A) Series Airplanes; Model Hawker 800, Hawker 800 (U-125A), Hawker 800XP, and Hawker 1000 Airplanes

  To prevent separation of the cylinder head lugs, which could prevent the main landing gear (MLG) from extending and result in a partial gear-up landing.

  Model DH.125, HS.125, BH.125, and BAe. 125 (U-125 and C-29A) series airplanes; Model Hawker 800, Hawker 800 (U-125A), Hawker 800XP, and Hawker 1000 airplanes; certificated in any category.

• AD 2001-13-05

  Effective 2001-08-01

  Raytheon Model BAe.125 Series 800A (C-29A and U-125 Military), 1000A, and 1000B Airplanes; Hawker 800 (U-125A Military) Airplanes; and Hawker 800XP and 1000 Series Airplanes

  To prevent the turbine air discharge duct or water separator outlet duct from disconnecting from the cold air unit turbine or from the water separator, resulting in the loss of air supply to maintain adequate cabin pressure.

  Model BAe.125 series 800A (C-29A and U-125 military), 1000A, and 1000B airplanes; Hawker 800 (U-125A military) airplanes, up to and including serial number 258406; and Hawker 800XP series airplanes, up to and including serial number 258483, and 1000 series airplanes; certificated in any category.

• AD 2001-04-10

  Effective 2001-04-06

  Pratt & Whitney Canada (PWC) Model PW305 and PW305A Turbofan Engines

  To prevent premature LPT disk failure due to cracking of the LPT disks, which could result in an uncontained engine failure and damage to the airplane.

  Pratt & Whitney Canada (PWC) Models PW305 and PW305A turbofan engines with stage 4 low pressure turbine (LPT) disks, part numbers (P/N's) 30A1457 and 30A1499. These engines are installed on but not limited to British Aerospace BAe. 125 1000A, BAe. 125 1000B, Hawker 1000, and Learjet 60 series airplanes.

• AD 2000-22-03

  Effective 2000-12-04 · recurring

  Raytheon Model DH.125, Model HS.125, Model BH.125, Model BAe.125 Series 800A (Including Major Variants C-29A and U1-25), Model Hawker 800, Model Hawker 800XP, and Model Hawker 1000 Series Airplanes

  To prevent erroneous altimeter and airspeed indications due to plugged or taped pitot/static and stall vent drain valves.

  Model DH.125, Model HS.125, Model BH.125, Model BAe.125, Model Hawker 800, Model Hawker 800XP, and Model Hawker 1000 series airplanes; as listed in Raytheon Aircraft Service Bulletin SB 34-3207, dated August 1999; excluding those airplanes on which all pitot/static drain vent valves have been modified with an insert in...

• AD 2000-02-35

  Effective 2000-03-13

  Raytheon Model Hawker 800 and 1000 Airplanes and Model DH.125, HS.125, BH.125, and BAe.125 Series Airplanes

  To prevent flaking of cadmium from certain oxygen system plumbing fittings and cone caps from blocking the valves and impairing the function of the oxygen system, which could deprive the crew and passengers of necessary oxygen during an emergency that requires oxygen.

  Models and series of airplanes as listed in the applicable service bulletin(s) specified in Table 1 of this AD, certificated in any category. Table 1 Raytheon Service Date of Service Model of Airplane Bulletin Bulletin DH.125, HS.125, BH.125 series 1A, SB 35-3169: September 1998. 1B, 3A, 3B, 400A, 400B, 401B, 403A, 403...

• AD 2000-01-02

  Effective 2000-02-15

  Raytheon Model BAe.125 Series 1000A and 1000B Airplanes and Model Hawker 1000 Series Airplanes

  To prevent the turbine air discharge duct in the air conditioning system from disconnecting from the CAU or water separator in flight, which could result in cabin depressurization.

  All Model BAe.125 series 1000A and 1000B airplanes and Model Hawker 1000 series airplanes, certificated in any category.

• AD 99-25-01

  Effective 2000-01-04

  Raytheon Model BAe.125 Series 1000A and 1000B, and Model Hawker 1000 Series Airplanes

  To prevent a hole in the P1 pitot pipes, which would lead to erroneous input to the instrumentation and warning systems associated with the pilot's instruments.

  All Model BAe.125 series 1000A and 1000B, and Model Hawker 1000 series airplanes; certificated in any category.

• AD 99-24-10

  Effective 2000-01-14 · recurring

  Precise Flight, Inc. Model SVS III Standby Vacuum Systems

  To detect and correct problems with the standby vacuum system before failure or malfunction and to provide operating procedures for the pilot regarding the use and limitations of this system.

  Model SVS III standby vacuum systems, installed on, but not limited to, the aircraft listed in the following chart. These systems can be installed either in accordance with the applicable supplemental type certificate (STC) or through field approval: Affected STC Make and model airplanes SA2160NM: Raytheon Beech Models...

• AD 99-23-10

  Effective 1999-12-17

  Raytheon Model Hawker 1000 Series Airplanes

  To prevent a short circuit due to wire chafing, which can cause a fire in the ventral fuel tank area.

  Model Hawker 1000 series airplanes, serial numbers 258151, 258159, and 259003 through 259052 inclusive, certificated in any category.

• AD 89-18-07

  Effective 1998-12-18

  Raytheon Model BAe.125, DH.125, BH.125, and HS.125 Series Airplanes

  To prevent control surface interference and jamming of flight controls.

  Model BAe.125, DH.125, BH.125, and HS.125 series airplanes; up to and including series 700; certificated in any category.

• AD 97-26-10

  Effective 1998-01-23

  Raytheon Model Hawker 1000 Series Airplanes

  Model Hawker 1000 series airplanes; serial numbers 258151, 258159, and 259003 through 259052 inclusive; certificated in any category.

• AD 97-09-05

  Effective 1997-05-30

  Raytheon Model BAe 125-1000A and Model Hawker 1000 Series Airplanes

  To prevent inadequate venting of cabin pressure in the event of rapid decompression, which could cause failure or deformation of certain structural members, and consequent reduced controllability of the airplane.

  All Model BAe 125-1000A and Model Hawker 1000 series airplanes, certificated in any category.

• AD 97-03-07

  Effective 1997-03-11 · recurring

  Raytheon Model Hawker 800 and 1000 and Model DH/BH/HS/BAe 125 Series Airplanes (Including Major Variants C29A, U125, and U125A Series Airplanes)

  To prevent the inability of the MLG to deploy and a consequent wheels-up landing.

  Model Hawker 800 and 1000 and Model DH/BH/HS/BAe 125 series airplanes (including major variants C29A, U125, and U125A series airplanes); equipped with main landing gear (MLG) sidestay assemblies on which Post-Mod 252091 steel jack pivots have been installed; certificated in any category.

• AD 96-22-03

  Effective 1996-12-11

  Beech (Raytheon) Model BAe 125 Series 1000A and Model Hawker 1000 Airplanes

  To prevent inadvertent deployment of a thrust reverser during flight, and consequent reduced controllability of the airplane.

  Model BAe series 1000A and Model Hawker 1000 airplanes; as identified in Hawker Service Bulletin SB.78-14-3691A, B&E, dated June 21, 1995; certificated in any category.

• AD 96-18-09

  Effective 1996-10-09

  Beech (Raytheon) Model BAe 125-800A and -1000A, and Model Hawker 800 and 1000 Series Airplanes

  To ensure that silver plated wiring is removed from the TKS metering pump and a possible fire hazard eliminated.

  Model BAe 125-800A and -1000A, and Model Hawker 800 and 1000 series airplanes; on which Modification 257676A has not been accomplished (reference Hawker Service Bulletin SB.30-61-7676A or Aerospace Systems and Technology Service Bulletin S.B.30-25); certificated in any category.

• AD 96-17-13

  Effective 1996-09-30

  Beech (Raytheon) Model BAe 125 Series 1000A and Model Hawker 1000 Airplanes

  To prevent reduced structural integrity of the elevator control circuit.

  Model BAe 125 series 1000A and Model Hawker 1000 airplanes; as listed in Hawker Service Bulletin SB 27-161, Revision 1, dated July 29, 1994; certificated in any category.

• AD 96-17-09

  Effective 1996-09-24

  Beech (Raytheon) Model Hawker 1000 and BAe 125-1000A Series Airplanes

  To prevent failure of a fuel hose assembly on the auxiliary power unit (APU), which could result in a malfunction of the APU, a potential fuel fire in the fuselage rear bay, and reduced structural integrity of the surrounding structure.

  Model Hawker 1000 and BAe 125-1000A series airplanes, post modification 259722C; certificated in any category.

• AD 96-12-17

  Effective 1996-07-15

  Beech (Raytheon) Model BAe 125 Series 800A and 1000A, and Model Hawker 800 and 1000 Airplanes

  To prevent incorrect fault displays in the cockpit and intermittent fault symptoms in the engine starting and battery emergency control circuits, as a result of imperfect soldered connections.

  Model BAe 125 series 800A and 1000A, and Model Hawker 800 and 1000 airplanes; as listed in Raytheon Corporate Jets Hawker Service Bulletin SB 24-317, dated December 22, 1994; certificated in any category.

• AD 96-11-17

  Effective 1996-07-09

  Beech (Raytheon) Model BAe 125 Series 1000A and Model Hawker 1000 Airplanes

  To prevent restriction or loss of the flight controls due to insufficient clearance and resultant chafing and damage to the flaps cable and/or turnbuckle and the airbrakes cable.

  Model BAe 125 series 1000A and Model Hawker 1000 airplanes, as listed in Hawker Service Bulletin SB.27-168, dated July 17, 1995; certificated in any category.

• AD 96-07-11

  Effective 1996-05-06

  Beech Model BAe 125-1000A and Hawker 1000 Series Airplanes

  All Model BAe 125-1000A and Hawker 1000 series airplanes, certificated in any category.

• AD 95-21-17

  Effective 1995-11-17

  Raytheon Corporate Jets Model Hawker 1000 and BAe 125-1000A Series Airplanes

  To prevent incorrect fault displays in the cockpit and possible electrical systems failures.

  Model Hawker 1000 and BAe 125-1000A series airplanes; as listed in Raytheon Service Bulletin SB 24-313, dated December 19, 1994; certificated in any category.

• AD 95-15-04

  Effective 1995-08-23

  Raytheon Corporate Jets Model BAe 125- 800A and -1000A Airplanes

  To prevent reduced structural integrity of the wing leading edge skin and wing anti-ice fluid distribution panel (TKS panel) interface joint, which could adversely affect the flight characteristics of the airplane.

  Model BAe 125-800A and -1000A airplanes, as listed in Raytheon Corporate Jets Service Bulletin S.B. 57-77, Revision 1, dated October 28, 1993, certificated in any category.

• AD 95-10-01

  Effective 1995-05-23 · superseded or removed

  Raytheon Model Hawker 1000 and BAe 125- 1000A Series Airplanes

  To prevent failure of a fuel hose assembly on the auxiliary power unit (APU), which could result in a malfunction of the APU, a potential fuel fire in the fuselage rear bay, and reduced structural integrity of the surrounding structure.

  Model Hawker 1000 and BAe 125-1000A series airplanes, post modification 259722C, certificated in any category.

• AD 94-26-12

  Effective 1995-02-03 · superseded or removed

  Raytheon Corporate Jets Model Hawker 800 and 1000 and Model DH/BH/HS/BAe 125 Series Airplanes

  To prevent the inability of the MLG to deploy and a consequent wheels-up landing.

  Model Hawker 800 and 1000 series airplanes and Model DH/BH/HS/BAe 125-1A through -1000A series airplanes; equipped with main landing gear (MLG) sidestay assemblies on which Post-Mod 252091 steel jack pivots have been installed; certificated in any category.

• AD 94-01-04

  Effective 1994-02-04

  Honeywell Traffic Alert and Collision Avoidance System II Computer Units, as Installed on Various Transport Category Airplanes

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

  Traffic Alert and Collision Avoidance System (TCAS) II computer units; part numbers 4066010-901, -902, and -903; as installed on, but not limited to, the following airplanes, certificated in any category: Airbus Industrie Model A300-600, A310-200, A310-300, A320-200, and A340 series airplanes; Boeing Model 727-100 and ...

Hawker 1000 / BAe125 Series1000 (certified family): price, specs and every tail

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