BAe 125 Series 800A / Hawker 800 airworthiness directives

• AD 2013-11-16

  Effective 2013-07-02

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

  This AD was prompted by reports of several instances of severe vibration and wing/aileron oscillation due to lack of sufficient flutter margin with winglets installed.

  This AD applies to Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Model BAe.125 Series 800A (including C-29A and U-125), and 800B airplanes; and Model Hawker 800 (including variant U-125A) and 800XP airplanes; certificated in any category; modified by Aviation Partners Inc...

• AD 2010-06-11

  Effective 2010-04-21

  Honeywell International Inc. TFE731 Series Turbofan Engines

  We are issuing this AD to prevent an uncontained failure of a second stage LPCR disc and/or a third stage LPCR disc due to cracks in the bore, which could result in damage to the airplane.

  This AD applies to Honeywell International Inc. TFE731-2, TFE731-2A, TFE731-2C, TFE731-3, TFE731-3A, TFE731-3AR, TFE731-3B, TFE731-3BR, TFE731-3C, TFE731-3CR, TFE731-3D, TFE731-3DR, TFE731-3R, TFE731-4, TFE731-4R, TFE731-5, TFE731-5AR, TFE731-5BR, and TFE731-5R series turbofan engines with certain second stage low-pres...

• 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 2008-21-01

  Effective 2008-10-22

  Hawker Beechcraft Corporation Model BAe.125 Series 800A (including C-29A and U-125) Airplanes, and Hawker Beechcraft Model Hawker 800XP Airplanes

  We are issuing this AD to prevent a fracture of the MLG casings and a collapse of the affected MLG, which could adversely affect the airplane's continued safe flight and landing.

  This AD applies to Hawker Beechcraft Corporation Model BAe.125 series 800A (including C-29A and U-125) airplanes, and Hawker Beechcraft Model Hawker 800XP airplanes, certificated in any category; having serial numbers identified in Hawker Beechcraft Mandatory Service Bulletin SB 32-3920, dated August 2008.

• AD 2008-19-12

  Effective 2008-10-27

  Honeywell International Inc. TFE731-4, -4R, -5, -5AR, -5BR, and -5R Series Turbofan Engines

  We are issuing this AD to prevent uncontainment of turbine blades and fragments of the LPT nozzle assembly, which could result in damage to the airplane.

  This AD applies to Honeywell International Inc. TFE731-4, - 4R, -5, -5AR, -5BR, and -5R series turbofan engines, with interstage turbine transition (ITT) duct, part number (P/N) 3075292-1; 3075292- 3; 3074766-1; 3077063-1; 3075655-1; 3075655-2; 3075699-1; or 3075699-3, installed. These engines are installed on, but not...

• AD 2006-16-18

  Effective 2008-07-18

  Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes

  We are issuing this AD to prevent a bearing error, which could lead to an airplane departing from its scheduled flight path, which could result in a reduction in separation from, and a possible collision with, other aircraft or terrain.

  This AD applies to Sandel Avionics Incorporated (Sandel) Model ST3400 terrain awareness warning system/radio magnetic indicator (TAWS/RMI) units approved under Technical Standard Order(s) C113, C151a, or C151b; as identified in Sandel ST3400 Service Bulletin SB3400-01, Revision B, dated September 15, 2004; as installed...

• AD 2008-02-19

  Effective 2008-03-06

  Honeywell International Inc. TFE731-2C, -3B, -3BR, -3C, -3CR, -3D, -3DR, -4R, -5AR, -5BR, -5R, -20R, -20AR, -20BR, -40, -40AR, -40R, and -60 Series Turbofan Engines

  We are issuing this AD to prevent uncontained failure of the HP turbine rotor assembly, which could result in damage to the airplane.

  This AD applies to Honeywell International Inc. (Honeywell) TFE731-2C, -3B, -3BR, -3C, -3CR, -3D, -3DR, -4R, -5AR, -5BR, -5R, - 20R, -20AR, -20BR, -40, -40AR, -40R, and -60 series turbofan engines with certain high pressure (HP) turbine rotor discs part numbers and serial numbers. These engines are installed on, but no...

• 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 2006-19-04

  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 2005-16-02

  Effective 2005-09-06

  Raytheon Model HS.125 Series 700A Airplanes, Model BAe.125 Series 800A Airplanes, and Model Hawker 800 and Hawker 800XP Airplanes

  We are issuing this AD to prevent smoke and fumes in the cockpit in the event that a blower motor seizes and overheats due to excessive current draw.

  This AD applies to Raytheon Model HS.125 series 700A airplanes, BAe.125 series 800A airplanes, and Model Hawker 800 and Hawker 800XP airplanes; certificated in any category; equipped with Brailsford TBL-2.5 blowers; as identified in Raytheon Service Bulletin SB 24-3272, Revision 1, dated October 2000.

• AD 2005-03-16

  Effective 2005-03-21

  Raytheon Model DH.125, HS.125, and BH.125 Series Airplanes; BAe.125 Series 800A (C-29A and U-125) and 800B Airplanes; and Hawker 800 (Including Variant U-125A) and 800XP Airplanes; Equipped with TFE731 Engines

  This AD was prompted by a report indicating that insulation on the wire harness passing through the firewall fairlead ignited on the fuselage side of the firewall.

  This AD applies to Raytheon Model DH.125, HS.125, and BH.125 series airplanes; BAe.125 series 800A (C-29A and U-125) and 800B airplanes; and Hawker 800 (including variant U-125A) and 800XP airplanes; certificated in any category; equipped with TFE731 engines; as identified in Raytheon Service Bulletin SB 26-3496, dated...

• AD 2004-12-02

  Effective 2004-07-14

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

  Model BAe.125 series 800A, 800A (C-29A), and 800B airplanes; and Model Hawker 800 airplanes, as listed in Raytheon Service Bulletin SB 24-3588, Revision 1, dated September 2003; certificated in any category.

• AD 2004-11-01

  Effective 2004-07-07

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

  To prevent incorrect wiring of the engine fire extinguisher bottles, which could result in one or both fire extinguisher bottles being discharged into the wrong engine nacelle.

  Model BAe.125 series 800A (including C-29A and U- 125 variant) and 800B airplanes; and Model Hawker 800 (including U- 125A variant) and 800XP airplanes; as listed in Raytheon Service Bulletin SB 26-3610, Revision 1, dated September 2003; certificated in any category.

• AD 2003-07-07

  Effective 2003-05-08

  Raytheon Model BAe.125 Series 800A, 800A (C-29A), 800A (U-125), and 800B Airplanes; Model BH.125 Series 400A Airplanes; Model DH.125 Series Airplanes; Model Hawker 800, 800 (U-125A), and 800XP Airplanes; and Model HS.125 Series F3B, F3B/RA, F400B, F403B, 1B, 1B-522, 1B/R-522, 1B/S-522, 3B, 3B/R, 3B/RA, 3B/RB, 3B/RC, 400B, 400B/1, 401B, 403A(C), and 403B Airplanes

  To prevent separation of a main landing gear (MLG) wheel due to loose or missing tie-bolts or tie-bolt nuts, with consequent damage to airplane structure or systems, decompression, loss of full braking ability, or injury to personnel on the ground.

  The following airplanes, certificated in any category: Table--Airplane Models, Serial Numbers, and Equipment Model-- Serial No.-- Equipped with-- BAe.125 series 800A: All: none. BAe.125 series 800A (C-29A): All: none. BAe.125 series 800A (U-125): All: none. BAe.125 series 800B: All: none. BH.125 series 400A: All: none....

• AD 2003-06-06

  Effective 2003-04-30

  Raytheon Model Hawker 800XP and 800 (Including Variant U-125A) Airplanes

  To prevent failure of certain attachment bolts due to manufacturing discrepancies, which could result in reduced structural integrity of the airplane, and loss of system function for flaps, controls, and landing gear.

  Model Hawker 800XP and 800 (including variant U- 125A) airplanes, certificated in any category; serial numbers 258287 through 258390, excluding the following serial numbers: 258289, 258291, 258292, 258293, 258294, 258295, 258301, 258303, 258310, 258312, 258313, 258315, 258321, 258336, 258343

• 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 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 2001-15-25

  Effective 2001-09-10

  Raytheon Model Hawker 800XP Series Airplanes and Model Hawker 800 (U-125A Military) Airplanes

  To prevent a main landing gear (MLG) gear-up landing and possible injury to passengers and crew.

  Model Hawker 800XP series airplanes, and Model Hawker 800 (U-125A military) airplanes; certificated in any category; as listed in Raytheon Service Bulletin SB 32-3386, dated June 2000.

• 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 2000-22-22

  Effective 2000-12-19

  Raytheon Model Hawker 800XP and Hawker 800 (U-125A) Series Airplanes

  To detect and correct chafing of the wire bundle exiting panel "JA" due to insufficient clearance from the fuel cross-feed valve operating lever, which could result in a fire in the area of the fuel system in a confined space.

  Model Hawker 800XP series airplanes, as listed in Raytheon Service Bulletin SB 24-3212, dated August 1999; and Hawker 800 (U-125A) series airplanes, as listed in Raytheon Service Bulletin SB 24-3213, dated February 2000; certificated in any category.

• 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 2000-08-07

  Effective 2000-05-31

  Raytheon Model BAe 125-800A and BAe 125-800B, Model Hawker 800, and Model Hawker 800XP Series Airplanes

  To prevent an engine fire from moving to the fuselage and to the lines that carry flammable fluid that are located inboard of the firewall.

  Model BAe 125-800A and BAe 125-800B, Model Hawker 800, and Model Hawker 800XP series airplanes; as listed in Raytheon Service Bulletin SB.54-1-3815B, Revision 1, dated May 1998; certificated in any category.

• 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 97-05-03

  Effective 1999-04-20

  AlliedSignal Avionics, Inc. Models GNS- Xls and GNS-Xl Flight Management Systems

  To prevent deviation from an intended flight path during a non- precision approach to an airport caused by inaccurate information from the GPS flight management system.

  Models GNS-Xls and GNS-Xl global positioning systems (GPS), part numbers (P/N) 17960-0102-XXXX and P/N 18355- 0101-XXXX, respectively, installed on, but not limited to the following aircraft, certificated in any category: Manufacturer Models British Aerospace, Ltd. (BAe): 146-100A and 146-200A Cessna Aircraft Corporati...

• 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 98-11-13

  Effective 1998-06-08

  Raytheon Model Hawker 800XP Series Airplanes, and Hawker 800 (U-125A Military Derivative) Airplanes

  To prevent obstructions of the discharge tubes of the fire extinguisher assemblies, which could result in improper distribution of the fire extinguishing agent within the nacelle in the event of a fire.

  Model Hawker 800XP series airplanes and Hawker 800 (U-125A military derivative) airplanes, as listed in Raytheon Service Bulletin SB.26-3197, dated April 1998; certificated in any category.

• AD 97-21-05

  Effective 1997-11-24

  Raytheon Model DH.125-400A; BH.125-400A and -600A; HS.125-600A and -700A; BAe 125-800A Series Airplanes; and Hawker 800 and Hawker 800 XP Series Airplanes Including Military Variants

  To prevent leaks in high pressure oxygen hose assemblies, which could result in insufficient oxygen quantity available to the passengers or crew if the cabin pressure altitude should rise to a level requiring emergency oxygen.

  All Model DH.125-400A, BH.125-400A and -600A, HS.125-600A and -700A, and BAe 125-800A series airplanes; and Model Hawker 800 and Hawker 800 XP series airplanes (including Military Variants C29A, U125, and U125A airplanes); having serial numbers 1 through 258294 inclusive; on which Modification 252036 has been installed...

• AD 97-21-03

  Effective 1997-11-19

  Raytheon Model BAe 125-800A Series Airplanes and Hawker 800 Series Airplanes

  Model BAe 125-800A series airplanes (including military variants C-29A and U-125) and Hawker 800 series airplanes, constructor's numbers 8091 and subsequent; equipped with Turbomach auxiliary power unit (APU) (Modification 259404B); certificated in any category.

• AD 97-18-07

  Effective 1997-10-03

  Raytheon Model BAe 125-800A Series Airplanes, and Model Hawker 800 and Hawker 800XP Series Airplanes

  To prevent overbias or overbalance of the rudder, which could result in reduced controllability of the airplane.

  Model BAe 125-800A, and Model Hawker 800 and Hawker 800XP series airplanes; on which Raytheon Modification 25F017A&B (reference Raytheon Service Bulletin SB.55-36-25F017A&B) has not been installed; 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 96-24-16

  Effective 1997-01-27 · superseded or removed

  Raytheon Model BAe 125-800A, Model Hawker 800, and Model Hawker 800XP Series Airplanes

  To prevent an engine fire from moving to the fuselage and flammable fluid carrying lines located inboard of the firewalls on the left and right engine pylons.

  Model BAe 125-800A series airplanes, Model Hawker 800 series airplanes including Special Variants (C29A, U125, and U125A), and Model Hawker 800XP series airplanes; on which the modification described in Raytheon Service Bulletin SB.54-1-3815B, or a production equivalent, has not been installed; certificated in any cate...

• 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 96-12-17

  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 96-12-16

  Effective 1996-07-15

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

  Model BAe 125 series 800A airplanes (including military variants C-29A and U-125); and Model Hawker 800 airplanes, excluding airplanes having constructor's numbers 258079 and 258213; 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 95-08-06

  Effective 1995-05-18

  Raytheon Corporate Jets Models DH/BH/ HS/BAe 125-1A to -700A Series Airplanes; BAe 125-800A Airplanes; and Hawker 800 Series Airplanes

  To prevent an electrical short in the standby static inverter due to the printed circuit boards being exposed to condensed moisture.

  Model DH/BH/HS/BAe 125-1A to -700A series airplanes, inclusive, on which Modification 252740 has been installed; Model BAe 125-800A airplanes having constructor's numbers prior to number 258248; and Hawker 800 series airplanes; 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 ...

BAe 125 Series 800A / Hawker 800: price, specs and every tail

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