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Hawker 1000 / BAe125 Series1000 (certified family) airworthiness directives FAA ADs that may apply, with the official text

In effect
31
Recurring
3
FAA ADs published since 1995 that name the BAE 125 SERIES 1000A, BAE 125-1000A and HAWKER 1000, through Oct 1, 2026. Recurring ADs repeat at set intervals until a terminating action.
See the 31 in effect
Hawker 1000 / BAe125 Series1000 (certified family) exterior illustration: Hawker 1000 reference airframe.
Illustration of the Hawker 1000 reference airframe. Individual aircraft and configurations vary. Hawker 1000 exterior reference for the qualified BAe125 Series1000 certified design. This illustration does not establish installed PW305B engines, service-bulletin modifications, equipment or cabin completion.
  • Superseded or removed6
  • Latest2016-13-13

Hawker 1000 / BAe125 Series1000 (certified family): price, specs and every tail number · Look up ADs by N-number · AD burden by model, ranked

IN EFFECT

31 Hawker 1000 / BAe125 Series1000 (certified family) ADs in effect, newest first

Informational only. These are FAA airworthiness directives whose published applicability names this make and model. Whether an AD applies to a particular aircraft depends on its serial number, installed engines, propellers, parts and modifications, and some ADs listed here will not apply. This list is not the official AD record and not a compliance determination: confirm applicability and compliance against the FAA’s Dynamic Regulatory System and the aircraft’s records with a certificated mechanic or inspector. Covers ADs published in the Federal Register since 1995, through Oct 1, 2026; older ADs, and engine, propeller and appliance ADs that do not name the aircraft, are not included.

  1. AD 2016-13-13 One-time

    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.

    Effective Aug 12, 2016 · Amendment 39-18577

    Applicability, as the AD words it

    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, and 259004 through 259042 inclusive. (2) Model Hawker 1000 airplanes, serial numbers 259003 and 259043 through 259052 inclusive.

    Federal Register Official PDF

  2. AD 2010-24-05 One-time Engine

    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.

    Effective Jan 3, 2011 · Amendment 39-16524 · Corrected Jan 4, 2011

    Applicability, as the AD words it

    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 airplanes and Learjet Inc. Learjet 60 airplanes.

    Federal Register Official PDF Correction (Jan 4, 2011)

  3. AD 2010-07-02 One-time

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

    Effective May 3, 2010 · Amendment 39-16246 · Replaces AD 2006-22-05

    Applicability, as the AD words it

    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) Model 4101 airplanes; Bombardier Model BD-700-1A10 airplanes; Bombardier Model CL-215-6B11 (CL-415 variant) airplanes; Cessna Model 560, 560XL, and 650 airplanes; Dassault-Aviation Model Mystere-Falcon 50 airplanes; 328 Support Services GmbH (Dornier) Model 328-100 and -300 airplanes; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes; Learjet Model 45 airplanes; Hawker Beechcraft Corporation Model Hawker 800XP and Hawker 1000 airplanes; and Sikorsky Model S-76A, S-76B, and S-76C aircraft. Table 1--Service Bulletins Affected by This AD INUs listed in Honeywell-- Revision-- Dated-- (1) Alert Service Bulletin 001: March 4, 2003. 7510134-34-A0016. (2) Alert Service Bulletin Original: July 11, 2003. 7510134-34-A0017. (3) Service Bulletin 7510134- Original: July 8, 2004. 34-0018. (4) Alert Service Bulletin Original: February 28, 2003. 7510100-34-A0034. (5) Alert Service Bulletin Original: July 11, 2003. 7510100-34-A0035. (6) Service Bulletin 7510100- Original: July 8, 2004. 34-0037.

    Federal Register Official PDF

  4. AD 2009-08-01 One-time

    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.

    Effective May 14, 2009 · Amendment 39-15874 · Replaces AD 2007-07-12

    Applicability, as the AD words it

    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 Manufacturer Model Bombardier, Inc: CL-600-2B16 (CL-601-3A, CL-601- 3R, and CL-604) airplanes. Dassault Aviation: Mystere-Falcon 900 airplanes. Gulfstream Aerospace Corporation: G-1159A and GV airplanes, and G- IV series airplanes. Lockheed: 382G series airplanes. Hawker Beechcraft (formerly Raytheon BAe.125 Series 800A (including Aircraft Company). C-29A and U-125) airplanes. Hawker 800XP and 1000 airplanes.

    Federal Register Official PDF

  5. AD 2006-19-04 One-time

    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.

    Effective Oct 17, 2006 · Amendment 39-14761

    Applicability, as the AD words it

    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 900EX airplanes, serial number (S/N) 97 and S/Ns 120 and subsequent; Dassault Model Falcon 2000EX airplanes, S/N 6 and S/Ns 28 and subsequent; EMBRAER Model EMB-135BJ, -135ER, -135KE, -135KL, and - 135LR airplanes; EMBRAER Model EMB-145, -145ER, -145MR, -145LR, - 145XR, -145MP, and -145EP airplanes; Learjet Model 45 airplanes; Lockheed Model 282-44A-05 (C-130B) airplanes; Lockheed Model 382G series airplanes; Raytheon Model Hawker 800 (including variant U- 125A), 800XP, and 1000 airplanes; certificated in any category. (1) Communication (COM) unit RCZ-833J part numbers (P/Ns) 7510700-763 and -863; RCZ-833K P/Ns 7510700-765 and -875; RCZ-851J P/N 7510700-813; RCZ-851K P/N 7510700-815; and RCZ-854J P/Ns 7510700-725 and -825. (2) Mode S transponder XS-856A P/Ns 7517400-865 and -885; XS- 856B P/Ns 7517400-866 and -886; and XS-857A P/Ns 7517400-876 and - 896.

    Federal Register Official PDF

  6. AD 2006-12-20 One-time

    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.

    Effective Jul 3, 2006 · Amendment 39-14646

    Applicability, as the AD words it

    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 accomplished. (2) All Model BAe.125 series 800A (including variants C-29A and U-125), 800B, 1000A, and 1000B airplanes. (3) All Model Hawker 800 (including variant U-125A) and 1000 airplanes; and Model Hawker 800XP airplanes, serial numbers 1 through 258768 inclusive.

    Federal Register Official PDF

  7. AD 2006-01-04 One-time

    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.

    Effective Feb 22, 2006 · Amendment 39-14443 · Replaces AD 94-11-03

    Applicability, as the AD words it

    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 December 2004.

    Federal Register Official PDF

  8. AD 2005-11-05 One-time Appliance

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

    Effective Jul 18, 2005 · Amendment 39-14107

    Applicability, as the AD words it

    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 aircraft SA2160NM: Raytheon Beech Models 23, A23, A23A, A23-19, 19A, B19, B19A, A23- 24, B23, C23, A24, A24R, B24R, C24R, 35, A35, B35, C35, D35, E35, F35, G35, 35R, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC, 4S(YT-34), A45(T-34A, B- 45), D45(T-34B), and Series 77. SA2161NM: Raytheon Beech Model V35B. SA2162NM: The Cessna Aircraft Company Models 321 (Navy OE-2), 172N, 172P, 172D, 172M, 172L, 172I, 172H (USAF T-41A), 172F (USAF T-41A), 172E, 172C, 172, 172Q, 172B, TR182, T182, 305B (Military T0-1D, 0- 1D, 0-1F), R172E Series, 175C, 175B, 175A, R172F (USAF T-41D), P172D, 150, 150A, 150C, 150B, 150D, A152, A150M, 150M, 152, A150L, 150K, 150J, 150H, 150G, 150F, 210-5 (205), 210-5A (205A), T210R, P210R, T210N, 210N, P210N, 210M, T210L, 210K, T210K, 210J, T210H, 210H, T210G, T210F, 210F, 210D, 210C, 210B, 210A, 210L, 210, A185F, A185E, 185E, 185C, 185B, 185A, 185, 140A, 305A (USAF 0-1A), 305C (USAF 0-1E), 305D (USAF 0-1G), 305F, 120, 170B, 170A, 170, 207A, T207, 207, 206, P206B, P206, P206C, TU206A, TU206G, TU206E, TU206C, P206D, U206G, U206F, U206E, U206D, U206C, U206A, TP206E, TP206D, TP206C, TP206A, P206E, TU206D, T188C, A188B, A188, 188A, and 188. SA2164NM: The Cessna Aircraft Company Model 180A. SA2167NM: The New Piper Aircraft, Inc. Models PA-16S and PA-16, Series PA-24, Models PA-24-400, PA-24-250, PA-24, PA-24-260, PA-18S-"135", PA- 18"105" (Special), PA-18AS-"135", PA-18A-"135", PA-18- "150", PA-19S, PA-19 (Army L-18C), PA-18S-"150", and PA-18- "135" (Army L-21B), Series PA-18, Models PA-18-"125" (Army L- 21A), PA-18S, PA-18A, PA-18, and PA-18S-"125", Series PA-19 and PA-20, Models PA-20, PA-20S, PA-20-"135", PA-20-"115", and PA- 22S-160, Series PA-22, Models PA-22-160, PA-22S-150, PA-22-150, PA- 22, PA-22-108, PA-22-135, and PA-22S-135, Series PA-28, Model PA- 28R-200, Series PA-28S and PA-28R, Models PA-28-236, PA-28-201T, PA-28R-180, PA-28RT-201T, PA-28RT-201, PA-28R-201, PA-28-181, PA- 28S-180, PA-28R-201T, PA-28S-160, PA-28-235, PA-28-180, PA-28-161, PA-28-160, PA-28-151, PA-28-150, and PA-28-140, Series PA-25 (Normal Category (Cat.)), Models PA-25-260 (Normal Cat.), PA-25- 235 (Normal Cat.),PA-25 (Normal Cat.), L-14, PA-12S, PA-12, PA-14, PA-15, PA-17, PA-38-112, PA-46-310P, and PA-32-260, Series PA-32 and PA-32R, Models PA-32-300, PA-32-301T, PA-32-301, PA-32R-301T, PA-32R-301(HP), PA-32R-301(SP), PA-32RT-300T, PA-32RT-300, PA-32R- 300, and PA-32S-300, Series PA-36, Models PA-36-375 (Normal Cat.), PA-36-300 (Normal Cat.), and PA-36-285 (Normal Cat.) SA2168NM: Learjet Inc. Model Learjet 24D Mooney Aircraft Corporation Models M20C, M20M, M20K, M20J, M20G, M20B, M20A, M20, M20F, M20E, and M22. SA2683NM: Aermacchi S.p.A. Models F.260, F.260B, S.205-22/R, S.205-18/F, S.205-18/R, S.205-20/F, S.205-20/R, S.208A, and S.208 Aerocar, Incorporated Model I Aerodifusion, S.L. Model Jodel D-1190S Aeromere S.A. Model Falco F.8.L Aeronautica Macchi S.p.A. Models AL60, AL60-B, AL60-F5, and AL60-C5 Aeronautica Macchi S.p.A. & Aerfer-Industrie Aerospaziali Meridionali S.p.A. Model AM-3 Aeronca Aircraft Corporation Models S15AC and 15AC Ag Cat Corporation Models G-164B, G-164, and G-164A Alliance Aircraft Group, LLC Models H-395 (USAF L-28A or U-10B), H-250, H-295 (USAF U-10D), HT-295, H-391 (USAF YL-24), H-391B, H-700, and H-395A American Champion Aircraft Corp. Models 7AC, 7FC, 7ACA, S7AC, 7BCM (L-16A), 7CCM (L-16B), 7DC, S7DC, 7EC, S7EC, 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB, 11BC, S11AC, S11BC, 11AC, 11CC, S11CC, 8KCAB, and 8GCBC Arctic Aircraft Company, Inc. Models S-1A, S-1A-65F, S-1A-85F, S-1A-90F, S-1B2, S- 1B1 (Army L-6), and S-1B1 (Army XL-6) Augustair, Inc. Models 2150A, 2180, and 2150 Avions Jodel Models D-1190, 150, D-140-B, and DR-1050 Bellanca Aircraft Corporation Models 14-19-2, 14-19- 3A, 17-30, 17-31, 17-31TC, 14-9, 14-9L, 14-12F-3, 14-13, 14-13-2, 14-13-3, 14-13-3W, 17-30A, 17-31A, and 17-31ATC Biemond, C. Model Teal CB1 Board, G.R. Model Columbia XJL-1 Booth, Lee F. dba Taylorcraft Aerospace Models F21, F21A, and F19 Chaparral Motors, Inc. Models 2T-1A-1 and 2T-1A-2 Clark Aircraft, Inc. Models 12 and 1000 Commander Aircraft Company Models 114A, 112, 112B, 112TCA, 114, and 112TC C. Itoh Aircraft Maintenance and Engineering Co., Ltd. Model N-62 DaimlerChrysler Aerospace AG Models Bolkow Jr., BO- 209-150 FV & RV, BO-209-160 FV & RV, and BO-209-150 FF Flugzeugwerke Altenrheim AG (FFA) Model AS 202/15 "BRAVO" Found Brothers Aviation Limited Model FBA-2C Fuji Heavy Industries, Ltd. Models FA-200-180AO, FA-200-180, and FA-200-160 Funk Aircraft Company Model Funk C Goodyear Aircraft Corporation Model GA-22A Gulfstream Aerospace Corporation Model 111 Jamieson Corporation, The Model J-2-L1B Kearns, Edward Scott Model Trojan A-2 Luscombe Aircraft Corporation Model 11A Luscombe, The Don, Aviation History Foundation, Inc. Models T-8F, 8A, 8E, 8D, 8B, 8, 8F, and 8C Maule Aerospace Technology, Inc. Models Bee Dee M-4-210, Bee Dee M-4- 180S, Bee Dee M-4-180C, Bee Dee M-4T, Bee Dee M-4-210S, Bee Dee M- 4S, Bee Dee M-4-210T, Bee Dee M-4-210C, Bee Dee M-4-220S, Bee Dee M-4-220T, Bee Dee M-5-180C, Bee Dee M-5-200, Bee Dee M-5-210TC, Bee Dee M-7-235, Bee Dee M-6-235, Bee Dee M-4C, Bee Dee M-5-220C, Bee Dee M-5-235C, Bee Dee M-6-180, Bee Dee M-5-210C, Bee Dee MX-7- 235, Bee Dee M-4, MX-7-160C, Bee Dee M-7 Series, Bee Dee MXT-7- 180, Bee Dee MT-7-235, Bee Dee M-8-235, Bee Dee MX-7-160, Bee Dee MXT-7-160, Bee Dee MX-7-180A, Bee Dee MXT-7-180A, Bee Dee MX-7- 180B, Bee Dee M-7-235B, Bee Dee M-6 Series, Bee Dee MX-7 Series, Bee Dee M-7-235C, Bee Dee M-4 …

    Federal Register Official PDF

  9. AD 2003-04-20 One-time

    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.

    Effective Apr 4, 2003 · Amendment 39-13069 · Replaces AD 2001-17-26

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  10. AD 2001-13-05 One-time

    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.

    Effective Aug 1, 2001 · Amendment 39-12285

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  11. AD 2001-04-10 One-time Engine

    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.

    Effective Apr 6, 2001 · Amendment 39-12129

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  12. AD 2000-22-03 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.

    Effective Dec 4, 2000 · Amendment 39-11949

    Applicability, as the AD words it

    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 accordance with Raytheon Aircraft Repair Design Office instructions; certificated in any category.

    Federal Register Official PDF

  13. AD 2000-02-35 One-time

    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.

    Effective Mar 13, 2000 · Amendment 39-11553

    Applicability, as the AD words it

    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, 403B, 600A, 600B, 700A, and 700B airplanes. BAe.125 series 800A (C-29A) SB 35-3171: September 1998. airplanes. BAe.125 series 800A and 800B SB 35-3034 and SB September 1998. airplanes, and Hawker 800 35-3170. airplanes. BAe.125 series 1000A and 1000B SB 35-3167 and SB September 1998. airplanes, and Hawker 1000 35-3168. airplanes.

    Federal Register Official PDF

  14. AD 2000-01-02 One-time

    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.

    Effective Feb 15, 2000 · Amendment 39-11499

    Applicability, as the AD words it

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

    Federal Register Official PDF

  15. AD 99-25-01 One-time

    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.

    Effective Jan 4, 2000 · Amendment 39-11444

    Applicability, as the AD words it

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

    Federal Register Official PDF

  16. AD 99-24-10 Recurring Appliance

    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.

    Effective Jan 14, 2000 · Amendment 39-11434

    Applicability, as the AD words it

    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 23, A23, A23A, A23-19, 19A, B19, B19A, A23-24, B23, C23, A24, A24R, B24R, C24R, 35, A35, B35, C35, D35, E35, F35, G35, 35R, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35- C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC, 4S (YT-34), A45 (T-34A, B-45), D45(T- 34B), and 77 Series. SA2161NM: Raytheon Beech Model V35B. SA2162NM: Cessna Models 120, 140, 140A, 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, A150L, 150M, 152, A152, A150K, A150M, 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAFT-41A), 172G, 172H (USAFT-41A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 175, 175A, 175B, 175C, P172D, R172E (USAFT-41B, USAFT41- 3, and USAFT-41D), R172F (USAFT-41D and USAFT-41C), R172G (USAFT-41D), R172H (USAFT-41D), R172J, R172K, 172RG, 177, 177A, 177B, 177RG, 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182RG, T182, T182RG, T182R, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 188, 188A, 188B, A188, A188B, T188C, 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D. TP206E, U206-A, U206-B, U206-C, U206-D, U206-E, U206-F, U206G, TU206-A, TU206-B, TU206-C, TU206-D, TU206-E, TU206-F, TU206-G, 207, 207A, T207, T207A, 210, 210A, 210B, 210C, 210D, 210E, 210F, 210-5 (205), 210-5A (205A), T210F, 210G, T-210G, 210H, T-210H, 210J, 205P, T-210J, 210K, T- 210K, T210L, 210L, 210M, T210M, 210N, P210N, T210N, 205T, 210R, P210R, 205U, T210R, 210-5, 210-5A, 305A (USAF 0- 1A), 305C (USAF 0-1E), 305D (USAF 0-1F), 305F, 305B (USAF T0-1D), 305E (0-1D or 0-1F), and 321 (Navy 0E-2). SA2163NM: Cessna Model U206G. SA2164NM: Cessna Model 180Q. SA2166NM: Cessna Model 177. SA2167NM: The New Piper Aircraft, Inc. (Piper) Models L-14, PA-12, PA-12S, PA-14, PA-15, PA-16, PA-16S, PA-17, PA-18, PA- 18A, PA-18S, PA-18-105 (Special), PA-18S-105 (SP), PA-18- 125 (Army L-21A), PA-18AS-125, PA-18S-125, PA-18-135, PA- 18A-135, PA-18AS-135, PA-18S-135, PA-18-150, PA-18A-150, PA-18AS-150, PA-18S-150, PA-19 (Army L-18C), PA-19S, PA- 20, PA-20S, PA-20-115, PA-20S-115, PA-20-135, PA-22, PA- 22-108, PA-22-135, PA-22S-135, PA-22-150, PA-22S-150, PA- 22-160, PA-22S-160, PA-24, PA-24-250, PA-24-260, PA-24- 400, PA-25, PA-25-235, PA-25-260, PA-32-260, PA-32RT-300, PA-32RT-301T, PA-32-300, PA-32RT-300T, PA-32-301, PA-32S- 300, PA-32R-301, PA-32-301T, PA-32R-300, PA-32R-301T, PA- 28-140, PA-28-141, PA-28-150, PA-28-151, PA-28-160, PA- 28S-160, PA-28-180, PA-28R-180, PA-28S-180, PA-28-235, PA- 28S-235, PA-28-181, PA-28-161, PA-28R-200, PA-28R-201, PA- 28R-201T, PA-28-236, PA-28RT-201, PA-28RT-201T, PA-28- 201T, PA-36-285, PA-36-300, PA-36-375, PA-38-112, and PA- 46-310P. SA2168NM: Mooney Models M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20M, and M22. SA2683NM: Aerocar, Inc. Model I, Aerodifusion, S.L. Model Jodel D- 1190S, Aeromere, S.A. Model Falco F.8.L., Aeronautica Macchi S.P.A. Models AL60, AL60-B, AL60-F5, and AL60-C5, Aeronautica Macchi & Aerfer Model AM-3, Aeronca Inc. Models 15AC and S15AC, Aerospatiale Model TB20 Trinidad, Arctic Aircraft Co., Inc. Models S-1A, S-1A-65F, S-1A- 85F, S-1A-90F, S-1B1 (Army L-67 XL-6), and S-1B2, Avions Mudry et Cie Model CAP 10B, American Champion Models (Bellanca, Aeronca) 7AC, 7ACA, S7AC (L-16A), 7BCM (L- 16B), 7CCM, 7DC, S7DC, 7EC, S7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCCA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB, 8KCAB, 8GCBC, 11AC, S11AC, 11BC, S11BC, 11CC, and S11CC, Bellanca Aircraft Corporation, Models 14-9, 14-9L, 14-12F- 3, 14-13, 14-13-2, 14-13-3, 14-13-3W, 14-19, 14-19-2, 14- 19-3A, 17-30, 17-31, 17-31TC, 17-30A, 17-31A, and 17- 31ATC, Biemond, C. Model Teal CB1, Board, G.R. Models Columbia XJL-1 and Bolkow Jr., Clark Aircraft, Inc. Models 12 and 1000, Falcon Aircraft Corporation Model F- 1, Flug und Fahrzeugwerke AG Model AS 202/15 "Brand," Found Brothers Model FBA-2C, Fuji Heavy Industries Models FA-200-160, FA-200-180, and FA-200-180AO, Funk Aircraft Model Funk C, Kearns, Edward Scott (Garcia, Henry S.) Model (Emigh) Trojan A-2, Swift Museum Foundation, Inc. Model (Globe) GC-1A, GC-1B, Goodyear Aircraft Model GA- 22A, Great Lakes Aircraft Model 2T-1A-1 and 2T-1A-2, Grumman American Models G-164, G-164A, G-164B, AA-1, AA- 1A, AA-1B, AA-1C, AA-5, AA-5A, and AA-5B, Commander Aircraft (Gulfstream) Models 112, (112A, 112B, 112TC, 112TCA, 114, and 114A, Helio Enterprises Models H-250, H- 295 (USAF U-10D), H-391 (USAF YL-24), H-395 (SAF L-28A), H-395A, HT-295, and H-700, Prop-Jets, Inc. (Interceptor Corp., Aero Commander, Meyers) Models 200, 200A, 200B, 200C, and 200D, C. Itoh Aircraft Maintenance & Engineering Co. LTD. Model N-62, Jamieson Corporation Model J-2-L1B, Jodel, Avion Models D-140-B, DR-1050, D- 1190, and 150, Lake Models C-1, C-2-IV, LA-4, LA-4-200, and LA-4-250, Luscombe Aircraft Corp. Models 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F, and 11A, Maule Aerospace Technology Corp. Models Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M-4- 180C, M-4-180S, M-4-210, M-4-201C, M-4-210S, M-4-210T, M- 4-220S, M-4-220T, M-5-180C, M-5-200, M-5-210C, M-5-210TC, M-T-220C, M-5-235, M-5-235C, M-6-180, M-6-235, M-7-235, MX-7-180, MX-7-235, Messerschmitt-Bolkow Models BO-209- 150 FV&RV, BO209-160 FV&RV, BO-209, and 150OFF, Nardi S.A. Model FN-333, Jimmie Thompson Enterprise (Navion Rangemaster Aircraft Corporation) Models Navion (L-17A), Navion A (L-17B, L-17C), Navion B, D, E, F, G, and H, White International Ltd. Models (Pitts) S-1S, S-1T, S-2, and S-2A, Procaer S.P.A. Models F 15/B, F 15/C, and F 15/ E, Gulfstream Aerospace Corporation (Rockwell) Models 111, 112, …

    Federal Register Official PDF

  17. AD 99-23-10 One-time

    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.

    Effective Dec 17, 1999 · Amendment 39-11406

    Applicability, as the AD words it

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

    Federal Register Official PDF

  18. AD 89-18-07 One-time

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

    To prevent control surface interference and jamming of flight controls.

    Effective Dec 18, 1998 · Amendment 39-10878

    Applicability, as the AD words it

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

    Federal Register Official PDF

  19. AD 97-26-10

    Raytheon Model Hawker 1000 Series Airplanes

    Effective Jan 23, 1998 · Amendment 39-10253 · Recurring or one-time: see the official AD

    Applicability, as the AD words it

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

    Federal Register Official PDF

  20. AD 97-09-05 One-time

    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.

    Effective May 30, 1997 · Amendment 39-10001

    Applicability, as the AD words it

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

    Federal Register Official PDF

  21. AD 97-03-07 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.

    Effective Mar 11, 1997 · Amendment 39-9913 · Replaces AD 94-26-12

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  22. AD 96-22-03 One-time

    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.

    Effective Dec 11, 1996 · Amendment 39-9792

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  23. AD 96-18-09 One-time

    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.

    Effective Oct 9, 1996 · Amendment 39-9733

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  24. AD 96-17-13 One-time

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

    To prevent reduced structural integrity of the elevator control circuit.

    Effective Sep 30, 1996 · Amendment 39-9723

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  25. AD 96-17-09 One-time

    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.

    Effective Sep 24, 1996 · Amendment 39-9718 · Replaces AD 95-10-01

    Applicability, as the AD words it

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

    Federal Register Official PDF

  26. AD 96-12-17 One-time

    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.

    Effective Jul 15, 1996 · Amendment 39-9660

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  27. AD 96-11-17 One-time

    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.

    Effective Jul 9, 1996 · Amendment 39-9641

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  28. AD 96-07-11

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

    Effective May 6, 1996 · Amendment 39-9560 · Recurring or one-time: see the official AD

    Applicability, as the AD words it

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

    Federal Register Official PDF

  29. AD 95-21-17 One-time

    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.

    Effective Nov 17, 1995 · Amendment 39-9404

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  30. AD 95-15-04 One-time

    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.

    Effective Aug 23, 1995 · Amendment 39-9307

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

  31. AD 94-01-04 One-time

    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.

    Effective Feb 4, 1994 · Amendment 39-8786

    Applicability, as the AD words it

    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 -200; 737-100, -200, -300, and -400; 747- 100, -200, -300, -400 and 747SP; 757-200 and -500; and 767-200 and - 300 series airplanes; Cessna Citation Model C550 and C560 series airplanes, and Cessna Citation III and VII series airplanes; Canadair Challenger Model CL-600-2B16 and -2A12 series airplanes; British Aerospace Model 125-800A; Gulfstream Model GII, GIIB, GIII, and GIV series airplanes; Lockheed Model L-1011 series airplanes; McDonnell Douglas Model DC-9-10, -20, -30-, -40, and -50; DC-10-10, -15, -30, and -40; MD-11; and DC-9-80 series airplanes; and Model MD-88 airplanes; Dassault Aviation Model Mystere-Falcon 50 and 900 series airplanes; Short Brothers Model SD3-60 series airplanes; de Havilland Model DHC-8-100 and DHC-7 series airplanes; Fokker Model F27 series airplanes; and Corporate Jets Limited Model BAe 125-800A and BAe 125-1000A series airplanes.

    Federal Register Official PDF

6 superseded or removed ADs
  1. AD 2007-07-12 Superseded by AD 2009-08-01

    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.

    Effective Apr 18, 2007 · Amendment 39-15009

    Applicability, as the AD words it

    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 identified in Table 1 of this AD. Table 1.--Known Affected Airplanes Manufacturer Model Bombardier, Inc: CL-600-2B16 (CL-601-3A, CL-601- 3R, and CL-604) airplanes. Dassault Aviation: Mystere-Falcon 900 airplanes. Gulfstream Aerospace Corporation: G-1159A, G-IV, and GV airplanes. Lockheed: 382G series airplanes. Raytheon Aircraft Company: BAe.125 Series 800A (including C-29A and U-125) airplanes. Hawker 800XP and 1000 airplanes.

    Federal Register Official PDF

  2. AD 2006-22-05 Superseded by AD 2010-07-02

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

    Effective Dec 1, 2006 · Amendment 39-14802 · Replaces AD 2003-04-06

    Applicability, as the AD words it

    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-700- 1A10 series airplanes; Model Bombardier CL-215-6B11 (CL-415 variant) series airplanes; Cessna Model 560, 560XL, and 650 airplanes; Dassault Model Mystere-Falcon 50 series airplanes; AvCraft Dornier Model 328-100 and -300 series airplanes; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 airplanes and Model EMB- 145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes; Learjet Model 45 airplanes; Raytheon Model Hawker 800XP and Hawker 1000 airplanes; and Sikorsky Model S-76A, S-76B, and S-76C aircraft. Table 1.--INU Part Numbers Part Nos. 7510100-811 through 7510100-814 inclusive. 7510100-831 through 7510100-834 inclusive. 7510100-901 through 7510100-904 inclusive. 7510100-911 through 7510100-914 inclusive. 7510100-921 through 7510100-924 inclusive. 7510100-931 through 7510100-934 inclusive.

    Federal Register Official PDF

  3. AD 2003-04-06 Superseded by AD 2006-22-05

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

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

    Effective Mar 11, 2003 · Amendment 39-13054

    Applicability, as the AD words it

    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 CL-215-6B11 (CL415 variant) series airplanes; Cessna Model 560, 560XL, and 650 airplanes; Dassault Model Mystere-Falcon 50 series airplanes; Dornier Model 328-100 and -300 series airplanes; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 series airplanes; Learjet Model 45 airplanes; Raytheon Model Hawker 800XP and Hawker 1000 airplanes; and Sikorsky Model S-76A, S-76B, and S-76C aircraft. Table 1 of this AD follows: Table 1.--Integrated Navigation Unit Part Numbers Part numbers 7510100-811 through 7510100-814 inclusive 7510100-831 through 7510100-834 inclusive 7510100-901 through 7510100-904 inclusive 7510100-911 through 7510100-914 inclusive 7510100-921 through 7510100-924 inclusive 7510100-931 through 7510100-934 inclusive

    Federal Register Official PDF

  4. AD 2001-17-26 Superseded by AD 2003-04-20

    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.

    Effective Oct 3, 2001 · Amendment 39-12417 · Corrected Jan 29, 2002

    Applicability, as the AD words it

    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.

    Federal Register Official PDF Correction (Jan 29, 2002)

  5. AD 95-10-01 Superseded by AD 96-17-09

    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.

    Effective May 23, 1995 · Amendment 39-9218

    Applicability, as the AD words it

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

    Federal Register Official PDF

  6. AD 94-26-12 Superseded by AD 97-03-07

    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.

    Effective Feb 3, 1995 · Amendment 39-9107

    Applicability, as the AD words it

    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.

    Federal Register Official PDF

Track these ADs for your Hawker 1000 / BAe125 Series1000 (certified family) in Radar

Radar reads the aircraft’s logbooks and ties each AD to the entries that show how and when it was complied with, with recurring ADs due by date and hours.

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QUESTIONS

Hawker 1000 / BAe125 Series1000 (certified family) AD questions

Source: FAA final rules under 14 CFR part 39, from the Federal Register. The FAA’s Dynamic Regulatory System holds the official list.

How many airworthiness directives apply to the Hawker 1000 / BAe125 Series1000 (certified family)?

37 FAA ADs published since 1995 name the Hawker 1000 / BAe125 Series1000 (certified family)'s type certificate models (BAE 125 SERIES 1000A, BAE 125-1000A and HAWKER 1000) in their applicability. 31 are still in effect as far as the Federal Register shows; the others were superseded by a later AD or removed. How many apply to one aircraft depends on its serial number, equipment and modifications.

Which Hawker 1000 / BAe125 Series1000 (certified family) ADs are recurring?

3 of the ADs in effect require actions that repeat, such as inspections at set intervals, until a terminating action is done. They are marked Recurring above. One-time ADs are complied with once, but the compliance record stays with the aircraft.

What is the latest Hawker 1000 / BAe125 Series1000 (certified family) airworthiness directive?

AD 2016-13-13, effective Aug 12, 2016: Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) Airplanes. The list is refreshed from the Federal Register every weekday.

How do I know whether an AD applies to my Hawker 1000 / BAe125 Series1000 (certified family)?

Read the AD's applicability paragraph, shown with each AD on this page, against the aircraft's serial number and its installed engines, propellers, parts and modifications. A certificated mechanic or inspector makes the determination and records the method of compliance in the maintenance records. The FAA's Dynamic Regulatory System holds the official list of ADs.

Why are engine and propeller ADs missing?

This page lists ADs whose applicability names the Hawker 1000 / BAe125 Series1000 (certified family) airframe, plus appliance ADs that list it among the aircraft they can be installed on. Engine and propeller ADs name the engine or propeller model rather than the aircraft, so check them by the installed engine and propeller models.

Every AD on your Hawker 1000 / BAe125 Series1000 (certified family), tied to the logbook entry that closed it.

Radar reads every logbook page, typed or handwritten, and builds one searchable record per tail: times, inspections, ADs and components, each tied to the page it came from.

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