Airworthiness Directive Lookup Free FAA AD search by N-number, make or model
Find the FAA airworthiness directives that may apply to an aircraft: 12,857 ADs from the Federal Register since 1995, through Oct 1, 2026, each with its applicability text and the official document. Free, no account.
N119U is a 1992 Hawker 1000 / BAe125 Series1000 (certified family) in the FAA registry (aircraft page). Matched on type certificate model BAE 125 SERIES 1000A, BAE 125-1000A, HAWKER 1000.
RESULTS
31 ADs in effect may apply to N119U
- In effect31
- Recurring3
- Superseded or removed6
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.
Also show 6 superseded or removed N119U’s registration record
- 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.
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.
- 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.
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.
- AD 2010-07-02 One-time
Various Aircraft Equipped With Honeywell Primus II RNZ-850( )/-851( ) Integrated Navigation Units
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.
- 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.
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.
- 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.
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.
- 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.
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.
- 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.
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.
- AD 2005-11-05 One-time Appliance
Precise Flight, Inc. Models SVS I and SVS IA Standby Vacuum Systems
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 …
- 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.
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.
- 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.
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.
- 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.
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.
- 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.
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.
- 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.
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.
- 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.
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.
- 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.
Applicability, as the AD words it
All Model BAe.125 series 1000A and 1000B, and Model Hawker 1000 series airplanes; certificated in any category.
- 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.
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, …
- 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.
Applicability, as the AD words it
Model Hawker 1000 series airplanes, serial numbers 258151, 258159, and 259003 through 259052 inclusive, certificated in any category.
- 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.
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.
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Raytheon Model Hawker 1000 Series Airplanes
Applicability, as the AD words it
Model Hawker 1000 series airplanes; serial numbers 258151, 258159, and 259003 through 259052 inclusive; certificated in any category.
- 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.
Applicability, as the AD words it
All Model BAe 125-1000A and Model Hawker 1000 series airplanes, certificated in any category.
- 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.
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.
- 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.
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.
- 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.
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.
- 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.
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.
- 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.
Applicability, as the AD words it
Model Hawker 1000 and BAe 125-1000A series airplanes, post modification 259722C; certificated in any category.
- 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.
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.
- 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.
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.
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Beech Model BAe 125-1000A and Hawker 1000 Series Airplanes
Applicability, as the AD words it
All Model BAe 125-1000A and Hawker 1000 series airplanes, certificated in any category.
- 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.
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.
- 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.
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.
- 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.
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.
Radar reads the 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.
QUESTIONS
AD lookup questions
Sources: FAA final rules under 14 CFR part 39, from the Federal Register; make and model from the FAA aircraft registry. The FAA’s Dynamic Regulatory System holds the official AD list.
What is an airworthiness directive (AD)?
An airworthiness directive is a legally enforceable rule the FAA issues under 14 CFR part 39 when it finds an unsafe condition in an aircraft, engine, propeller or appliance that is likely to exist in others of the same design. It says which products it applies to and what must be done, and by when: an inspection, a part replacement, a modification or a limitation. No one may operate a product to which an AD applies except in accordance with it.
How do I look up the ADs for my aircraft?
Type the N-number, or the make and model, into the box above. Radar finds the aircraft's make and model in the FAA registry and lists every AD published in the Federal Register whose applicability names it, newest first, with the AD's own applicability text and a link to the official document. The FAA's Dynamic Regulatory System (drs.faa.gov) holds the official list.
Does every AD in the results apply to my aircraft?
Not necessarily. An AD can be limited to serial number ranges, to aircraft with certain parts or modifications installed, or to a configuration. The results are ADs that may apply because they name the make and model. A certificated mechanic or inspector determines applicability against the aircraft's serial number and records, and records how each applicable AD was complied with.
What is the difference between a recurring and a one-time AD?
A one-time AD is complied with once, for example by replacing a part. A recurring (repetitive) AD requires an action again at an interval, such as an inspection every 100 hours or every 12 months, until a terminating action ends it. Radar marks an AD Recurring when its text requires repetitive actions; always read the AD for the intervals.
What does superseded mean?
When the FAA replaces an AD with a new one, the old AD is superseded: its requirements are carried into, or replaced by, the new AD. Results show the ADs in effect by default; superseded and removed ADs can be shown for the history.
Where does this data come from?
The Federal Register, where the FAA publishes every AD as a final rule. Radar reads each one from the Federal Register API (12,857 ADs since 1995) and refreshes the list every weekday. Make and model come from the FAA aircraft registry. ADs issued before 1995 are not in the Federal Register's online edition and are not included.
Are engine and propeller ADs included?
Only when their applicability names the aircraft. Most engine and propeller ADs name the engine or propeller model, so check those by the installed engine and propeller models. Appliance ADs that list the aircraft among those the appliance can be installed on are included and marked Appliance.
Know which ADs apply, and where each one was signed off.
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.