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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.

N1293E is a 1996 Cessna 208B Grand Caravan in the FAA registry (aircraft page). Matched on type certificate model 208B.

RESULTS

16 ADs in effect may apply to N1293E

  • In effect16
  • Recurring3
  • Superseded or removed3

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.

Show only ADs in effect N1293E’s registration record

  1. AD 2021-04-10 Recurring

    Textron Aviation, Inc. Airplanes

    This AD was prompted by reports of loose elevator torque tube attach fasteners.

    Effective Apr 12, 2021 · Amendment 39-21431

    Applicability, as the AD words it

    This AD applies to Textron Aviation Inc. (Textron) (type certificate previously held by Cessna Aircraft Company) Model 208 airplanes, serial numbers 20800564 through 20800594 and 20800603 through 20800605; and Model 208B airplanes, serial numbers 208B5141 through 208B5285, 208B5287 through 208B5305, 208B5307 through 208B5312, 208B5314, 208B5316 through 208B5344, 208B5346 through 208B5350, 208B5353, 208B5354, 208B5356 through 208B5359, 208B5362 through 208B5366, 208B5401, 208B5403, 208B5404, and 208B5408; certificated in any category.

  2. AD 2009-15-05 One-time

    Cessna Aircraft Company Models 208 and 208B Airplanes

    We are issuing this AD to detect and correct loose bridle cable clamps, which could result in the swaged ball unseating from the recess in the servo drum and contacting the cable guard pin.

    Effective Jul 27, 2009 · Amendment 39-15968

    Applicability, as the AD words it

    This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial No. 208: 20800500 through 20800504. 208B: 208B1216, 208B2001, 208B2003 through 208B2023, 208B2025 through 208B2029, 208B2031 through 208B2037, 208B2040, 208B2042, and 208B2043.

  3. AD 2009-10-14 One-time Propeller

    Hartzell Propeller Inc. Steel Hub Turbine Propellers

    We are issuing this AD to prevent separation of the propeller blade counterweight slug, which could lead to injury and damage to the airplane.

    Effective Jun 4, 2009 · Amendment 39-15910

    Applicability, as the AD words it

    This AD applies to the Hartzell Propeller Inc. steel hub turbine propellers listed in Table 1 of this AD, with any counterweight slug attachment bolts, part number (P/N) B-3386-14H, LFC manufacturing lot 224, installed. These propellers are installed on, but not limited to, the airplanes listed in Table 1 of this AD. Table 1--Propeller Models Applicability Airplane Propeller model manufacturer Airplane model HC-B3TN-5K: AERO COMMANDER: 680T, 680V, 681. HC-B3TN-5DL, -5FL, -5NL: AERO COMMANDER: 690(A, B, C), 695A. HC-A3MVF-7B: AEROSPACE N22B, N24A, N22S, TECHNOLOGIES. N22C. HC-A3VF-7, -7B: AEROSPACE N22B, N24A, N22S, TECHNOLOGIES. N22C. HC-B5MP-3A, -3C: AIR TRACTOR: AT-502A. HC-B5MP-3C: AIR TRACTOR: AT-503, 602. HC-B5MA-3D(T): AIR TRACTOR: AT-802. HC-B5MP-3F: AIR TRACTOR: AT-802. HC-B5MA-5A: ANTONOV: AN-38. HC-B3TN-5V: AYRES: S-2R. HC-B4TN-5NL, -5PL: AYRES: S-2R(-1340), -G(5, 6, 10), -R3S, - R1820, -T(6, 11, 15, 34, 45, 65). HC-B5MP-3C: AYRES: S-2R(HG)-T65. HC-B3TN-3AE: AYRES: S-2R-T( ). HC-B3TN-5K: BAE (JETSTREAM): 137. HC-B4MP-3A: BEECH: 1900C. HC-B4MP-3B: BEECH: 300, 300LW. HC-B3TF-7A: BEECH: A36, A36TC. HC-B4MP-3C: BEECH: B300, B300C. HC-B4MN-5AL: CASA: C-212-CC, -CF. HC-B3TF-7A: CESSNA: 206. HC-B3TF-7: CESSNA: 402. HC-B3MN-3: CESSNA: 208, 208A, 208B. HC-B3TN-3AEY, -3AF: CESSNA: 208, 208A, 208B. HC-B3TF-7A: CESSNA: P210N. HC-B3TN-3AEY: DE HAVILLAND CANADA. DHC-3. HC-B4TN-5NL: DE HAVILLAND CANADA. DHC-3. HC-B5MA-3M: DE HAVILLAND CANADA. DHC-4. HC-B4TN-5ML: DORNIER: DO228-100, -101, - 200, -201, -202, - 212. HC-B4TN-5L: DORNIER: DO228-200, -201, - 202, -212. HC-B5MA-3(J, M, C): DOUGLAS: DC-3C. HC-B5MA-2: EMBRAER: EMB-314. HC-B4TN-5EL, -5HL, -5KL: FAIRCHILD AIRCRAFT.. SA-226T(B). HC-B3TF-7, -7A: FLUG & FAHRZEUGWERKE AS202/32TP. AG. HC-B3TF-7A: FUJI: KM-2D (T-5). HC-B5MP-5: GRUMMAN: S-2. HC-B5MA-5H: GRUMMAN: S-2F3AT. HC-3BTF-7A: MAULE: M-7-420, MX(T)-7- 420. HC-B4TN-5DL, -5GL, -5JL: MITSUBISHI: MU-2B-25A, -26A, - 30, -35A, -36A, -40 (MU-2P), -60 (MU- 2N). HC-B5MP-3(A): NORD: 262 FRAKES. HC-B5MP-3C: NORMAN AEROPLANE: NAC 6-65. HC-B5MP-3D: POLISH AVIATION M-28, -28B. (MIELEC). HC-B5MP-3G: POLISH AVIATION M-28B. (MIELEC). HC-B3TN-5U: PZL MIELEC: M18. HC-B4TN-5NL: PZL MIELEC: M18. HC-B5MP-5BL: PZL MIELEC: M18. HC-B5MP-3C: PZL MIELEC: M18, M18A, M18B. HC-B4MN-5B: ROCKWELL: OV-10 (LEFT SIDE). HC-B4MN-5BL: ROCKWELL: OV-10 (RIGHT SIDE). HC-B5MP-3A: SHORT BROTHERS: SD3-30. HC-B5MP-3C: SHORT BROTHERS: SD3-60-200, SD3- SHERPA-200. HC-B3TF-7A: SIAI MARCHETTI F.260C, D. (AERMACCHI). HC-B3TF-7A: SIAI MARCHETTI SM-1019. (AERMACCHI). HC-B3TF-7A: SIAI MARCHETTI SF600 CANGURO. (VULCANAIR). HC-B5MP-3(F): THRUSH AIRCRAFT: S-2R-T660. HC-B3TN-5FL, -5NL: TWIN COMMANDER: 690A, 690B, 690C. HC-B3TF-7A: VALMET: L-90TP. HC-B3TF-7A: VULCANAIR AP68TP-300, -600. (PARTENAVIA).

  4. AD 2009-05-12 One-time

    Cessna Aircraft Company Models 208 and 208B Airplanes

    We are issuing this AD to prevent the cable attach fitting on the aileron upper quadrant assembly from rotating and possibly contacting or interfering with the aileron lower quadrant assembly, which could result in limited roll control and reduced handling capabilities.

    Effective Apr 15, 2009 · Amendment 39-15836

    Applicability, as the AD words it

    This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. 208: 20800001 through 20800415 and 20800417 through 20800419. 208B: 208B0001 through 208B1081, 208B1083 through 208B1215, 208B1217 through 208B1257, 208B1259 through 208B1305, 208B1307, and 208B1309 through 208B1310.

  5. AD 2008-13-06 One-time

    Cessna Aircraft Company Models 208 and 208B Airplanes

    We are issuing this AD to detect and correct damaged wiring of the auto-control wing de-ice system, fuel quantity indication, and low fuel annunciation systems.

    Effective Jul 30, 2008 · Amendment 39-15569

    Applicability, as the AD words it

    This AD applies to the following airplane models and serial numbers that are certificated in any category: Models Serial Nos. 208: 20800001 through 20800415. 208B: 208B0001 through 208B1299.

  6. AD 2006-16-18 One-time

    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.

    Effective Jul 18, 2008 · Amendment 39-15557

    Applicability, as the AD words it

    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 on various small and transport category airplanes, certificated in any category, including, but not limited, to the airplane models listed in Table 1 of this AD. Table 1.--Manufacturers/Airplane Models Manufacturer Airplane model(s) Airbus: A300. Avions Marcel Dassault-Breguet Aviation (AMD/BA).. Falcon 10. Boeing: 727, 737, 747. Bombardier (LearJet): 24, 35, 36, 55. British Aerospace (Operations) Limited: Jetstream Series 3101. Cessna: 208, 208B, 421C; 501, 525, 550, 560, 650, S550. Embraer: EMB-120. Dassault-Aviation: Mystere-Falcon 50, Mystere-Falcon 200. Gulfstream: G-I, G-1159A (G-III) Israel Aircraft Industries (IAI): 1124, 1125 Westwind Astra. McDonnell Douglas: DC-10. Piper: PA-31T2. Raytheon: 58; 1900D, 400; A36; BAe.125 Series 800A; HS.125 Series 600A/700A; Hawker 800-XP; 200, 300, 350; A200, B100, B200, B300, C90, C90A, C90B, E90, F90; MU-300-10. Sabreliner: 60 (NA-265-60). Twin Commander: 500-A, 695A. Viking Air Limited: DHC-6.

  7. AD 2007-10-15 One-time

    Cessna Aircraft Company Models 208 and 208B Airplanes

    Effective Jun 21, 2007 · Amendment 39-15056 · Replaces AD 2006-06-06

    Applicability, as the AD words it

    This AD applies to Models 208 and 208B, all serial numbers, that are certificated in any category.

  8. AD 2006-06-06 Superseded by AD 2007-10-15

    The Cessna Aircraft Company Models 208 and 208B Airplanes

    Effective Mar 24, 2006 · Amendment 39-14514 · Replaces AD 2005-07-01 · Corrected Apr 5, 2006

    Applicability, as the AD words it

    This AD affects Models 208 and 208B, all serial numbers, that are certificated in any category.

  9. AD 2006-01-11 One-time

    The Cessna Aircraft Company Models 208 and 208B Airplanes

    Effective Feb 22, 2006 · Amendment 39-14450 · Corrected Mar 16, 2006

    Applicability, as the AD words it

    This AD affects Models 208 and 208B, all serial numbers, that are certificated in any category.

  10. AD 2005-14-12 Recurring Propeller

    Hartzell Propeller Inc. Models HC-B3TN-2, HC-B3TN-3, HC-B3TN-5, HC-B3MN-3, HC-B4TN-3, HC-B4TN-5, HC-B4MN-5, HC-B4MP-3, HC-B4MP-5, and HC-B5MP-3 Propellers

    We are issuing this AD to prevent propeller mounting bolt failures or improperly secured propellers, which could lead to separation of the propeller from the airplane.

    Effective Jul 29, 2005 · Amendment 39-14189

    Applicability, as the AD words it

    This AD applies to Hartzell Propeller Inc. models HC-B3TN-2, HC-B3TN-3, HC-B3TN-5, HC-B3MN-3, HC-B4TN-3, HC-B4TN-5, HC-B4MN-5, HC-B4MP-3, HC-B4MP-5, and HC-B5MP-3 propellers installed with propeller mounting bolts, part number (P/N) B-3339. These propellers are installed on, but not limited to, the airplanes listed in the following Table 1: Table 1.--Airplanes That Propellers Are Installed on, But Not Limited To ADVANCED AERO & STRUCTURES, INC. 450. AEROCOMMANDER: 680T, 680V, 681, 690, 690A, 690B, 690C, 695, 695A. AEROSPATIALE (SOCATA): TB-31 (Non U.S. type certificated (TC'd) product). AIR TRACTOR: AT-300, AT-301, AT-302, AT-400, AT-401, AT-402, AT-402A, AT-402B, AT- 501, AT-502, AT-502A, AT-502B, AT-503, AT-503A, AT-602, AT-802. AMERICAN AVIATION (GRUMMAN): G-164, G-164B, G-164B-15T, G-164B-34T, G-164D. AYRES: S-2R, S-2R-R1340, S-2R-R3S, S-2R-G1, S-2R-G5, S-2R-G6, S-2R-G10, S- 2R-T6, S-2R-T11, S-2R-T15, S-2R-T34, S-2R-T-45, S-2R-T65, S-2RHG- T65. BAE 137. BEECH (Raytheon): (D, E)18 (C, S), (T, C)45(G, H, J), and E18S-9700 (with turbine conversions), 100, A100, A100A, B100, 1900C, 200(T), 200C(T), B200(T), B200C(T), 300, 300LW, B300, 65-90, -A90, -A90-1, -A90-2, - A90-4, B90, C90, C90A, E90, F90, H90, 99, 99A, A99, A99A, B99, C99, A36 and A36TC (with turbine conversions), 34C, T34C, T34C-1. CASA: C-212-CB, C-212-CC, C-212-CF-CF. CESSNA: 208, 208A, 208B, 402, 421B, 421C, 425, 441, P210N (with turbine conversions). DE HAVILLAND DH114. DE HAVILLAND CANADA: DHC-2, DHC-2 MKIII, DHC-3, DH6-1, DHC-6-100, DHC-6-200, DHC-6-300. DORNIER: 128-6, DO228-100, -101, -200, -201, -202, -212. DOUGLAS DC-3C (with turbine conversions). EMBRAER: EMB-110-P1, -P2, EMB-111, EMB-121A1, EMB-312 (Non U.S. TC'd product). ENAER T-35-TX (Non U.S. TC'd product). FAIRCHILD AIRCRAFT: SA226-AT, -T, -TB, -TC. FAIRCHILD-HILLER (PILATUS) AU-23 (Non U.S. TC'd product). FLUG & FAHRZEUGWERKE AG AS202/32TP (Non U.S. TC'd product). FUJI KM-2D (T-5) (Non U.S. TC'd product). GRUMMAN S-2 (with turbine conversions). GRUMMAN (GULFSTREAM AERO) G73 (with turbine conversions). GRUMMAN (MCKINNON) G21E, G (with turbine conversions). HAFEI AVIATION INDUSTRY CO. Y12, Y12IV (Non U.S. TC'd product). HELIO: HST-550, -550A. ICA (ROMANIA) IAR-825TP (Non U.S. TC'd product). ISRAEL AIRCRAFT INDUSTRIES: 101, 101B. KOREAN AEROSPACE INDUSTRIES KTX-IT (Non U.S. TC'd product). MAULE: M-7-420, MX (T)-7-420. MITSUBISHI: MU-2B, MU-2B-10, -15, -20, -25, -26, -30, -35, -36, -40, -60, MU-2B- 25A, -26A, -35A, -36A. NORD 262 (FRAKES), and (NORD) Model 262(A) modified by Supplemental Type Certificate (STC) SA2369SW. NORMAN AEROPLANE: NA 6, NAC 6-65 (Non U.S. TC'd product). POLISH AVIATION (MIELEC): M-28, M-28B. PACIFIC AEROSPACE FU24(A)-950/-954. PACIFIC AEROSPACE (FLETCHER): FU-24 CRESCO 08-600, FU-24 CRESCO 08-750XL. PIAGGIO P-166 DL3. PILATUS: PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, PC-6/C1-H2, PC-7. PIPER: PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, PA-42, PA-42-720, PA-42-- 720R. PROP JETS INC. 400 (Non U.S. TC'd product). PZL MIELEC: M18, M18A, M18B, M27, PZL-106BT, PZL-130TE. ROCKWELL OV-10. SCHWEIZER (GRUMMAN) G-164, G-164A and G-164B (with turbine conversions). SHORT BROTHERS: SC7 SERIES 3, SD3-30 VARIANT 200, SD3-SHERPA VARIANT 200, SD3-60 VARIANT 200, SD3-60 SHERPA VARIANT 200. SIAI MARCHETTI (AERMACCHI): F.260C, F.260D, SM-1019, SF600 CANGURO. VALMET L-90TP (Non U.S. TC'd product). VULCANAIR (PARTENAVIA): AP68TP-300, AP68TP-600. WALLAROO 605 (Non U.S. TC'd product). WEATHERLY 620TP.

  11. AD 2005-01-19 One-time Appliance

    GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

    Effective Feb 23, 2005 · Amendment 39-13944 · Replaces AD 2004-10-15

    Applicability, as the AD words it

    This AD affects GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S transponders that include software versions 3.00, 3.01, 3.02, 3.04, or 3.05 that are installed on, but not limited to, the following airplanes, certificated in any category: Manufacturer Model (1) Aermacchi S.p.A: S.205-18/F, S.205-18/R, S.205-20/R, S.205- 22/R, S208, S.208A, F.260, F.260B, F.260C, F.260D, F.260E, F.260F, S.211A. (2) Aeronautica Macchi S.p.A. AL 60, AL 60-B, AL 60-F5, AL 60-C5, AM-3. (3) Aerostar Aircraft PA-60-600 (Aerostar 600), PA-60-601 Corporation. (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), PA-60- 700P (Aerostar 700P), 360, 400. (4) Alexandria Aircraft, LLC. 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-31, 17-31TC, 17-30A, 17-31A, 17-31ATC (5) Alliance Aircraft Group 15A, 20, H-250, H-295 (USAFU-10D), HT- LLC. 295, H391 (USAFYL-24), H391B, H-395 (USAFL-28A or U-10B), H-395A, H-700, H- 800, HST-550, HST-550A (USAF AU-24A), 500. (6) American Champion 402, 7GCA, 7GCB, 7KC, 7GCBA, 7GCAA, Aircraft Corp. 7GCBC, 7KCAB, 8KCAB, 8GCBC. (7) Sky International Inc: A-1, A-1A, A-1B, S-1S, S-1T, S-2, S-2A, S- 2S, S-2C. (8) B-N Group Ltd: BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-8, BN-2A-20, BN-2A-21, BN- 2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN- 2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN- 2B-26, BN-2B-27, BN-2T, BN-2T-4R, BN-2A MK.III, BN2A MK. III-2, BN2A MK. 111-3. (9) Bellanca: 14-13, 14-13-2, 14-13-3, 14-13-3W. (10) Bombardier Inc: (Otter) DHC-3, DHC-6-1, DHC-6-100, DHC-6- 200, DHC-6-300. (11) Cessna Aircraft Company. 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T041A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, 172RG, P172D, R172E (USAF T-41 B) (USAF T-41 C AND D), R172F (USAF T-41 D), R175G, R172H (USAF T-41 D), R172J, R172K, 175, 175A, 175B, 175C, 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, 182S, 182T, R182, T182, TR182, T182T, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 190, (LC-126A, B, C) 195, 195A, 195B, 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, P210N, T210N, 210R, P210R, T210R, 210-5 (205), 210-5A (205A), 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H, 207, 207A, T207, T207A, 208, 208A, 208B, 310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 320, 320A, 320B, 320C, 320D, 320E, 320F, 320-1, 335, 340, 340A, 336, 337, 337A (USAF 02B), 337B, T337B, 337C, 337E, T337E, T337C, 337D, T337D, M337B (USAF 02A), 337F, T337F, T337G, 337G, 337H, P337H, T337H, T337H-SP, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, 404, 406, 441. (12) Cirrus Design SR20, SR22. Corporation. (13) Commander Aircraft 112, 112TC, 112B, 112TCA, 114, 114A, Company. 114B, 114TC. (14) de Havilland Inc: DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III. (15) Dynac Aerospace (Volaire) 10, (Volaire) 10A, (Aero Corporation. Commander) 100, (Aero Commander) 100A, (Aero Commander) 100-180. (16) Diamond Aircraft DA 20-A1, DA20-C1, DA 40. Industries. (17) Empressa Brasileira de EMB-110P1, EMB-110P2. Aeronautica S.A. EMBRAER. (18) Extra Flugzeugbau Gmbh.. EA300, EA300L, EA300S, EA300/200, EA-400. (19) Fairchild Aircraft SA26-T, SA26-AT, SA226-T, SA226-AT, SA226- Corporation. T(B), SA227-AT, SA227-TT, SA226-TC, SA227-AC (C-26A), SA227-CC, SA227-DC (C- 26B). (20) Global Amphibians, LLC.. Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, Lake Model 250. (21) Grob-Werke: G115, G115A, G115B, G115C, G115C2, G115D, G115D2, G115EG, G120A. (22) Lancair Company: LC40-550FG. (23) LanShe Aerospace, LLC... MAC-125C, MAC-145, MAC-145A, MAC-145B. (24) Learjet Inc: 23. (25) Lockheed Aircraft 18. Corporation. (26) Luscombe Aircraft 11A, 11E. Corporation. (27) Maule Aerospace Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M- Technology, Inc. 4180C, M-4-180S, M-4-180T, M-4-210, M-4- 210C, M-4-210S, M-4-210T, M-4-220, M-4- 220S, M-4-220T, M-5-180C, M-5-200, M-5- 210C, M-5-210TC, M-5-220C, M-5-235C, M-6- 180, M-6-235, M-7-235, MX-7-235, MX-7- 180, MX-7-420, MXT-7-180, MT-7-235, M-8- 235, MX-7-160, MXT-7-160, MX-7-180A, MXT- 7-180A, MX-7-180B, M-7-235B, M-7-235A, M- 7-235C, MX-7-180C, M-7-260, MT-7-260, M- 7-260C, M-7-420AC, MX-7-160C, MX-7- 180AC, M-7-420A, MT-7-420. (28) Mitsubishi Heavy MU-2B-25, MU-2B-35, MU-2B-26, MU-2B-36, Industries, Ltd. MU-2B-26A, MU-2B-36A, MU-2B-40, MU-2B- 60, MU-2B, MU-2B-20, MU-2B-15. (29) Mooney Airplane Company, M20, M20A, M20B, M20C, M20D, M20E, M20F, Inc. M20G, M20J, M20K, M20L, M20M, M20R, M20S, M22. (30) Moravan a.s: Z-242L, Z-143L. (31) Navion Aircraft Company, NAVION, Navion (L-17A), Navion (L17B), Ltd. Navion (L-17C), Navion B, Navion D, Navion E, Navion F, Navion G, Navion H. (32) New Piper Aircraft, Inc. PA-12, PA-12S, PA-18, PA-18S, PA-18 "105" (Special), PA-18S "105" (Special), PA-18A, PA-18 "125" (Army L- 21A), PA-18S "125," PA-18AS "125," PA-18 "135" (Army L-21B), PA-18A "135," PA-18S "135," PA-18 "150," PA-18A "150," PA-18S "150," PA-18AS "150," PA-19 (Army L-18B), PA-19S, PA- 20, PA-20S, PA-20 "115," PA-20S "115," PA-20 "135," PA-20S "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-23, PA-23-160, PA-23-235, PA-23- 250, PA-E23-250, PA-24, PA-24-250, PA-24- 260, PA-24-400, PA-28-140, PA-28-150, PA- 28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-235, PA-28S-160, PA-28R-180, PA- 28S-180, PA-28-181, PA-28R-200, PA-28R- 201, PA-28R-201T, PA-28RT-201, PA-28RT- 201T, PA-28-201T, PA-28-236, PA-30, PA- 39, PA-40, PA-31P, PA-31T, PA-31T1, PA- 31T2, PA-31T3, PA-31P-350, PA-32-260, PA- 32-300, PA-32S-300, …

  12. AD 2004-17-01 Recurring

    Cessna Aircraft Company Models 208 and 208B Airplanes

    Effective Sep 26, 2004 · Amendment 39-13772 · Replaces AD 2002-22-17

    Applicability, as the AD words it

    This AD affects the following airplane models and serial numbers that are certificated in any category: (1) Group 1 (retains the actions from AD 2003-21-04, and adds all flap bellcranks to the applicability): Model Serial Nos. 208: 20800001 through 20800369. 208B: 208B0001 through 208B1014, 208B1017, 208B1018, 208B1020 through 208B1024, 208B1026, and 208B1029 through 208B1033. (2) Group 2 (retains the requirement of AD 2002-22-17 that you repetitively inspect the inboard forward flap bellcranks for cracks, eventually replace these bellcranks, and provides the option of installing the new design flap bellcrank to increase the life limits and terminate the repetitive inspections): Models 208 and 208B airplanes, all serial numbers.

  13. AD 2004-10-15 Superseded by AD 2005-01-19 Appliance

    GARMIN International Inc. GTX 330 Mode S Transponders and GTX 330D Diversity Mode S Transponders

    Effective Jul 9, 2004 · Amendment 39-13645

    Applicability, as the AD words it

    This AD affects GARMIN International Inc. GTX 330/330D Mode S transponders that are installed on, but not limited to, the following airplanes, certificated in any category: Manufacturer Model (1) Aermacchi S.p.A: S.205-18/F, S.205-18/R, S.205-20/R, S.205- 22/R, S.208, S.208A, F.260, F.260B, F.260C, F.260D, F.260E, F.260F, S.211A. (2) Aeronautica Macchi S.p.A. AL 60, AL 60-B, AL 60-F5, AL 60-C5, AM-3. (3) Aerostar Aircraft PA-60-600 (Aerostar 600), PA-60-601 Corporation. (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), PA-60- 700P (Aerostar 700P), 360, 400. (4) Alexandria Aircraft, LLC. 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-31, 17-31TC, 17-30A, 17-31A, 17- 31ATC. (5) Alliance Aircraft Group 15A, 20, H-250, H-295, (USAFU-10D), HT- LLC. 295, H391 (USAFYL-24), H391B, H-395 (USAFL-28A or U-10B), H-395A, H-700, H- 800, HST-550, HST-550A (USAF AU-24A), 500. (6) American Champion 402, 7GCA, 7GCB, 7KC, 7GCBA, 7GCAA, Aircraft Corp. 7GCBC, 7KCAB, 8KCAB, 8GCBC. (7) Sky International Inc: A-1, A-1A, A-1B, S-1S, S-1T, S-2, S-2A, S- 2S, S-2C. (8) B-N Group Ltd: BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN-2T-4R, BN-2A MK.III, BN2A MK.III-2, BN2A MK.111-3. (9) Bellanca: 14-13, 14-13-2. 14-13-3. 14-13-3W. (10) Bombardier Inc: (Otter) DHC-3, DHC-6-1, DHC-6-100, DHC-6- 200, DHC-6-300. (11) Cessna Aircraft Company. 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H, (USAF T041A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, 172RG, P172D, R172E (USAF T-41 B) (USAF T-41 C AND D), R172F (USAF T-41 D), R175G, R172H (USAF T-41 D), R172J, R172K, 175, 175A, 175B, 175C, 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, 182S, 182T, R182, T182, TR182, T182T, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 190, (LC-126A, B, C) 195, 195A, 195B, 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, P210N, T210N, 210R, P210R, T210R, 210-5 (205), 210-5A (205A), 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H, 207, 207A, T207, T207A, 208, 208A, 208B, 310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 320, 320A, 320B, 320C, 320D, 320E, 320F, 320-1, 335, 340, 340A, 336, 337, 337A (USAF 02B), 337B, T337B, 337C, 337E, T337E, T337C, 337D, T337D, M337B (USAF 02A), 337F, T337F, T337G, 337G, 337H, P337H, T337H, T337H-SP, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, 404, 406, 441. (12) Cirrus Design SR20, SR22. Corporation. (13) Commander Aircraft 112, 112TC, 112B, 112TCA, 114, 114A, Company. 114B, 114TC. (14) de Havilland Inc: DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III. (15) Dynac Aerospace (Volaire) 10, (Volaire) 10A, (Aero Corporation. Commander) 100, (Aero Commander) 100A, (Aero Commander) 100-180. (16) Diamond Aircraft DA-20-A1, DA20-C1, DA 40. Industries. (17) Empressa Brasileira de EMB-110P1, EMB-110PE. Aeronautica S.A. EMBRAER. (18) Extra Flugzeugbau Gmbh.. EA300, EA300L, EA300S, EA300/200, EA-400. (19) Fairchild Aircraft SA26-T, SA26-AT, SA226-T, SA226-AT, SA226- Corporation. T(B), SA227-AT, SA227-TT, SA226-TC, SA227-AC (C-26A), SA227-CC, SA227-DC (C- 26B). (20) Global Amphibians, LLC.. Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, Lake Model 250. (21) Grob-Werke: G115, G115A, G115B, G115C, G115C2, G115D, G115D2, G115EG, G120A. (22) Lancair Company: LC40-550FG. (23) LanShe Aerospace, LLC... MAC-125C, MAC-145, MAC-145A, MAC-145B. (24) Learjet Inc: 23. (25) Lockheed Aircraft 18. Corporation. (26) Luscombe Aircraft 11A, 11E. Corporation. (27) Maule Aerospace Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M- Technology, Inc. 4180C, M-4-180S, M-4-180T, M-4-210, M-4- 210C, M-4-210S, M-4-210T, M-4-220, M-4- 220S, M-4-220T, M-5-180C, M-5-200, M-5- 210C, M-5-210TC, M-5-220C, M-5-235C, M-6- 180, M-6-235, M-7-235, MX-7-235, MX-7- 180, MX-7-420, MXT-7-180, MT-7-235, M-8- 235, MX-7-160, MXT-7-160, MX-7-180A, MXT- 7-180A, MXT-7-180B, M-7-235B, M-7-235A, M-7-235C, M-7-180C, M-7-260, MT-7-260, M- 7-260C, M-7-420AC, MX-7-160C, MX-7- 180AC, M-7-420A, MT-7-420. (28) Mitsubishi Heavy MU-2B-25, MU-2B-35, MU-2B-26, MU-2B-36, Industries, Ltd. MU-2B-26A, MU-2B-36A, MU-2B-40, MU-2B- 60, MU-2B, MU-2B-20, MU-2B-20, MU-2B-15. (29) Mooney Airplane Company, M20, M20A, M20B, M20C, M20D, M20E, M20F, Inc. M20G, M20J, M20K, M20L, M20M, M20R, M20S, M22. (30) Moravan a.s: Z-242L, Z-143L. (31) Navion Aircraft Company, NAVION, Navion (L-17A), Navion (L-17B), Ltd. Navion (L-17C), Navion B, Navion D, Navion E, Navion F, Navion G, Navion H. (32) New Piper Aircraft, Inc. PA-12, PA-12S, PA-18, PA-18S, PA-18 "105" (Special), PA-18S "105" (Special), PA-18A, PA-18 "125" (Army L- 21A), PA-18S "125," PA-18AS "125," PA-18 "135" (Army L-21B), PA-18A "135," PA-18S "135," PA-18 "150," PA-18A "150," PA-18S "150," PA-18AS "150," PA-19 (Army L-18B), PA-19S, PA- 20, PA-20S, PA-20 "115," PA-20S "115," PA-20 "135," PA-20S "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-23, PA-23-160, PA-23-235, PA-23- 250, PA-E23-250, PA-24, PA-24-250, PA-24- 260, PA-24-400, PA-28-140, PA-28-150, PA- 28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-235, PA-28S-160, PA-28R-180, PA- 28S-180, PA-28-181, PA-28R-200, PA-28R- 201, PA-28R-201T, PA-28RT-201, PA-28RT- 201T, PA-28-201T, PA-28-236, PA-30, PA- 39, PA-40, PA-31P, PA-31T, PA-31T1, PA- 31T2, PA-31T3, PA-31P-350, PA-32-260, PA- 32-300, PA-32S-300, PA-32R-300, PA-32RT- 300, PA-32RT-300T, PA-32R-301 (SP), PA- 32R-301 (HP), PA-32R-301T, …

  14. AD 2004-08-17 One-time

    Cessna Aircraft Company Models 208 and 208B Airplanes

    We are issuing this AD to detect and correct loose and improperly tied nuts on the wing struts, which could result in an attachment nut coming off the bolt.

    Effective May 17, 2004 · Amendment 39-13587

    Applicability, as the AD words it

    This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial Numbers 208: 20800370 and 20800371. 208B: 208B1034 through 208B1043, 208B1045, 208B1046, and 208B1048.

  15. AD 2003-21-04 One-time

    Cessna Aircraft Company Models 208 and 208B Airplanes

    We are issuing this AD to prevent failure of the right inboard forward flap bell crank due to cracks, deformation, or missing/incomplete welds.

    Effective Oct 21, 2003 · Amendment 39-13339

    Applicability, as the AD words it

    This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial No. 208: 20800001 through 20800369. 208B: 208B0001 through 208B1014, 208B1017, 208B1018, 208B1020 through 208B1024, 208B1026, and 208B1029 through 208B1033.

  16. AD 2002-22-17 Superseded by AD 2004-17-01

    Cessna Aircraft Company Models 208 and 208B Airplanes

    Effective Dec 31, 2002 · Amendment 39-12944

    Applicability, as the AD words it

    This AD applies to each airplane identified in paragraph (a) of this AD, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/ operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if you have not eliminated the unsafe condition, specific actions you propose to address it. (f) Where can I get information about any already-approved alternative methods of compliance? Contact Paul Nguyen, Aerospace Engineer, FAA, Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: 316-946-4125; facsimile: 816-946-4407. (g) What if I need to fly the airplane to another location to comply with this AD? The FAA can issue a special flight permit under Sec. Sec. 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate your airplane to a location where you can accomplish the requirements of this AD. (h) Are any service bulletins incorporated into this AD by reference? Actions required by this AD must be done in accordance with Cessna Service Bulletin No. CAB02-1, dated February 11, 2002. The Director of the Federal Register approved this incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51. You may get copies from Cessna Aircraft Company, Product Support, PO Box 7706, Wichita, Kansas 67277; telephone: (316) 517-5800; facsimile: (316) 942-9006. You may view copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC. (i) When does this amendment become effective? This amendment becomes effective on December 31, 2002. Issued in Kansas City, Missouri, on October 31, 2002. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 02-28408 Filed 11-8-02; 8:45 am] BILLING CODE 4910-13-P

  17. AD 97-25-04 One-time

    Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes

    To prevent loss of airplane control or engine overspeed with consequent loss of engine power caused by the power levers being positioned below the flight idle stop while the airplane is in flight.

    Effective Jan 21, 1998 · Amendment 39-10227

    Applicability, as the AD words it

    Models 208, 208A, 208B, 425, and 441 airplanes, all serial numbers, certificated in any category.

  18. AD 97-01-13 One-time

    Cessna Aircraft Company 100, 200, 300, and 400 Series Airplanes

    To prevent fuel, oil, or hydraulic systems failure caused by a collapsed hose.

    Effective Feb 3, 1997 · Amendment 39-9884

    Applicability, as the AD words it

    All serial numbers of Models 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L, F150M, FA150K, FA150L, FRA150L, FRA150M, 152, A152, F152, FA152, 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172RG, FP172, F172D, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P, FR172E, FR172F, FR172G, FR172H, FR172J, FR172K, P172D, R172E(T41), R172F(T41), R172G(T41), R172H(T41), R172J, R172K, 175, 175A, 175B, 175C, 177, 177A, 177B, 177RG, F177RG, 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, F182P, F182Q, FR182, T182, R182, TR182, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 188, 188A, 188B, A188, A188A, A188B, T188C, 206, P206A, P206B, P206C, P206D, P206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, TP206, TP206A, TP206B, TP206C, TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, 207, 207A, T207, T207A, 208, 208B, 210, 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, 210R, T210F, P210N, P210R, 210-5 (205), 210-5A (205A), T303, 310P, 310Q, 310R, T310P, 310Q, 310R, 335, 336, 337, 337A, 337B, 337C, 337D, 337E, 337F, 337G, 337H, F337E, F337F, F337G, F337H, FT337E, FT337F, FT337GP FT337HP, FTB337, T337B, T337C, T337D, T337E, T337F, T337G, T337H, T337H-SP, M337B, P337H, 340, 340A, 401, 401A, 401B, 402, 402A, 402B, 402C, 404, F406, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, and 425 airplanes, certificated in any category.

  19. AD 96-09-15 One-time

    Cessna Aircraft Company Models 208 and 208B Airplanes

    Effective Jun 11, 1996 · Amendment 39-9591 · Corrected Jun 17, 1996, May 28, 1996

    Applicability, as the AD words it

    Models 208 and 208B airplanes (all serial numbers), certificated in any category.

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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.