Cessna Caravan airworthiness directives FAA ADs that may apply, with the official text
- In effect
- 25
- Recurring
- 5
- Superseded or removed6
- Latest2021-04-10
Cessna Caravan: price, specs and every tail number · Look up ADs by N-number · AD burden by model, ranked
IN EFFECT
25 Caravan 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.
- AD 2021-04-10 Recurring
Textron Aviation, Inc. Airplanes
This AD was prompted by reports of loose elevator torque tube attach fasteners.
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.
- 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.
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.
- 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.
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).
- 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.
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.
- AD 2008-26-10 One-time
Cessna Aircraft Company 172, 175, 177, 180, 182, 185, 188, 206, 207, 208, 210, 303, 336, and 337 Series Airplanes
We are issuing this AD to prevent erroneous indications from the altimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information and possibly result in loss of control.
Applicability, as the AD words it
This AD applies to all serial numbers (S/Ns) of the airplanes listed in Table 1 of this AD, certificated in any category, that: (1) Were initially delivered from the manufacturer between January 1, 1993, and March 31, 2008, unless the modification/rework required in AD 2008-10-02 has been done and you remain in compliance with that AD; or (2) Have a part number (P/N) 2013142-18 installed as a replacement part anytime after January 1, 1993, unless the modification/rework required in AD 2008-10-02 has been done and you remain in compliance with that AD.
- 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.
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.
- 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.
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.
- AD 2008-10-02 One-time
Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series Airplanes
We are issuing this AD to prevent erroneous indications from the altimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information and possibly result in loss of control.
Applicability, as the AD words it
This AD applies to airplanes listed in Table 1 and Table 2 of this AD that: (1) Have a part number (P/N) 2013142-18 alternate static air source selector valve installed after November 19, 2007; and (2) Are certificated in any category: Table 1.--Applicability for Airplanes That Had the Affected Part Installed at Manufacture Model Serial Nos. (S/Ns) 172S: 172S10672 through 172S10674, 172S10676, 172S10678 through 172S10680, 172S10682, 172S10683, and 172S10685. 182T: 18282062 and 18282065. T182T: T18208822 and T18208828. 208: 20800417, 20800418, and 20800419. 208B: 208B1294 through 208B1310.
- AD 2007-10-15 One-time
Cessna Aircraft Company Models 208 and 208B Airplanes
Applicability, as the AD words it
This AD applies to Models 208 and 208B, all serial numbers, that are certificated in any category.
- AD 2006-01-11 One-time
The Cessna Aircraft Company Models 208 and 208B Airplanes
Applicability, as the AD words it
This AD affects Models 208 and 208B, all serial numbers, that are certificated in any category.
- AD 2005-25-08 One-time Appliance
Shadin ADC-2000 Air Data Computers
Applicability, as the AD words it
This AD affects Shadin ADC-2000 air data computers (ADC), part numbers (P/N) 962830A-1-S-8, 962830A-2-S-8, 962830A-3-S-8, configurations B, C, and D, that are installed in, but not limited to, the following aircraft (all serial numbers), and are certificated in any category: Manufacturer Model Alliance Aircraft Group, LLC: H-250 B-N Group Ltd: BN2A Bombardier Inc: DHC-3, DHC-6 Cessna Aircraft Company: 172, 180, 180E, 185, 206, 206E, 206F, 206G 208, 210L, 310 deHavilland Inc: DHC-2 The New Piper Aircraft, Inc: PA-28-180, PA-28-181, PA-31- 350, PA-32-300, PA-32-301, PA-32R-300, PA-34-200T
- 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.
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.
- AD 2005-01-19 One-time Appliance
GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders
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, …
- AD 2004-25-16 Appliance
Kelly Aerospace Power Systems Part Number (P/N) 14D11, A14D11, B14D11, C14D11, 23D04, A23D04, B23D04, C23D04, or P23D04 Fuel Regulator Shutoff Valves (Formerly Owned by ElectroSystems, JanAero Devices, Janitrol, C&D, FL Aerospace, and Midland-Ross Corporation)
Applicability, as the AD words it
What aircraft are affected by this AD? This AD applies to aircraft equipped with a Kelly Aerospace part number (P/N) 14D11, A14D11, B14D11, C14D11, 23D04, A23D04, B23D04, C23D04 or P23D04 fuel regulator shutoff valve used with Kelly Aerospace B1500, B2030, B2500, B3040, B3500, B4050, or B4500 B-Series combustion heaters. The following is a list of aircraft where the B-Series combustion heater could be installed. This is not a comprehensive list and aircraft not on this list that have the heater installed through field approval or other methods are still affected by this AD: Manufacturer Aircraft models/series (1) Bombardier Inc: CL-215, CL-215T, and CLT-415. (2) Cessna Aircraft Company: 208, T303, 310F, 310G, 310H, 310I, 310J, 310K, 310L, 310N, 310P, 310Q, 320C, 320D, 320E, 320F, 337 Series, 340, 340A, 414, 414A, 421, 421A, 421B, and 421C. (3) The New Piper Aircraft, Inc... PA-23 Series, PA-30, PA-31 Series, PA-34 Series, PA-39, and PA-44 Series. (4) Raytheon Aircraft Corporation. 95-B55 Series, 58, 58TC, 58P, 60, A60, and 76.
- AD 2004-21-05 Recurring Appliance
Kelly Aerospace Power Systems B-Series Combustion Heaters Models B1500, B2030, B2500, B3040, B3500, B4050, and B4500 (Formerly Owned by JanAero Devices, Janitrol, C&D, FL Aerospace, and Midland-Ross Corporation)
We are issuing this AD to prevent combustion by-products (carbon-monoxide exhaust) and fuel leakage from the combustion heaters caused by failure of the combustion heater system.
Applicability, as the AD words it
This AD affects Kelly Aerospace Power Systems B-Series Combustion Heaters, Models B1500, B2030, B2500, B3040, B3500, B4050, and B4500, marked as meeting the standards of TSO-C20, that are installed on, but not limited to, the following aircraft (all serial numbers), and are certificated in any category: Manufacturer Models Raytheon Aircraft Company: 58, 58P, 58TC, 60, A60, 76, and 95-B55 Series. Bombardier Inc: CL-215-1A10 (Water Bomber) CL215-6B11 (CL-215T Variant) (CL415 Variant) . The Cessna Aircraft Company: 208, 310F, 310G, 310H, 310I, 310J, 310K, 310L, 310N, 310P, 320C, 320D, 320E, 320F, 337 Series, 340, 340A, 414, 414A, 421, 421A, 421B, and 421C.
- AD 2004-17-01 Recurring
Cessna Aircraft Company Models 208 and 208B Airplanes
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.
- 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.
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.
- 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.
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.
- AD 2001-23-17 One-time Appliance
GARMIN International GNS 430 Units
Applicability, as the AD words it
This AD applies to the GNS 430 units that are specified in paragraph (a)(1) of this AD and are installed on aircraft. These GNS 430 units are installed in, but not limited to, aircraft that are certificated in any category and presented in paragraph (a)(2) of this AD: (1) GNS 430 Units, part number 011-00280-00: serial numbers 9630001, 96300002, 96300017, 96300028, 96300034, 96300040, 96300068, 96300104, 96300108, 96300122, 96300125, 96300130, 96300142, 96300149, 96300161, 96300165, 96300218, 96300222, 96300232, 96300269, 96300272, 96300308, 96300333, 96300340, 96300348, 96300354, 96300369, 96300372, 96300382, 96300394, 96300411, 96300413, 96300429, 96300437, 96300451, 96300484, 96300485, 96300489, 96300504, 96300506, 96300513, 96300522, 96300549, 96300563, 96300585, 96300587, 96300618, 96300621, 96300624, 96300628, 96300641, 96300653, 96300664, 96300713, 96300734, 96300756, 96300766, 96300781, 96300785, 96300786, 96300808, 96300831, 96300837, 96300842, 96300846, 96300866, 96300870, 96300872, 96300899, 96300916, 96300923, 96300925, 96300929, 96300941, 96300961, 96300984, 96300987, 96301021, 96301108, 96301130, 96301280, and 96301296 through 96303200. (2) Aircraft with the GNS 430 Unit Installation (other aircraft could have field approval installations): TC holder Airplane models Cessna Aircraft Company: 172, 182, 206, 208, 210, 401, 402, 404, 406, 411, 414, 414A, 421A, 421B, 421C, 425, 441, 500, 550, S550, 552, 560, 560XL, 501, 525, and 551. Mooney Aircraft: M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, and M22. Raytheon Aircraft Company: Beech Models E33, F33, G33, E33A, F33A, E33C, F33C, 35, 35R, A35, B35, B35TC, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35TC, V35A, V35A-TC, V35B, V35B-TC, 36, A36, A36TC, 50, B50, C50, D50, D50A, D50B, D50C, D50E, E50, F50, G50, H50, J50, 60, A60, B60, 65-90, 65-A90, B90, C90, C90A, C90B, E90, F90, 100, A100, B100, 95-55, 95-A55, 95-B55, 95-C55, D-55, E55, 58, 58P, and 58TC. Socata: TBM 700. The New Piper Aircraft, Inc.. J3C-40, J3C-50, J3C-50S (Army L-4, L-4B, L-4H, and L-4J), J3C-65 (Navy NE-1 and NE-2), J3C-65S, J3F-50, J3F-50S, J3F-60, J3F-60S, J3F-65 (Army L-4D), J3F-65S, J3L, J3L-S, J3L-65 (Army L-4C), J3L-65S, J4, J4A, J4A-S, J4E (Army L-4E), J5A (Army L-4F), J5A-80, J5B (Army L-4G), J5C, AE-1, HE-1, PA-11, PA-11S, PA-12, PA-12S, PA-14, PA-15, PA-16, PA-16S, PA- 17, PA-18, PA-18A, PA-18A (Restricted), PA-18S, PA-18-"105" (Special), PA-18S- "105" (Special), PA-18-"125" (Army L- 21A), PA-18AS-"125", PA-18S-"125",
- AD 2001-20-01 Recurring Engine
Pratt & Whitney Canada PT6A-25C and -114A Series Turboprop Engines
Applicability, as the AD words it
This airworthiness directive (AD) applies to PT6A-25C and -114A Series turboprop engines, that have incorporated P&WC S.B. 1510, which are installed on but not limited to Pilatus PC-7 and Cessna 208 Caravan airplanes.
- AD 98-25-02 One-time Appliance
BFGoodrich Avionics Systems, Inc. SKYWATCH SKY497 Installations with a Top-Mounted Antenna
To prevent the display of target indicators on the wrong side of the aircraft caused by an internal component failure in the SKY497 installations with a top-mounted antenna, which could result in the pilot making an incorrect initial maneuver based on the displayed information while trying to visually acquire the aircraft.
Applicability, as the AD words it
SKYWATCH SKY497 installations with a top-mounted antenna that are installed on, but not limited to, the following aircraft, all serial numbers, certificated in any category: Manufacturer Aircraft models and/or series Raytheon: Beech 90, 100, 200, and 300 Series. Cessna: 172, 182, 206, 208, 210, 300, 400, and 500 Series. Piper: PA-23, PA-31-360, PA-31T, PA-32, PA-34, PA-42, and PA-46. Hawker: HS-700 and HS-800. Mitsubishi: MU-2 Series. Dassault: F10. Mooney: M20 Series. Bombardier: DHC-6 Series. West- wind: 1124. Bell: 407. Eurocopter: AS365. Socata: TBM700.
- 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.
Applicability, as the AD words it
Models 208, 208A, 208B, 425, and 441 airplanes, all serial numbers, certificated in any category.
- AD 97-04-12 One-time Engine
Pratt & Whitney Canada PT6 Series Turboprop Engines
To prevent engine power reduction due to malfunction of the compressor BOV, which could result in a forced landing and loss of the aircraft.
Applicability, as the AD words it
Pratt & Whitney Canada (PWC) PT6 series turboprop engines manufactured after January 1, 1995, or any PT6 series engines that have had their compressor bleed-off valve (BOV) changed after January 1, 1995, and which are installed in single-engine aircraft including, but not limited to the following aircraft: Air Tractor AT, Ayres Turbo Thrush Commander, Cessna 208 Caravan, Argo Aircraft G169B, Embraer EMB-312 Tucano, Frakes AF-CAT, Pilatus PC-6, PC-7, PC-9, and PC-12, Schweitzer AG-CAT, Aerospatiale Socata TBM- 700, and Raytheon (Beech) T-34C.
- 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.
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.
- AD 96-09-15 One-time
Cessna Aircraft Company Models 208 and 208B Airplanes
Applicability, as the AD words it
Models 208 and 208B airplanes (all serial numbers), certificated in any category.
Federal Register Official PDF Correction (Jun 17, 1996)Correction (May 28, 1996)
6 superseded or removed ADs
- AD 2006-06-06 Superseded by AD 2007-10-15
The Cessna Aircraft Company Models 208 and 208B Airplanes
Applicability, as the AD words it
This AD affects Models 208 and 208B, all serial numbers, that are certificated in any category.
- 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
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, …
- AD 2002-22-17 Superseded by AD 2004-17-01
Cessna Aircraft Company Models 208 and 208B Airplanes
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
- AD 2001-17-13 Superseded by AD 2004-25-16 Appliance
JanAero Devices Part Number (P/N) 14D11, A14D11, B14D11, C14D11, 23D04, A23D04, B23D04, and C23D04 Fuel Regulator Shutoff Valves
Applicability, as the AD words it
This AD applies to aircraft equipped with a JanAero Devices part number 14D11, A14D11, B14D11, C14D11, 23D04, A23D04, B23D04, or C23D04 fuel regulator shutoff valve used with JanAero Devices B1500, B2030, B2500, B3040, B3500, B4050, or B4500 B-Series combustion heaters. The following is a list of aircraft where the B-Series combustion heater could be installed. This is not a comprehensive list and aircraft not on this list that have the heater installed through field approval or other methods are still affected by this AD: Manufacturer Aircraft models Raytheon Aircraft Corporation Beech 95-B55 Series, 58, 58TC, 58P, 60, (Beech). A60, and 76. Canadair: CL-215, CL-215T, and CLT-415. Cessna Aircraft Company 208, 303, 310F, 310G, 310H, 310I, 310J, (Cessna). 310K, 310L, 310M, 310N, 310P, 310Q, 320C, 320D, 320E, 320F, 337 Series, 340, 340A, 414, 414A, 421, 421A, 421B, and 421C. The New Piper Aircraft, Inc. PA-23 Series, PA-30, PA-31 Series, PA-34 (Piper). Series, PA-39, and PA-44.
- AD 2001-08-01 Superseded by AD 2001-17-13 Appliance
JanAero Devices 14D11 and 23D04 Series Fuel Regulator and Shutoff Valves
Applicability, as the AD words it
This AD applies to airplanes equipped with JanAero Series 14D11 or 23D04 fuel regulator and shutoff valves installed with the following B-Series combustion heaters. (1) Affected B-Series combustion heater models: B1500, B2030, B2500, B3040, B3500, B4050, B4500. (2) The following is a list of airplanes where the B-Series combustion heater could be installed. This is not a comprehensive list and airplanes not on this list that have the heater installed through field approval or other methods are still affected by this AD: Manufacturer Airplane model Beech: 95-B55 Series, 58, 58TC, 58P, 60, A60, and 76. Canadair: CL-215, CL-215T, and CLT- 415. Cessna: 208, 303, 310F, 310G, 310H, 310I, 310J, 310K, 310L, 310M, 310N, 310O, 310P, 3210C, 320D, 320E, 320F, 337 Series, 340, 340A, 414, 414A, 421, 421A, 421B, and 421C. Piper: PA-23, PA-30, PA-31 Series, PA-34, and PA-44. (b) Who must comply with this AD? Anyone who wishes to operate any airplane that is equipped with one of the above referenced JanAero combustion heaters must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to prevent fuel leakage into the combustion heater, which could result in a hazardous fire. (d) What must I do to address this problem? To address this problem, unless already done, you must do the following actions: Action Compliance time Procedures (1) Visually inspect the Within the next 25 Do this following installed fuel regulator hours time-in- INSTALLATION and shutoff valve used with service (TIS) after INSPECTION and JanAero Devices Combustion May 10, 2001 (the ALTERNATIVE VISUAL Heaters, Models B1500- effective date of INSPECTION B4500, for fuel leaks. this AD). procedures in JanAero Devices Service Bulletin No. A-107, dated January 8, 2001. (2) Pressure test the fuel Within the next 25 Do the following regulator and shutoff valve hours time-in- PRESSURE TEST FOR for leakage. service (TIS) after LEAKAGE procedures May 10, 2001 (the in JanAero Devices effective date of Service Bulletin this AD) and after No. A-107, dated the inspection in January 8, 2001. paragraph (d)(1) of this AD. (3) If fuel leaks are found, Before further Do the following replace with a new valve
- AD 96-20-07 Superseded by AD 2004-21-05 Appliance
JanAero Devices B-Series Combustion Heaters, Models B1500, B2030, B3040, and B4050 (formerly owned by Janitrol, C&D, FL Aerospace, and Midland-Ross Corporation)
To prevent an airplane fire or explosion caused by failure of the heater combustion tube assembly or combustion air pressure switch.
Applicability, as the AD words it
B-Series combustion heaters, Models B1500, B2030, B3040, and B4050, marked as meeting the standards of TSO-C20, that do not incorporate a ceramic combustion tube and a part number (P/N) 94E42 combustion air pressure switch, and are installed on, but not limited to, the following aircraft (all serial numbers), certificated in any category: Manufacturer Models and series model airplanes Beech: Models 95-B55 Series, 58, 58TC, 58P, 60, A60, and 76. Canadair: Models CL-215, CL-215T, and CLT-415. Cessna: Models 208, 303, 310F, 310G, 310H, 310I, 310J, 310K, 310L, 310M, 310N, 310O, 310P, 320C, 320D, 320E, 320F, 337 series, 340, 340A, 414, 414A, 421, 421A, 421B, and 421C.
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.
QUESTIONS
Caravan 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 Caravan?
31 FAA ADs published since 1995 name the Cessna Caravan's type certificate models (208 and 208B) in their applicability. 25 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 Caravan ADs are recurring?
5 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 Caravan airworthiness directive?
AD 2021-04-10, effective Apr 12, 2021: Textron Aviation, Inc. Airplanes. The list is refreshed from the Federal Register every weekday.
How do I know whether an AD applies to my Caravan?
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 Cessna Caravan 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 Caravan, 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.