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.
N873T is a 1965 Beechcraft 95-B55 (T42A) in the FAA registry (aircraft page). Matched on type certificate model 95-B55.
RESULTS
15 ADs in effect may apply to N873T
- In effect15
- Recurring4
- Superseded or removed4
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Also show 4 superseded or removed N873T’s registration record
- AD 2009-25-01 One-time
Hawker Beechcraft Corporation Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A, A36, A36TC, B36TC, E55, E55A, F33A, and V35B Airplanes
We are issuing this AD to detect and correct an incorrect washer installed in the pilot and copilot shoulder harnesses.
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that are certificated in any category: (1) Group 1 Airplanes (retains the actions and applicability from AD 91-18-19): Model Serial Nos. (SNs) 58, 58A: TH-733 through TH-1609. 58P, 58PA: TJ-3 through TJ-497. 58TC, 58TCA: TK-1 through TK-151. 95-B55, 95-B55A: TC-1947 through TC-2456. A36: E-825 through E-2578. B36TC: EA-242 and EA-273 through EA- 509. E55, E55A: TE-1078 through TE-1201. F33A: CE-634 through CE-1536. V35B: D-9862 through D-10403. (2) Group 2 Airplanes (aligns certain SNs applicability to Models A36TC airplanes): Model SNs A36TC: EA-1 through EA-241 and EA-243 through EA-272.
-
Hawker Beechcraft Corporation (Type Certificates No. 3A15, No. 3A16, No. A23CE, and No. A30CE Previously Held by Raytheon Aircraft Company) F33 Series and Models G33, V35B, A36, A36TC, B36TC, 95-B55, D55, E55, A56TC, 58, 58P, 58TC, G58, and 77 Airplanes
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that have a part number (P/N) 35-380132-1 through 35-380132- 53 circuit breaker toggle switch installed and are certificated in any category: Models Serial Nos. (1) F33 and G33: CD-1235 through CD-1304. (2) F33A: CE-290 through CE-1791. (3) F33C: CJ-26 through CJ-179. (4) V35B: D-9069 through D-10403. (5) A36: E-185 through E-3629 and E-3631 through E-3635. (6) A36TC and B36TC: EA-1 through EA-695. (7) 95-B55: TC-1913, TC-1936 through TC-2456. (8) D55: TE-452 through TE-767. (9) E55: TE-768 through TE-1201. (10) A56TC: TG-84 through TG-94. (11) 58: TH-1 through TH-2124. (12) 58P: TJ-3 through TJ-497. (13) 58TC: TK-1 through TK-151. (14) G58: TH-2126, TH-2127, TH-2131 through TH-2134, TH-2136, TH-2137, TH-2139 through TH-2141, and TH-2143 through TH-2150. (15) 77: WA-1 through WA-312.
-
Raytheon Aircraft Company (The Beech Aircraft Company and BEECH previously held Type Certificate Nos. 3A15, 3A16, 5A3, and A-777) Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A45 (T-34A, B45), D45 (T-34B), 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B (T-42A), 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 95, B95, B95A, D95A, and E95 Airplanes
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers (SNs) that are certificated in any category: (1) Group 1 (maintains the actions from AD 72-22-01): Model SNs (i) 35-33, 35-A33, 35-B33, 35-C33, CD-1 through CD-1256. E33, F33, and G33. (ii) 35-C33A, E33A, and F33A: CE-1 through CE-349. (iii) E33C and F33C: CJ-1 through CJ-30. (iv) 35, A35, B35, C35, D35, E35, D-1 through D-9287. F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, and V35B. (v) 36 and A36: E1 through E-283. (vi) A45 (T-34A, B45) and D45 (T- All. 34B). (vii) 95-55, 95-A55, 95-B55, and TC-1 through TC-1402. 95-B55A. (viii) 95-C55, 95-C55A, D55, D55A, TE-1 through TE-846. E55, and E55A. (ix) 56TC and A56TC: TG-1 through TG-94. (x) 58: TH-1 through TH-174. (xi) 95, B95, B95A, D95A, and E95. TD-2 through TD-721. (2) Group 2: Model 95-B55B (T-42A) airplanes, SNs TF-1 through TF-70.
- AD 2005-18-20 Recurring Propeller
Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers
We are issuing this AD to prevent Goodrich "FASTprop" propeller de-icers from detaching from the propeller blade, resulting in damage to the airplane, and possible injury to passengers and crewmembers.
Applicability, as the AD words it
This AD applies to Goodrich De-icing and Specialty Systems "FASTprop" propeller de-icers, part numbers (P/Ns) P4E1188 series, P4E1601 series, P4E2200 series, P4E2271-10, P4E2575-7, P4E2575-10, P4E2598-10, P5855BSW, P6199SW, P6592SW, P6662SW, and P6975-11, installed. These propeller de-icers are installed on, but not limited to, the airplanes listed in Table 1 of this AD. Table 1.--Goodrich "FASTprop" Propeller De-Icers De-icer P/N Installed on, but not limited to P4E1188-2: Metal propellers operated up to 2,900 rpm on: Cessna 210E, 210F, 210G, 210H, 210J, 210K, 210L, T210F, T210G, T210H, T210J, T210K, and T210L. With Supplemental Type Certificate (STC) SA1-502 on Raytheon (Beech) D18C, D18S, E18S, G18S, H18, C45G, C45H, TC45G, and TC45H. P4E1188-3: Metal propellers operated up to 2,900 rpm on: Raytheon (Beech) D18C, D18S, E18S, E18S-9700, G18S, H18, C-45G, C- 45H, C-45J, TC-45G. TC-45H, TC-45J (SNB-5), and JRB-6. With STC SA1-503 on Raytheon (Beech), E50, F50, G50, H50, J50, and 65. With STC SA15EA on Raytheon (Beech) E50, F50, G50, H50, J50, 65, and 65-80. Raytheon (Beech) 55, B55, D55, D55A, E55, 95-C55, 95-C55A, 58, 95- 55, 95-A55, 95-B55, 56TC, 60, 65, 65-80, 65-90, 65-A90, B90, C90, 99, 99A, A99, A99A, 100, and A100. With STC SA1-506 on Cessna 310. With McCauley props on Cessna 310, 320, 340, 401, 402, 411, 414, and 421. With STC SA2424WE on Cessna 402. With STC SA132EA on Twin Commander (Gulfstream) 560A, 560E, 680, 680E, and 720. With STC SA179EA on Twin Commander (Gulfstream) 560F, 680FL, 680FL(P), and 680-F. With STC SA1-520 on Twin Commander (Gulfstream) 560A, 560E 680, 680E, and 720. On the following models equipped with 90-amp generator: Twin Commander (Gulfstream) 500B, 500S, and 500U. With STC SA1-607 on Twin Commander (Gulfstream) 500A. With STC SA2478SW on Twin Commander (Gulfstream) 500. With STC SA2891WE or STC SA2691WE on Twin Commander (Gulfstream) 680F, 680FP, and 680FL(P). Twin Commander (Gulfstream) 680V, 680T, 680W, and 681. Mitsubishi Heavy Industries MU-2 series. With STC SA195EA on Piper PA-23-250, E23-250 (serial number (SN) 27-2505 up). Piper PA-31 (SN 31-5 up), PA-31-300 (SN 31-5 up), PA-31-325 (SN31- 5 up), and PA-31-350 (SN 31-5001 up). P4E1188-4: Metal propellers operated up to 2,900 rpm on: B-N Group Ltd. (Britten Norman) BN-2, BN-2A, and BN-2A Mark III series, Vulcanair (Partenavia) P-68, Piper Aerostar 600, 601, and 601P. On the following models equipped with 3-blade props: Short Brothers SC7 series 3, M7 Aerospace (Fairchild) SA26-T, SA26- AT, SA226-T, SA226-AT, and SA226-TC. The following models equipped with 70-amp alternators and Hartzell HC-A3XK props: Twin Commander (Gulfstream) 500B, 500S, and 500U. The following models equipped with 70-amp alternator and Hartzell HC-C3YR-2 props: Twin Commander (Gulfstream) 500S and 500U. The following model with 70- or 100-amp alternators and Hartzell HC-C3YR-R props: Twin Commander (Gulfstream) 500S (SN 3115 up). With STC SA2478SW on model Twin Commander (Gulfstream) 500. With STC SA2691WE or SA2891WE on the following models: Twin Commander (Gulfstream) 680F, 680FL, and 680FLP. P4E1188-5: Metal propellers operated up to 2,900 rpm on: With Hartzell HC-B3TN-3 props on Raytheon (Beech) D18C, D18S, E18S, E18S-9700, G18S, H18, C45G, C45H, TC45G, TC45H, C45J, TC45J (SN B-5), JRB-6, 99, 99A, A99, A99A, 99B, B99, 100, A100, A100A, A100C, and B100. With Hartzell HC-B3TN-3 props on Raytheon (Beech) 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, B90, C90, E90, and H90. With Hartzell HC-B3TN-3 props on Bombardier (deHavilland) DHC-6- 300, Israel Aircraft Industries 101 Arava, Mitsubishi Heavy Industries MU-2B-10, -15, -20, -25, -26, -30, -35, -36, MU-2 Series, Pilatus PC-6, Piper PA-31T (SN 31T-7400002 up), and PA31T1. With STC SA2293SW on British Aerospace (Scotland) Handley Page Jetstream 137 Mark I. AeroSpace Technologies of Australia (Government Aircraft Factories) N22B. Short Brothers SC7 series 3 equipped with 4-blade props. P4E1188-6: Metal propellers operated up to 2,900 rpm on: With Hartzell HC-B3TN-5( ) props on Cessna 425 and 441. Embraer EMB-110P1 and 110P2. Short Brothers SC7 series 3 equipped with 3-blade props. M7 Aerospace (Fairchild) SA226-T, SA226-AT, and SA226-TC. P4E1188-7: Metal propellers operated up to 2,900 rpm on: Mitsubishi Heavy Industries MU-2B, MU-2B-26A, MU-2B-36A, MU-2B-40, and MU-2B-60. P4E1601-3: Metal propellers operated up to 2,900 rpm on: Piper PA31 (SN 5 up), PA31-300 (SN 5 up), PA31-325 (SN 5up), PA31P (SN 31P-3 up), and PA31-350 (SN 31-5001 up). P4E1601-4: Metal propellers operated up to 2,900 rpm on: Raytheon (Beech) 65-88. P4E1601-5: Metal propellers operated up to 2,900 rpm on: Casa C212CB. Twin Commander (Gulfstream) 690 and 690A. P4E1601-7: Metal propellers operated up to 2,900 rpm on: Raytheon (Beech) B55, E55, 56TC, 58P, and 60. With STC SA2369SW on Nord 262A. The following models equipped with 70- or 100-amp alternator and Hartzell HC-C3YR-2 props: Twin Commander (Gulfstream) 500S (SN 3115 up) and Twin Commander (Gulfstream) 685. Short Brothers SD3-30. P4E1601-10: Metal propellers operated up to 2,900 rpm on: Raytheon (Beech) B55, E55, 56TC, 58P, and 60. Twin Commander (Gulfstream) 690C and 695. M7 Aerospace (Fairchild) SA-226-TB, SA227-AC, SA227-TT, and SA227- AT. P4E2200-2: Metal propellers operated up to 2,900 rpm on: With STC SA00719LA on Raytheon (Beech) A36. With STC SA00718LA on Raytheon (Beech) B36TC. Raytheon (Beech) V35 equipped with 2- or 3-blade McCauley props. P4E2200-3: Metal propellers operated up to 2,900 rpm on: Raytheon (Beech) E50, F50, G50, H50, and J50. Cessna E310J, T310P, 310, 310E, 310J, 310K, 310L, 310N, 320, 320D, 320F, 40, 402A, 402B, 411, 411A, 414, 421, 421A, and 421B. Piper PA23-250. P4E2200-4: Metal propellers operated up to 2,900 rpm on: B-N Group Ltd. (Britten Norman) BN-2A Mark III, BN-2, BN-2A. Piper 600, 601, 601P. P4E2200-10: Metal propellers operated up to 2,900 rpm on: With Volpar Turboliner conversion on the following models: …
- 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 97-18-02R1 Recurring Propeller
Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers with Aluminum Blades
To prevent blade separation due to cracked blades, hubs, or blade clamps, which can result in loss of control of the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) series and HA- A2V20-1B series propellers with aluminum blades. These propellers are installed on but not limited to the aircraft listed in the following Table 1: Table 1.-Affected Aircraft Manufacturer Aircraft model Aero Commander (Twin Commander): 500; 500A; 500B, 500S, and 500U; 520; 560; 560A, 560E; 680, 680E, 720; 680F, 680FP, 680FL, 680FLR; B1 (CALLAIR). Aeromere: FALCO F.8.L. Aeronautica Macchi: AL60-F5; AM-3. Bauger: SAIL PLANE. Beech: 35 SERIES BONANZA; 35-C33 DEBONAIR; 35-C33A, E33A, F33A; 50 SERIES TWIN BONANZA; 58P, 58TC BARON; 95-55, 95-A55, 95-B55 BARON; 65, A65, 65-(B)80, 65-A80, A65- 8200, 70. Bellanca: 14-13; 14-19; 14-19-2; 14-19-3; 7GCA, 7GCB, 7GCC; DW-1 EAGLE. Camair: 480. Cessna: 170; 170A; 172 SKYHAWK; 175; 180, A, B, C, D, E, F, G, H; 182, A, B, C, D, E, G, H, J, K, L, M; 210, A, B, C, 5, 5A; 310, A, B, C, D, E, F, G, H, E310H; 320, 320-1 SKYKNIGHT; 320A, 320B; 402 BUSINESSLINER; 411; WREN 460; WREN 460H, J, K, L, M. deHavilland: DH104 DOVE; DH114 HERON. Dornier: DO27Q-6; DO28A-1; DO28B-1. Fuji: T-3, LM-2. GAF--Gov't. Aircraft Factories: N22B, N24A, N22S, N22C. Goodyear: (Loral); GA22A GOODYEAR BLIMP; GZ19, 19A GOODYEAR BLIMP. Great Lakes: 2T-1A-2. Grumman: G44, G44A WIDGEON; G21C, D GOOSE. Helio: H-391 COURIER; H-391B COURIER; H-395A COURIER. Luscombe: 11; 11A. Mooney: M20. Multitech (Temco): D16 TWIN NAVION; D16A TWIN NAVION. Nardi: FN-333. Navion: NAVION B; NAVION, NAVION A. Pacific Aerospace (Fletcher): FU-24, FU-24A. Piaggio: P-149D; P136-L1 ROYAL GULL; P136-L2 ROYAL GULL; P149D; P166 ROYAL GULL. Pilatus: PC-3; PC-6; PC-6-H1, -H2 PORTER. Piper: PA-E23-250 AZTEC; PA14 FAMILY CRUISER; PA18(A)(S)-150 SUPER CUB; PA18A-150 SUPER CUB; PA22-150, PA22S-150 TRIPACER; PA23 SERIES APACHE; PA23-160 APACHE; PA23- 235 AZTEC; PA23-250 AZTEC; PA24-250 COMANCHE; PA24-400 COMANCHE; PA24S COMANCHE; PA28 CHEROKEE; PA28-140 CHEROKEE. Prop Jets Inc: 200; 200A,B,C. Republic (STOL Amphibian): RC3 SEABEE. Scottish Aviation (BAE): B.206 SERIES 2 BEAGLE. Stinson: L-5; 108, -1, -2, -3; 108-2-3. Sud Aviation (SOCATA): GY.80-150 GARDAN; GY.80-160 GARDAN HORIZON. Swift: GC-1B. Taylorcraft: 20. Texas Bullet: 205. Windecker: EAGLE.
- AD 2003-01-03 One-time Propeller
Hartzell Propeller Inc. Model ( )HC-( )2Y( )-( ) propellers
To prevent in-flight propeller blade separation resulting in airframe and engine damage, and possible loss of the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Hartzell Propeller Inc. model ( )HC-( )2Y( )-( ) propellers, with propeller hub part numbers (P/N's) D-6522-1, D-6522-2, D-6529-1, and D-6559-3, with the serial numbers (SN's) listed in the following Table 1: Table 1.--Applicable Propellers and Hubs Propeller SN Hub SN Hub P/N AU11115B: A61365B D-6522-1 AU11116B: A61366B D-6522-1 AU11117B: A61367B D-6522-1 AU11119B: A61369B D-6522-1 AU11125B: A61375B D-6522-1 AU11131B: A61381B D-6522-1 AU11134B: A61384B D-6522-1 AU11135B: A61385B D-6522-1 AY515B: A61397B D-6522-2 AY516B: A61398B D-6522-2 CH36140B: A61409B D-6529-1 CH36141B: A61410B D-6529-1 CH36151B: A61420B D-6529-1 CH36152B: A61421B D-6529-1 CH36153B: A61422B D-6529-1 CH36157B: A61427B D-6529-1 EU376B: A61443B D-6559-3 CH36172B: A61547B D-6529-1 CH36159B: A61553B D-6529-1 CH36160B: A61554B D-6529-1 CH36162B: A61556B D-6529-1 CH36163B: A61557B D-6529-1 CH36165B: A61560B D-6529-1 CH36188B: A61563B D-6529-1 CH36193B: A61568B D-6529-1 CH36194B: A61569B D-6529-1 CH36195B: A61570B D-6529-1 CH36196B: A61571B D-6529-1 CH36178B: A61573B D-6529-1 CH36179B: A61574B D-6529-1 CH36181B: A61576B D-6529-1 CH36182B: A61577B D-6529-1 CH36183B: A61578B D-6529-1 CH36198B: A61583B D-6529-1 CH36199B: A61584B D-6529-1 CH36200B: A61585B D-6529-1 CH36201B: A61586B D-6529-1 CH36202B: A61587B D-6529-1 CH36203B: A61588B D-6529-1 CH36204B: A61589B D-6529-1 CH36205B: A61590B D-6529-1 CH36209B: A61594B D-6529-1 CH36211B: A61596B D-6529-1 CH36212B: A61597B D-6529-1 CH36213B: A61598B D-6529-1 CH36215B: A61601B D-6529-1 CH36216B: A61602B D-6529-1 AU11145B: A61603B D-6522-1 AU11147B: A61605B D-6522-1 AU11155B: A61613B D-6522-1 AY520B: A61743B D-6522-2 AU11175B: A61893B D-6522-1 These propellers are installed on, but not limited to the following: AMERICAN CHAMPION 8GCBC, 8KCAB AERMACCHI S.p.A. S.208, S.208A BEECH 95 series BELLANCA 14-19-3, 14-19-3A CESSNA 170 series, 172 series, 175 series, 177, A188A, A188B, T188C, 310 series DIAMOND AIRCRAFT DA-40 LAKE (REVO) LA-4, LA-4-200 MAULE Aerospace Technology, Inc. M(T)-7-235( ), M-5-235C, M-6-235, M(X)-7-235 MOONEY M20 series Pilatus BRITTEN-NORMAN LTD BN-2 series, MK III, MK III-2, MK III-3 PIPER PA-23, PA-23-160, PA-24, PA-24-260, PA-25-260, PA-28-140, PA-32-300, PA-32S-300, PA-34-200, PA-44-180T SOCATA--Groupe AEROSPATIALE MS-200, MS 894A, MS 894E, TB-20, TB-21 Sky International Inc (Husky) A-1, S-1T, S-2A, S-2S (previous owners were Christian Industries; Aviat, Inc.; White International, LTD.) Univair Aircraft Corporation 108 series (previous owner was Stinson) Vulcanair S.p.A. P68 series (previous owner was Partenavia Construzioni Aeronautiche S.p.A)
- 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 2001-23-10 One-time
Raytheon Aircraft Company 33, T-34, 35, 36, 55, 56, 58, and 95 Series 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 (f) 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. (g) Where can I get information about any already-approved alternative methods of compliance? Contact Paul DeVore, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4142; facsimile: (316) 946-4407. (h) 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 sections 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. You must adhere to the limitations presented in the appendix to this AD. (i) Are any service bulletins incorporated into this AD by reference? Actions required by this AD must be done in accordance with Raytheon Mandatory Service Bulletin SB 27-3478, Issued: September 2001. The Director of the Federal Register approved this incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51. You can get copies from Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676- 3140. You may view this information at 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. (j) When does this amendment become effective? This amendment becomes effective on December 13, 2001. Appendix to Docket No. 2001-CE-35-AD The following must be adhered to in order to obtain a special flight permit as specified in paragraph (h). Limitations--Flaps must be retracted for all takeoffs. Emergency Procedures Asymmetrical Flaps Attempt to retract the flaps. If flaps will not retract, the airplane will have a tendency to roll in the direction of the retracted flap. This roll tendency will increase with increasing speed. Use aileron trim and reduce speed as required to reduce roll forces. Flaps-Up or Asymmetrical-Flap Landing Follow all published Before Landing Procedures except for airspeed. Maintain the published Flaps-Up Approach Speed. If this speed is not published, use one of the following: (a) Multiply the highest indicated flaps-up stall speed, found in the Performance Section, by 1.3. or (b) For Bonanza Series, T-34A, T-34B, and 45, add 10 knots to the published Flaps-Down Landing Approach Speed. (c) For Baron Series, add 15 knots to the published Flaps-Down Landing Approach speed. Plan on longer landing distance. Issued in Kansas City, Missouri, on November 13, 2001. James E. Jackson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-29019 Filed 11-20-01; 8:45 am] BILLING CODE 4910-13-P
- AD 2000-18-02 One-time
Raytheon Aircraft Company Models A65, A65-8200, 65-B80, 70, 95-A55, 95-B55, 95-C55, D55, E55, 56TC, A56TC, 58, 58P, 58TC, and 95-B55B (T42A) 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 Gary D. Park, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (314) 946-4123; facsimile: (314) 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 sections 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, provided that the following is complied with: (1) Pass the tap test inspection specified in Raytheon Mandatory Service Bulletin SB 27-3396, Rev. 1, Revised: June, 2000; and (2) Restrict airspeed to maneuvering speed. (h) Are any service bulletins incorporated into this AD by reference? You must accomplish the replacement required by this AD in accordance with Raytheon Mandatory Service Bulletin SB 27-3396, Rev. 1, Revised: June, 2000. The Director of the Federal Register approved this incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51. You can get copies from Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201. You can look at copies at 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 September 22, 2000. Issued in Kansas City, Missouri, on August 24, 2000. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 00-22427 Filed 9-6-00; 8:45 am] BILLING CODE 4910-13-U
- AD 98-21-21 One-time Appliance
Bob Fields Aerocessories Inflatable Door Seals
To prevent smoke and a possible fire in the cockpit caused by overheating of the electric door seal inflation systems, which could result in passenger injury.
Applicability, as the AD words it
Inflatable door seals, installed either in accordance with the applicable supplemental type certificate (STC) or through field approval, that are installed on, but not limited to, the following aircraft: Affected STC Make and model aircraft affected SA3735NM: Cessna Models 170, 170A, and 170B Airplanes. SA4136WE: Cessna Models 310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, 310I, 310J, 310K, 310L, 310N, 310P, 310Q, 310R, T310P, T310Q, and T310R Airplanes. SA2226NM: Cessna Models P210N and P210R Airplanes. SA3736NM: Cessna Models 185, 185A, 185B, 185C, 185D, A185E, and A185F Airplanes. SA4177WE: Cessna Models 175, 175A, 175B, and 175C Airplanes. SA4212WE: Cessna Models 210, 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N, 210-5 (205), and 210-5A (205A) Airplanes. SA4213WE: Cessna Models 310, 310A, 310B, 310C, 310D, 310F, 310G, 310H, 310I, 310J, 310K, 310L, 310N, 310P, 310Q, 310R, T310P, T310Q, and T310R Airplanes. SA4283WE: Cessna Models 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, and 172N Airplanes. SA4284WE: Cessna Models 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, and 180K Airplanes. SA4285WE: Cessna Models 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, R182, and TR182 Airplanes. SA4286WE: Cessna Models 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, and TU206G Airplanes. SA4287WE: Cessna Models 320, 320A, 320B, 320C, 320D, 320E, 320F, and 320-1 Airplanes. SA4180WE: Raytheon (Beech) Models 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, and B36TC Airplanes. SA4184WE: Raytheon (Beech) Models 95, B95, B95A, E95, 95-55, 95-A55, 95-B55, 95-B5A, 95- B55B, 95-C55, D55, E55, 56TC, 58, and 58A Airplanes. SA4239WE: Raytheon (Beech) Models 58P, 58PA, 58TC, and 58TCA Airplanes. SA4240WE: Raytheon (Beech) Models 50, B50, C50, D50, D50A, D50B, D50C, D50E, D50E-5990, E50, F50, G50, H50, and J50 Airplanes. SA4282WE: Raytheon (Beech) Models 35, A35, B35, C35, D35, E35, F35, G35, and 35R Airplanes. SA4178WE: Mooney Models M20, M20A, M20C, M20D, M20E, M20F, M20G, M20J, and M20K Airplanes. SA4472NM: Aerostar Models PA-60-601P, PA-60-602P, and PA-60-700P Airplanes. SA4234WE: The New Piper Aircraft, Inc. (Piper) Models PA-34-200, PA-34-200T, and PA-34- 220T Airplanes. SA4179WE: Piper Models PA-24, PA-24-250, PA-24-260, and PA-24-400 Airplanes. SA4235WE: Piper Models PA-44-180 and PA-44-180T Airplanes. SA4236WE: Piper Models PA-28-140, PA-28-150, PA-28- 160, PA-28-180, PA-28-235, PA-28-151, PA- 28-181, PA-28-161, PA-28-236, PA-28- 201T, PA-285-160, PA-28S-160, PA-28S- 180, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, and PA-28RT- 201T Airplanes. SA4237WE: Piper Models PA-23, PA-23-160, PA-23-235, PA-23-250, and PA-E23-250 Airplanes. SA4238WE: Piper Models PA-30, PA-39, and PA-40 Airplanes. SA4385WP: Piper Models PA-31, PA-31-300, PA-31-325, and PA-31-350 Airplanes. SA4288WE: Piper Models PA-32-260, PA-32-300, PA-32S- 300, PA-32-301, PA-32-301T, PA-32R-300, PA-32R-301, PA-32R-301T, PA-32RT-300, and PA-32RT-300T Airplanes. SA2511NM: Bellanca Models 17-30, 17-31, and 17-31TC Airplanes. SA2510NM: Bellanca Models 17-30A, 17-31A, and 17- 31ATC Airplanes. SA4316WE: Wing Aircraft Company Model D-1 Airplanes.
- AD 97-21-02 One-time Engine
Teledyne Continental Motors E-165, E- 185, E-225, O-470 and IO-470 Series Reciprocating Engines
To prevent extreme side loading of the piston, and consequent failure of the piston and engine.
Applicability, as the AD words it
Teledyne Continental Motors (TCM) new and rebuilt Model O-470 and IO-470 series reciprocating engines with serial numbers (S/Ns) listed in Table 1 of TCM Critical Service Bulletin (CSB) No. CSB97-10A, dated July 15, 1997; and TCM Model E-165, E- 185, E-225, O-470 and IO-470 series reciprocating engines, regardless of S/N, which have cylinder(s) with part number and purchase date as shown in Table 2 of TCM CSB No. CSB97-10A, dated July 15, 1997. These engines are installed on but not limited to the following aircraft: Bellanca Models 14-19-2 and 14-19-3; Cessna Models 180, 180A through K, 182, 182A through R, 185, 185A through E, 188, 188A, 188B, 210, 210A through C, 210-5 (205), 210-5A (205A), 305A, 305C, 305D, 305F, 310, 310A through Q, E310H, E310J, 310J-1; Frontier-Aerospace, Inc. (Fletcher) Models FU-24 and FU-24A; Luscombe Aircraft Corporation Model 11A; Navion models Navion, Navion A, and Navion D through G; Prop-Jets, Inc. Models 200, 200A through C; Raytheon (formerly Beech) Models 35, A35 through P35, 35R, 35-33, 35-A355, 35-B33, 35-C33, E33, F33, 45 (YT-34), A45 (T- 34A, B-45), D45 (T-34B), 95-55, 95-55A, 95-B55, 95-B55A and 95-B55B; Reims models F182P and F182Q; and Twin Commander Aircraft, Inc. Model 500-A.
- AD 97-18-02 Recurring Propeller
Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers With Aluminum Blades
To prevent blade separation due to cracked blades, hubs, or blade clamps, which can result in loss of control of the airplane.
Applicability, as the AD words it
Hartzell Propeller Inc. ()HC-()(2,3)(X,V)()-() series and HA-A2V20-1B series propellers with aluminum blades. These propellers are installed on but not limited to the following aircraft: Manufacturer Aircraft Model Aero Commander (Twin Commander) 500 AERO COMMANDER 500A AERO COMMANDER 500B, 500S, 500U AERO COMMANDER 520 AERO COMMANDER 560 AERO COMMANDER 560A, 560E AERO COMM. 680, 680E, 720 AERO COMM. 680F, FP, FL, FLR AERO COMMANDER B1 (CALLAIR) Aeromere FALCO F.8.L Aeronautica Macchi AL60-F5 AM-3 Bauger SAIL PLANE Beech 35 SERIES BONANZA 35-C33 DEBONAIR 35-C33A, E33A, F33A 50 SERIES TWIN BONANZA 58P, 58TC BARON 95-55, 95-A55, 95-B55 BARON 65, A65, 65-(B)80, 65-A80, 70 A65-8200, 70 Bellanca 14-13 14-19 14-19-2 14-19-3 7GCA, 7GCB, 7GCC DW-1 EAGLE Camair 480 Cessna 170 170A 172 SKYHAWK 175 180, A, B, C, D, E, F, G, H 182, A, B, C, D, E 182F, G, H, J, K, L, M 210, A, B, C, 5, 5A 310, 310A 310B, 310C 310D, E, F, G, H, E310H 320, 320-1 SKYKNIGHT 320A, 320B 402 BUSINESSLINER 411 WREN 460 WREN 460H, J, K, L, M deHavilland DH104 DOVE DH114 HERON Dornier DO27Q-6 DO28A-1 DO28B-1 Fuji T-3, LM-2 GAF--Gov't. Aircraft Factories N22B, N24A, N22S, N22C Goodyear (Loral) GA22A GOODYEAR BLIMP GZ19, 19A GOODYEAR BLIMP Great Lakes 2T-1A-2 Grumman G44, G44A WIDGEON G21C, D GOOSE Helio H-391 COURIER H-391B COURIER H-395A COURIER Luscombe 11 11A Mooney M20 Multitech (Temco) D16 TWIN NAVION D16A TWIN NAVION Nardi FN-333 Navion NAVION B NAVION, NAVION A Pacific Aerospace (Fletcher) FU-24, FU-24A Piaggio P-149D P136-L1 ROYAL GULL P136-L2 ROYAL GULL P149D P166 ROYAL GULL Pilatus PC-3 PC-6; PC-6-H1, -H2 PORTER Piper PA-E23-250 AZTEC PA14 FAMILY CRUISER PA18(A)(S)-150 SUPER CUB PA18A-150 SUPER CUB PA22-150, PA22S-150 TRIPACER PA23 SERIES APACHE PA23-160 APACHE PA23-235 AZTEC PA23-250 AZTEC PA24-250 COMANCHE PA24-400 COMANCHE PA24S COMANCHE PA28 CHEROKEE PA28-140 CHEROKEE Prop Jets Inc. 200 200A,B,C Republic (STOL Amphibian) RC3 SEABEE Scottish Aviation (BAE) B.206 SERIES 2 BEAGLE Stinson L-5 108, -1, -2, -3 108-2-3 Sud Aviation (SOCATA) GY.80-150 GARDAN GY.80-160 GARDAN HORIZON Swift GC-1B Taylorcraft 20 Texas Bullet 205 Windecker EAGLE
- AD 97-14-15 One-time
Raytheon Aircraft Company (Formerly Known as Beech Aircraft Corporation) Models E33, F33, G33, E33A, F33A, E33C, F33C, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, V35TC, V35ATC, V35BTC, 36, A36, A36TC, B36TC, 50, B50, C50, 95-55, 95A55, 95B55, 95C55, D55, E55, 56TC, A56TC, 58, 58TC, 95, B95, B95A, D95A, and E95 Airplanes
To prevent unintentional opening of the cabin side door and the utility door from the interior of the airplane, which if not detected and corrected, could result in loss of control of the airplane.
Applicability, as the AD words it
Models E33, F33, G33, E33A, F33A, E33C, F33C, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, V35TC, V35ATC, V35BTC, 36, A36, A36TC, B36TC, 50, B50, C50, 95-55, 95A55, 95B55, 95C55, D55, E55, 56TC, A56TC, 58, 58TC, 95, B95, B95A, D95A, and E95 airplanes (all serial numbers), certificated in any category.
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.