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.
N407PC is a 1996 Beechcraft A36 in the FAA registry (aircraft page). Matched on type certificate model A36.
RESULTS
31 ADs in effect may apply to N407PC
- In effect31
- Recurring6
- Superseded or removed4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.
Show only ADs in effect N407PC’s registration record
- AD 2019-23-10 One-time
Textron Aviation Inc. (Type Certificate Previously Held by Beechcraft Corporation) Airplanes
This AD was prompted by reports of cracked and fractured right aileron flight control cable end fittings (terminal attachment fittings).
Applicability, as the AD words it
This AD applies to the following Textron Aviation Inc. (Type Certificate previously held by Beechcraft Corporation) airplanes, certificated in any category: (1) Models E33, E33A, E33C, F33, G33, 35-C33, 35-C33A, S35, V35, V35A, and 36, all serial numbers (S/Ns); (2) Model F33A, S/Ns CE-290 through CE-680; (3) Model F33C, S/Ns CJ-26 through CJ-128; (4) Model V35B, S/Ns D-9069 through D-9961; and (5) Model A36, S/Ns E-185 through E-925.
- AD 2019-21-08 Superseded by AD 2019-23-10
Textron Aviation Inc. (Type Certificate Previously Held by Beechcraft Corporation) Airplanes
This AD was prompted by reports of cracked and fractured right aileron flight control cable end fittings (terminal attachment fittings).
Applicability, as the AD words it
This AD applies to the following Textron Aviation Inc. (Type Certificate previously held by Beechcraft Corporation) airplanes, certificated in any category: (1) Models E33, E33A, E33C, F33, G33, 35-C33, 35-C33A, K35, M35, N35, P35, S35, V35, V35A, and 36, all serial numbers (S/Ns); (2) Model F33A, S/Ns CE-290 through CE-680; (3) Model F33C, S/Ns CJ-26 through CJ-128; (4) Model V35B, S/Ns D-9069 through D-9961; and (5) Model A36, S/Ns E-185 through E-925.
- AD 2010-13-10 One-time Propeller
Ontic Engineering and Manufacturing, Inc. Propeller Governors, Part Numbers C210776, T210761, D210760, and J210761
We are issuing this AD to prevent loss of propeller pitch control, damage to the propeller governor, and internal damage to the engine, which could prevent continued safe flight or safe landing.
Applicability, as the AD words it
This AD applies to Ontic Engineering and Manufacturing, Inc. propeller governors, part numbers (P/Ns) C210776, T210761, D210760, and J210761, as listed by serial number on pages 3 and 4 of Ontic Engineering and Manufacturing, Inc. Mandatory Service Bulletin (MSB) No. SB-DES-353, Revision A, dated December 16, 2009. (d) These propeller governors are installed on, but not limited to, American Champion Aircraft Corporation Model 7GCAA (governor P/N T210761), Diamond Aircraft Industries, Inc. Model DA-40 (governor P/ N C210776), Hawker Beechcraft Model A36 (governor P/N D210760), and Industria Aeronautica Neiva S/A (subsidiary of Embraer) model EMB- 202A (governor P/N J210761) airplanes.
- 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.
- AD 2009-16-03 Superseded by AD 2014-05-29 Engine
Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating Engines With Superior Air Parts, Inc. (SAP) Cylinder Assemblies Installed
We are issuing this AD to prevent the separation of the cylinder head, which could result in immediate loss of engine power, possible structural damage to the engine, and possible fire in the engine compartment.
Applicability, as the AD words it
This AD applies to Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 series reciprocating engines with SAP investment cast cylinder assemblies, part numbers (P/Ns) SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P, installed. These engines are installed on, but not limited to, the airplanes listed in Table 1 of this AD. Table 1--Teledyne Continental Motors-Related Aircraft Models Engine model Aircraft manufacturer Aircraft model designation IO-520-A: Cessna: 210 D, E, F, G, & H. IO-520-A: Cessna: 206. IO-520-A: Cessna: P206. IO-520-A: Rockwell: 200 D. IO-520-B: Beechcraft: 36 Bonanza. IO-520-B: Beechcraft: A36. IO-520-B: Navion: Range Master. IO-520-BA: Beechcraft: A36. IO-520-BA: Beechcraft: S & V35, V35A, V35B. IO-520-BA: Beechcraft: C33 A. IO-520-BA: Beechcraft: E33 A & C. IO-520-BA: Beechcraft: F33 A & C. IO-520-BA: Navion: Range Master. IO-520-BB: Beechcraft: A36. IO-520-BB: Beechcraft: V35B. IO-520-BB: Beechcraft: F33 A. IO-520-C & CB: Beechcraft: C55-E55 Baron. IO-520-D: Bellanca: 17-30 Viking. IO-520-D: Cessna: A188-300 AG Truck. IO-520-D: Cessna: 185. IO-520-E: (Cessna 310): Exec 600. IO-520-E: (Beech Baron): Pres 600. IO-520-F: Cessna: 207. IO-520-F: Cessna: U206. IO-520-K: Bellanca: 17-30A. IO-520-L: Cessna: 210 K, L, M, N & R. IO-520-L: Cessna: 210N II. IO-520-L: Cessna: 210R. IO-520-M: Cessna: 310R. IO-520-MB: Cessna: 310R. IO-550-A: Cessna: 310 Conversion. IO-550-B: Beechcraft: A36. IO-550-B: (Beech Bonanza): Foxstar. IO-550-C: Beechcraft: 58 Baron. IO-550-D: Cessna: 185/188 Conversion. IO-550-E: Cessna: 310 Conversion. IO-550-F: Cessna: 206/207 Conversion. IO-550-L: Cessna: 210 Conversion.
- 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).
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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.
- 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.
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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 2007-08-04 One-time Propeller
McCauley Propeller Systems Models 3A32C406/82NDB-X and D3A32C409/82NDB-X Propellers
We are issuing this AD to prevent blade or hub failure that could result in separation of a propeller blade and loss of control of the airplane.
Applicability, as the AD words it
This AD applies to McCauley Propeller Systems models 3A32C406/82NDB-X and D3A32C409/82NDB-X propellers, herein referred to as C406 and C409 propellers, respectively. These propellers are installed on, but not limited to, the airplanes in the following Table 1: Table 1.--Airplanes That Propellers Are Installed On, But Not Limited To Airplane models With engine model Beech: A35, B35, C35, D35, E35, F35, G35, Teledyne Continental Motors H35, J35, K35, M35, N35, P35, S35, (TCM) IO-520 series and IO-550 V35, V35A, V35B, 35-33, 35-A33, 35- series reciprocating engines. B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, 36, A36, A45, and D45. Beech: A36TC, B36TC, S35, V35A, V35B: TCM TSIO-520 series reciprocating engines. Navion: A (L-17B, C), B, D, E, F, G, and H. TCM IO-550 and TSIO-520 series reciprocating engines.
- AD 2007-04-19R1 One-time Appliance
Superior Air Parts, Inc. (SAP), Cylinder Assemblies Part Numbers Series: SA47000L, SA47000S, SA52000, SA55000, SL32000W, SL32000WH, SL32006W, SL36000TW, SL36000W, and SL36006W
We are issuing this AD to prevent cylinder separation that can lead to engine failure, a possible engine compartment fire, and damage to the airplane.
Applicability, as the AD words it
This AD applies to Superior Air Parts, Inc. (SAP), cylinder assemblies, manufactured between April 2005 and November 2005, part numbers (P/Ns): SA47000L-A1, SA47000L-A20P, SA47000S-A1, SA47000S- A20P, SA47000S-A21P, SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, and SA55000-A20P, installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines. These P/N cylinder assemblies may be installed in the TCM engine models listed in the following Table 1. Table 1.--Affected Teledyne Continental Engine Models Engine model O-470: -G, -K, -L, -M, -P, -R, -S, - U. IO-470: -C, -D, -E, -F, -G, -H, -L, - M, -N, -P, -R, -S, -U, -V. IO-520: -A, B, BA, C, CB, D, E, F, J, K, L, M, BB, MB. TSIO-520: -AF, B, BB, C, CE, D, DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, UB, VB, WB. IO-550: -A, B, C, D, E, F, L. These engine models are installed in, but not limited to, the aircraft models listed in the following Table 2: Table 2.--Teledyne Continental Motors-Related Aircraft Models Engine model Aircraft manufacturer Aircraft model designation IO-470-C: Beechcraft: J, K, M35. IO-470-D: Cessna: 310 G & H. IO-470-D: Rockwell: 200 A, B, & C. IO-470-E: Cessna: 210 & A. IO-470-F: Bellanca: 14-19-3. IO-470-F: Cessna: 185. IO-470-H: Sierra Hotel Aero, Navion F & G (Rangemaster). Inc. (Navion). IO-470-L: Beechcraft: B55 Baron. IO-470-M: Gulfstream: 500 A. IO-470-N: Beechcraft: N & P. IO-470-N: Beechcraft: G33. IO-470-S: Cessna: 210 B & C. IO-470-S: Cessna: 205. IO-470-U: Cessna: 310 I & J. IO-470-V/VO: Cessna: 310K, L, N, P & Q. IO-520-A: Cessna: 210 D, E, F, G, & H. IO-520-A: Cessna: 206. IO-520-A: Cessna: P206. IO-520-A: Rockwell: 200 D. IO-520-B: Beechcraft: 36 Bonanza. IO-520-B: Beechcraft: A36. IO-520-B: Sierra Hotel Aero, Navion H. Inc. (Navion). IO-520-BA: Beechcraft: A36. IO-520-BA: Beechcraft: S & V35, V35A, V35B. IO-520-BA: Beechcraft: C33 A. IO-520-BA: Beechcraft: E33 A & C. IO-520-BA: Beechcraft: F33 A & C. IO-520-BA: Sierra Hotel Aero, Navion G (Rangemaster). Inc.. IO-520-BA: Sierra Hotel Aero, Navion H. Inc.. IO-520-BB: Beechcraft: A36. IO-520-BB: Beechcraft: V35B. IO-520-BB: Beechcraft: F33 A. IO-520-C & CB: Beechcraft: C55-E55 Baron. IO-520-D: Bellanca: 17-30 Viking. IO-520-D: Cessna: A188-300 AG Truck. IO-520-D: Cessna: 185. IO-520-E: (Cessna 310): Exec 600. IO-520-E: (Beech Baron): Pres 600. IO-520-F: Cessna: 207. IO-520-F: Cessna: U206. IO-520-K: Bellanca: 17-30A. IO-520-L: Cessna: 210 K, L, M, N & R. IO-520-L: Cessna: 210N II. IO-520-L: Cessna: 210R. IO-520-M: Cessna: 310R. IO-520-MB: Cessna: 310R. IO-550-A: Cessna: 310 Conversion. IO-550-B: Beechcraft: A36. IO-550-B: (Beech Bonanza): Foxstar. IO-550-C: Beechcraft: 58 Baron. IO-550-D: Cessna: 185/188 Conversion. IO-550-E: Cessna: 310 Conversion. IO-550-F: Cessna: 206/207 Conversion. IO-550-L: Cessna: 210 Conversion. O-470-M: Cessna: 310. O-470-G: Beechcraft: H35. O-470-K: Bellanca: 14-19-2. O-470-K: Cessna: 180 (230 HP). O-470-L: Cessna: 182. O-470-L: Cessna: 180D. O-470-M: Cessna: 310 B. O-470-P: Sierra Hotel Aero, Navion. Inc. (Navion). O-470-R: Cessna: 188-230. O-470-R: Cessna: 182. O-470-R: Cessna: 180 E-J. O-470-S: Cessna: 182. O-470-U: Cessna: 182. O-470-U: Cessna: 180 K. TSIO-520-AF: Cessna: P210N II. TSIO-520-B: Cessna: 320D, E & F. TSIO-520-B: Cessna: T310-Q & R. TSIO-520-BB: Cessna: T310R. TSIO-520-BE: Piper: PA-46-310 Malibu. TSIO-520-C: Cessna: T210 F, G, & H. TSIO-520-C: Cessna: TU206. TSIO-520-C: Cessna: TP206. TSIO-520-C&CB: Beechcraft: 58 Baron. TSIO-520-CE: Cessna: T210R. TSIO-520-CF: Cessna: P210R. TSIO-520-D: Beechcraft: V35, V35A, V35B-TC. TSIO-520-E: Cessna: 402, A & B. TSIO-520-E: Cessna: 401, A & B. TSIO-520-EB: Cessna: 335. TSIO-520-G: Cessna: T207. TSIO-520-H: Cessna: T210 J, K & L. TSIO-520-J: Cessna: 210 J. TSIO-520-J: Cessna: 414. TSIO-520-J: Riley Conversions: 340 Super Riley. TSIO-520-L&LB: Beechcraft: 58P Baron. TSIO-520-L&LB: Beechcraft: 58TC Baron. TSIO-520-M: Cessna: T207. TSIO-520-M: Cessna: TU206. TSIO-520-N: Cessna: 414-II Chancellor. TSIO-520-N: Cessna: 340. TSIO-520-NB: Cessna: 414-II. TSIO-520-NB: Cessna: 340. TSIO-520-P: Cessna: P210N. TSIO-520-R: Cessna: T210 M. TSIO-520-R: Cessna: T210N II. TSIO-520-T: Cessna: T188C AG Husky. TSIO-520-UB: Beechcraft: A36TC Bonanza. TSIO-520-UB: Beechcraft: B36TC. TSIO-520-VB: Cessna: 402 C. TSIO-520-WB: Beechcraft: 58P Baron. TSIO-520-WB: Beechcraft: 58TC Baron. This AD also applies to SAP, cast cylinder assemblies, P/Ns SL32000W-A1, SL32000W-A20P, SL32000W-A21P, SL32000WH-A1, SL32000WH- A20P, SL32006W-A1, SL32006W-A20P, SL32006W-A21P, SL36000TW-A1, SL36000TW-A20P, SL36000TW-A21P, SL36000TW-A22P, SL36000W-A1, SL36000W-A20P, SL36000W-A21P, SL36006W-A1, SL36006W-A20P, and SL36006W-A21P, installed in Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines and Avco Lycoming 540 series reciprocating engines. These P/N cylinder assemblies may be installed in the LE and AL engine models listed in the following Table 3. Table 3.--Affected Lycoming Engines and Avco Lycoming Engine Models Engine model O-320: -A, -B, -C, -D, -E, H. IO-320: -B, -D, -E. LIO-320: -B. AIO-320: -A, -B, -C. AEIO-320: -D, -E. O-360: -A, -B, -C, -D, -F, -G, -J. IO-360: -B, -L, -M. LO-360: -A. AEIO-360: -B, -H. HO-360: -C. HIO-360: -B. O-540: -A, -B, -E, -F, -G, -H, -J. IO-540: -A, -C, -D, -N, -T, -V, -W. AEIO-540: -D. These engine models are installed in, but not limited to, the aircraft models listed in the following Table 4: Table 4.--Lycoming Engines and Avco Lycoming-Related Aircraft Models Engine model Aircraft manufacturer Aircraft model designation O-320-A: Mooney Aircraft: Mark 20A. O-320-A1A: Piper Aircraft: PA-23-150 Apache. O-320-A1A: Piper Aircraft: PA-22-150 Tri-Pacer. O-320-A1A: Piper Aircraft: PA-22S-150 Tri-Pacer. O-320-A1A: Piper Aircraft: PA-25 Pawnee. O-320-A1A: Doyne Aircraft: Doyn-Cessna 170,170A,170B. O-320-A1A: Dinfia: Ranquel 1A-46. O-320-A1A: Simmering-Graz Pauker Flamingo SGP-M-222. O-320-A1A: …
- AD 2007-04-19 One-time Appliance
Superior Air Parts, Inc. (SAP), Cast Cylinder Assemblies Part Numbers Series: SA47000L, SA47000S, SA52000, SA55000, SL32000W, SL32000WH, SL32006W, SL36000TW, SL36000W, and SL36006W
We are issuing this AD to prevent cylinder separation that can lead to engine failure, a possible engine compartment fire, and damage to the airplane.
Applicability, as the AD words it
This AD applies to Superior Air Parts, Inc. (SAP), cast cylinder assemblies, part numbers (P/Ns): SA47000L-A1, SA47000L- A20P, SA47000S-A1, SA47000S-A20P, SA47000S-A21P, SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, SA55000-A20P installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines. These P/N cylinder assemblies may be installed in the TCM engine models listed in the following Table 1. Table 1.--Affected Teledyne Continental Engine Models Engine model O-470: -G, -K, -L, -M, -P, -R, -S, -U. IO-470: -C, -D, -E, -F, -G, -H, -L, -M, -N, -P, -R, -S, -U, -V. IO-520: -A, B, BA, C, CB, D, E, F, J, K, L, M, BB, MB. TSIO-520: -AF, B, BB, C, CE, D, DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, UB, VB, WB. IO-550: -A, B, C, D, E, F, L. These engine models are installed in, but not limited to, the aircraft models listed in the following Table 2: Table 2.--Teledyne Continental Motors-Related Aircraft Models Aircraft Aircraft model Engine model manufacturer designation IO-470-C: Beechcraft: J, K, M35. IO-470-C: Navion: Navion. IO-470-D: Cessna: 310 G & H. IO-470-D: Rockwell: 200 A, B, & C. IO-470-E: Cessna: 210 & A. IO-470-F: Bellanca: 14-19-3. IO-470-F: Cessna: 185. IO-470-H: Navion: Range Master. IO-470-L: Beechcraft: B55 Baron. IO-470-M: Gulfstream: 500 A. IO-470-N: Beechcraft: N & P. IO-470-N: Beechcraft: G33. IO-470-S: Cessna: 210 B & C. IO-470-S: Cessna: 205. IO-470-U: Cessna: 310 I & J. IO-470-V/VO: Cessna: 310K, L, N, P, & Q. IO-520-A: Cessna: 210 D, E, F, G, & H. IO-520-A: Cessna: 206. IO-520-A: Cessna: P206. IO-520-A: Rockwell: 200 D. IO-520-B: Beechcraft: 36 Bonanza. IO-520-B: Beechcraft: A36. IO-520-B: Navion: Range Master. IO-520-BA: Beechcraft: A36. IO-520-BA: Beechcraft: S & V35, V35A, V35B. IO-520-BA: Beechcraft: C33 A. IO-520-BA: Beechcraft: E33 A & C. IO-520-BA: Beechcraft: F33 A & C. IO-520-BA: Navion: Range Master. IO-520-BB: Beechcraft: A36. IO-520-BB: Beechcraft: V35B. IO-520-BB: Beechcraft: F33 A. IO-520-C & CB: Beechcraft: C55-E55 Baron. IO-520-D: Bellanca: 17-30 Viking. IO-520-D: Cessna: A188-300 AG Truck. IO-520-D: Cessna: 185. IO-520-E: (Cessna 310): Exec 600. IO-520-E: (Beech Baron): Pres 600. IO-520-F: Cessna: 207. IO-520-F: Cessna: U206. IO-520-K: Bellanca: 17-30A. IO-520-L: Cessna: 210 K, L, M, N, & R. IO-520-L: Cessna: 210N II. IO-520-L: Cessna: 210R. IO-520-M: Cessna: 310R. IO-520-MB: Cessna: 310R. IO-550-A: Cessna: 310 Conversion. IO-550-B: Beechcraft: A36. IO-550-B: (Beech Bonanza)... Foxstar. IO-550-C: Beechcraft: 58 Baron. IO-550-D: Cessna: 185/188 Conversion. IO-550-E: Cessna: 310 Conversion. IO-550-F: Cessna: 206/207 Conversion. IO-550-L: Cessna: 210 Conversion. O-470-M: Cessna: 310. O-470-G: Beechcraft: H35. O-470-K: Bellanca: 14-19-2. O-470-K: Cessna: 180 (230 HP). O-470-L: Cessna: 182. O-470-L: Cessna: 180D. O-470-M: Cessna: 310 B. O-470-P: Navion: Navion. O-470-R: Cessna: 188-230. O-470-R: Cessna: 182. O-470-R: Cessna: 180 E-J. O-470-S: Cessna: 182. O-470-U: Cessna: 182. O-470-U: Cessna: 180 K. TSIO-520-AF: Cessna: P210N II. TSIO-520-B: Cessna: 320D, E & F. TSIO-520-B: Cessna: T310-Q & R. TSIO-520-BB: Cessna: T310R. TSIO-520-BE: Piper: PA-46-310 Malibu. TSIO-520-C: Cessna: T210 F, G, & H. TSIO-520-C: Cessna: TU206. TSIO-520-C: Cessna: TP206. TSIO-520-C&CB: Beechcraft: 58 Baron. TSIO-520-CE: Cessna: T210R. TSIO-520-CF: Cessna: P210R. TSIO-520-D: Beechcraft: V35, V35A, V35B- TC. TSIO-520-E: Cessna: 402, A & B. TSIO-520-E: Cessna: 401, A & B. TSIO-520-EB: Cessna: 335. TSIO-520-G: Cessna: T207. TSIO-520-H: Cessna: T210 J, K, & L. TSIO-520-J: Cessna: 210 J. TSIO-520-J: Cessna: 414. TSIO-520-J: Riley Conversions. 340 Super Riley. TSIO-520-L&LB: Beechcraft: 58P Baron. TSIO-520-L&LB: Beechcraft: 58TC Baron. TSIO-520-M: Cessna: T207. TSIO-520-M: Cessna: TU206. TSIO-520-N: Cessna: 414-II Chancellor. TSIO-520-N: Cessna: 340. TSIO-520-NB: Cessna: 414-II. TSIO-520-NB: Cessna: 340. TSIO-520-P: Cessna: P210N. TSIO-520-R: Cessna: T210 M. TSIO-520-R: Cessna: T210N II. TSIO-520-T: Cessna: T188C AG Husky. TSIO-520-UB: Beechcraft: A36TC Bonanza. TSIO-520-UB: Beechcraft: B36TC. TSIO-520-VB: Cessna: 402 C. TSIO-520-WB: Beechcraft: 58P Baron. TSIO-520-WB: Beechcraft: 58TC Baron. This AD also applies to SAP, cast cylinder assemblies, P/Ns SL32000W-A1, SL32000W-A20P, SL32000W-A21P, SL32000WH-A1, SL32000WH- A20P, SL32006W-A1, SL32006W-A20P, SL32006W-A21P, SL36000TW-A1, SL36000TW-A20P, SL36000TW-A21P, SL36000TW-A22P, SL36000W-A1, SL36000W-A20P, SL36000W-A21P, SL36006W-A1, SL36006W-A20P, and SL36006W-A21P installed in Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines and Avco Lycoming 540 series reciprocating engines. These P/N cylinder assemblies may be installed in the LE and AL engine models listed in the following Table 3. Table 3.--Affected Lycoming Engines and Avco Lycoming Engine Models Engine model O-320: -A, -B, -C, -D, -E, H. IO-320: -B, -D, -E. LIO-320: -B. AIO-320: -A, -B, -C. AEIO-320: -D, -E. O-360: -A, -B, -C, -D, -F, -G, -J. IO-360: -B, -L, -M. LO-360: -A. AEIO-360: -B, -H. HO-360: -C. HIO-360: -B. O-540: -A, -B, -E, -F, -G, -H, -J. IO-540: -A, -C, -D, -N, -T, -V, -W. AEIO-540: -D. These engine models are installed in, but not limited to, the aircraft models listed in the following Table 4: Table 4.--Lycoming Engines and Avco Lycoming-Related Aircraft Models Aircraft Aircraft model Engine model manufacturer designation O-320-A: Mooney Aircraft.. Mark 20A. O-320-A1A: Piper Aircraft... PA-23-150 Apache. O-320-A1A: Piper Aircraft... PA-22-150 Tri-Pacer. O-320-A1A: Piper Aircraft... PA-22S-150 Tri-Pacer. O-320-A1A: Piper Aircraft... PA-25 Pawnee. O-320-A1A: Doyne Aircraft... Doyn-Cessna 170,170A,170B. O-320-A1A: Dinfia: Ranquel 1A-46. O-320-A1A: Simmering-Graz Flamingo SGP-M-222. Pauker. O-320-A1A: Aviamilano: Scricciolo P-19. O-320-A1A: Vos Helicopter Co Spring Bok. O-320-A1A: Mooney Aircraft.. Mark 20A. O-320-A1B: Piper Aircraft... PA-22-150 Tri-Pacer. O-320-A1B: Piper …
- AD 2006-03-08 One-time Appliance
Aero Advantage ADV200 Series (Part Numbers ADV211CC and ADV212CW) Vacuum Pumps
Applicability, as the AD words it
This AD affects ADV200 series (part numbers (P/Ns) ADV211CC and ADV212CW) vacuum pumps installed on, but not limited to, the following aircraft that are certificated in any category. These vacuum pumps can be installed under supplemental type certificate number SA10126SC, through field approval, or other methods: Make Model Alexandria Aircraft, LLC: 14-19, 14-19-2, 14-19-3, 17-30, 17-31, 17-31TC, 17-30A, 17-31A, and 17- 31ATC. Alliance Aircraft Group, LLC: H-295 (USAF U10D). American Champion Aircraft Corp: 7AC, 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBC, 7HC, 7KC, 7KCAB, 8GCBC, and 8KCAB. Cessna Aircraft Company, The: 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, R182, T182, TR182, 172RG, R172E, R172F, R172H, R172J, 152, A152, 210, 210-5 (205), 210-5A (205A), 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, P210N, T210G, T210H, T210M, T210N, T210R, 185, 185A, 185B, 185C, 185D, 185E, 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 120, 140, 170, 170A, 170B, 177, 177A, 177B, 207, 207A, T207, T207A, 177RG, 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, 188, 188A, 188B, A188, A188A, and A188B. Commander Aircraft Company: 112, 112B, 112TC, 114, and 114A. Dynac Aerospace Corporation: Aero Commander 100. Global Amphibians, LLC: Lake LA-4-200, Lake Model 250. Maule Aerospace Technology, Inc: M-4-210, M-4-220, M-5-180C, M-5-200, M- 5-235C, M-6-180, and M-6-235. Mooney Aircraft Corporation: M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20M, and M22. Navion Aircraft Company, Ltd: Navion G and Navion H. Piper Aircraft, Inc., The New: PA-23, PA-23-160, PA-23-235, PA-23-250 (Navy UO-1), PA-E23-250, PA-24, PA-24- 250, PA-24-260, PA-18, PA-18-105 (Special), PA-18-135, PA-18-150, PA- 20-115, PA-20-135, PA-22-108, PA-22- 135, PA-22-150, PA-22-160, PA-25, PA- 25-235, PA-25-260, PA-28-140, PA-28- 150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28-201T, PA- 28-235, PA-28-236, PA-28R-180, PA-28R- 200, PA-28R-201, PA-28R-201T, PA-28RT- 201, PA-28RT-201T, PA-25, PA-25-235, PA-25-260, J5A-80, J5A (Army L-4F), J5B (Army L-4G), J5C, PA-12, PA-36- 285, PA-36-300, PA-36-375, PA-38-112, PA-30, PA-39, PA-40, PA-31, PA-31- 300, PA-31-325, PA-31-350, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA- 32R-300, PA-32R-301 (HP), PA-32R- 301T, PA-32RT-300T, PA-31P, and PA-36- 300. Raytheon Aircraft Company: 35-33, 35-A33, 35-B33, 35-C33, 35- C33A, 36, A36, A36TC, B36TC, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, V35, V35A, V35B, D45 (Military T-34B), 35, 35R, A35, B35, C35, D35, E35, F35, G35, 19A, 23, A23, A23A, A24, A24R, B19, B23, B24R, C23, and C24R. Rogers, Burl A: 15AC and S15AC. SOCATA--Groupe Aerospatiale: MS 885, MS 892A-150, MS 892E-150, MS 893A, MS 893E, Rallye 150 ST, Rallye 150 T, TB 10, TB 20, and TB 9 Tiger Aircraft LLC: AA-1, AA-1A, AA-1B, AA-1C, AA-5, AA- 5A, and AA-5B.
- 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 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 2005-11-05 One-time Appliance
Precise Flight, Inc. Models SVS I and SVS IA Standby Vacuum Systems
Applicability, as the AD words it
This AD affects Models SVS I and SVS IA standby vacuum systems (SVS), installed on, but not limited to, the following aircraft that are certificated in any category. These systems can be installed under the applicable supplemental type certificate (STC) or through field approval: Affected STC Make and model/series aircraft SA2160NM: Raytheon Beech Models 23, A23, A23A, A23-19, 19A, B19, B19A, A23- 24, B23, C23, A24, A24R, B24R, C24R, 35, A35, B35, C35, D35, E35, F35, G35, 35R, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC, 4S(YT-34), A45(T-34A, B- 45), D45(T-34B), and Series 77. SA2161NM: Raytheon Beech Model V35B. SA2162NM: The Cessna Aircraft Company Models 321 (Navy OE-2), 172N, 172P, 172D, 172M, 172L, 172I, 172H (USAF T-41A), 172F (USAF T-41A), 172E, 172C, 172, 172Q, 172B, TR182, T182, 305B (Military T0-1D, 0- 1D, 0-1F), R172E Series, 175C, 175B, 175A, R172F (USAF T-41D), P172D, 150, 150A, 150C, 150B, 150D, A152, A150M, 150M, 152, A150L, 150K, 150J, 150H, 150G, 150F, 210-5 (205), 210-5A (205A), T210R, P210R, T210N, 210N, P210N, 210M, T210L, 210K, T210K, 210J, T210H, 210H, T210G, T210F, 210F, 210D, 210C, 210B, 210A, 210L, 210, A185F, A185E, 185E, 185C, 185B, 185A, 185, 140A, 305A (USAF 0-1A), 305C (USAF 0-1E), 305D (USAF 0-1G), 305F, 120, 170B, 170A, 170, 207A, T207, 207, 206, P206B, P206, P206C, TU206A, TU206G, TU206E, TU206C, P206D, U206G, U206F, U206E, U206D, U206C, U206A, TP206E, TP206D, TP206C, TP206A, P206E, TU206D, T188C, A188B, A188, 188A, and 188. SA2164NM: The Cessna Aircraft Company Model 180A. SA2167NM: The New Piper Aircraft, Inc. Models PA-16S and PA-16, Series PA-24, Models PA-24-400, PA-24-250, PA-24, PA-24-260, PA-18S-"135", PA- 18"105" (Special), PA-18AS-"135", PA-18A-"135", PA-18- "150", PA-19S, PA-19 (Army L-18C), PA-18S-"150", and PA-18- "135" (Army L-21B), Series PA-18, Models PA-18-"125" (Army L- 21A), PA-18S, PA-18A, PA-18, and PA-18S-"125", Series PA-19 and PA-20, Models PA-20, PA-20S, PA-20-"135", PA-20-"115", and PA- 22S-160, Series PA-22, Models PA-22-160, PA-22S-150, PA-22-150, PA- 22, PA-22-108, PA-22-135, and PA-22S-135, Series PA-28, Model PA- 28R-200, Series PA-28S and PA-28R, Models PA-28-236, PA-28-201T, PA-28R-180, PA-28RT-201T, PA-28RT-201, PA-28R-201, PA-28-181, PA- 28S-180, PA-28R-201T, PA-28S-160, PA-28-235, PA-28-180, PA-28-161, PA-28-160, PA-28-151, PA-28-150, and PA-28-140, Series PA-25 (Normal Category (Cat.)), Models PA-25-260 (Normal Cat.), PA-25- 235 (Normal Cat.),PA-25 (Normal Cat.), L-14, PA-12S, PA-12, PA-14, PA-15, PA-17, PA-38-112, PA-46-310P, and PA-32-260, Series PA-32 and PA-32R, Models PA-32-300, PA-32-301T, PA-32-301, PA-32R-301T, PA-32R-301(HP), PA-32R-301(SP), PA-32RT-300T, PA-32RT-300, PA-32R- 300, and PA-32S-300, Series PA-36, Models PA-36-375 (Normal Cat.), PA-36-300 (Normal Cat.), and PA-36-285 (Normal Cat.) SA2168NM: Learjet Inc. Model Learjet 24D Mooney Aircraft Corporation Models M20C, M20M, M20K, M20J, M20G, M20B, M20A, M20, M20F, M20E, and M22. SA2683NM: Aermacchi S.p.A. Models F.260, F.260B, S.205-22/R, S.205-18/F, S.205-18/R, S.205-20/F, S.205-20/R, S.208A, and S.208 Aerocar, Incorporated Model I Aerodifusion, S.L. Model Jodel D-1190S Aeromere S.A. Model Falco F.8.L Aeronautica Macchi S.p.A. Models AL60, AL60-B, AL60-F5, and AL60-C5 Aeronautica Macchi S.p.A. & Aerfer-Industrie Aerospaziali Meridionali S.p.A. Model AM-3 Aeronca Aircraft Corporation Models S15AC and 15AC Ag Cat Corporation Models G-164B, G-164, and G-164A Alliance Aircraft Group, LLC Models H-395 (USAF L-28A or U-10B), H-250, H-295 (USAF U-10D), HT-295, H-391 (USAF YL-24), H-391B, H-700, and H-395A American Champion Aircraft Corp. Models 7AC, 7FC, 7ACA, S7AC, 7BCM (L-16A), 7CCM (L-16B), 7DC, S7DC, 7EC, S7EC, 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB, 11BC, S11AC, S11BC, 11AC, 11CC, S11CC, 8KCAB, and 8GCBC Arctic Aircraft Company, Inc. Models S-1A, S-1A-65F, S-1A-85F, S-1A-90F, S-1B2, S- 1B1 (Army L-6), and S-1B1 (Army XL-6) Augustair, Inc. Models 2150A, 2180, and 2150 Avions Jodel Models D-1190, 150, D-140-B, and DR-1050 Bellanca Aircraft Corporation Models 14-19-2, 14-19- 3A, 17-30, 17-31, 17-31TC, 14-9, 14-9L, 14-12F-3, 14-13, 14-13-2, 14-13-3, 14-13-3W, 17-30A, 17-31A, and 17-31ATC Biemond, C. Model Teal CB1 Board, G.R. Model Columbia XJL-1 Booth, Lee F. dba Taylorcraft Aerospace Models F21, F21A, and F19 Chaparral Motors, Inc. Models 2T-1A-1 and 2T-1A-2 Clark Aircraft, Inc. Models 12 and 1000 Commander Aircraft Company Models 114A, 112, 112B, 112TCA, 114, and 112TC C. Itoh Aircraft Maintenance and Engineering Co., Ltd. Model N-62 DaimlerChrysler Aerospace AG Models Bolkow Jr., BO- 209-150 FV & RV, BO-209-160 FV & RV, and BO-209-150 FF Flugzeugwerke Altenrheim AG (FFA) Model AS 202/15 "BRAVO" Found Brothers Aviation Limited Model FBA-2C Fuji Heavy Industries, Ltd. Models FA-200-180AO, FA-200-180, and FA-200-160 Funk Aircraft Company Model Funk C Goodyear Aircraft Corporation Model GA-22A Gulfstream Aerospace Corporation Model 111 Jamieson Corporation, The Model J-2-L1B Kearns, Edward Scott Model Trojan A-2 Luscombe Aircraft Corporation Model 11A Luscombe, The Don, Aviation History Foundation, Inc. Models T-8F, 8A, 8E, 8D, 8B, 8, 8F, and 8C Maule Aerospace Technology, Inc. Models Bee Dee M-4-210, Bee Dee M-4- 180S, Bee Dee M-4-180C, Bee Dee M-4T, Bee Dee M-4-210S, Bee Dee M- 4S, Bee Dee M-4-210T, Bee Dee M-4-210C, Bee Dee M-4-220S, Bee Dee M-4-220T, Bee Dee M-5-180C, Bee Dee M-5-200, Bee Dee M-5-210TC, Bee Dee M-7-235, Bee Dee M-6-235, Bee Dee M-4C, Bee Dee M-5-220C, Bee Dee M-5-235C, Bee Dee M-6-180, Bee Dee M-5-210C, Bee Dee MX-7- 235, Bee Dee M-4, MX-7-160C, Bee Dee M-7 Series, Bee Dee MXT-7- 180, Bee Dee MT-7-235, Bee Dee M-8-235, Bee Dee MX-7-160, Bee Dee MXT-7-160, Bee Dee MX-7-180A, Bee Dee MXT-7-180A, Bee Dee MX-7- 180B, Bee Dee M-7-235B, Bee Dee M-6 Series, Bee Dee MX-7 Series, Bee Dee M-7-235C, Bee Dee M-4 …
- AD 2004-08-10 One-time Engine
Engine Components Incorporated (ECi) Reciprocating Engine Cylinders
We are issuing this AD to prevent loss of engine power due to cracks in the cylinder head and possible engine failure caused by separation of a cylinder head.
Applicability, as the AD words it
This AD applies to Teledyne Continental Motors (TCM) TSIO- 520-NB, -VB, and -WB engines that are modified by supplemental type certificate (STC) SE4327SW, STC SE09104SC, or STC SE09261SC for operation at 325 HP or greater, (the so-called RAM TSIO-520-NB, -VB, or -WB Series III, IV, and VII reciprocating engines; and Teledyne Continental Motors (TCM) model 520 and 550 series reciprocating engines with certain ECi reciprocating engine cylinders, part number (P/N) AEC631397, installed. These engines are installed on, but not limited to the airplanes listed in the following Table 1: Table 1.--List of Airplanes That Use the Affected Engines Airplane manufacturer and model Engine model AERFER/AERMECCHI AM, 3: GTSIO-520-C AERO COMMANDER: 200D: IO-520-A 500A COLEMILL CONVERSION: IO-520-E 685: GTSIO-520-K AISA: F20, PEGASO: IO-520-K AMBROSIN MF-151: IO-520-F AVIONES PIHAO: IO-520-D BEAGLE (U.K.): B206S: GTSIO-520-C BEECHCRAFT BARON: C55: IO-520-CB, -C D55: IO-520-CB, -C E55: IO-520-CB, -C 58: IO-520-CB 58P: TSIO-520-LB 58P: TSIO-520-L 58P: TSIO-520-WB 58TC: TSIO-520-LB 58TC: TSIO-520-L 58TC: TSIO-520-WB BEECHCRAFT BONANZA: A36: IO-550-B E33A: IO-520-BA E33A: IO-520-BB E33B: IO-520-B F33: IO-520-BB F33A: IO-520-B F33A: IO-520-BA F33A: IO-520-BB S35: IO-520-B ST35: TSIO-520-D V35: IO-520-BB V35A: IO-520-B V35A-TC: TSIO-520-D V35B: IO-520-B V35B: IO-520-BA V35B: IO-520-BB A36: IO-520-B A36: IO-520-BA A36: IO-520-BB A36-TC: TSIO-520-UB BEECHCRAFT DEBONAIR: C33A: IO-520-B VIKING 300: IO-520-A IO-520-D IO-520-K BONNAIRE 185: IO-520-D BONNAIRE 188 CONVERSION: IO-520-D BURNS BA42: IO-520-D CESSNA: SUPER SKYLANE A, B, C, D, E: IO-520-A TURBO SUPER SKYLANE: TSIO-520-C SKYWAGON A185 E,F: IO-520-D SKYWAGON A185FII: IO-520-D AG SPRAYER 188-300: IO-520-D A188-230: IO-520-D AG TRUCK (A 188B) -300: IO-520-D AG HUSKEY (A 188C) -310: TSIO-520-T AG WAGON (A 188B): IO-520-D SUPER SKYWAGON U206, A: IO-520-A U206B, C, D, E, F: IO-520-F TURBO SKYWAGON TU206 A: IO-520-C TU206B, C, D, E, F: TSIO-520-C STATIONAIR U206: IO-520-F TU206: TIOS-520-C U206FII-300: IO-520-F U206G-300: IO-520-F U206GII-300: IO-520-L TU206G-310: TSIO-520-M SUPER SKYLANE P206A: IO-520-A P206B, C, D, E: IO-520-A TURBO P 206 A, B, C, D, E: TSIO-520-C SKYWAGON 207: IO-520-F TURBO 207: TSIO-520-G STATIONAIR 207A, 207AII: IO-520-F STATIONAIR 8, 811: IO-520-F T-STATIONAIR 811: TSIO-520-M 210 CENTURION D, E, F, G, H: IO-520-A 210 CENTURION J: IO-520-J 210 CENTURION K, L, M, N, R: IO-520-L 210 CENTURION TURBO: TSIO-520-C 210 CENTURION TURBO: TSIO-520-H 210 CENTURION TURBO K, L: TSIO-520-H TURBO 210 J, K, L: TSIO-520-H TURBO 210 MII, NII: TSIO-520-R TURBO 210R: TSIO-520-R PRESSURIZED CENTURION P210N: TSIO-520-P PRESSURIZED CENTURION P210NII: TSIO-520-AF PRESSURIZED CENTURION P210R: TSIO-520-CE T303 CRUSADER: TSIO-520-AE T303 CRUSADER: LTSIO-520-AE 310R: IO-520-MB 310R: IO-520-M TURBO 310 P, Q: TSIO-520-B TURBO 310 R: TSIO-520-BB TURBO 310 R: TSIO-520-B EXECUTIVE SKYNIGHT D, E, F: TSIO-520-B 335: TSIO-520-EB 340: TSIO-520-K 340A: TSIO-520-NB, -N 401 A, 401 B: TSIO-520-E 402 A, 402 B: TSIO-520-E 402C: TSIO-520-VB 404 TITAN: GTSIO-520-M 411, 411A: GTSIO-520-C 414: TSIO-520-J 414, 414 A: TSIO-520-NB, -N 421A: GTSIO-520-D 421B: GTSIO-520-H 421C: GTSIO-520-L 421C: GTSIO-520-N JANOX JAVILON: IO-520-B NAVION: RANGEMASTER MODEL H: IO-520-B RANGEMASTER MODEL H: IO-520-BA PIPER: MALIBU: TSIO-520-BE PRINAIR: DE HAVILLAND HERON: IO-520-E WINDECKER EAGLE: IO-520-C
- AD 2003-01-01 One-time
Raytheon Aircraft Company Beech Models 36, A36, A36TC, B36TC, 58, and 58A 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 T.N. Baktha, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946-4155; facsimile: (316) 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. (h) Are any service bulletins incorporated into this AD by reference? (1) Actions required by this AD must be done in accordance with Raytheon Mandatory Service Bulletin SB 53-3341, Rev. 1, Revised: May 2000, or Raytheon Mandatory Service Bulletin SB 53-3341, Rev. 2, Revised: October, 2002. (i) The Director of the Federal Register approved the incorporation by reference of Raytheon Mandatory Service Bulletin SB 53-3341, Rev. 2, Revised: October, 2002, under 5 U.S.C. 552(a) and 1 CFR part 51. (ii) The Director of the Federal Register previously approved the incorporation by reference of Raytheon Mandatory Service Bulletin SB 53-3341, Rev. 1, Revised May, 2000, as of February 16, 2001 (66 FR 1253, January 8, 2001). (2) You may get copies from Raytheon Aircraft Company, PO Box 85, Wichita, Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676-3140. 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) Does this AD action affect any existing AD actions? This amendment supersedes AD 2000-26-16, Amendment 39-12066. (j) When does this amendment become effective? This amendment becomes effective on February 27, 2003. Issued in Kansas City, Missouri, on December 30, 2002. James E. Jackson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 03-148 Filed 1-7-03; 8:45 am] BILLING CODE 4910-13-P
- 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 2001-11-03 One-time
Raytheon Aircraft Company Beech Models F33A, A36, B36TC, 58/58A, C90A, B200, and 1900D Airplanes
Applicability, as the AD words it
This AD applies to each airplane with a KA-33 cooling blower 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 (h) 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. (i) Where can I get information about any already-approved alternative methods of compliance? Contact Todd Dixon, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4152; facsimile: (316) 946-4407. (j) 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. (k) 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 34-3267, Issued: March, 1999, Raytheon Mandatory Service Bulletin SB 34-3268, Issued: April, 2000, Raytheon Mandatory Service Bulletin SB 34-3269, Issued: January 2000, and Raytheon Mandatory Service Bulletin SB 34-3269, Revision 1, Revised: October, 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 the Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085. You can look at 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. (l) When does this amendment become effective? This amendment becomes effective on July 20, 2001. Issued in Kansas City, Missouri, on May 21, 2001. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-13581 Filed 6-5-01; 8:45 am] BILLING CODE 4910-13-P
- AD 2001-08-08 Recurring
Raytheon Aircraft Company Beech Models 35-C33A, E33A, E33C, F33A, F33C, S35, V35, V35A, V35B, 36, and A36 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? You can contact Mr. Peter Hakala, Aerospace Engineer, FAA, Rotorcraft Directorate, Special Certification Office, 2601 Meacham Boulevard, Fort Worth, Texas 76193-0190; telephone: (817) 222-5145; facsimile: (817) 222-5785. (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. (1) In order for this permit to be granted, the airplane must pass the push/pull test specified in Tornado Alley Turbo, Inc., Mandatory Service Bulletin Number TAT 98-1, dated November 21, 1998. (2) Anyone who holds at least a private pilot certificate, as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7), may accomplish the push/pull test referenced in paragraph (g)(1) of this. You must make an entry into the aircraft records that shows compliance with this portion of the AD, in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (h) How do I get copies of the documents referenced in this AD? You may obtain a copy of the service documents referenced in this AD from Tornado Alley Turbo, Inc., 300 Airport Road, Ada, Oklahoma 74820; telephone: toll free 1-877-359-8284, or (580) 332-3510; facsimile: (580) 332-4577; or you may examine this document at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106. (i) When does this amendment become effective? This amendment becomes effective on June 7, 2001. Issued in Kansas City, Missouri, on April 12, 2001. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-9750 Filed 4-19-01; 8:45 am] BILLING CODE 4910-13-P
- AD 2000-26-16 Superseded by AD 2003-01-01
Raytheon Aircraft Company Beech Models A36, B36TC, and 58 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 T.N. Baktha, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4155; facsimile: (316) 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. (h) 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 53-3341, Revision 1, revised May 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 67201-0085; telephone: (800) 429-5372 or (316) 676- 3140. You can look at 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 February 16, 2001. Issued in Kansas City, Missouri, on December 22, 2000. Marvin R. Nuss, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-183 Filed 1-5-01; 8:45 am] BILLING CODE 4910-13-P
- AD 2000-24-04 One-time
Raytheon Aircraft Company Beech Models A36, B36TC, and 58 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 C. DeVore, Aerospace Engineer, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4142; facsimile: (316) 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. (h) 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 27-3265, Issued: January 2000. The director of the Federal Register approved this incor- poration 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, KS 67201-0085; or on the Internet at http://www.raytheon.com/rac/servinfo/27-3265.pdf. This file is in Adobe Portable Document Format. The Acrobat Reader is available at http://www.adobe.com/>. You can look at 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 January 5, 2001. Issued in Kansas City, Missouri, on November 20, 2000. Marvin R. Nuss, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 00-30318 Filed 12-1-00; 8:45 am] BILLING CODE 4910-13-P
- AD 2000-20-14 One-time
Raytheon Aircraft Company Beech Models A36 and B36TC 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? You can contact Jeff Pretz, Aerospace Engineer, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4153; facsimile: (316) 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. (h) 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 No. SB 53-3375, dated December 1999. 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; on the Internet at http://www.raytheon.com/rac/servinfo/53-3375.pdf>. This file is in Adobe Portable Document Format. The Acrobat Reader is available at http://www.adobe.com/>. You can look at 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 20001. (i) When does this amendment become effective? This amendment becomes effective on November 28, 2000. Issued in Kansas City, Missouri, on September 28, 2000. Issued in Kansas City, Missouri, on September 28, 2000. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 00-25549 Filed 10-12-00; 8:45 am] BILLING CODE 4910-13-P
- AD 99-24-10 Recurring Appliance
Precise Flight, Inc. Model SVS III Standby Vacuum Systems
To detect and correct problems with the standby vacuum system before failure or malfunction and to provide operating procedures for the pilot regarding the use and limitations of this system.
Applicability, as the AD words it
Model SVS III standby vacuum systems, installed on, but not limited to, the aircraft listed in the following chart. These systems can be installed either in accordance with the applicable supplemental type certificate (STC) or through field approval: Affected STC Make and model airplanes SA2160NM: Raytheon Beech Models 23, A23, A23A, A23-19, 19A, B19, B19A, A23-24, B23, C23, A24, A24R, B24R, C24R, 35, A35, B35, C35, D35, E35, F35, G35, 35R, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35- C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC, 4S (YT-34), A45 (T-34A, B-45), D45(T- 34B), and 77 Series. SA2161NM: Raytheon Beech Model V35B. SA2162NM: Cessna Models 120, 140, 140A, 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, A150L, 150M, 152, A152, A150K, A150M, 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAFT-41A), 172G, 172H (USAFT-41A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 175, 175A, 175B, 175C, P172D, R172E (USAFT-41B, USAFT41- 3, and USAFT-41D), R172F (USAFT-41D and USAFT-41C), R172G (USAFT-41D), R172H (USAFT-41D), R172J, R172K, 172RG, 177, 177A, 177B, 177RG, 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182RG, T182, T182RG, T182R, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 188, 188A, 188B, A188, A188B, T188C, 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D. TP206E, U206-A, U206-B, U206-C, U206-D, U206-E, U206-F, U206G, TU206-A, TU206-B, TU206-C, TU206-D, TU206-E, TU206-F, TU206-G, 207, 207A, T207, T207A, 210, 210A, 210B, 210C, 210D, 210E, 210F, 210-5 (205), 210-5A (205A), T210F, 210G, T-210G, 210H, T-210H, 210J, 205P, T-210J, 210K, T- 210K, T210L, 210L, 210M, T210M, 210N, P210N, T210N, 205T, 210R, P210R, 205U, T210R, 210-5, 210-5A, 305A (USAF 0- 1A), 305C (USAF 0-1E), 305D (USAF 0-1F), 305F, 305B (USAF T0-1D), 305E (0-1D or 0-1F), and 321 (Navy 0E-2). SA2163NM: Cessna Model U206G. SA2164NM: Cessna Model 180Q. SA2166NM: Cessna Model 177. SA2167NM: The New Piper Aircraft, Inc. (Piper) Models L-14, PA-12, PA-12S, PA-14, PA-15, PA-16, PA-16S, PA-17, PA-18, PA- 18A, PA-18S, PA-18-105 (Special), PA-18S-105 (SP), PA-18- 125 (Army L-21A), PA-18AS-125, PA-18S-125, PA-18-135, PA- 18A-135, PA-18AS-135, PA-18S-135, PA-18-150, PA-18A-150, PA-18AS-150, PA-18S-150, PA-19 (Army L-18C), PA-19S, PA- 20, PA-20S, PA-20-115, PA-20S-115, PA-20-135, PA-22, PA- 22-108, PA-22-135, PA-22S-135, PA-22-150, PA-22S-150, PA- 22-160, PA-22S-160, PA-24, PA-24-250, PA-24-260, PA-24- 400, PA-25, PA-25-235, PA-25-260, PA-32-260, PA-32RT-300, PA-32RT-301T, PA-32-300, PA-32RT-300T, PA-32-301, PA-32S- 300, PA-32R-301, PA-32-301T, PA-32R-300, PA-32R-301T, PA- 28-140, PA-28-141, PA-28-150, PA-28-151, PA-28-160, PA- 28S-160, PA-28-180, PA-28R-180, PA-28S-180, PA-28-235, PA- 28S-235, PA-28-181, PA-28-161, PA-28R-200, PA-28R-201, PA- 28R-201T, PA-28-236, PA-28RT-201, PA-28RT-201T, PA-28- 201T, PA-36-285, PA-36-300, PA-36-375, PA-38-112, and PA- 46-310P. SA2168NM: Mooney Models M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20M, and M22. SA2683NM: Aerocar, Inc. Model I, Aerodifusion, S.L. Model Jodel D- 1190S, Aeromere, S.A. Model Falco F.8.L., Aeronautica Macchi S.P.A. Models AL60, AL60-B, AL60-F5, and AL60-C5, Aeronautica Macchi & Aerfer Model AM-3, Aeronca Inc. Models 15AC and S15AC, Aerospatiale Model TB20 Trinidad, Arctic Aircraft Co., Inc. Models S-1A, S-1A-65F, S-1A- 85F, S-1A-90F, S-1B1 (Army L-67 XL-6), and S-1B2, Avions Mudry et Cie Model CAP 10B, American Champion Models (Bellanca, Aeronca) 7AC, 7ACA, S7AC (L-16A), 7BCM (L- 16B), 7CCM, 7DC, S7DC, 7EC, S7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCCA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB, 8KCAB, 8GCBC, 11AC, S11AC, 11BC, S11BC, 11CC, and S11CC, Bellanca Aircraft Corporation, Models 14-9, 14-9L, 14-12F- 3, 14-13, 14-13-2, 14-13-3, 14-13-3W, 14-19, 14-19-2, 14- 19-3A, 17-30, 17-31, 17-31TC, 17-30A, 17-31A, and 17- 31ATC, Biemond, C. Model Teal CB1, Board, G.R. Models Columbia XJL-1 and Bolkow Jr., Clark Aircraft, Inc. Models 12 and 1000, Falcon Aircraft Corporation Model F- 1, Flug und Fahrzeugwerke AG Model AS 202/15 "Brand," Found Brothers Model FBA-2C, Fuji Heavy Industries Models FA-200-160, FA-200-180, and FA-200-180AO, Funk Aircraft Model Funk C, Kearns, Edward Scott (Garcia, Henry S.) Model (Emigh) Trojan A-2, Swift Museum Foundation, Inc. Model (Globe) GC-1A, GC-1B, Goodyear Aircraft Model GA- 22A, Great Lakes Aircraft Model 2T-1A-1 and 2T-1A-2, Grumman American Models G-164, G-164A, G-164B, AA-1, AA- 1A, AA-1B, AA-1C, AA-5, AA-5A, and AA-5B, Commander Aircraft (Gulfstream) Models 112, (112A, 112B, 112TC, 112TCA, 114, and 114A, Helio Enterprises Models H-250, H- 295 (USAF U-10D), H-391 (USAF YL-24), H-395 (SAF L-28A), H-395A, HT-295, and H-700, Prop-Jets, Inc. (Interceptor Corp., Aero Commander, Meyers) Models 200, 200A, 200B, 200C, and 200D, C. Itoh Aircraft Maintenance & Engineering Co. LTD. Model N-62, Jamieson Corporation Model J-2-L1B, Jodel, Avion Models D-140-B, DR-1050, D- 1190, and 150, Lake Models C-1, C-2-IV, LA-4, LA-4-200, and LA-4-250, Luscombe Aircraft Corp. Models 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F, and 11A, Maule Aerospace Technology Corp. Models Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M-4- 180C, M-4-180S, M-4-210, M-4-201C, M-4-210S, M-4-210T, M- 4-220S, M-4-220T, M-5-180C, M-5-200, M-5-210C, M-5-210TC, M-T-220C, M-5-235, M-5-235C, M-6-180, M-6-235, M-7-235, MX-7-180, MX-7-235, Messerschmitt-Bolkow Models BO-209- 150 FV&RV, BO209-160 FV&RV, BO-209, and 150OFF, Nardi S.A. Model FN-333, Jimmie Thompson Enterprise (Navion Rangemaster Aircraft Corporation) Models Navion (L-17A), Navion A (L-17B, L-17C), Navion B, D, E, F, G, and H, White International Ltd. Models (Pitts) S-1S, S-1T, S-2, and S-2A, Procaer S.P.A. Models F 15/B, F 15/C, and F 15/ E, Gulfstream Aerospace Corporation (Rockwell) Models 111, 112, …
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Raytheon Aircraft Company Beech Models A36, B36TC, 58, 58A, C90A, B200, B300, and 1900D Airplanes
Applicability, as the AD words it
The following Beech airplane models and serial numbers, certificated in any category: Model Serial Nos. A36: E-3058 through E-3156, E-3158 through E- 3170, E-3172 through E-3177, E-3180 through E-3185, E-3187 through E-3198, E- 3200, and E-3202. B36TC: EA-594 through EA-610, EA-613, EA-615, EA- 616, EA-618, EA-619, and EA-621. 58 and 58A: TH-1806 through TH-1840, TH-1842 through TH-1854, TH-1856, TH-1860 through TH- 1867, and TH-1870. C90A: LJ-1459 through LJ-1504, LJ-1506 through LJ-1523, and LJ-1525 through LJ-1530. B200: BB-1551 through BB-1591, BB-1593 through BB-1622, and BB-1624 through BB-1627. B300: FL-152 through FL-179, FL-181 through FL- 187, FL-189, FL-190, FL-192, FL-194, FL- 196 through FL-205, FL-207, FL-210, and FL-211. 1900D: UE-1 through UE-319, UE-321, UE-323 through UE-328, UE-330 and UE-332.
- AD 99-05-13 Removed 2000-07-12
Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC, 60, 65, 70, 76, 77, 80, 88, and 95 Series Airplanes
Applicability, as the AD words it
The following airplane models and serial numbers, certificated in any category: Model Serial No. B17L: all serial numbers. SB17L: all serial numbers. B17B: all serial numbers. B17R (Army UC-43H): all serial numbers. C17L (Army UC-43J): all serial numbers. SC17L: all serial numbers. C17B (Army UC-43G): all serial numbers. SC17B: all serial numbers. C17R (Army UC-43E): all serial numbers. SC17R: all serial numbers. D17A (Army UC-43F): all serial numbers. D17R (Army UC-43A): all serial numbers. D17S (Army UC-43, UC-43B, Navy GB-1, GB-2) all serial numbers. SD17S: all serial numbers. E17B (Army UC-43D: all serial numbers. SE17B: all serial numbers. E17L: all serial numbers. F17D (UC-43C): all serial numbers. SF17D: all serial numbers. G17S: all serial numbers. D18S: all serial numbers. E18S: all serial numbers. E18S-9700: all serial numbers. G18S: all serial numbers. G18S-9150: all serial numbers. H18: all serial numbers. A23-19: all serial numbers. 19A: all serial numbers. M19A: all serial numbers. B19: all serial numbers. 23: all serial numbers. A23: all serial numbers. A23A: all serial numbers. B23: all serial numbers. C23: all serial numbers. A23-24: all serial numbers. A24: all serial numbers. A24R: all serial numbers. B24R: all serial numbers. C24R: all serial numbers. F33A: CE-290 through CE-1791. E33C and F33C: CJ-26 through CJ-179. 35: all serial numbers. 35R: all serial numbers. A35: all serial numbers. B35: all serial numbers. C35: all serial numbers. D35: all serial numbers. E35: all serial numbers. F35: all serial numbers. G35: all serial numbers. H35: all serial numbers. J35: all serial numbers. K35: all serial numbers. M35: all serial numbers. N35: all serial numbers. P35: all serial numbers. S35: all serial numbers. V35: all serial numbers. V35TC: all serial numbers. V35A: all serial numbers. V35A-TC: all serial numbers. V35B: all serial numbers. V35B-TC: all serial numbers. 36: all serial numbers. A36: E-185 through E-3046. A36TC: all serial numbers. B36TC: EA-242 through EA-591. 45: all serial numbers. A45: all serial numbers. D45: all serial numbers. 50: all serial numbers. B50: all serial numbers. C50: all serial numbers. D50: all serial numbers. D50A: all serial numbers. D50B: all serial numbers. D50C: all serial numbers. D50E: all serial numbers. E50: all serial numbers. F50: all serial numbers. G50: all serial numbers. H50: all serial numbers. J50: all serial numbers. 95-55: all serial numbers. 95-A55: all serial numbers. 95-B55: all serial numbers. 95-C55: all serial numbers. D55: all serial numbers. E55: all serial numbers. 56TC: all serial numbers. A56TC: all serial numbers. 58: TH-1 through TH-1798. 58P: all serial numbers. 58TC: all serial numbers. 60: all serial numbers. A60: all serial numbers. B60: all serial numbers. 65: all serial numbers. A65: all serial numbers. A65-8200: all serial numbers. 70: all serial numbers. 76: all serial numbers. 77: all serial numbers. 65-80: all serial numbers. 65-A80: all serial numbers. 65-B80: all serial numbers. 65-88: all serial numbers. 95: all serial numbers. B95: all serial numbers. B95A: all serial numbers. D95A: all serial numbers. E95: all serial numbers.
- AD 98-25-13 One-time Propeller
McCauley Propeller Systems Models 2A36C23/84B-0 and 2A36C82/84B-2 Propellers
To prevent possible cracks in the propeller blade threaded retention area from progressing to blade separation, which can result in loss of aircraft control.
Applicability, as the AD words it
McCauley Propeller Systems (formerly McCauley Accessory Division, The Cessna Aircraft Company) Models 2A36C23/84B- 0 and 2A36C82/84B-2 propellers installed on, but not limited to, Raytheon (formerly Beech) 35-B33, 35-A33, 35-33, 35-C33, 35-C33A, 36, A36, A45, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B Model aircraft, and S35, V35, V35A, V35B series aircraft.
- 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 97-26-17 One-time Engine
Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, IO-520, LIO-520, TSIO-520, LTSIO-520 Series, and Rolls-Royce plc IO-360 and TSIO-360 Series Reciprocating Engines
To prevent crankshaft failure and subsequent engine failure.
Applicability, as the AD words it
Teledyne Continental Motors (TCM) IO-360, LTSIO- 360, TSIO-360, IO-520, LIO-520, LTSIO-520 and TSIO-520 series reciprocating engines built on or prior to December 31, 1980; rebuilt TCM IO-360, LTSIO-360, TSIO-360, IO-520, LIO-520, LTSIO-520 and TSIO-520 series reciprocating engines with serial numbers lower than those listed in TCM Critical Service Bulletin (SB) No. CSB96-8, dated June 25, 1996; TCM factory overhauled IO-360, LTSIO-360, TSIO- 360, IO-520, LIO-520, LTSIO-520 and TSIO-520 series reciprocating engines with serial number of 901203H and lower; and Rolls-Royce, plc IO-360 and TSIO-360 series reciprocating engines with any serial number. These engines are installed on but not limited to the following aircraft: Raytheon (formerly Beech) models 95-C55, 95- C55A, D55, D55A, E55, E55A, 58, 58A, 58P, 58PA, 58TC, 58TCA, S35, V35, V35A, V35B, E33A, E33C, 35-C33A, 36, A36, F33A, F33C and A36TC; Bellanca model 17-30A; Cessna models 172XP, A185, A188, T188C, 206, T206, 207, T207, 210, T210, P210, 310R, T310P, T310Q, T310R, 320D, 320E, 320F, 336, 337, T337, P337, 340, 401, 402, 414 and T41B/C; Colemill conversion of Commander 500A; Goodyear Airship Blimp 22; Maule Model M-4-210, M-4-210C, M-4-210S, M-4-210T, and M-5-210C; Mooney model M20-K; Navion model H; Pierre Robin HR 100; The New Piper Aircraft, Inc. (formerly Piper Aircraft Company) models PA28- 201T, PA28R-201T, PA28RT-201T, PA34-200T and PA34-220T; Prinair Dehavilland Heron; Reims models FR172, F337 and FT337; and Swift Museum Foundation, Inc. models GC-1A and GC-1B equipped with the IO- 360 engine.
- AD 97-16-10 One-time Appliance
RAPCO, Inc. Filter, Part Numbers RA- 1J4-4, RA-1J4-6, and RA-1J4-7 From Lot Numbers 05597, 07797, and 12597
To prevent failure of the flight instruments during flight because of a failed in-line pressure filter, which could cause loss of control of the airplane.
Applicability, as the AD words it
Filter Part Numbers (P/N) RA-1J4-4, RA-1J4-6, or RA-1J4-7 from Lot Numbers 05597, 07797, or 12597 installed on, but not limited to, the following airplanes, certificated in any category: Manufacturer Model Cessna Aircraft Company (Cessna): 310R and T310R. Raytheon Aircraft Company (Raytheon) E33A, F33A, V35A, V35B, 36, (formerly known as Beech Aircraft A36, 58, 65-B80, 70, 95- Corporation). B55, D55, E55. The New Piper Aircraft, Inc. (Piper): PA-31-300, PA-31-325, PA- 31P, PA-31P-350, PA-31T, PA- 34-200T.
- 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.
- AD 96-19-01 Recurring Engine
Allison 250 Series Turbine Engines
To prevent bearing failure due to bearing separator instability, which can result in subsequent turbine and engine failure.
Applicability, as the AD words it
Allison Model 250-B15G,-B17F, -B17F/1, -B17F/2, - C20, -C20B, -C20F, -C20J, -C20S, -C20W, -R, -C20R/1, -C20R/2, -C20R/ 4, -C28B, -C28C, -C30, -C30P, -C30M, and -C30G turbine engines, with Superior Air Parts, Inc. Parts Manufacture Approval (PMA) bearings, Part Number (P/N) A6871505 and P/N A23007152, installed. These engines are installed on but not limited to the following aircraft: Aerospace Technologies of Australia PTY Ltd. N-22 and N-24; Agusta S.p.A A109 series, SF600 series; Beech Aircraft Corp. A36 and T34 (Tradewind Turbines conversion); Bell Helicopter Textron Model 47 (Soloy Conversion), OH58 series, 206 series, 230, 430; Cessna 206 and 207 (Soloy Conversions); Enstrom Helicopter Corp. TH28, 480; Eurocopter Deutschland GmbH BO105 series; Eurocopter France AS355 series; Flugzeugwerke Altenrheim AG (FFA) AS202 series; Hiller Aviation UH12 series (Soloy Conversions); Maule Aerospace Technology Corp. MX-7 series; McDonnell Douglas Helicopter Co. OH6 series, 500 series, MD500 series, MD520N series, MD530 series; Partenavia Costruzioni Aeronautiche S.p.A P68 series; Pilatus Britten-Norman Ltd. BN-2T; and Sikorsky Aircraft Division S76 series. Note: This airworthiness directive (AD) applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines 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 the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.
- AD 95-09-08 One-time Propeller
McCauley Model 2A37C223/90RB Propellers
To prevent cylinder screw failure that could result in loss of propeller control and subsequent loss of aircraft control.
Applicability, as the AD words it
McCauley Model 2A37C223/90RB two bladed propellers with the following Propeller Serial Numbers: 901074-901092, 901094-901099, 901315-901320, 901322-901336, 901338-901340, 902816, 902818-902821; 910044, 910046-910051, 910161-910164, 910166, 910169-910170, 910172, 910174, 910176-910181, 911694, 911696, 912019, 912057, 912060, 912062, 912912; 920256-920260, 920262, 920264, 920266. The above McCauley Model 2A37C223/90RB serial-numbered propellers are installed on but not limited to Beech Debonair 35-33, -A33, -B33, -C33, -C33A; E33, E33A, E33C, F33, F33A, F33C, and G33; and Beech Bonanza 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, and A36 aircraft. Note: The above is not an exhaustive list of aircraft which may contain the affected serial-numbered McCauley Model 2A37C223/90RB propellers. It is not possible to identify all aircraft using the affected propeller model because of installation approvals made by Supplemental Type Certificate or FAA Form 337 "Major Repair and Alteration," etc. It is the responsibility of the owner, operator, and person returning the aircraft to service to determine if an aircraft has an affected propeller.
- AD 95-04-03 Recurring
Beech Aircraft Corporation 33, 35, and 36 Series Airplanes
To prevent spar carry-through frame structure failure, which, if not detected and corrected, could result in severe structural damage to the wing.
Applicability, as the AD words it
The following model and serial number airplanes, certificated in any category: Models Serial numbers 35-33, 35-A33, 35-B33, 35-C33, E33, F33, and G33.. CD-1 through CD- 1304. 35-C33A, E33A, and F33A: CE-1 through CE- 1192. E33C and F33C: CJ-1 through CJ-179. H35, J35, K35, M35 N35, P35, S35, V35, V35A, and D-4866 through D- V35B. 10403. 36 and A36: E-1 through E-2397. A36TC and B36TC: EA-1 through EA-471.
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.