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.
Matched on type certificate model SR22 (Cirrus).
RESULTS
17 ADs in effect may apply to SR22
- In effect17
- Recurring3
- Superseded or removed5
Informational only. These are FAA airworthiness directives whose published applicability names this make and model. Whether an AD applies to a particular aircraft depends on its serial number, installed engines, propellers, parts and modifications, and some ADs listed here will not apply. This list is not the official AD record and not a compliance determination: confirm applicability and compliance against the FAA’s Dynamic Regulatory System and the aircraft’s records with a certificated mechanic or inspector. Covers ADs published in the Federal Register since 1995, through Oct 1, 2026; older ADs, and engine, propeller and appliance ADs that do not name the aircraft, are not included.
- AD 2024-24-11 Recurring
Cirrus Design Corporation Airplanes
This AD was prompted by a report of failure of the upper power lever.
Applicability, as the AD words it
This AD applies to Cirrus Design Corporation Model SR20, SR22, and SR22T airplanes, certificated in any category, that are equipped with upper power lever part number (P/N) 19181-001, 19181-002, or 46505-001.
- AD 2020-16-08 One-time Appliance
Aspen Avionics, Inc.
This AD was prompted by an automatic reset occurring when the display internal monitor detects a potential fault causing intermittent loss of airspeed, attitude, and altitude information during flight.
Applicability, as the AD words it
(1) This AD applies to Aspen Avionics, Inc., Evolution Flight Display (EFD) EFD1000 Primary Flight Display part number (P/N) 910- 00001-011, EFD1000 Multi-Function Display P/N 910-00001-012, and EFD1000 Emergency Backup Display P/N 910-00001-017 units that meet both conditions in paragraphs (c)(1)(i) and (ii) of this AD. (i) Software version 2.10 or 2.10.1 is installed; (ii) Independent attitude, altitude, and airspeed back-up instruments are not installed. (2) These flight display units may be installed on, but are not limited to, the following airplanes, certificated in any category: (i) Aermacchi S.p.A. Model S.205-18/F, S.205-18/R, S.205-20/F, S.205-20/R, S.205-22/R, S.208, and S.208A airplanes; (ii) Aeronautica Macchi S.p.A. Model AL 60 (previously designated as Model LASA 60), AL 60-B, AL 60-C5, and AL 60-F5 airplanes; (iii) Aerostar Aircraft Corporation Model PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), and PA- 60-602P (Aerostar 602P) airplanes; (iv) Alexandria Aircraft, LLC (type certificate previously held by Bellanca, Inc.), Model 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-30A, 17-31, 17-31A, 17-31ATC, and 17-31TC airplanes; (v) American Champion Aircraft Corp. Model 402, 7ECA, 7GCAA, 7GCBC, 7KCAB, 8GCBC, and 8KCAB airplanes; (vi) CEAPR (type certificate previously held by APEX) Model CAP 10 B airplanes; (vii) Cirrus Design Corporation Model SR20 and SR22 airplanes; (viii) Commander Aircraft Corporation (type certificate previously held by CPAC, Inc.) Model 112, 112B, 112TC, 112TCA, 114, 114A, 114B, and 114TC airplanes; (ix) Consolidated Vultee Aircraft Corporation, Stinson Division Model V-77 (Army AT-19) airplanes; (x) Cougar Aircraft Corporation (type certificate previously held by SOCATA, S.A.) Model GA-7 airplanes; (xi) Diamond Aircraft Industries Inc. Model DA20-A1 and DA20-C1 airplanes; (xii) Diamond Aircraft Industries Inc. (type certificate previously held by Diamond Aircraft Industries GmbH) Model DA 40 and DA 40 F airplanes; (xiii) Discovery Aviation, Inc. (type certificate previously held by Liberty Aerospace Incorporated), Model XL-2 airplanes; (xiv) Dynac Aerospace Corporation Model Aero Commander 100, Aero Commander 100A, Aero Commander 100-180, Volaire 10, and Volaire 10A airplanes; (xv) EADS-PZL "Warszawa-Okecie" S.A. (type certificate previously held by Panstwowe Zaklady Lotnicze) Model PZL-104 WILGA 80, PZL-104M WILGA 2000, PZL-104MA WILGA 2000, PZL-KOLIBER 150A, and PZL-KOLIBER 160A airplanes; (xvi) Extra Flugzeugproduktions- und Vertriebs- GmbH (type certificate previously held by Extra Flugzeugbau GmbH) Model EA 300, EA 300/L, EA 300/S, EA 300/200, and EA 300/LC airplanes; (xvii) Frakes Aviation Model G-44 (Army OA-14, Navy J4F-2), G- 44A, and SCAN Type 30 airplanes; (xviii) FS 2003 Corporation (type certificate previously held by The New Piper Aircraft, Inc.) Model PA-12 and PA-12S airplanes; (xix) GROB Aircraft AG (type certificate previously held by GROB Aerospace GmbH i.l.) Model G115, G115A, G115B, G115C, G115C2, G115D, G115D2, G115EG, and G120A airplanes; (xx) Helio Aircraft, LLC, Model H-250, H-295 (USAF U-10D), H-391 (USAF YL-24), H-391B, H-395 (USAF L-28A and U-10B), H-395A, H-700, H-800, HST-550, HST-550A (USAF AU-24A), and HT-295 airplanes; (xxi) Interceptor Aviation Inc. (type certificate previously held by Interceptor Aircraft Corporation) Model 200, 200A, 200B, 200C, 200D, and 400 airplanes; (xxii) Lockheed Martin Aeronautics Company Model 402-2 airplanes; (xxiii) Maule Aerospace Technology, Inc. (type certificate previously held by Maule Aircraft Corporation), Model Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M-4-180C, M-4-180S, M-4-180T, M-4-210, M-4- 210C, M-4-210S, M-4-210T, M-4-220, M-4-220C, M-4-220S, M-4-220T, M- 5-180C, M-5-200, M-5-210C, M-5-210TC, M-5-220C, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, M-7-420A, M-7-420AC, M-8-235, MT-7-235, MT-7-260, MT-7-420, MX-7- 160, MX-7-160C, MX-7-180, MX-7-180A, MX-7-180AC, MX-7-180B, MX-7- 180C, MX-7-235, MX-7-420, MXT-7-160, MXT-7-180, and MXT-7-180A airplanes; (xxiv) Mooney Aircraft Corporation Model M22 airplanes; (xxv) Mooney International Corporation (type certificate previously held by Mooney Aviation Company, Inc.) Model M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, M20TN, M20U, and M20V airplanes; (xxvi) Pacific Aerospace Ltd. (type certificate previously held by Found Aircraft Canada, Inc.) Model FBA-2C, FBA-2C1, and FBA-2C2 airplanes; (xxvii) Pilatus Aircraft Ltd. Model PC-6, PC-6-H1, PC-6-H2, PC- 6/350, PC-6/350-H1, PC-6/350-H2, PC6/A, PC-6/A-H1, PC-6/A-H2, PC-6/ B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes; (xxviii) Piper Aircraft, Inc. (type certificate previously held by The New Piper Aircraft, Inc.), Model PA-18, PA-18 "105" (Special), PA-18 "125" (Army L-21A), PA-18 "135" (Army L-21B), PA-18 "150," PA-18A, PA-18A "135," PA-18A "150," PA-18AS "125," PA-18AS "135," PA-18AS "150," PA-18S, PA-18S "105" (Special), PA-18S "125," PA-18S "135," PA-18S "150," PA-19 (Army L-18C), PA-19S, PA-20, PA-20 "115," PA-20 "135," PA-20S, PA-20S "115," PA-20S "135," PA-22, PA-22-108, PA-22-135, PA-22- 150, PA-22-160, PA-22S-135, PA-22S-150, PA-22S-160, PA-23, PA-23- 160, PA-23-235, PA-23-250, PA-24, PA-24-250, PA-24-260, PA-24-400, PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, 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-28S-160, PA- 28S-180, PA-30, PA-32-260, PA-32-300, PA-32-301, PA-32-301FT, PA-32- 301T, PA-32-301XTC, PA-32R-300, PA-32R-301 (HP), PA-32R-301 (SP), PA-32R-301T, PA-32RT-300, PA-32RT-300T, PA-32S-300, PA-34-200, PA- 34-200T, PA-34-220T, PA-39, PA-40, PA-44-180, PA-44-180T, PA-46- 310P, and PA-46-350P airplanes; (xxix) Polskie Zaklady Lotnicze Spolka zo.o. (type certificate previously held by PZL MIELEC) Model PZL M26 01 airplanes; (xxx) Revo, …
- AD 2019-01-02 Recurring Appliance
Aspen Avionics, Inc., Evolution Flight Display Units
This AD was prompted by reports of repetitive uncommanded resetting of the flight display units.
Applicability, as the AD words it
(1) This AD applies to Aspen Avionics, Inc., Evolution Flight Display (EFD) EFD1000 Primary Flight Display, EFD1000 Multi-Function Display (MFD), EFD1000 Emergency Backup Display, or EFD500 MFD units, that are installed on various aircraft and meet all conditions in paragraphs (c)(1)(i), (c)(1)(ii), and (c)(1)(iii) of this AD. (i) Software version 2.9 (SW 2.9) is installed; (ii) The Flight Information Service-Broadcast (FIS-B) Weather Interface option is enabled; and (iii) Independent airspeed, attitude, and altitude back-up instruments are not installed. (2) Airplanes known to have these flight display units installed include, but are not limited to, the following: (i) Aermacchi S.p.A. Model S.205--18/F, S.205--18/R, S.205--20/ F, S.205--20/R, S.205--22/R, S.208, and S.208A airplanes; (ii) Aeronautica Macchi S.p.A. Model AL 60 (previously designated as Model LASA 60), AL 60-B, AL 60-C5, and AL 60-F5 airplanes; (iii) Aerostar Aircraft Corporation Model PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), and PA- 60-602P (Aerostar 602P) airplanes; (iv) Alexandria Aircraft, LLC (type certificate previously held by Bellanca, Inc.), Model 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-30A, 17-31, 17-31A, 17-31ATC, and 17-31TC airplanes; (v) American Champion Aircraft Corp. Model 402, 7ECA, 7GCAA, 7GCBC, 7KCAB, 8GCBC, and 8KCAB airplanes; (vi) APEX Aircraft Model CAP 10 B airplanes; (vii) Cirrus Design Corporation Model SR20 and SR22 airplanes; (viii) Commander Aircraft Corporation (type certificate previously held by CPAC, Inc.) Model 112, 112B, 112TC, 112TCA, 114, 114A, 114B, and 114TC airplanes; (ix) Consolidated Vultee Aircraft Corporation, Stinson Division, Model V-77 (Army AT-19) airplanes; (x) Diamond Aircraft Industries, Inc., Model DA20-A1 and DA20-C1 airplanes; (xi) Diamond Aircraft Industries, Inc. (type certificate previously held by Diamond Aircraft Industries GmbH), Model DA 40 and DA 40F airplanes; (xii) Discovery Aviation, Inc. (type certificate previously held by Liberty Aerospace Incorporated), Model XL-2 airplanes; (xiii) Dynac Aerospace Corporation Model Aero Commander 100, Aero Commander 100A, Aero Commander 100-180, Volaire 10, and Volaire 10A airplanes; (xiv) EADS-PZL "Warszawa-Okecie" S.A. (type certificate previously held by Panstwowe Zaklady Lotnicze) Model PZL-104 WILGA 80, PZL-104M WILGA 2000, PZL-104MA WILGA 2000, PZL-KOLIBER 150A, and PZL-KOLIBER 160A airplanes; (xv) Extra Flugzeugproduktions- und Vertriebs- GmbH (type certificate previously held by Extra Flugzeugbau GmbH) Model EA 300, EA 300/L, EA 300/S, EA 300/200, and EA 400 airplanes; (xvi) Frakes Aviation (type design controlled by FAA, Southern Region, for Grumman American Aviation Corporation) Model G-44 (Army OA-14, Navy J4F-2), G-44A, and SCAN Type 30 airplanes; (xvii) FS 2003 Corporation (type certificate previously held by The New Piper Aircraft, Inc.) Model PA-12 and PA-12S airplanes; (xviii) GROB Aircraft AG (type certificate previously held by GROB Aerospace GmbH i.l.) Model G115, G115A, G115B, G115C, G115C2, G115D, G115D2, G115EG, and G120A airplanes; (xix) Helio Aircraft, LLC, Model H-250, H-295 (USAF U-10D), H- 391 (USAF UL-24), H-391B, H-395 (USAF L-28A and U-10B), H-395A, H- 700, H-800, HST-550, HST-550A (USAF AU-24A), and HT-295 airplanes; (xx) Interceptor Aviation, Inc. (type certificate previously held by Interceptor Aircraft Corporation), Model 200, 200A, 200B, 200C, 200D, and 400 airplanes; (xxi) Lockheed Martin Aeronautics Company Model 402-2 airplanes; (xxii) Maule Aerospace Technology, Inc. (type certificate previously held by Maule Aircraft Corporation), Model Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M-4-180C, M-4-180S, M-4-180T, M-4-210, M-4- 210C, M-4-210S, M-4-210T, M-4-220, M-4-220C, M-4-220S, M-4-220T, M- 5-180C, M-5-200, M-5-210C, M-5-210TC, M-5-220C, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, M-7-420A, M-7-420AC, M-8-235, MT-7-235, MT-7-260, MT-7-420, MX-7- 160, MX-7-160C, MX-7-180, MX-7-180A, MX-7-180AC, MX-7-180B, MX-7- 180C, MX-7-235, MX-7-420, MXT-7-160, MXT-7-180, and MXT-7-180A airplanes; (xxiii) Mooney Aircraft Corporation Model M22 airplanes. (xxiv) Mooney International Corporation (type certificate previously held by Mooney Aviation Company, Inc.) Model M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, and M20S airplanes; (xxv) Pacific Aerospace, Ltd. (type certificate previously held by Found Aircraft Canada, Inc.), Model FBA-2C, FBA-2C1, and FBA-2C2 airplanes; (xxvi) Pilatus Aircraft, Ltd., Model PC-6, PC-6-H1, PC-6-H2, PC- 6/350, PC-6/350-H1, PC-6/350-H2, PC6/A, PC-6/A-H1, PC-6/A-H2, PC-6/ B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes; (xxvii) Piper Aircraft, Inc. (type certificate previously held by The New Piper Aircraft, Inc.), Model PA-18, PA-18 "105" (Special), PA-18 "125" (Army L-21A), PA-18 "135" (Army L-21B), PA-18 "150," PA-18A, PA-18A"135," PA-18A "150," PA-18AS "125," PA-18AS "135," PA-18AS "150," PA-18S, PA-18S "105" (Special), PA-18S "125," PA-18S "135," PA-18S "150," PA-19 (Army L-18C), PA-19S, PA-20, PA-20 "115," PA-20 "135," PA-20S, PA-20S "115," PA-20S "135," PA-22, PA-22-108, PA-22-135, PA-22- 150, PA-22-160, PA-22S-135, PA-22S-150, PA-22S-160, PA-23, PA-23- 160, PA-23-235, PA-23-250, PA-24, PA-24-250, PA-24-260, PA-24-400, PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, 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-28S-160, PA- 28S-180, PA-30, PA-32-260, PA-32-300, PA-32-301, PA-32-301FT, PA-32- 301T, PA-32-301XTC, PA-32R-300, PA-32R-301 (HP), PA-32R-301 (SP), PA-32R-301T, PA-32RT-300, PA-32RT-300T, PA-32S-300, PA-34-200, PA- 34-200T, PA-34-220T, PA-39, PA-40, PA-44-180, PA-44-180T, PA-46- 310P, and PA-46-350P airplanes; (xxviii) Polskie Zaklady Lotnieze Spolka zo.o (type certificate previously held by PZL MIELEC) Model PZL M26 01 …
- AD 2009-26-01 One-time
Cirrus Design Corporation Model SR22 Airplanes
We are issuing this AD to detect and correct anti-ice fluid distribution lines with improperly installed compression fittings, which could result in anti-ice fluid distribution line separation.
Applicability, as the AD words it
This AD applies to Model SR22 airplanes; serial numbers 3409, 3411 through 3430, 3432 through 3441, 3443 through 3450, 3455 through 3465, 3467, 3468, 3470 through 3472, 3485, 3486, 3488, 3489, 3491 through 3493, 3495 through 3500, 3504, 3505, 3512, 3513, 3517, 3524, 3525, 3528, and 3546 that are: (1) Equipped with an anti-ice system approved for flight into known icing; and (2) Certificated in any category.
- AD 2009-05-05 One-time Appliance
Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)
We are issuing this AD to prevent certain conditions from existing when PFDs display incorrect attitude, altitude, and airspeed information.
Applicability, as the AD words it
This AD applies to Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs), part numbers (P/Ns) 700-00006-000, 700- 00006-001, 700-00006-002, 700-00006-003, and 700-00006-100 with any serial number listed in Avidyne Service Bulletin No. 601-00006-096, Revision 1, dated July 14, 2008. Paragraph (d) of this AD gives procedures to determine if an affected serial number is installed on your airplane. This AD applies to affected serial number PFDs that are installed on, but not limited to the airplanes below that are certificated in any category. (1) Adam Aircraft Model A500; (2) Cessna Aircraft Company Model 441 (STEC Alliant Supplemental Type Certificate (STC) No. SA09547AC-D incorporated); (3) Cessna Aircraft Company Models LC42-550FG and LC41-550FG (Columbia Aircraft Manufacturing and The Lancair Company previously held the type certificate for these airplanes); (4) Cirrus Design Corporation Models SR20 and SR22; (5) Diamond Aircraft Industries GmbH Model DA 40; (6) Hawker Beechcraft Corporation Model E90 (STEC Alliant STC No. SA09545AC-D incorporated); (7) Hawker Beechcraft Corporation Model 200 series (STEC Alliant STC No. SA09543AC-D incorporated); and (8) Piper Aircraft, Inc. Models PA-28-161, PA-28-181, PA-28R- 201, PA-32R-301 (HP), PA-32R-301T, PA-32-301FT, PA-32-301XTC, PA-34- 220T, PA-44-180, PA-46-350P, PA-46R-350T, and PA-46-500TP. (d) If you have one of the affected part number PFDs installed on your airplane, you must positively show that it is not one of the affected serial numbers or comply with paragraph (f), all subparagraphs, as applicable in this AD. Under 14 CFR 43.7, the owner/operator holding at least a private pilot certificate is allowed to do the check in paragraph (d)(1) of this AD. All other actions must be done by a certificated mechanic, unless noted differently. (1) Do a logbook check of aircraft records (previously referred to in AD 2008-06-28 R1 as "maintenance records") to determine if any PFD (P/Ns 700-00006-000, 700-00006-001, 700-00006-002, 700- 00006-003, or 700-00006-100) with any affected serial number listed in Avidyne Service Bulletin No. 601-00006-096, Revision 1, dated July 14, 2008, is installed. (i) If, as a result of the logbook check, you positively identify that the PFD installed does not have a serial number affected by this AD, then only paragraph (f)(5) of this AD applies to you. (ii) If, as a result of the logbook check, you cannot positively identify the serial number of the PFD, do the visual inspection required in paragraph (d)(2) of this AD. (iii) If, as a result of the logbook check, you find any PFD installed with an affected serial number, do the actions required by paragraph (f) of this AD, including all subparagraphs as applicable. (2) If, as a result of the above logbook check, you cannot positively identify the serial number of the PFD, visually inspect any PFD (P/Ns 700-00006-000, 700-00006-001, 700-00006-002, 700- 00006-003, or 700-00006-100) for any affected serial number listed in Avidyne Service Bulletin No. 601-00006-096, Revision 1, dated July 14, 2008. (i) If, as a result of this visual inspection, you positively identify that the PFD installed does not have a serial number affected by this AD, then only paragraph (f)(5) of this AD applies to you. (ii) If, as a result of this visual inspection, you identify that the PDF installed does have a serial number affected by this AD, do the actions required in paragraph (f) of this AD, including all subparagraphs as applicable.
- AD 2008-14-13 One-time
Cirrus Design Corporation Model SR20 and SR22 Airplanes
We are issuing this AD to prevent in-flight failure of the cabin door, which could result in door separation from the airplane.
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that are certificated in any category: Models Serial Nos. SR20: 1423 through 1906. SR22: 0795 and 0820 through 2912.
- AD 2008-06-28 Superseded by AD 2009-05-05 Appliance
Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)
We are issuing this AD to prevent certain conditions from existing when PFDs display incorrect attitude, altitude, and airspeed information.
Applicability, as the AD words it
None. Applicability (c) This AD applies to Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs) (Part Numbers (P/Ns) 700-00006-000, 700- 00006-001, 700-00006-002, 700-00006-003, and 700-00006-100) that are installed on, but not limited to the following airplanes that are certificated in any category: (1) Adam Aircraft Model A500; (2) Cessna Aircraft Company Model 441 (STEC Alliant Supplemental Type Certificate (STC) No. SA09547AC-D incorporated); (3) Cessna Aircraft Company Models LC42-550FG and LC41-550FG (Columbia Aircraft Manufacturing and The Lancair Company previously held the type certificate for these airplanes); (4) Cirrus Design Corporation Models SR20 and SR22; (5) Diamond Aircraft Industries GmbH Model DA 40; (6) Hawker Beechcraft Corporation Model E90 (STEC Alliant STC No. SA09545AC-D incorporated); (7) Hawker Beechcraft Corporation Model 200 series (STEC Alliant STC No. SA09543AC-D incorporated); and (8) Piper Aircraft, Inc. Models PA-28-161, PA-28-181, PA-28R- 201, PA-32R-301 (HP), PA-32R-301T, PA-32-301FT, PA-32-301XTC, PA-34- 220T, PA-44-180, PA-46-350P, PA-46R-350T, and PA-46-500TP.
- AD 2008-03-16 One-time
Cirrus Design Corporation Models SR20 and SR22 Airplanes
We are issuing this AD to prevent the possibility of jamming of the rudder-aileron interconnect system, which may result in loss of rudder and aileron flight controls.
Applicability, as the AD words it
This AD applies to Model SR20 airplanes, serial numbers (SN) 1005 through 1861, and Model SR22 airplanes, SN 0002 through 2333, SN 2335 through 2419, and SN 2421 through 2437, that are certificated in any category.
- AD 2007-24-13 One-time
Cirrus Design Corporation Model SR22 Airplanes
We are issuing this AD to prevent moisture from accumulating along the wing shear web where it may freeze in certain conditions.
Applicability, as the AD words it
This AD applies to Model SR22 airplanes, serial numbers 2334, 2420, and 2438 through 2749, that are certificated in any category.
- AD 2007-16-10 One-time Engine
Teledyne Continental Motors Reciprocating (TCM) Engine Models IO-550-N, TSIO-520-BE, TSIO-550-A, TSIO-550-B, TSIO-550-C, TSIO-550-E, and TSIO-550-G
We are issuing this AD to prevent the turbine rotor from separating from the shaft of the turbocharger due to a machining defect in the turbocharger compressor.
Applicability, as the AD words it
This AD applies to: (1) Teledyne Continental Motors (TCM) models TSIO-520-BE, TSIO- 550-A, TSIO-550-B, TSIO-550-C, TSIO-550-E, and TSIO-550-G reciprocating engines with a Kelly Aerospace Power Systems turbocharger, TCM part number (P/N) 646677, with certain serial numbers (SNs), installed on or after March 20, 2007. These engines are installed on, but not limited to, Adam Aircraft A500, Columbia Aircraft Manufacturing LC41-550FG, Mooney Airplane Company M20TN (Acclaim), and Piper Aircraft Incorporated PA-46-310P (Malibu) airplanes. (2) TCM IO-550-N reciprocating engines modified to Engine Technologies Incorporated supplemental type certificate (STC) SE10589SC to install turbocharger, P/N 466304-0003, with certain SNs, installed on or after March 20, 2007. These engines are installed on, but not limited to, Cirrus Design Corporation Aircraft Model SR22 modified to Engine Technologies Incorporated STC SA10588SC.
- AD 2007-14-03 One-time
Cirrus Design Corporation Models SR20 and SR22 Airplanes
We are issuing this AD to correct pick-up collar support fasteners of the CAPS, which could result in the premature separation of the collar.
Applicability, as the AD words it
This AD applies to Model SR20 airplanes, serial numbers (SN) 1005 through 1798, and Model SR22 airplanes, SN 0002 through 2437, that: (1) Are certificated in any category; and (2) have not incorporated the actions in their entirety of Cirrus Alert Service Bulletin No. SB A2X-95-10 R1, Issued April 2, 2007, Revised: April 10, 2007.
- AD 2006-21-03 One-time
Cirrus Design Corporation Models SR20 and SR22 Airplanes
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers (S/N) that are certificated in any category: (1) Group 1: Model SR20 Airplanes, S/N 1005 through 1600. (2) Group 2: Model SR22 Airplanes, S/N 0002 through 1739. (3) Group 3: Model SR20 Airplanes, S/N 1005 through 1592. (4) Group 4: Model SR22 Airplanes, S/N 0002 through 1727.
- AD 2006-19-10 Recurring
Cirrus Design Corporation Models SR20 and SR22 Airplanes
We are issuing this AD to prevent the crew seats from folding forward during emergency landing with dynamic loads with consequent occupant injury.
Applicability, as the AD words it
This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. (1) SR20: 1005 through 1600. (2) SR22: 0002 through 1727.
- AD 2006-07-06 One-time
Cirrus Design Corporation Models SR20 and SR22 Airplanes
Applicability, as the AD words it
This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. SR20: 1005 through 1581. SR22: 0002 through 1643 and 1645 through 1662.
- AD 2005-17-19 Superseded by AD 2006-19-10
Cirrus Design Corporation Models SR20 and SR22 Airplanes
Applicability, as the AD words it
This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. (1) SR20: 1005 through 1455. (2) SR22: 0002 through 1044.
- AD 2005-01-19 One-time Appliance
GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders
Applicability, as the AD words it
This AD affects GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S transponders that include software versions 3.00, 3.01, 3.02, 3.04, or 3.05 that are installed on, but not limited to, the following airplanes, certificated in any category: Manufacturer Model (1) Aermacchi S.p.A: S.205-18/F, S.205-18/R, S.205-20/R, S.205- 22/R, S208, S.208A, F.260, F.260B, F.260C, F.260D, F.260E, F.260F, S.211A. (2) Aeronautica Macchi S.p.A. AL 60, AL 60-B, AL 60-F5, AL 60-C5, AM-3. (3) Aerostar Aircraft PA-60-600 (Aerostar 600), PA-60-601 Corporation. (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), PA-60- 700P (Aerostar 700P), 360, 400. (4) Alexandria Aircraft, LLC. 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-31, 17-31TC, 17-30A, 17-31A, 17-31ATC (5) Alliance Aircraft Group 15A, 20, H-250, H-295 (USAFU-10D), HT- LLC. 295, H391 (USAFYL-24), H391B, H-395 (USAFL-28A or U-10B), H-395A, H-700, H- 800, HST-550, HST-550A (USAF AU-24A), 500. (6) American Champion 402, 7GCA, 7GCB, 7KC, 7GCBA, 7GCAA, Aircraft Corp. 7GCBC, 7KCAB, 8KCAB, 8GCBC. (7) Sky International Inc: A-1, A-1A, A-1B, S-1S, S-1T, S-2, S-2A, S- 2S, S-2C. (8) B-N Group Ltd: BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-8, BN-2A-20, BN-2A-21, BN- 2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN- 2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN- 2B-26, BN-2B-27, BN-2T, BN-2T-4R, BN-2A MK.III, BN2A MK. III-2, BN2A MK. 111-3. (9) Bellanca: 14-13, 14-13-2, 14-13-3, 14-13-3W. (10) Bombardier Inc: (Otter) DHC-3, DHC-6-1, DHC-6-100, DHC-6- 200, DHC-6-300. (11) Cessna Aircraft Company. 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T041A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, 172RG, P172D, R172E (USAF T-41 B) (USAF T-41 C AND D), R172F (USAF T-41 D), R175G, R172H (USAF T-41 D), R172J, R172K, 175, 175A, 175B, 175C, 177, 177A, 177B, 177RG, 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, R182, T182, TR182, T182T, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 190, (LC-126A, B, C) 195, 195A, 195B, 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, P210N, T210N, 210R, P210R, T210R, 210-5 (205), 210-5A (205A), 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H, 207, 207A, T207, T207A, 208, 208A, 208B, 310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 320, 320A, 320B, 320C, 320D, 320E, 320F, 320-1, 335, 340, 340A, 336, 337, 337A (USAF 02B), 337B, T337B, 337C, 337E, T337E, T337C, 337D, T337D, M337B (USAF 02A), 337F, T337F, T337G, 337G, 337H, P337H, T337H, T337H-SP, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, 404, 406, 441. (12) Cirrus Design SR20, SR22. Corporation. (13) Commander Aircraft 112, 112TC, 112B, 112TCA, 114, 114A, Company. 114B, 114TC. (14) de Havilland Inc: DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III. (15) Dynac Aerospace (Volaire) 10, (Volaire) 10A, (Aero Corporation. Commander) 100, (Aero Commander) 100A, (Aero Commander) 100-180. (16) Diamond Aircraft DA 20-A1, DA20-C1, DA 40. Industries. (17) Empressa Brasileira de EMB-110P1, EMB-110P2. Aeronautica S.A. EMBRAER. (18) Extra Flugzeugbau Gmbh.. EA300, EA300L, EA300S, EA300/200, EA-400. (19) Fairchild Aircraft SA26-T, SA26-AT, SA226-T, SA226-AT, SA226- Corporation. T(B), SA227-AT, SA227-TT, SA226-TC, SA227-AC (C-26A), SA227-CC, SA227-DC (C- 26B). (20) Global Amphibians, LLC.. Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, Lake Model 250. (21) Grob-Werke: G115, G115A, G115B, G115C, G115C2, G115D, G115D2, G115EG, G120A. (22) Lancair Company: LC40-550FG. (23) LanShe Aerospace, LLC... MAC-125C, MAC-145, MAC-145A, MAC-145B. (24) Learjet Inc: 23. (25) Lockheed Aircraft 18. Corporation. (26) Luscombe Aircraft 11A, 11E. Corporation. (27) Maule Aerospace Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M- Technology, Inc. 4180C, M-4-180S, M-4-180T, M-4-210, M-4- 210C, M-4-210S, M-4-210T, M-4-220, M-4- 220S, M-4-220T, M-5-180C, M-5-200, M-5- 210C, M-5-210TC, M-5-220C, M-5-235C, M-6- 180, M-6-235, M-7-235, MX-7-235, MX-7- 180, MX-7-420, MXT-7-180, MT-7-235, M-8- 235, MX-7-160, MXT-7-160, MX-7-180A, MXT- 7-180A, MX-7-180B, M-7-235B, M-7-235A, M- 7-235C, MX-7-180C, M-7-260, MT-7-260, M- 7-260C, M-7-420AC, MX-7-160C, MX-7- 180AC, M-7-420A, MT-7-420. (28) Mitsubishi Heavy MU-2B-25, MU-2B-35, MU-2B-26, MU-2B-36, Industries, Ltd. MU-2B-26A, MU-2B-36A, MU-2B-40, MU-2B- 60, MU-2B, MU-2B-20, MU-2B-15. (29) Mooney Airplane Company, M20, M20A, M20B, M20C, M20D, M20E, M20F, Inc. M20G, M20J, M20K, M20L, M20M, M20R, M20S, M22. (30) Moravan a.s: Z-242L, Z-143L. (31) Navion Aircraft Company, NAVION, Navion (L-17A), Navion (L17B), Ltd. Navion (L-17C), Navion B, Navion D, Navion E, Navion F, Navion G, Navion H. (32) New Piper Aircraft, Inc. PA-12, PA-12S, PA-18, PA-18S, PA-18 "105" (Special), PA-18S "105" (Special), PA-18A, PA-18 "125" (Army L- 21A), PA-18S "125," PA-18AS "125," PA-18 "135" (Army L-21B), PA-18A "135," PA-18S "135," PA-18 "150," PA-18A "150," PA-18S "150," PA-18AS "150," PA-19 (Army L-18B), PA-19S, PA- 20, PA-20S, PA-20 "115," PA-20S "115," PA-20 "135," PA-20S "135," PA-22, PA-22-108, PA-22-135, PA-22S-135, PA-22-150, PA-22S-150, PA-22-160, PA-22S- 160, PA-23, PA-23-160, PA-23-235, PA-23- 250, PA-E23-250, PA-24, PA-24-250, PA-24- 260, PA-24-400, PA-28-140, PA-28-150, PA- 28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-235, PA-28S-160, PA-28R-180, PA- 28S-180, PA-28-181, PA-28R-200, PA-28R- 201, PA-28R-201T, PA-28RT-201, PA-28RT- 201T, PA-28-201T, PA-28-236, PA-30, PA- 39, PA-40, PA-31P, PA-31T, PA-31T1, PA- 31T2, PA-31T3, PA-31P-350, PA-32-260, PA- 32-300, PA-32S-300, …
- AD 2004-10-15 Superseded by AD 2005-01-19 Appliance
GARMIN International Inc. GTX 330 Mode S Transponders and GTX 330D Diversity Mode S Transponders
Applicability, as the AD words it
This AD affects GARMIN International Inc. GTX 330/330D Mode S transponders that are installed on, but not limited to, the following airplanes, certificated in any category: Manufacturer Model (1) Aermacchi S.p.A: S.205-18/F, S.205-18/R, S.205-20/R, S.205- 22/R, S.208, S.208A, F.260, F.260B, F.260C, F.260D, F.260E, F.260F, S.211A. (2) Aeronautica Macchi S.p.A. AL 60, AL 60-B, AL 60-F5, AL 60-C5, AM-3. (3) Aerostar Aircraft PA-60-600 (Aerostar 600), PA-60-601 Corporation. (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), PA-60- 700P (Aerostar 700P), 360, 400. (4) Alexandria Aircraft, LLC. 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-31, 17-31TC, 17-30A, 17-31A, 17- 31ATC. (5) Alliance Aircraft Group 15A, 20, H-250, H-295, (USAFU-10D), HT- LLC. 295, H391 (USAFYL-24), H391B, H-395 (USAFL-28A or U-10B), H-395A, H-700, H- 800, HST-550, HST-550A (USAF AU-24A), 500. (6) American Champion 402, 7GCA, 7GCB, 7KC, 7GCBA, 7GCAA, Aircraft Corp. 7GCBC, 7KCAB, 8KCAB, 8GCBC. (7) Sky International Inc: A-1, A-1A, A-1B, S-1S, S-1T, S-2, S-2A, S- 2S, S-2C. (8) B-N Group Ltd: BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN-2T-4R, BN-2A MK.III, BN2A MK.III-2, BN2A MK.111-3. (9) Bellanca: 14-13, 14-13-2. 14-13-3. 14-13-3W. (10) Bombardier Inc: (Otter) DHC-3, DHC-6-1, DHC-6-100, DHC-6- 200, DHC-6-300. (11) Cessna Aircraft Company. 170, 170A, 170B, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H, (USAF T041A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, 172RG, P172D, R172E (USAF T-41 B) (USAF T-41 C AND D), R172F (USAF T-41 D), R175G, R172H (USAF T-41 D), R172J, R172K, 175, 175A, 175B, 175C, 177, 177A, 177B, 177RG, 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, R182, T182, TR182, T182T, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, 190, (LC-126A, B, C) 195, 195A, 195B, 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, P210N, T210N, 210R, P210R, T210R, 210-5 (205), 210-5A (205A), 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H, 207, 207A, T207, T207A, 208, 208A, 208B, 310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 320, 320A, 320B, 320C, 320D, 320E, 320F, 320-1, 335, 340, 340A, 336, 337, 337A (USAF 02B), 337B, T337B, 337C, 337E, T337E, T337C, 337D, T337D, M337B (USAF 02A), 337F, T337F, T337G, 337G, 337H, P337H, T337H, T337H-SP, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, 404, 406, 441. (12) Cirrus Design SR20, SR22. Corporation. (13) Commander Aircraft 112, 112TC, 112B, 112TCA, 114, 114A, Company. 114B, 114TC. (14) de Havilland Inc: DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III. (15) Dynac Aerospace (Volaire) 10, (Volaire) 10A, (Aero Corporation. Commander) 100, (Aero Commander) 100A, (Aero Commander) 100-180. (16) Diamond Aircraft DA-20-A1, DA20-C1, DA 40. Industries. (17) Empressa Brasileira de EMB-110P1, EMB-110PE. Aeronautica S.A. EMBRAER. (18) Extra Flugzeugbau Gmbh.. EA300, EA300L, EA300S, EA300/200, EA-400. (19) Fairchild Aircraft SA26-T, SA26-AT, SA226-T, SA226-AT, SA226- Corporation. T(B), SA227-AT, SA227-TT, SA226-TC, SA227-AC (C-26A), SA227-CC, SA227-DC (C- 26B). (20) Global Amphibians, LLC.. Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, Lake Model 250. (21) Grob-Werke: G115, G115A, G115B, G115C, G115C2, G115D, G115D2, G115EG, G120A. (22) Lancair Company: LC40-550FG. (23) LanShe Aerospace, LLC... MAC-125C, MAC-145, MAC-145A, MAC-145B. (24) Learjet Inc: 23. (25) Lockheed Aircraft 18. Corporation. (26) Luscombe Aircraft 11A, 11E. Corporation. (27) Maule Aerospace Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M- Technology, Inc. 4180C, M-4-180S, M-4-180T, M-4-210, M-4- 210C, M-4-210S, M-4-210T, M-4-220, M-4- 220S, M-4-220T, M-5-180C, M-5-200, M-5- 210C, M-5-210TC, M-5-220C, M-5-235C, M-6- 180, M-6-235, M-7-235, MX-7-235, MX-7- 180, MX-7-420, MXT-7-180, MT-7-235, M-8- 235, MX-7-160, MXT-7-160, MX-7-180A, MXT- 7-180A, MXT-7-180B, M-7-235B, M-7-235A, M-7-235C, M-7-180C, M-7-260, MT-7-260, M- 7-260C, M-7-420AC, MX-7-160C, MX-7- 180AC, M-7-420A, MT-7-420. (28) Mitsubishi Heavy MU-2B-25, MU-2B-35, MU-2B-26, MU-2B-36, Industries, Ltd. MU-2B-26A, MU-2B-36A, MU-2B-40, MU-2B- 60, MU-2B, MU-2B-20, MU-2B-20, MU-2B-15. (29) Mooney Airplane Company, M20, M20A, M20B, M20C, M20D, M20E, M20F, Inc. M20G, M20J, M20K, M20L, M20M, M20R, M20S, M22. (30) Moravan a.s: Z-242L, Z-143L. (31) Navion Aircraft Company, NAVION, Navion (L-17A), Navion (L-17B), Ltd. Navion (L-17C), Navion B, Navion D, Navion E, Navion F, Navion G, Navion H. (32) New Piper Aircraft, Inc. PA-12, PA-12S, PA-18, PA-18S, PA-18 "105" (Special), PA-18S "105" (Special), PA-18A, PA-18 "125" (Army L- 21A), PA-18S "125," PA-18AS "125," PA-18 "135" (Army L-21B), PA-18A "135," PA-18S "135," PA-18 "150," PA-18A "150," PA-18S "150," PA-18AS "150," PA-19 (Army L-18B), PA-19S, PA- 20, PA-20S, PA-20 "115," PA-20S "115," PA-20 "135," PA-20S "135," PA-22, PA-22-108, PA-22-135, PA-22S-135, PA-22-150, PA-22S-150, PA-22-160, PA-22S- 160, PA-23, PA-23-160, PA-23-235, PA-23- 250, PA-E23-250, PA-24, PA-24-250, PA-24- 260, PA-24-400, PA-28-140, PA-28-150, PA- 28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-235, PA-28S-160, PA-28R-180, PA- 28S-180, PA-28-181, PA-28R-200, PA-28R- 201, PA-28R-201T, PA-28RT-201, PA-28RT- 201T, PA-28-201T, PA-28-236, PA-30, PA- 39, PA-40, PA-31P, PA-31T, PA-31T1, PA- 31T2, PA-31T3, PA-31P-350, PA-32-260, PA- 32-300, PA-32S-300, PA-32R-300, PA-32RT- 300, PA-32RT-300T, PA-32R-301 (SP), PA- 32R-301 (HP), PA-32R-301T, …
- AD 2002-24-08 One-time
Cirrus Design Corporation Models SR20 and SR22 Airplanes
Applicability, as the AD words it
This AD applies to each airplane identified in paragraph (a) of this AD, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/ operator must request approval for an alternative method of compliance in accordance with paragraph (f) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if you have not eliminated the unsafe condition, specific actions you propose to address it. (g) Where can I get information about any already-approved alternative methods of compliance? Contact Gregory J. Michalik, Aerospace Engineer, FAA, Chicago ACO, 2300 East Devon Avenue, Des Plaines, IL 60018; telephone: (847) 294-7135; facsimile: (847) 294- 7834. (h) What if I need to fly the airplane to another location to comply with this AD? The FAA can issue a special flight permit under sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate your airplane to a location where you can accomplish the requirements of this AD. (i) Are any service bulletins incorporated into this AD by reference? Actions required by this AD must be done in accordance with Cirrus Service Bulletin SB 20-95-03, Issued: June 10, 2002; Cirrus Service Bulletin SB 20-95-04, Issued: July 10, 2002; Cirrus Service Bulletin SB 20-95-05, Issued: July 10, 2002; Cirrus Service Bulletin SB 20-95-05, Rev 1: dated August 14, 2002; Cirrus Service Bulletin SB 22-95-03, Issued: June 10, 2002; Cirrus Service Bulletin SB 22-95-04, Issued: July 10, 2002; Cirrus Service Bulletin SB 22- 95-05, Issued: July 10, 2002; and Cirrus Service Bulletin SB 22-95- 05, Rev 1: dated August 14, 2002. The Director of the Federal Register approved this incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51. You may get copies from Cirrus Design Corporation, 4515 Taylor Circle, Duluth, MN 55811; telephone: (218) 727-2737. 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. (j) Does this AD action affect any existing AD actions? This amendment supersedes AD 2002-05-05, Amendment 39-12673. (k) When does this amendment become effective? This amendment becomes effective on January 24, 2003. Issued in Kansas City, Missouri, on November 26, 2002. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 02-30685 Filed 12-9-02; 8:45 am] BILLING CODE 4910-13-P
- AD 2002-21-02 One-time
Cirrus Design Corporation Model SR20 and SR22 Airplanes
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial numbers SR20 1005 through 1241, except 1235, 1237, and 1238. SR22 0002 through 0333, except 0309, 0322, 0323, and 0328. (b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to prevent loss of the self-locking retaining nut on the roll and yaw trim cartridges during flight, which could result in jamming of the corresponding flight control system. Such jamming could lead to loss of control of the airplane. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance Procedures (1) Replace the self-locking Within the next 10 In accordance with retaining nut on the yaw hours time-in- Cirrus Alert trim cartridge and the roll service after Service Bulletin SB trim cartridge with a new November 8, 2002 A20-27-06, Issued: self-locking retaining nut, (the effective date September 20, 2002, part number MS21044N3. of this AD), unless and Cirrus Alert already Service Bulletin SB accomplished. A22-27-03, Issued: September 20, 2002, as applicable. (2) Do not install any self- As of November 8, Not applicable. locking retaining nut on 2002 (the effective the yaw trim cartridge or date of this AD). the roll trim cartridge that is not part number MS21044N3. (e) Can I comply with this AD in any other way? You may use an alternative method of compliance or adjust the compliance time if: (1) Your alternative method of compliance provides an equivalent level of safety; and (2) The Manager, Chicago Aircraft Certification Office (ACO), approves your alternative. Submit your request through an FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Chicago ACO. Note: 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 Gregory J. Michalik, Aerospace Engineer, FAA, Chicago ACO, 2300 East Devon Avenue, Des Plaines, IL 60018; telephone: (847) 294-7135; facsimile: (847) 294- 7834. (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 o
- AD 2002-13-04 Superseded by AD 2011-26-07 Appliance
Teledyne Continental Motors
To prevent engine failure and loss of control of the airplane due to migration of the magneto impulse coupling stop pin out of the magneto frame and into the gear train of the engine.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Teledyne Continental Motors (TCM) C-125, C145, O-300, IO-360, TSIO-360, and LTSIO-520-AE series reciprocating engines with Unison Industries (Slick) Magnetos, models 6314, 6324, and 6364, with magneto serial numbers of 99110001 through 9912999 inclusive. These engines are used on, but not limited to Cessna 170, 170A, 170B, 172, 172A through 172H, 172XP, 336, 337, and T303, Beagle B242-C, Cirrus SR20 and SR22, Globe Swift GC-1A and GC-1B, Maule M4, Piper PA-28R-201T and PA-34, and Reims (Cessna) FA172, F337, and FR172.
- AD 2002-05-05 Superseded by AD 2002-24-08
Cirrus Design Corporation Models SR20 and SR22 Airplanes
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial Numbers (1) Group 1 SR20: 1148 through 1178, except 1151 SR22: 0029 through 0160, except 0159 (2) Group 2 SR20: 1005 through 1147 SR22: 0002 through 0028 (b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to initially limit the chance of failure of the CAPS activation system in an emergency situation and eventually eliminate this potential failure. Failure of this system would result in occupant injury and/or loss of life and loss of aircraft. (d) What must I do to address this problem? To address this problem, you must perform the following actions, unless already accomplished: Actions Compliance Procedures (1) For Group 1 airplanes: Prior to further The owner/operator in order reduce the need to flight after March holding at least a use the CAPS system in a 19, 2002 (the private pilot loss of aircraft control effective date of certificate as emergency situation, this AD) until the authorized by incorporate the following installation section 43.7 of the into the Limitation Section required by Federal Aviation of the airplane flight paragraph (d)(2) of Regulations (14 CFR manual (AFM): this AD is 43.7) may "(i) Do not operate the accomplished. incorporate into airplane in instrument the AFM the flight rules (IFR) information conditions, only operate specified in the airplane in visual paragraphs flight rules (VFR) (d)(1)(i) and conditions; and. (d)(1)(ii) of this (ii) Operate the airplane AD. Make an entry during daytime hours only, into the aircraft do not operate at night.. records showing compliance with this portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (2) For all affected For Group 1 In accordance with airplanes: in order to airplanes: within Ballistic Recovery prevent the cable housing the next 10 hours Systems Inc. from going into the rock
- AD 2001-25-03 One-time
Cirrus Design Corporation Models SR20 and SR22 Airplanes
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. SR20: 1134 through 1159. SR22: 0003 through 0119. (b) Who must comply with this AD? Anyone who wishes to operate any of the above airplanes must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to detect and replace understrength rivets in the elevator and rudder, which could result in failure of the control surfaces. Such failure could lead to a loss of control of the airplane in flight. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance Procedures (1) Inspect for Within the next 10 For Model SR 20 understrength rivets on the hours time-in- airplanes, follow elevator torque tube and service after the ACCOMPLISHMENT rudder hinge. December 17, 2001 INSTRUCTIONS (the effective date section in Cirrus of this AD). Design Service Bulletin SB 20-55- 06, issued November 27, 2001. For Model SR 22 airplanes, follow the ACCOMPLISHMENT INSTRUCTIONS section in Cirrus Design Service Bulletin SB 22-55- 03, issued November 27, 2001. (2) If an understrength Before further For Model SR 20 rivet is found, replace it flight after the airplanes, follow with a new rivet, part inspection the ACCOMPLISHMENT number MS20470AD4, or FAA- referenced in INSTRUCTIONS approved equivalent part paragraph (d)(1) of section in Cirrus number. this AD. Design Service Bulletin SB 20-55- 06, issued November 27, 2001. For Model SR 22 airplanes, follow the ACCOMPLISHMENT INSTRUCTIONS section in Cirrus Design Service Bulletin SB 22-55- 03, issued November 27, 2001. (3) Do not install part As of December 17, Not Applicable. number MS20470A4 rivet. 2001 (the effective date of this AD).
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.