# N428AM: 2020 Cirrus Design SR22

- Status: Valid registration
- Airframe: [Cirrus Design SR22](https://openairdocs.org/model/cirrus-design-sr22) (registry code 2130001, 4 seats)
- Engine: [Continental IO-550-N](https://openairdocs.org/engine/continental-io-550-n) (registry code 17215)
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E3SO](https://openairdocs.org/tcds/E3SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 4896
- Year built: 2020
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: March 4, 2020
- Certificate issued: April 21, 2020
- Expires: April 30, 2030
- Mode S code: A51963
- Registered owner: [T G Mendell Corp](https://openairdocs.org/faa-owner/T%20G%20MENDELL%20CORP)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.7734° N, 73.9563° W: Placed by OpenAirDocs at the center of ZIP code 10075, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=428AM
- Page: https://openairdocs.org/aircraft/N428AM

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 34 in force

### Matched by airframe (Cirrus Design SR22)

- [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2009-26-01](https://openairdocs.org/ad/2009-26-01): Ice and Rain protection · Cirrus Design SR22. Effective Dec 21, 2009
- [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009
- [AD 2008-14-13](https://openairdocs.org/ad/2008-14-13): Upper door hinge · Cirrus Design SR20 and SR22. Effective Aug 14, 2008
- [AD 2008-03-16](https://openairdocs.org/ad/2008-03-16): Rudder, aileron, and rudder-aileron interconnect rigging · Cirrus Design SR20 and SR22. Effective Mar 11, 2008
- [AD 2007-24-13](https://openairdocs.org/ad/2007-24-13): Install a drain hole in the left and right outboard wing tips · Cirrus Design SR22. Effective Dec 4, 2007
- [AD 2007-14-03](https://openairdocs.org/ad/2007-14-03): Cirrus Airplane Parachute System (CAPS) · Cirrus Design SR20 and SR22. Effective Aug 16, 2007
- [AD 2006-21-03](https://openairdocs.org/ad/2006-21-03): Brake caliper piston O-ring seals · Cirrus Design SR20 and SR22. Effective Nov 17, 2006
- [AD 2006-19-10](https://openairdocs.org/ad/2006-19-10): Adjust crew seat break-over bolts · Cirrus Design SR20 and SR22. Effective Oct 24, 2006
- [AD 2006-07-06](https://openairdocs.org/ad/2006-07-06): Wire harness · Cirrus Design SR20 and SR22. Effective May 11, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2002-24-08](https://openairdocs.org/ad/2002-24-08): Cable clamp · Cirrus Design SR20 and SR22. Effective Jan 24, 2003
- [AD 2002-21-02](https://openairdocs.org/ad/2002-21-02): Self-locking retaining nut · Cirrus Design SR20 and SR22. Effective Nov 8, 2002
- [AD 2001-25-03](https://openairdocs.org/ad/2001-25-03): Rivets In Elevator and Rudder · Cirrus Design SR20 and SR22. Effective Dec 17, 2001

### Matched by engine (Continental IO-550-N)

- [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023
- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023
- [AD 2020-16-11](https://openairdocs.org/ad/2020-16-11): SUMMARY: Reciprocating Cylinder Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 23 more. Effective Sep 21, 2020
- [AD 2016-16-12](https://openairdocs.org/ad/2016-16-12): Cylinder assemblies · Continental Motors LTSIO-520-AE, TSIO-520-A, TSIO-520-AE and 89 more. Effective Sep 15, 2016
- [AD 2014-05-29](https://openairdocs.org/ad/2014-05-29): SAP replacement parts manufacturer approval (PMA) investment cast cylinder assemblies · Continental Motors TSIO-520-A, TSIO-520-AE, TSIO-520-AF and 55 more. Effective Apr 25, 2014
- [AD 2012-10-13](https://openairdocs.org/ad/2012-10-13): Starter adapters · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Jun 8, 2012
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2007-16-10](https://openairdocs.org/ad/2007-16-10): Kelly Aerospace Power Systems turbochargers · Turbonormalizing system (Engine Technologies STC SE10589SC or SA10588SC). Effective Aug 23, 2007
- [AD 2004-08-10](https://openairdocs.org/ad/2004-08-10): Serial-numbered (SN) cylinders · Modify Teledyne Continental TSIO-520-NB engine (RAM Aircraft Limited Partnership STC SE09104SC or 4 others). Effective May 5, 2004
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 93-08-17](https://openairdocs.org/ad/93-08-17): Oil Pick-Up Tube · Continental Motors IO-470-A, IO-470-C, IO-470-D and 104 more. Effective Aug 23, 1993
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991
- [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988

### Historical (superseded or no longer in force)

- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008
- [AD 2005-17-19](https://openairdocs.org/ad/2005-17-19) (historical): Crew seat recline locks · Cirrus Design SR20 and SR22. Effective Oct 13, 2005
- [AD 2002-05-05](https://openairdocs.org/ad/2002-05-05) (historical): Limitation Section - Cirrus Aircraft Parachute System (CAPS) Activation Cable · Cirrus Design SR20 and SR22. Effective Mar 19, 2002
- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2011-25-51](https://openairdocs.org/ad/2011-25-51) (historical): Starter Adapter Gear Shaft · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Dec 28, 2011
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 2009-16-03](https://openairdocs.org/ad/2009-16-03) (historical): Cylinder assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 55 more. Effective Sep 9, 2009
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more

## Information bulletins (advisory) (28 in force)

- [SAIB AIR-21-05R1](https://openairdocs.org/saib/AIR-21-05R1): Engine Exhaust; Inlet check valves on turbochargers used in the Tornado Alley Turbo, Inc. turbonormalizing systems. Issued Mar 29, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-13-43R1](https://openairdocs.org/saib/CE-13-43R1): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Sep 30, 2013
- [SAIB CE-11-50](https://openairdocs.org/saib/CE-11-50): Flight Controls, Flaps. Issued Aug 26, 2011
- [SAIB CE-08-12R1](https://openairdocs.org/saib/CE-08-12R1): Electrical Power. Issued Mar 16, 2011
- [SAIB CE-11-09](https://openairdocs.org/saib/CE-11-09): Navigation  Flight Management Computing Software System. Issued Jan 5, 2011
- [SAIB CE-09-46](https://openairdocs.org/saib/CE-09-46): Landing Gear, Nose. Issued Jul 31, 2009
- [SAIB CE-09-32](https://openairdocs.org/saib/CE-09-32): Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount. Issued May 29, 2009
- [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency. Issued Oct 21, 2008
- [SAIB CE-08-46](https://openairdocs.org/saib/CE-08-46): Powerplant Exhaust & Air Conditioning. Issued Sep 9, 2008
- [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006
- [SAIB CE-06-30](https://openairdocs.org/saib/CE-06-30): . Issued Feb 9, 2006
- [SAIB CE-06-07](https://openairdocs.org/saib/CE-06-07): . Issued Nov 4, 2005
- [SAIB CE-05-88](https://openairdocs.org/saib/CE-05-88): . Issued Sep 30, 2005
- [SAIB CE-05-77](https://openairdocs.org/saib/CE-05-77): . Issued Jul 27, 2005
- [SAIB CE-04-74](https://openairdocs.org/saib/CE-04-74): . Issued Aug 3, 2004
- [SAIB CE-03-09](https://openairdocs.org/saib/CE-03-09): . Issued Dec 16, 2002
- [SAIB CE-02-34](https://openairdocs.org/saib/CE-02-34): . Issued Jun 19, 2002
- [SAIB NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [SAIB NE-18-16](https://openairdocs.org/saib/NE-18-16): POWERPLANT  Alternator Drive Coupling. Issued Jun 20, 2018
- [SAIB NE-17-11](https://openairdocs.org/saib/NE-17-11): POWERPLANT  Engine damage as a result of kickback. Issued May 10, 2017
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-10-07](https://openairdocs.org/saib/NE-10-07): Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.. Issued Nov 2, 2009
- [SAIB NE-09-08](https://openairdocs.org/saib/NE-09-08): Reciprocating Engine Cylinder Section. Issued Jan 30, 2009
- [SAIB NE-02-41](https://openairdocs.org/saib/NE-02-41): . Issued Aug 8, 2002
- [SAIB AIR-21-05](https://openairdocs.org/saib/AIR-21-05) (historical): Engine Exhaust; Inlet check valves on turbochargers used in the Tornado Alley Turbo, Inc. turbonormalizing systems. Issued Mar 17, 2021
- [SAIB CE-13-43](https://openairdocs.org/saib/CE-13-43) (historical): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Aug 30, 2013
- [SAIB CE-08-12](https://openairdocs.org/saib/CE-08-12) (historical): Electrical Power. Issued Feb 27, 2008

## NTSB investigations

None matched to N428AM.

## FAA accident and incident reports

None matched to N428AM.

## Reports on N428AM not matched to an aircraft (2)

They name N428AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19970616017699I](https://openairdocs.org/incident/19970616017699I), Jun 16, 1997: Bag JETSTM3201 (N428AM), Columbia, MO. Narrative: transtate airlines, inc., flight 7066 departed jln enroute to stl 06/16/97. During flight, the right engine duct cap light illuminated. ATC was…
- [Incident 19940525028759I](https://openairdocs.org/incident/19940525028759I), May 25, 1994: Bag JETSTM3201 (N428AM), Evansville, IN. Flames smoke left engine while holding on taxiway. Evacated left engine deferred. Fire bottles refilled.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N428AM not matched to an aircraft (41)

They name N428AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR RAIA0002015](https://openairdocs.org/sdr/RAIA0002015), Feb 24, 2000: CONTROLLER. FAILED. 7395 - MWA - ON TAXI OUT, RIGHT ENGINE FIRE INDICATION ILLUMINATED. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF FIRE, REPLACED RIGHT ENGINE FIRE WIRE CONTROL
- [SDR RAIA9912030](https://openairdocs.org/sdr/RAIA9912030), Dec 10, 1999: BYPASS VALVE. FAILED. 7531-LEX- LEFT EGT GAUGE FLUCTUATED BETWEEN 400 AND FULL SCALE. MAINTENANCE DEFERRED PER MEL 76-2 CAT C. MAINTENANCE REPLACED LEFT ENGINE FUEL BYPASS VALVE.
- [SDR RAIA9910003](https://openairdocs.org/sdr/RAIA9910003), Oct 1, 1999: DELTA PP BOX. FAILED. 7330 - STL - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT DELTA P/P BOX.
- [SDR RAIA990648](https://openairdocs.org/sdr/RAIA990648), Jun 27, 1999: VALVE. FAILED. BMI - FLT 7325 - LEFT ENGINE BYPASSING FUEL. MAINTENANCE REPLACED LEFT ENGINE FUEL BYPASS VALVE. (X)
- [SDR RAIA990342](https://openairdocs.org/sdr/RAIA990342), Mar 26, 1999: TACH GENERATOR. FAILED. FLT 7332 - STL - LEFT ENGINE RPM FELL TO 35 PERCENT. MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR INSERT. (M)
- [SDR RAIA990337](https://openairdocs.org/sdr/RAIA990337), Mar 25, 1999: TACH GENERATOR. FAILED. FLT 7448 - STL - RIGHT RPM INDICATION FLUCTUATING. MAINTENANCE REPLACED RIGHT TACH GENERATOR. (M)
- [SDR RAIA990327](https://openairdocs.org/sdr/RAIA990327), Mar 18, 1999: MASTER CYLINDER. FAILED. FLT 7100 - STL - CAPTAINS LEFT BRAKE WEAK. MAINTENANCE SERVICED CAPTAINS LEFT BRAKE MASTER CYLINDER. (M)
- [SDR RAIA981103](https://openairdocs.org/sdr/RAIA981103), Nov 3, 1998: PROPELLER. FAILED. FLT 7478 - STL - LEFT PROP HEAT WON'T TO 10 AMPS. MAINTENANCE REPLACED LEFT PROP ASSY. (M)
- [SDR RAIA980903](https://openairdocs.org/sdr/RAIA980903), Sep 6, 1998: ENGINE. MALFUNCTIONED. FLT 7508 - STL - RIGHT ENGINE EGT FLUCTUATES 100 DEGREES WITH SRL ON. MAINTENANCE DEFERRED RIGHT SRL 76-1 CAT C. (M)
- [SDR RAIA980812](https://openairdocs.org/sdr/RAIA980812), Aug 18, 1998: SWITCH. FAILED. FLT 7089 - SPI - RIGHT BETA CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT ENGINE BETA PRESSURE SWITCH. (M)
- [SDR RAIA980805](https://openairdocs.org/sdr/RAIA980805), Aug 6, 1998: SWITCH. FAILED. FLT 7486 - STL - RIGHT ENGINE OIL CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED RIGHT OIL PRESSURE SWITCH. (M)
- [SDR RAIA980202](https://openairdocs.org/sdr/RAIA980202), Feb 3, 1998: TACH GENERATOR. FAILED. FLT 7336 - STL - LEFT ENGINE RPM WENT TO ZERO DURING CLIMB. MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR. (M)
- [SDR RAIA980111](https://openairdocs.org/sdr/RAIA980111), Jan 13, 1998: SWITCH. FAILED. FLT 7418 - STL - NOSE GEAR DOWN AND LOCKED INDICATION FLICKERS WITH GEAR IN THE UP AND LOCKED POSITION. MAINTENANCE REPLACED NOSE GEAR DOWN LOCK SWITCH. (M)
- [SDR RAIA971010](https://openairdocs.org/sdr/RAIA971010), Oct 13, 1997: TACH GENERATOR. FAILED. FLT 7312 - STL - RIGHT ENGINE RPM WENT TO '0' ON TAKEOFF. MAINTENANCE REPLACED RIGHT ENGINE TACH GENERATOR. (M)
- [SDR RAIA970621](https://openairdocs.org/sdr/RAIA970621), Jun 24, 1997: COMPRESSOR. FAILED. STL - FLT 7069 - RIGHT ENGINE DID NOT ACHIEVE TARGET TORQUE ON TAKEOFF. MAINTENANCE REPLACED RIGHT ENGINE DUE TO COMPRESSOR AND HOT SECTION DEGRADATION. (X)
- [SDR RAIA970612](https://openairdocs.org/sdr/RAIA970612), Jun 16, 1997: CONTROL UNIT. FAILED. JLN - FLT 7066 - RIGHT DUCT FAIL CAP LIGHT ILLUMINATED IN-FLIGHT. REPLACED DUCT FAIL CONTROL UNIT. (X)
- [SDR RAIA970227](https://openairdocs.org/sdr/RAIA970227), Feb 23, 1997: ACTUATOR. FAILED. STL - FLT 7508 - LEFT OIL COOLER FLAP STUCK OPEN. MAINTENANCE REPLACED OIL COOLER FLAP ACTUATOR. (M)
- [SDR RAIA970107](https://openairdocs.org/sdr/RAIA970107), Jan 6, 1997: LAMP. INOPERATIVE. VESTIBULE EMERGENCY LIGHT INOP. REPLACED LAMP. (M)
- [SDR RAIA970106](https://openairdocs.org/sdr/RAIA970106), Jan 6, 1997: SCREW. REQ ADJUST. CGI - FLT 7393 - NR 2 ENGINE ONLY PRODUCE 50 PERCENT TORQUE. ADJUSTED TAKEOFF RPM. (M)
- [SDR RAIA960911](https://openairdocs.org/sdr/RAIA960911), Sep 15, 1996: WINDSCREEN. CRACKED. STL - FLT 7466 - DURING CRUISE, THE FLIGHT OFFICERS FORWARD WINDSCREEN CRACKED. MAINTENANCE REPLACED THE FLIGHT OFFICERS WINDSCREEN. (M)
- [SDR RAIA960535](https://openairdocs.org/sdr/RAIA960535), May 29, 1996: PROP GOVERNOR. FAILED. STL - FLT 7092 - NR 2 ENGINE WOULD NOT PRODUCE REQUIRED TORQUE. REMOVED AND REPLACED PROP GOVERNOR. (M)
- [SDR RAIA960429](https://openairdocs.org/sdr/RAIA960429), Apr 22, 1996: TQ SIGNAL COND. OUT OF ADJUST. STL - FLT 7442 - RIGHT ENGINE DID NOT MAKE TARGET TORQUE. MX ADJUSTED TORQUE SIGNAL CONDITIONER, GROUND RUNS GOOD. (M)
- [SDR RAIA960426](https://openairdocs.org/sdr/RAIA960426), Apr 17, 1996: SWITCH. OUT OF ADJUST. STL - 7420 - PASSENGER DOOR LIGHT ILLUMINATED DURING FLIGHT. MAINTENANCE ISSUED DMI 52-2. MAINTENANCE CLEARED DMI BY ADJUSTING PAX DOOR MICROSWITCH. (M)
- [SDR RAIA960240](https://openairdocs.org/sdr/RAIA960240), Feb 25, 1996: TQ SIGNAL COND. OUT OF ADJUST. STL - FLT NR 7448 - LEFT ENGINE DID NOT ACHIEVE TARGET TORQUE, ABORTED TAKEOFF. MAINTENANCE ADJUSTED LEFT TORQUE SIGNAL CONDITIONER PERFORMED GROUNDS RUNS OPERA
- [SDR RAIA960223](https://openairdocs.org/sdr/RAIA960223), Feb 17, 1996: TACH GENERATOR. FAILED. STL - FLT NR 7031 - RIGHT RPM INDICATOR FAILED IN FLIGHT. MAINTENANCE REPLACED RIGHT TACH GENERATOR PERFORMED GROUND RUNS OPERATIONAL CHECK GOOD. (M)
- [SDR RAIA960213](https://openairdocs.org/sdr/RAIA960213), Feb 6, 1996: SWITCH. FAILED. STL - FLT 7068 - LT MAIN GEAR DOWN AND LOCKED GREEN INDICATOR REMAINS ILLUMINATED AT ALL TIMES. MAINTENANCE REPLACED LEFT DOWNLOCK SWITCH, GEAR SWING GOOD. (X)
- [SDR RAIA960136](https://openairdocs.org/sdr/RAIA960136), Jan 21, 1996: FUEL CONTROL. OUT OF ADJUST. STL - FLT 7058 - LEFT ENGINE WOULD ONLY ACHIEVE 97.5 PERCENT RPM. MAINTENANCE ADJUSTED SCREW 'X', PERFORMED GROUND RUNS, OPERATIONAL CHECK GOOD. ENGINE TT, 9,06
- [SDR RAIA960114](https://openairdocs.org/sdr/RAIA960114), Jan 10, 1996: ANTI-ICE VALVE. FAULTY. STL - FLT 7492 - RIGHT ENGINE ANTI-ICE FAILED IN-FLIGHT. CIRCUIT BREAKER WOULD NOT RESET. MAINTENANCE REPLACED RIGHT ENGINE ANTI-ICE VALVE, OPERATION CHECK GOOD
- [SDR RAIA951212](https://openairdocs.org/sdr/RAIA951212), Dec 12, 1995: PITOT DRAIN. MOISTURE. COU - FLT NR 7036 - CAPTAINS AIRSPEED STUCK AT 90 KNOTS. MAINTENANCE DRAINED CAPTAINS PITOT DRAIN FROM MOISTURE. PITOT/STATIC SYSTEM CHECK GOOD. (M)
- [SDR RAIA951203](https://openairdocs.org/sdr/RAIA951203), Dec 4, 1995: TQ SIGNAL COND. OUT OF ADJUST. STL - FLT 7 - RIGHT ENGINE ONLY ACHIEVED 95 PERCENT TORQUE. MAINTENANCE SWAPPED TORQUE SIGNAL CONDITIONER BRIDGE. ADJUSTED SIGNAL CONDITIONER PER GARRETT DSC SE
- [SDR RAIA951202](https://openairdocs.org/sdr/RAIA951202), Dec 4, 1995: TQ SIGNAL COND. OUT OF ADJUST. STL - FLT NR 7059 - RIGHT ENGINE ONLY ACHIEVED 95 PERCENT TORQUE. MAINTENANCE ADJUSTED RIGHT ENG TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTINGS. GROUND P
- [SDR RAIA951125](https://openairdocs.org/sdr/RAIA951125), Nov 17, 1995: GASKET. LEAKING. STL - FLT NR 7073 - LOW TORQUE ON TAKEOFF. REPLACED BLEED AIR GASKET. (M)
- [SDR RAIA951120](https://openairdocs.org/sdr/RAIA951120), Nov 15, 1995: GASKET. LEAKING. FLT NR 7310 - STL - RIGHT ENGINE ONLY MADE 90 PERCENT TORQUE, TARGET TORQUE 100 PERCENT. MAINTENANCE REMOVED AND REPLACED P3 BLEED GASKETS. OPERATIONAL CHECK GO
- [SDR RAIA951119](https://openairdocs.org/sdr/RAIA951119), Nov 14, 1995: BLEED LINE. CRACKED. FLT NR 7409 - EVV - LEFT ENGINE TEMP SPIKED TO 700. MAINTENANCE REMOVED AND REPLACED P3 BLEED LINE, OPERATIONAL CHECK GOOD. (M)
- [SDR RAIA951116](https://openairdocs.org/sdr/RAIA951116), Nov 13, 1995: SWITCH. DIRTY. FLT NR 7364 - STL - DURING TAKEOFF, SQUAT SWITCH STUCK AND COULD NOT GET THE GEAR TO RETRACT AND OIL COOLER DOOR DOES NOT CLOSE. MAINTENANCE CLEANED NOSE GEAR S
- [SDR RAIA951019](https://openairdocs.org/sdr/RAIA951019), Oct 14, 1995: TQ SIGNAL COND. OUT OF ADJUST. STL - FLT NR 7341 - RIGHT ENGINE ACHIEVED 90 PERCENT TORQUE. MAINTENANCE RECALIBRATED RIGHT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SHEETS. CHECKED FOR BLE
- [SDR RAIA950902](https://openairdocs.org/sdr/RAIA950902), Sep 2, 1995: FUEL CONTROL. FAILED. DEC - FLT 7303 - LEFT TORQUE 70 PERCENT. MAINTENANCE REPLACED LEFT FCU. GROUND RUNS REVEALED NORMAL OPERATION. AIRCRAFT TT, 9723.0. ENGINE TT, 8974. (X)
- [SDR RAIA950507](https://openairdocs.org/sdr/RAIA950507), May 11, 1995: CONNECTOR. MOISTURE. STL - FLT 7341 - LEFT ENGINE LOST POWER, TORQUE DROPPED TO 50 PERCENT. MAINTENANCE CLEANED AND RESEATED LEFT FUEL BY-PASS VALVE CONNECTOR. PERFORMED GROUND RUNS
- [SDR RAIA950306](https://openairdocs.org/sdr/RAIA950306), Mar 7, 1995: SWITCH. FAILED. STL - FLT 7305 - THE LT ENGINE FIRE WARNING SOUNDED. MAINTENANCE REPLACED THE FIRE DETECTION PRESS TO TEST SWITCH. (W)
- [SDR RAIA950127](https://openairdocs.org/sdr/RAIA950127), Jan 18, 1995: BEARING. WORN. STL - FLT 7307 - ACFT ROLLS TO THE RT WHEN FLAPS SELECTED TO 35 DEGREES. MAINTENANCE DISCOVERED RT CENTER FLAP HINGE BEARING TO BE WORN. MAINTENANCE REPLACED RT
- [SDR RAIA950115](https://openairdocs.org/sdr/RAIA950115), Jan 16, 1995: CONTROL CABLE. LOOSE. STL - ON APPROACH, WHEN FLAP SETTING IS SELECTED, AIRCRAFT ROLLS TO THE RIGHT. UPON INSPECTION, MAINTENANCE DISCOVERED AILERON CONTROL CABLE TENSION TO BE LOW. 

## STCs that may be installed (OpenAirDocs) (147, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Cirrus Design SR22)

- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA12273IB](https://openairdocs.org/stc/SA12273IB): Installation of the MT-Propeller Entwicklung GmbH MTV-9-D/198-52() propeller. MT-Propeller Entwicklung GmbH
- [STC SA02216SE](https://openairdocs.org/stc/SA02216SE): Removal of mechanical link between engine throttle control and propeller RPM control. Installation of a separate RPM control lever, linkage between Cirrus RPM cable/cam followers, center console to accommodate three-lever configuration, new knobs for all levers, and new installation hardware (nuts, bolts, etc). Skyryse Inc
- [STC SA12064WI](https://openairdocs.org/stc/SA12064WI): Hardware and software updates for the Garmin G1000 Integrated Avionics System. Garmin International Inc
- [STC SA12084BO](https://openairdocs.org/stc/SA12084BO): Installation of the 700-00212-110 and the 700-00212-010 12-inch Vantage Displays Systems with Attitude Reference System and the 700-00236-000 Air Data Computers System. Avidyne Corporation
- [STC SA12080BO](https://openairdocs.org/stc/SA12080BO): Installation of Prodigy model 90901() LED Landing Light. Whelen Aerospace Technologies
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC
- [STC SA12027IB](https://openairdocs.org/stc/SA12027IB): Installation of the MT-Propeller Entwicklung GmbH MTV-14-D/195-30() propeller. MT-Propeller Entwicklung GmbH
- [STC SA02558CH](https://openairdocs.org/stc/SA02558CH): Installation of a L-3 Communications Avionics Systems SmartDeck Flight Guidance and Display System. Acron Aviation Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA02924CH](https://openairdocs.org/stc/SA02924CH): Installation of M-T Propeller model MTV-14-D/195-30( ) 4 bladed propeller. McFarlane Aviation LLC
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02551AK](https://openairdocs.org/stc/SA02551AK): Installation of SKYDISPLAY Aircraft Interface Device (AID). AeroDisplay LLC
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA10532SC](https://openairdocs.org/stc/SA10532SC): Installation of XM Satellite Radio Wireless equipment. Heads Up Technologies Inc
- [STC SA04575CH](https://openairdocs.org/stc/SA04575CH): Installation of access panel in accordance with Kelly Aerospace Thermal Systems Installation Manual NC-19-092, revision E, or later FAA approved revision. Kelly Aerospace Thermal Systems LLC
- [STC SA00199BO](https://openairdocs.org/stc/SA00199BO): Installation of Aerox Oxygen System. Aerox Aviation Oxygen Systems LLC
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04468CH](https://openairdocs.org/stc/SA04468CH): Installation of Hartzell Propeller model 4C1-F650A1/76C04-0.6 or 4C1-F650A1/76C04B-0.6 i. Hartzell Propeller Inc
- [STC SA02329AK](https://openairdocs.org/stc/SA02329AK): Installation of a fixed-mounted Max-Viz® Enhanced Vision System (EVS) Model 100 or Model 600 to include a sensor with conformal housing that displays imagery on any FAA-approved monitor with NTSC RS-170 video interface capability. PECO Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01234WI-D](https://openairdocs.org/stc/SA01234WI-D): Installation of Bendix/King KMH 880 Multi-Hazard Awareness System or Bendix/King KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS). Honeywell International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA10195SC](https://openairdocs.org/stc/SA10195SC): Installation of an engine driven vapor cycle air conditioning system. Air Comm Corporation
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc

All 147: https://openairdocs.org/aircraft/N428AM/stcs.md

## Related

- Other Cirrus Design SR22 aircraft: https://openairdocs.org/model/cirrus-design-sr22/aircraft.md
- The Continental IO-550-N engine: https://openairdocs.org/engine/continental-io-550-n.md

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