# N45GL: 2006 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: 1870
- Year built: 2006
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: March 25, 2006
- Certificate issued: September 13, 2012
- Expires: September 30, 2028
- Mode S code: A57064
- Registered owners: [Optimal Aircraft Management Nc LLC](https://openairdocs.org/faa-owner/OPTIMAL%20AIRCRAFT%20MANAGEMENT%20NC%20LLC), [Falk David Jr](https://openairdocs.org/faa-owner/FALK%20DAVID%20JR), [Ctls Ventures Inc](https://openairdocs.org/faa-owner/CTLS%20VENTURES%20INC)
- Location: [Sanford, MI](https://openairdocs.org/faa-place/MI/Sanford)
- Owner type: Co-owned, fractional ownership
- Owner's area on the map: 43.7066° N, 84.4189° W: Placed by OpenAirDocs at the center of ZIP code 48657, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=45GL
- Page: https://openairdocs.org/aircraft/N45GL

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 N45GL.

## FAA accident and incident reports

None matched to N45GL.

## Reports on N45GL not matched to an aircraft (2)

They name N45GL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19940522028829I](https://openairdocs.org/incident/19940522028829I), May 22, 1994: Beech 1900C (N45GL), Bismarck, ND. Engine shutdown in flight due low oil pressure. NR1 compressor bearing bad.
- [Incident 19940407016409I](https://openairdocs.org/incident/19940407016409I), Apr 7, 1994: Beech 1900C (N45GL), Fergus Falls, MN. Propeller went to partial feather on takeoff. Aborted. Beta valve out of adjustment. Improper maintenance.

## 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 N45GL not matched to an aircraft (41)

They name N45GL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 051003](https://openairdocs.org/sdr/051003), May 10, 2003: CIRCUIT BREAKER. INOPERATIVE. PILOT REPORTED THAT HE HAD TO MANUALY EXTEND THE LANDING GEAR.
- [SDR 2004F00019](https://openairdocs.org/sdr/2004F00019), Jan 21, 2003: SPRING. BROKEN. LOW FUEL PRESSURE LIGHT CAME ON IN FLT, ELECTRIC BOOST PUMP WAS TURNED ON AND EXTINGUISHED LIGHT. MAINTENANCE REMOVED THE LOW PRESSURE FUEL PUMP AND FOUND THE D
- [SDR 2004F00023](https://openairdocs.org/sdr/2004F00023), Dec 24, 2002: ACTUATOR. FAILED. ON LANDING IN AKN, NOSE GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE. FERRY TO ANCHORAGE AFTER VERIFYING GEAR DOWN AND LOCKED, GREEN LIGHT CAME ON DURING TAXI 
- [SDR 2004F00016](https://openairdocs.org/sdr/2004F00016), Dec 3, 2002: RELAY. CONTAMINATED. ON APPROACH TO LANDING IN ANCHORAGE, THE PILOT SELECTED LANDING GEAR DOWN TWICE WITH NO EFFECT. THE GEAR WAS EXTENDED MANUALLY AND THE LANDING WAS WITHOUT INCID
- [SDR 2004F00013](https://openairdocs.org/sdr/2004F00013), Nov 21, 2002: CONNECTOR. DAMAGED. AT LANDING IN ANCHORAGE, PILOT REPORTED MLG WAS SLOW TO GO DOWN, THE LANDING GEAR WARNING HORN WOULD NOT SILENCE AND INTRANSIT LIGHTS REMAINED ON WITH THREE GRE
- [SDR ACE0822021](https://openairdocs.org/sdr/ACE0822021), Aug 26, 2002: RELAY. CONTAMINATED. ON APPROACH TO LANDING, THE LANDING GEAR WOULD NOT NORMALLY EXTEND. THE FLIGHT CREW USED THE ALTERNATE HAND PUMP FOR EXTENSION AND PERFORMED AND UNEVENTFUL LAND
- [SDR YAD2003F00002](https://openairdocs.org/sdr/YAD2003F00002), Aug 20, 2002: CONNECTOR. SHORTED. DURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHT TURNED ON. TROUBLESHOOTING REVEALED INTERNAL SHORTING
- [SDR ACE0820021](https://openairdocs.org/sdr/ACE0820021), Aug 20, 2002: CONNECTOR. SHORTED. DURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHTS TURNED ON, TROUBLE SHOOTING REVEALED INTERNAL SHORTI
- [SDR ACE0729021](https://openairdocs.org/sdr/ACE0729021), Jul 31, 2002: OIL COOLER. CRACKED. MAINTENANCE FOUND OIL LEAKING FROM THE RIGHT ENGINE COWLING. INVESTIGATION REVEALED A CRACKED OIL COOLER. OIL COOLER WAS REPLACED. THE REMOVED OIL COOLER WAS IN
- [SDR ACE0603021](https://openairdocs.org/sdr/ACE0603021), Jun 4, 2002: RELAY. BURNED. ON APPROACH, THE LANDING GEAR WAS SELECTED DOWN AND THE GEAR EXTENDED NORMALLY, GIVING THREE GREEN SAFE INDICATIONS. MOMENTS AFTER GETTING THE GEAR DOWN AND SAF
- [SDR ACE0510021](https://openairdocs.org/sdr/ACE0510021), May 10, 2002: WINDSHIELD. CRACKED. ON CLIMB OUT, RT WINDSHIELD CRACKED. AIRCRAFT IMMEDIATELY RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. WINDSHIELD REPLACED.
- [SDR ACE0206021](https://openairdocs.org/sdr/ACE0206021), Feb 6, 2002: DOWNLOCK SWITCH. INOPERATIVE. PILOT REPORTED THAT ON APPROACH TO ANCHORAGE, WHEN THE LANDING GEAR WAS SELECTED DOWN. THE NOSE GEAR, GREEN DOWN AND LOCK LAMP FAILED TO ILLUMINATE (THE GEAR UN
- [SDR ACE0119021](https://openairdocs.org/sdr/ACE0119021), Jan 19, 2002: LINE. CRACKED. FLIGHT CREW REPORTED THAT THE NR 2 ENGINE FLAMED OUT EN ROUTE. ATTEMPTED RESTART WAS UNSUCCESSFUL. THE ENGINE WAS SECURED AND ACCOMPLISHED UNEVENTFUL LANDING. M
- [SDR ACE0117021](https://openairdocs.org/sdr/ACE0117021), Jan 18, 2002: RELAY. BURNED. THE PILOT REPORTED THAT AFTER DEPARTURE FROM HPB, THE LANDING GEAR SELECTOR HANDLE WAS INOPERATIVE AND WOULD NOT RAISE THE LANDING GEAR. THE FLIGHT CONTINUED, W
- [SDR ACE1024011](https://openairdocs.org/sdr/ACE1024011), Oct 24, 2001: RELAY. BURNED. ON ARRIVAL, THE LANDING GEAR MOTOR CIRCUIT BREAKER POPPED, THE LOW HYDRAULIC LEVEL ENUNCIATOR CAME ON AND THE GEAR HAD TO BE MANUALLY EXTENDED. AN UNEVENTFUL LA
- [SDR ACE1018011](https://openairdocs.org/sdr/ACE1018011), Oct 18, 2001: LANDING GEAR. ICED. ON ARRIVAL, THE LANDING GEAR SELECTOR HAD TO BE CYCLED MULTIPLE TIMES TO ACHIEVE GEAR DOWN AND SAFE INDICATION. MAINTENANCE COULD NOT DUPLICATE THE FAULT AND IN
- [SDR YAD2001F00008](https://openairdocs.org/sdr/YAD2001F00008), Jul 25, 2001: SWITCH. FAILED. CABIN ALTITUDE WAS NOTED AT 16,000 FT (DUE IMPACT - DAMAGE TO FUSELAGE) IN FLIGHT - CREW STATED USING SUPPLEMENTAL OXYGEN AT THIS POINT. CABIN ALTITUDE WARNING 
- [SDR 20010425CW012](https://openairdocs.org/sdr/20010425CW012), Jan 21, 2001: ENGINE. FAILED. ON RETURN LEG OF ROUND TRIP, PILOT NOTICED AN ORANGE FLASH FRO THE RIGHT HAND ENGINE. ENGINE ITT STARTED RISING AND THE POWER STARTED RISING AND THE POWER START
- [SDR 20010601CW002](https://openairdocs.org/sdr/20010601CW002), Sep 8, 2000: WINDSHIELD. CRACKED. WINDSHIELD CRACKED A FL20. THE FLIGHT CREW CANCELED THE INTENDED FLIGHT AND RETURNED TO ANCHORAGE, WITHOUT FURTHER PROBLEMS.
- [SDR 20010601CW006](https://openairdocs.org/sdr/20010601CW006), Aug 31, 2000: SWITCH. DISCONNECTED. WHILE PERFORMING ENGINE FIRE EXTINGUISHER SYSTEM TEST IAW B1900C MM CAMP NR2 INSPECTION TEMP REVISION 26-1, FOUND NR 1 AND NR 2 ENGINE SQUIB POWER SWITCH DISCON
- [SDR 20010425CW016](https://openairdocs.org/sdr/20010425CW016), Jul 17, 2000: CLAMP. UNSECURE. NR 1 ENGINE POWER FAILED TO REDUCE BELOW 2200 LBS. TORQUE FOR LANDING. THE ENGINE WAS SHUT DOWN IN FLIGHT JUST PRIOR TO LANDING. A NON EVENTFUL LANDING WAS ACCO
- [SDR 20010607CW007](https://openairdocs.org/sdr/20010607CW007), Nov 23, 1999: SWITCH. DISCONNECTED. WHILE PERFORMING A NEW INSPECTION REQUIREMENT, FOUND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENGINE FIRE EXTINGUISHER ANNUNCIATOR/ACTUATOR ASSEMBLY. FOUN
- [SDR 2000ZZZX423](https://openairdocs.org/sdr/2000ZZZX423), Nov 23, 1999: SWITCH. DISCONNECTED. WHILE PERFORMING 'NEW' INSP REQUIREMENT, FND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENG FIRE EXTING ANNUNCIATOR/ACTUATOR ASSY. FOUND SQUIB SWITCH MODULE
- [SDR 99ZZZX4654](https://openairdocs.org/sdr/99ZZZX4654), Nov 3, 1999: ANNUNCIATOR. FAILED. FAILURE OF NON-FIELD REPLACEABLE IFR GPS 'LEG' ANNUNCIATION. THIS COMPONENT IS THE INDICATOR/SWITCHING UNIT OF A CERTIFIED IFR GPS NAVIGATION SYSTEM.
- [SDR 20000502AP014](https://openairdocs.org/sdr/20000502AP014), Jul 12, 1999: BULKHEAD. CRACKED. DURING A ROUTINE ACE CAMP INSPECTION NR 6, HEAVY AFT FUSELAGE AND EMPENNAGE, FOUND MULTIPLE CRACKS IN CANTED BULKHEAD, STATION 588.10, IN EXCESS OF CRACK LIMITS
- [SDR 99ZZZX1147](https://openairdocs.org/sdr/99ZZZX1147), Mar 2, 1999: FUEL PUMP. FAILED. 67.6 HOURS AFTER OVERHAUL, DRIVESHAFT BROKE. PUMP TURNS NORMAL, NO DAMAGE DETECTED INSIDE PUMP.
- [SDR 99ZZZM184](https://openairdocs.org/sdr/99ZZZM184), Jan 25, 1999: LINE. RUPTURED. PILOT REPORTED CAPTAINS LEFT BRAKE VERY WEAK. BRAKE SYSTEM BLEED, OPS CHECKED GOOD. THE NEXT DAY, THE FLEXIBLE BRAKE LINES (UPPER) IN THE GEAR WELLS, LEFT AND R
- [SDR 98ZZZX3399](https://openairdocs.org/sdr/98ZZZX3399), Aug 27, 1998: RELAY. CONTAMINATED. LANDING GEAR FAILED TO EXTEND WITH GEAR HANDLE SELECTION. LANDING GEAR EXTENDED USING HAND PUMP SYSTEM, GEAR INDICATIONS WERE NORMAL. FOUND LANDING GEAR PUMP RE
- [SDR 98ZZZX3397](https://openairdocs.org/sdr/98ZZZX3397), Aug 20, 1998: SPAR CAP ASSY. CORRODED. FOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWA
- [SDR 98ZZZX1871](https://openairdocs.org/sdr/98ZZZX1871), Apr 26, 1998: FUEL LINE. CHAFED. ON NR 1 ENGINE - STARTER/GENERATOR COOLING DUCT HOSE CAME IN CONTACT WITH AN ENGINE FUEL LINE AND CHAFED A HOLE THROUGH THE TUBING WALL THICKNESS CAUSING FUEL T
- [SDR 97ZZZX4834](https://openairdocs.org/sdr/97ZZZX4834), Aug 11, 1997: TERMINAL. SEPARATED. AIRCRAFT DEPARTED ANC FOR FAI. CLLIMBING OUT OF 8,000 FEET, NR 2 PROPELLER AUTOFEATHERED. FLIGHT CREW SECURED NR 2 ENGINE AND RETURNED TO ANC. LANDING WAS NORMA
- [SDR GLBA96222](https://openairdocs.org/sdr/GLBA96222), Nov 11, 1996: RELAY. FAILED. ORD - GEAR DID NOT EXTEND. EXTENDED GEAR MANUALLY. REMOVED AND REPLACED LANDING GEAR RELAY. OPS CHECKS GOOD. (X)
- [SDR GLBA96209](https://openairdocs.org/sdr/GLBA96209), Oct 24, 1996: PROP GOVERNOR. MALFUNCTIONED. BMG - DURING LANDING AT 110 KTS THE RIGHT PROP RPM DECREASES TO 900 AND THE LEFT STAYS AT 1400. RIGHT TORQUE INCREASES SLIGHTLY AND AIRCRAFT YAWS HEAVY TO THE L
- [SDR GLBA96039](https://openairdocs.org/sdr/GLBA96039), Feb 26, 1996: MOTOR RELAY. FAILED. ESC - THE CREW REPORTED LANDIGN GEAR WOULD NOT EXTEND AND HAD TO MANUALLY EXTEND GEAR. AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED LAN
- [SDR 95ZZZM483](https://openairdocs.org/sdr/95ZZZM483), Aug 15, 1995: TRUSS. CRACKED. ESC - DURING THE ROUTINE TRUSS INSPECTION REQUIRED BY AD95-02-18, A .75 INCH CRACK WAS FOUND NEAR THE LINSEED OIL PLUG OF THE INBOARD AREA 'A' OF THE RIGHT TRUS
- [SDR 95ZZZM489](https://openairdocs.org/sdr/95ZZZM489), Jul 27, 1995: RECEIVER/TRANS. INTERMITTENT. DVL - THE CREW ELECTED AN AIR TURNBACK AFTER THE WEATHER RADAR PICTURE SHRUNK AND THE HORIZONTAL WAS INTERMITTENT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED FOLLOW
- [SDR 95ZZZX2508](https://openairdocs.org/sdr/95ZZZX2508), Apr 2, 1995: AILERON. DENTED. ORD - WHILE PARKED WITHOUT PASSENGERS ON BOARD, THE LEFT WING TIP AND OUTBOARD TRAILING EDGE WERE DENTED BY A BAG CART TOW TRACTOR. MAINTENANCE REMOVED THE AILE
- [SDR 95ZZZX2509](https://openairdocs.org/sdr/95ZZZX2509), Apr 1, 1995: ENGINE OIL. LOW. DLH - INBOUND TO DLH, CREW EXPERIENCED THE RT ENGINE OIL PRESSURE FLUCTUATION BETWEEN 40-100 PSI ACCOMPANIED BY THE ILLUMINATION OF THE RT OIL PRESSURE ANNUNCIA
- [SDR 95ZZZX2021](https://openairdocs.org/sdr/95ZZZX2021), Mar 25, 1995: RIVET. LOOSE. SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND 4 RIVETS IN RT FUEL TANK TOP SIDE BETWEEN THE NACELLE AND STALL FORCE LOOSE AND LEAKING FUEL. THE RIVETS WERE
- [SDR 95ZZZX1965](https://openairdocs.org/sdr/95ZZZX1965), Mar 25, 1995: TE SKIN. CRACKED. SPW - DURING ROUTINE MAINTENANCE, RUDDER TRAILING EDGE FAIRING WAS FOUND CRACKED AND HAD SEVERAL WORKING RIVETS. THE CRACK WAS REPAIRED AND RIVETS WERE REPLACED
- [SDR 95ZZZZ103](https://openairdocs.org/sdr/95ZZZZ103), Jan 30, 1995: RIVETS. LOOSE. SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE RIGHT WING SEEPING FUEL OUTBOARD OF THE NACELLE ALONG THE SPAR. SEVERAL RIVETS WERE REPLACED AND THE AREA

## 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/N45GL/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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