# N310FL: 2009 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: 3534
- Year built: 2009
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: December 22, 2009
- Certificate issued: March 22, 2023
- Expires: March 31, 2030
- Mode S code: A34759
- Registered owner: [D & T Outlaw Properties LLC](https://openairdocs.org/faa-owner/D%20%26%20T%20OUTLAW%20PROPERTIES%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8313° N, 96.7712° W: Placed by OpenAirDocs at the center of ZIP code 75206, 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=310FL
- Page: https://openairdocs.org/aircraft/N310FL

From the FAA registry file of October 24, 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 N310FL.

## FAA accident and incident reports

None matched to N310FL.

## Reports on N310FL not matched to an aircraft (1)

They name N310FL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19840929058339I](https://openairdocs.org/incident/19840929058339I), Sep 29, 1984: Bac 111* (N310FL), Indianapolis, IN. Smoke in the cabin during switching pressurization from APU to CO2 air source. Could not be duplicated on ground.

## 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 N310FL not matched to an aircraft (52, newest 50)

They name N310FL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR F3LA200400110](https://openairdocs.org/sdr/F3LA200400110), Oct 4, 2004: FLOORBEAM. CORRODED. DURING A-4 CHECK, INSPECTION REPORTED PARTITION SUPPORT CORRODED AT FLOORBEAM, STA 986.5 - 1006, RBL 16. REPLACED PARTITION SUPPORT AT FLOORBEAM PER SRM 51-40-0
- [SDR F3LA200400109](https://openairdocs.org/sdr/F3LA200400109), Oct 4, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT CORRODED AT STA 1010, RBL 10. REPLACED FLOORBEAM SUPPORT PER SRM 51-40-02, 51-40-05 AND BAC DRAWING 65C3
- [SDR F3LA200400107](https://openairdocs.org/sdr/F3LA200400107), Oct 2, 2004: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR WEBS AFT OF STA 1016 FLOORBEAM, CENTER OF FUSELAGE, CORRODED. REPLACED FLOOR WEB HAT CHANNEL, STA 1016, BL 0, PER DR
- [SDR F3LA200400108](https://openairdocs.org/sdr/F3LA200400108), Oct 1, 2004: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL SUPPORT CORRODED AT STA 986.5 - 1006, RBL 20. REPLACED FLOOR SUPPORT INTERCOSTAL PER SRM 51-40-02 AND 53-60-51
- [SDR F3LA200400106](https://openairdocs.org/sdr/F3LA200400106), Sep 30, 2004: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED L2 MOP SILL CORRODED. REPLACED L2 MOP SILL PER SRM 51-10-2 AND 51-40-02.
- [SDR F3LA200400105](https://openairdocs.org/sdr/F3LA200400105), Sep 30, 2004: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED R2 MOP SILL CORRODED. REPLACED R2 MOP SILL PER SRM 51-10-2 AND 51-40-02.
- [SDR F3LA200400103](https://openairdocs.org/sdr/F3LA200400103), Sep 28, 2004: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL FROM STA 947 - 986 LEFT OF CENTER CORRODED AT FLOOR PANEL NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-40
- [SDR F3LA200400104](https://openairdocs.org/sdr/F3LA200400104), Sep 28, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, FLOORBEAM GOUGED AND CORRODED AT STA 947.5 - 967, RBL 16. REPLACED DAMAGED INTERCOSTAL PER SRM 51-40-02 AND 53-60-51.
- [SDR F3LA200400102](https://openairdocs.org/sdr/F3LA200400102), Sep 28, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT AT STA 947.5 - 967, LBL 14, CORRODED. REPLACED INTERCOSTAL AT STA 947.5 - 967, LBL 14, PER SRM 51-40-02,
- [SDR F3LA200400100](https://openairdocs.org/sdr/F3LA200400100), Sep 27, 2004: FLOOR SUPPORT. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CRACKED AT STA 927 - 947.5, RBL 16. REMOVED FLOOR SUPPORT TO REPLACE CRACKED FLANGE. REPAIRED CRACKED FLANGE
- [SDR F3LA200400099](https://openairdocs.org/sdr/F3LA200400099), Sep 27, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 947.5 CORRODED AT FLOOR PANEL NUT PLATES. REPAIRED FLOORBEAM UPPER CHORD PER SRM 53-00-51, 51-40-02, 51-2
- [SDR F3LA200400098](https://openairdocs.org/sdr/F3LA200400098), Sep 27, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986.5 CORRODED AT FLOOR PANEL NUT PLATES. REPLACED FLOORBEAM UPPER CHORD AT STA 986.5 PER SRM 53-60-51, 5
- [SDR F3LA200400097](https://openairdocs.org/sdr/F3LA200400097), Sep 16, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN STA 294.5 AND 312, 10.5 INCHES FROM CENTER LT, CORRODED AT STA 312 END. REMOVED UPPER T-CHORD ON FLOOR S
- [SDR F3LA200400096](https://openairdocs.org/sdr/F3LA200400096), Sep 16, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 328 CRACKED 20 INCHES IN FROM FUSELAGE OUTER SKIN. VERTICAL ANGLE CRACKED ON LOWER END LT. REPLACED SHEAR
- [SDR F3LA200400095](https://openairdocs.org/sdr/F3LA200400095), Sep 16, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTED REPORTED FLOORBEAM AT STA 967, LBL 42, CORRODED AT FLOOR PANEL SCREW NUT PLATE. FOUND FLOORBEAM TO BE CORRODED BEYOND LIMITS PER SRM
- [SDR F3LA200400094](https://openairdocs.org/sdr/F3LA200400094), Sep 16, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967, RBL 27.16, CORRODED AT FLOOR PANEL SCREW NUT PLATE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR 
- [SDR F3LA200400093](https://openairdocs.org/sdr/F3LA200400093), Sep 14, 2004: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED TOP OF FLOORBEAM AT STA 294.5 CORRODED IN SEVERAL SPOTS FROM 10 INCHES LEFT OF CENTER TO 40 INCHES RT OF CENTER. ALL SCREW
- [SDR F3LA200400092](https://openairdocs.org/sdr/F3LA200400092), Sep 2, 2004: SKIN. DENTED. DURING C-4 CHECK, COMPLIED WITH RW0000198, DENT IN FUSELAGE, AFT OF CARGO DOOR AT STA 500-500A. REMOVED DAMAGE, FABRICATED, LOCATED AND INSTALLED REPAIR IAW BAC
- [SDR F3LA200400089](https://openairdocs.org/sdr/F3LA200400089), Aug 21, 2004: STRUCTURE. CRACKED. ON WALK AROUND, MAINTENANCE REPORTED A 4-INCH CRACK IN RT FWD TOP WHEEL WELL. REPAIRED IAW SRM 53-10-51, PAGE 213, FIGURE 203.
- [SDR F3LA200200167](https://openairdocs.org/sdr/F3LA200200167), Jun 10, 2002: STRAP. TORN. DURING C-2 CHECK, INSPECTION REPORTED FLOORBEAM STABILIZER STRAP TORN AND MISSING A SECTION, STA 312 TO 328, BL -0-. REPLACED DAMAGED STABILIZER STRAP PER SRM 5
- [SDR F3LA200200166](https://openairdocs.org/sdr/F3LA200200166), Jun 10, 2002: STRAP. TORN. DURING C-2 CHECK, INSPECTION REPORTED SMALL TEAR IN FLOORBEAM STABILIZER STRAP AT STA 328, LBL 8, AND FASTENER HEADS WORN DOWN. REPLACED DAMAGED STABILIZER STRA
- [SDR F3LA200200165](https://openairdocs.org/sdr/F3LA200200165), Jun 10, 2002: SPLICE. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED FLOOR SPLICE IN AFT CARGO COMPARTMENT AT BS 767 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SPLICE PER SRM 53-60-
- [SDR F3LA200200160](https://openairdocs.org/sdr/F3LA200200160), Jun 5, 2002: DOOR FRAME. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED HOLE IN AFT CARGO DOOR FWD FRAME CAP WEB. FABRICATED AND INSTALLED WEB REPAIR PER SRM 51-70-13, 51-10-02 AND 51-70-13.
- [SDR F3LA200200159](https://openairdocs.org/sdr/F3LA200200159), Jun 5, 2002: CARGO TRACK. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TRACK IN CARGO COMPARTMENT AT RBL 13.8, BETWEEN STA 795 AND 827. REMOVED DAMAGED AREA, FABRICATED AND I
- [SDR F3LA200200158](https://openairdocs.org/sdr/F3LA200200158), Jun 5, 2002: FRAME. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED FRAME AT STA 460, RBL 7 TO 14, DAMAGED. FABRICATED AND INSTALLED REPAIR AND FRAME CLIP PER SRM 53-00-07.
- [SDR F3LA200200157](https://openairdocs.org/sdr/F3LA200200157), Jun 5, 2002: FLOOR SUPPORT. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 767. FABRICATED AND INSTALLED REPAIR ON CARGO TRACK AT STA 767, RBL 13
- [SDR F3LA200200156](https://openairdocs.org/sdr/F3LA200200156), Jun 5, 2002: FLOOR SUPPORT. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT STA 767, RBL 3. REMOVED CORROSION ON FLOOR SUPPORT, FABRICATED REPLACEMENT PARTS AND INSTALL
- [SDR F3LA200200155](https://openairdocs.org/sdr/F3LA200200155), Jun 5, 2002: FAIRING. CRACKED. DURING C-2 CHECK, INSPECTION REPORTED UPPER HINGE FAIRING AT L1 DOOR BENT AT FWD END AND CRACKED AT AFT END. FABRICATED AND INSTALLED REPLACEMENT UPPER L1 DOOR 
- [SDR F3LA200100036](https://openairdocs.org/sdr/F3LA200100036), Feb 25, 2001: BUSHING. WORN. AIR TURNBACK. FLIGHT CREW REPORTED VIBRATION TO FLIGHT CONTROLS DURING CLIMB. NO VIBRATION INDICATION, ALL ENGINE INDICATIONS NORMAL. CYCLED GEAR AT LOWER SPEED
- [SDR F3LA00062](https://openairdocs.org/sdr/F3LA00062), Mar 23, 2000: STRUCTURE. BROKEN. DEN - DURING C-7 CHECK INSPECTION, REPORTED EXPANSION JOINT FORWARD OF CENTER FUEL TANK, LEFT OF CENTER LINE, BROKEN. MAINTENANCE REPLACED CHANNEL ASSY PER SRM 
- [SDR F3LA00028](https://openairdocs.org/sdr/F3LA00028), Mar 20, 2000: HOUSING. CORRODED. DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION AT CORNER ATTACH BOLT NUTPLATES OF R-2 DOOR TORQUE BOX. MAINTENANCE REMOVED AND REPLACED TORQUE BOX HOUSIN
- [SDR F3LA00054](https://openairdocs.org/sdr/F3LA00054), Mar 19, 2000: CHANNEL. CRACKED. DURING C-7 CHECK INSPECTION REPORTED CABIN FLOOR EXPANSION JOINT CHANNEL CRACKED AT BS 540 BL 0 TO RBL 20. MAINTENANCE REMOVED AND REPLACED RIGHT CENTER EXPANSI
- [SDR F3LA00053](https://openairdocs.org/sdr/F3LA00053), Mar 19, 2000: SHEAR TIE. CRACKED. DEN - DURING C-7 CHECK INSPECTION REPORTED SHEAR TIE CRACKED AT STRINGER 6R. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PE
- [SDR F3LA00052](https://openairdocs.org/sdr/F3LA00052), Mar 19, 2000: FLOOR SUPPORT. CRACKED. DEN - DURING C-7 CHECK INSPECTION REPORTED FLOOR SUPPORT BETWEEN BS 787 AND BS 820, RBL 16, CRACKED AND CORRODED. MAINTENANCE REPLACED FLOOR SUPPORT IAW SRM 53-
- [SDR F3LA00051](https://openairdocs.org/sdr/F3LA00051), Mar 19, 2000: ANGLE. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED TIE ANGLE UNDER CABIN FLOOR CRACKED AT BS 727B, LBL 47. MAINTENANCE REPLACED TIE ANGLE PER SRM 51-10-2. (M)
- [SDR F3LA00019](https://openairdocs.org/sdr/F3LA00019), Mar 19, 2000: ANGLE. CRACKED. DEN - DURING C-7 CHECK INSPECTION, FOUND TIE ANGLE UNDER CABIN FLOOR CRACKED AT STATION 727B, LBL 47. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT TIE ANGLE
- [SDR F3LA00050](https://openairdocs.org/sdr/F3LA00050), Mar 18, 2000: ANGLE. CORRODED. DEN - DURING C-7 CHECK INSPECTION REPORTED CORROSION ON R-2 DOOR THRESHOLD SCUFF PLATE SUPPORT ANGLE. MAINTENANCE REMOVED CORROSION PER SRM 51-10-2, AND CLEANED
- [SDR F3LA00049](https://openairdocs.org/sdr/F3LA00049), Mar 18, 2000: ANGLE. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 9R AND STRINGER 10R. MAINTENANCE REPLACED SUPPO
- [SDR F3LA00048](https://openairdocs.org/sdr/F3LA00048), Mar 18, 2000: ANGLE. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 10R AND STRINGER 11R. MAINTENANCE REPLACED SUPP
- [SDR F3LA00047](https://openairdocs.org/sdr/F3LA00047), Mar 18, 2000: ANGLE. CRACKED. DEN - DURNG C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 11R AND STRINGER 12R. MAINTENANCE REPLACED SUPPO
- [SDR F3LA00046](https://openairdocs.org/sdr/F3LA00046), Mar 18, 2000: ANGLE. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN SUPPORT ANGLE ON FRAME FORWARD OF R1 DOOR, BETWEEN STRINGER 12R AND STRINGER 13R. MAINTENANCE REPLACED SUPP
- [SDR F3LA00026](https://openairdocs.org/sdr/F3LA00026), Mar 17, 2000: FLOORBOARD. CORRODED. DEN - DURING C-7 CHECK INSPECTION, FOUND CORROSION ON FLOORBOARD ATTACH ANGLE STATION 960 TO 986.5, STRINGER 17R. MAINTENANCE REMOVED CORROSION, TREATED, PRIMED
- [SDR F3LA00025](https://openairdocs.org/sdr/F3LA00025), Mar 17, 2000: DOOR FRAME. CORRODED. DEN - DURING C-7 CHECK INSPECTION REPORTED, FOUND CORROSION AT LOWER FORWARD CORNER OF AFT CARGO DOOR FRAME BETWEEN S25R AND S26R. MAINTENANCE FABRICATED, AND I
- [SDR F3LA00024](https://openairdocs.org/sdr/F3LA00024), Mar 17, 2000: FRAME. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED FUSELAGE FRAME CRACKED ON TOP FLANGE AND RADIUS AT STATION 727B, STRINGER 23R, IN AFT CARGO PIT. MAINTENANCE REMOVED
- [SDR F3LA00023](https://openairdocs.org/sdr/F3LA00023), Mar 17, 2000: SHEAR TIE. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED SHEAR TIE CRACKED AT STATION 294, STRINGER 6R. MAINTENANCE FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 51-10-2. (
- [SDR F3LA00022](https://openairdocs.org/sdr/F3LA00022), Mar 17, 2000: BRACKET. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED CORNER BRACKET CRACKED UNDER FLOORBEAM AT STATION 767, RBL 60. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT ANGL
- [SDR F3LA00034](https://openairdocs.org/sdr/F3LA00034), Mar 15, 2000: SKIN. DAMAGED. DEN - DURING C-7 CHECK, INSPECTION REPORTED HOLE IN LOWER SURFACE OF AILERON AT OUTBOARD END. MAINTENANCE REMOVED AILERON. REPAIRED HOLE PER SRM 51-70-04 AND 51
- [SDR F3LA00061](https://openairdocs.org/sdr/F3LA00061), Mar 14, 2000: WEB. CRACKED. DEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN AFT CARGO DOOR OPENING WEB, BS 847 - BS 867, STRINGER 26. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND 
- [SDR F3LA00021](https://openairdocs.org/sdr/F3LA00021), Mar 14, 2000: WEB. CORRODED. DEN - DURNG C07 CHECK INSPECTION, FOUND CORROSION ON AFT CARGO DOOR OPENING WEB AT FORWARD SIDE OF DOOR, STAITON 847-867, STRINGER 26. MAINTENANCE FABRICATED AN
- [SDR F3LA00020](https://openairdocs.org/sdr/F3LA00020), Mar 14, 2000: WEB. CORRODED. DEN - DURING C-7 CHECK INSPECTION, FOUND CORROSION ON AFT CARGO DOOR OPENING WEB AT FORWARD SIDE OF DOOR, STATION 787, BETWEEN STRINGER 23 AND 25. MAINTENANCE F

All 52: https://openairdocs.org/aircraft/N310FL/unmatched-reports.md

## 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 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 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 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/N310FL/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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