# N427CA: 1976 Cessna 310R - Status: Valid registration - Airframe: [Cessna 310R](https://openairdocs.org/model/cessna-310r) (registry code 2074245, 6 seats) - Engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032) - Data sheets: [TCDS 3A10](https://openairdocs.org/tcds/3A10) (Textron Aviation Inc.), [TCDS E5CE](https://openairdocs.org/tcds/E5CE) (Continental Aerospace Technologies, Inc.) (OpenAirDocs) - Serial number: 310R0653 - Year built: 1976 - Type: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: April 12, 1976 - Certificate issued: February 9, 2016 - Expires: February 28, 2029 - Mode S code: A515D3 - Registered owner: [Chippewa Aerospace Inc](https://openairdocs.org/faa-owner/CHIPPEWA%20AEROSPACE%20INC) - Location: [Gainesville, FL](https://openairdocs.org/faa-place/FL/Gainesville) - Owner type: Corporation - Owner's area on the map: 29.7722° N, 82.2834° W: Placed by OpenAirDocs at the center of ZIP code 32609, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=427CA - Page: https://openairdocs.org/aircraft/N427CA 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. The registry lists only the engine series, so ADs for every Continental IO-520 model are included. ## ADs that may apply (OpenAirDocs): 57 in force ### Matched by airframe (Cessna 310R) - [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 2016-17-08](https://openairdocs.org/ad/2016-17-08): Elevator Tab Control System · Textron 310, 310A, 310B and 46 more. Effective Sep 12, 2016 - [AD 2014-03-03](https://openairdocs.org/ad/2014-03-03): Placards and Markings · Cessna 310, 310A, 310B and 37 more. Effective Apr 7, 2014 - [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 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998 - [AD 98-04-28](https://openairdocs.org/ad/98-04-28): AFM - Limitations Section - Icing · Cessna 310R, 335, 340A and 12 more. Effective Mar 13, 1998 - [AD 97-16-10](https://openairdocs.org/ad/97-16-10): Filters · Cessna 310R, T310R, 36 and 17 more. Effective Sep 18, 1997 - [AD 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997 - [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 90-02-13](https://openairdocs.org/ad/90-02-13): Main Landing Gear · Cessna 310, 310A, 310B and 40 more. Effective Feb 5, 1990 - [AD 87-21-02 R1](https://openairdocs.org/ad/87-21-02-R1): Fuel Filler Openings · Cessna 310D, 310E, 310F and 41 more. Effective Jun 16, 1989 - [AD 76-08-02 R2](https://openairdocs.org/ad/76-08-02-R2): Wing Tip Nose Cap · Cessna 310, 310A, 310B and 41 more. Effective Jan 31, 1983 - [AD 80-13-14](https://openairdocs.org/ad/80-13-14): Fuel Flow Transducer · Cessna 310R, 335, 340A and 4 more. Effective Jul 22, 1980 - [AD 78-11-05](https://openairdocs.org/ad/78-11-05): Autopilot Actuator · Cessna 210M, 310R, 340A and 9 more. Effective Jun 5, 1978 - [AD 76-04-03](https://openairdocs.org/ad/76-04-03): ARC PA-500A Actuators · Cessna 172L, 172M, 177B and 43 more. Effective Feb 26, 1976 - [AD 75-23-07](https://openairdocs.org/ad/75-23-07): Emergency Exit Window · Cessna 310Q, 310R, T310Q and 1 more. Effective Nov 13, 1975 - [AD 73-07-07](https://openairdocs.org/ad/73-07-07): Fuel Hoses & Electrical Wiring Chafing · Cessna 310C, 310D, 310E and 19 more. Effective Apr 6, 1973 - [AD 72-03-07](https://openairdocs.org/ad/72-03-07): Landing Gear Failure · Cessna 310, 310A, 310B and 30 more. Effective Feb 9, 1972 - [AD 57-04-01](https://openairdocs.org/ad/57-04-01): Aileron Hinge · Cessna 310, 310A, 310B and 15 more ### Matched by engine (Continental IO-520 series) - [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 2023-09-09](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 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 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022 - [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 2012-03-06](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 2009-19-07](https://openairdocs.org/ad/2009-19-07): EQ3 cylinders · Continental Motors IO-470-C, IO-470-D, IO-470-E and 72 more. Effective Oct 7, 2009 - [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 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 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998 - [AD 97-26-17](https://openairdocs.org/ad/97-26-17): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 90 more. Effective Jan 23, 1998 - [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995 - [AD 95-03-14](https://openairdocs.org/ad/95-03-14): Engine Mount Brackets · Continental Motors IO-346-A, IO-346-B, IO-520-C and 2 more. Effective Mar 13, 1995 - [AD 93-16-15](https://openairdocs.org/ad/93-16-15): Fuel Pump Drive Shaft · Continental Motors IO-520-B, IO-520-BA, IO-520-BB and 27 more. Effective Dec 14, 1993 - [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 88-17-03](https://openairdocs.org/ad/88-17-03): Starter Adapter Shaftgear Assembly · Continental Motors IO-520-BA, IO-520-BB, IO-550-B and 4 more. Effective Aug 10, 1988 - [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 - [AD 86-13-04 R3](https://openairdocs.org/ad/86-13-04-R3): Cylinder Assemblies · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 44 more. Effective Feb 24, 1988 - [AD 87-14-02](https://openairdocs.org/ad/87-14-02): Starter Adapter Shaftgear · Continental Motors IO-520-BA, IO-520-BB, IO-550-B and 4 more. Effective Oct 5, 1987 - [AD 81-24-06](https://openairdocs.org/ad/81-24-06): Engine Driven Fuel Pumps · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 51 more. Effective Nov 23, 1981 - [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981 - [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980 - [AD 80-01-04](https://openairdocs.org/ad/80-01-04): Cylinder Holddown Flange Assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 44 more. Effective Jan 25, 1980 - [AD 79-05-09](https://openairdocs.org/ad/79-05-09): Oil Pump Assembly Or Oil Pressure Relief Valve Screw And/Or Plunger · Teledyne Continental Motors 6-285-CA, GTSIO-520-C, GTSIO-520-D and 60 more. Effective Mar 12, 1979 - [AD 77-05-04](https://openairdocs.org/ad/77-05-04): Crankshaft · Continental Motors IO-470-L, IO-520-D, IO-520-F and 6 more. Effective Mar 11, 1977 - [AD 70-14-07](https://openairdocs.org/ad/70-14-07): Fuel Injection Pump · Continental Motors IO-360-A, IO-360-C, IO-360-D and 25 more. Effective Nov 22, 1974 - [AD 72-24-03](https://openairdocs.org/ad/72-24-03): Oil Filter Adapter · Continental Motors IO-360-A, IO-520-B, IO-520-C and 3 more. Effective Nov 15, 1972 - [AD 98-01-08](https://openairdocs.org/ad/98-01-08): Exhaust Roller Rocker Arm · Roller rocker arm P/N PE 92I intake and PE92E exhaust (Performance Engineering STC SE8594SW) - [AD 77-13-22](https://openairdocs.org/ad/77-13-22): Crankcase Cracks · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 22 more ### Historical (superseded or no longer in force) - [AD 2016-07-24](https://openairdocs.org/ad/2016-07-24) (historical): Elevator Tab Control System · Textron 310, 310A, 310B and 46 more. Effective Apr 26, 2016 - [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 2022-04-04](https://openairdocs.org/ad/2022-04-04) (historical): 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 Mar 29, 2022 - [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 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 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 94-09-07](https://openairdocs.org/ad/94-09-07) (historical): Engine Mount Brackets · Teledyne Continental Motors IO-346-A, IO-346-B, IO-520-C and 2 more. Effective Jul 5, 1994 - [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more - [AD 87-23-08](https://openairdocs.org/ad/87-23-08) (historical): Crankshafts · Teledyne Continental Motors IO-520 Series (all) and TSIO-520 Series (all). Effective Nov 30, 1987 - [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) (20 in force) - [SAIB CE-13-27R1](https://openairdocs.org/saib/CE-13-27R1): Flight Controls Frayed Flap Extend Cables. Issued Jan 5, 2022 - [SAIB AIR-21-20](https://openairdocs.org/saib/AIR-21-20): TE FLAP CONTROL SYSTEM, Flight Controls –Flap Cable Tension. Issued Dec 16, 2021 - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-14-11R1](https://openairdocs.org/saib/CE-14-11R1): Landing Gear; Nose Landing Gear Trunnions. Issued Sep 23, 2015 - [SAIB CE-14-19](https://openairdocs.org/saib/CE-14-19): Landing Gear; Main Landing Gear (MLG) Torque Link. Issued May 30, 2014 - [SAIB CE-10-01](https://openairdocs.org/saib/CE-10-01): Fuel: Fuel Tank Selector Valve Systems. Issued Oct 5, 2009 - [SAIB CE-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009 - [SAIB CE-09-16](https://openairdocs.org/saib/CE-09-16): Landing Gear: Main Landing Gear Torque Tube. Issued Mar 3, 2009 - [SAIB ACE-99-05](https://openairdocs.org/saib/ACE-99-05): . Issued Nov 17, 1998 - [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-07-09R1](https://openairdocs.org/saib/NE-07-09R1): Periodic Inspections of ECi Cylinder Assemblies for Cracks in the Aluminum Head. Issued Mar 21, 2007 - [SAIB NE-02-41](https://openairdocs.org/saib/NE-02-41): . Issued Aug 8, 2002 - [SAIB CE-14-11](https://openairdocs.org/saib/CE-14-11) (historical): Landing Gear; Nose Landing Gear Trunnions. Issued Feb 25, 2014 ## NTSB investigations None matched to N427CA. ## FAA accident and incident reports None matched to N427CA. ## 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 N427CA not matched to an aircraft (38) They name N427CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR COMA2011101050076](https://openairdocs.org/sdr/COMA2011101050076), Oct 7, 2011: PROXIMITY SENSOR. OUT OF ADJUST. ON CLIMBOUT FROM BUF RECEIVED LEFT MAIN GEAR DISAGREE WARNING DURING GEAR RETRACTION. FOLLOWED QRH, EMERGENCY DECLARED, A/C RETURNED TO BUF LANDED SAFELY. ADJUS - [SDR COMA2011071550046](https://openairdocs.org/sdr/COMA2011071550046), Jul 14, 2011: SELECTOR VALVE. FAILED. ON CLIMBOUT FROM GRR RECEIVED GEAR DISAGREE WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO GRR AND LANDED SAFEY. REMOVED AND REPLACED MLG SELECTOR VALVE. - [SDR COMA201107550045](https://openairdocs.org/sdr/COMA201107550045), Jul 14, 2011: WIRE HARNESS. DEFECTIVE. ON CLIMBOUT FROM DTW RECEIVED GEAR DISAGREE WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW AND LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR WOW N - [SDR COMA2011071550044](https://openairdocs.org/sdr/COMA2011071550044), Jul 14, 2011: WIRE HARNESS. DEFECTIVE. ON CLIMBOUT FROM DTW RECEIVED GEAR DISAGREE WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW AND LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR WOW N - [SDR COMA2010081950178](https://openairdocs.org/sdr/COMA2010081950178), Aug 19, 2010: FLOORBEAM. CORRODED. CORROSION FOUND AROUND 4 EACH NUT PLATES FS 589 - 618 LBL 27. REMOVED AND REPLACED FLOORBEAM UPPER CAP IAW CRJ SRM 51-42-21. - [SDR COMA2010081850177](https://openairdocs.org/sdr/COMA2010081850177), Aug 18, 2010: DOOR FRAME. CRACKED. FOUND CRACKED FRAME MEMBER IN LOWER AFT SIDE OF CARGO DOOR P/N 601R35027-31. REPLACED CARGO DOOR LOWER AFT FRAME MEMBER P/N 601R35027-31 IAW CRJ SRM 51-42-06. - [SDR COMA2010081650176](https://openairdocs.org/sdr/COMA2010081650176), Aug 16, 2010: ANGLE. CRACKED. FS 559 CAP ANGLE CRACKED AT RBL 18. CUT OUT DAMAGED AREA AND INSTALLED NEW CAP ANGLE SECTION IAW REO 601R-53-41-260 AND DEVIATION REO 601R-53-41-609. - [SDR COMA2010081650175](https://openairdocs.org/sdr/COMA2010081650175), Aug 14, 2010: BULKHEAD. CRACKED. BULKHEAD WEB CRACKED AROUND PARK BRAKE CABLE CUTOUT, FS 202.75, LBL 23.71. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563 AND DEVIATIO - [SDR COMA2010081350173](https://openairdocs.org/sdr/COMA2010081350173), Aug 12, 2010: BULKHEAD. CRACKED. AT FS 621.00 FORWARD SIDE OF THE REAR PRESSURE BULKHEAD, THE LINTLE FITTING AREA AT LBL 27.50 IS CRACKED. REPAIRED AFT PRESSURE BULKHEAD IAW REO601R-53-61-1230 - [SDR COMA0860178](https://openairdocs.org/sdr/COMA0860178), Mar 16, 2008: THRUST REVERSER. MALFUNCTIONED. FLIGHT 5015 - ON CLIMBOUT FROM YYZ PASSING THROUGH 8000 FT, RECEIVED RIGHT REV UNLOCK CAUTION MESSAGE. AIRCRAFT DIVERTED TO BUF AND LANDED SAFELY. TRANSFERRED T - [SDR COMA0860115](https://openairdocs.org/sdr/COMA0860115), Feb 8, 2008: ENGINE. VIBRATION. FLIGHT 5024 - DURING CRUISE, RIGHT ENGINE N1 VIBE SHOWED AMBER DASHES AT IDLE AND RIGHT ENGINE VIBE INDICATION SHOWED 3.0. DECLARED EMERGENCY, DIVERTED TO STL, - [SDR COMA0760555](https://openairdocs.org/sdr/COMA0760555), Sep 3, 2007: LIGHT. INOPERATIVE. FLIGHT 5088 - FORWARD FLOOR EMERGENCY FLOOR STRIP NOT ILLUMINATING. REMOVED AND REPLACED FLEX LAMP ASSEMBLY. - [SDR COMA0760544](https://openairdocs.org/sdr/COMA0760544), Aug 26, 2007: CONTROL HANDLE. FAULTY. FLIGHT 5618 - RECEIVED FLAP FAIL CAUTION MESSAGE AFTER LANDING. REPLACED FLAP CONTROL HANDLE. NO FURTHER DEFECTS. - [SDR COMA0760455](https://openairdocs.org/sdr/COMA0760455), Jun 27, 2007: SEAL. UNKNOWN. FLIGHT 5638 - AIRCRAFT LOST PRESSURE, AND PAX DOOR HAS LOUD SQUEALING NOISE. DECLARED EMERGENCY, LANDED JAX WITHOUT INCIDENT. INSPECTED MAIN CABIN DOOR, NO DEFE - [SDR COMA0660622](https://openairdocs.org/sdr/COMA0660622), Nov 9, 2006: CONTROLLER. FAULTY. FLIGHT 5117 - RIGHT WINDOW HEAT MESSAGE CAME ON JUST AFTER TAKEOFF. REPLACED RIGHT SIDE WINDOW CONTROLLER. - [SDR COMA0660609](https://openairdocs.org/sdr/COMA0660609), Nov 3, 2006: CONNECTOR. DIRTY. FLIGHT 5197- EMERGENCY FLOOR LIGHTING AT SEAT 8A IS INOPERATIVE. REMOVED AFFECTED LIGHTING STRIP. INSPECTED, CLEANED CONNECTORS AND REINSTALLED. OPERATIONAL CHE - [SDR COMA0660553](https://openairdocs.org/sdr/COMA0660553), Sep 25, 2006: SELECTOR VALVE. FAULTY. FLIGHT 5010- GEAR DISAGREE WARNING RECEIVED ON TAKE-OFF. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED.REPLACED MLG SELECTOR VALVE. PERFO - [SDR COMA0660552](https://openairdocs.org/sdr/COMA0660552), Sep 18, 2006: BULB. BURNED OUT. FLIGHT 5186- LT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. RELAMPED LT FORWARD OVERWING EMERGENCY LIGHT. NO FURTHER DEFECTS. - [SDR COMA0660538](https://openairdocs.org/sdr/COMA0660538), Sep 10, 2006: SELECTOR VALVE. FAULTY. FLIGHT 5069 - EN ROUTE CVG-DSM RECEIVED A RIGHT LANDING GEAR DISAGREE MESSAGE. REPLACED THE MLG SELECTOR VALVE ASSEMBLY. - [SDR COMA0660274](https://openairdocs.org/sdr/COMA0660274), Mar 21, 2006: OIL SYSTEM. LOW. FLIGHT 5712- AFTER TAKEOFF FROM CVG, RECEIVED A RIGHT ENGINE LOW OIL PRESSURE WARNING MESSAGE, OIL PRESSURE FLUCTUATED BETWEEN 23 AND 45 PSI. FLIGHT RETURNED TO - [SDR COMA0660137](https://openairdocs.org/sdr/COMA0660137), Feb 11, 2006: WARNING LIGHT. ILLUMINATED. FLIGHT 5689 - EN ROUTE CVG-GRR RECEIVED A LEFT COWL ANTI-ICE CAUTION MESSAGE, FLIGHT RETURNED TO CVG. PERFORMED AN OPERATIONAL CHECK OF THE ENGINE COWL ANTI-ICE - [SDR COMA0560363](https://openairdocs.org/sdr/COMA0560363), Jun 21, 2005: WIRE. DAMAGED. FWD SECTION OF EMERGENCY FLOOR LIGHTING INOPERABLE. WARDROBE EMERGENCY LIGHT WIRING DAMAGED. REPAIRED WIRING AND EMERGENCY LIGHTS. OPERATION SATISFACTORY. - [SDR COMA0560066](https://openairdocs.org/sdr/COMA0560066), Jan 17, 2005: SERVO. INSTALLED. FLIGHT 5154 ON FINAL WITH A/P OFF, FO'S ELEVATOR CONTROLS JAMMED. WHEN PRESSURE APPLIED CONTROLS BROKEN FREE. COULD NOT DUPLICATE INSPECTION OF FLIGHT CONTROLS - [SDR COMA0560039](https://openairdocs.org/sdr/COMA0560039), Jan 13, 2005: SEAL. INOPERATIVE. FLIGHT 5179 CABIN WOULD NOT PRESSURIZE. REPLACED THE CABIN DOOR SEAL. - [SDR COMA0560031](https://openairdocs.org/sdr/COMA0560031), Jan 7, 2005: CONTROL SYSTEM. UNKNOWN. FLIGHT 5134 T/O ABORTED DUE TO STIFF ELEVATOR CONTROL. COULD NOT DUPLICATE. INSPECTED ELEVATOR CONTROL SYSTEM, NO DEFECTS FOUND. FLIGHT CHECK SATISFACTORY. - [SDR COMA0460516](https://openairdocs.org/sdr/COMA0460516), Sep 16, 2004: INTERCOSTAL. CORRODED. LEFT HAND INTERCOSTAL CORRODED IN CABIN AT LBL 36 AND LBL 27 AT FS 484. REPAIRED IAW REO 601R-53-41-059. - [SDR COMA0460523](https://openairdocs.org/sdr/COMA0460523), Sep 16, 2004: FLOOR SUPPORT. CRACKED. LT FLOOR SUPPORT ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. - [SDR COMA0460409](https://openairdocs.org/sdr/COMA0460409), Jul 19, 2004: DOUBLER. CRACKED. RIGHT HAND 640 FRAME DOUBLERS CRACKED. REPAIRED IAW REO 601R-53-61-1089. - [SDR COMA0460410](https://openairdocs.org/sdr/COMA0460410), Jul 19, 2004: DOUBLER. CRACKED. LEFT HAND 640 FRAME DOUBLERS CRACKED. REPAIRED IAW REO 601R-53-61-1089. - [SDR COMA0460332](https://openairdocs.org/sdr/COMA0460332), May 23, 2004: ELEMENT. MALFUNCTIONED. FLIGHT 5436 MLG BAY OVERTEMP WARNING. REPLACED RT MLG BAY SENSING ELEMENT. - [SDR COMA0460303](https://openairdocs.org/sdr/COMA0460303), May 10, 2004: FLOOR SUPPORT. CRACKED. CARGO FLOOR SILL IS TORN WHERE THE FOLD DOWN PROTECTIVE EDGE ATACH BRACKET IS LOCATED AT STATION FS 574.0. C/W 601R-53-61-690. - [SDR COMA0360496](https://openairdocs.org/sdr/COMA0360496), Nov 11, 2003: PROXIMITY SWITCH. MALFUNCTIONED. FLIGHT 5579 DURING CLIMBOUT OF TRI RECEIVED A GEAR DISAGREE WARNING MESSAGE, AIRCRAFT RETURNED TO THE FIELD. ADJUSTED THE NOSE LANDING GEAR PROXIMITY SWITCH. - [SDR COMA0360495](https://openairdocs.org/sdr/COMA0360495), Nov 11, 2003: DETECTOR. MALFUNCTIONED. FLIGHT 5579 DURING CLIMBOUT OF ATL RECEIVED A MLG BAY OVERHEAT CAUTION, AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT TRI. DEFERRED THE MLG BAY OVERHEAT DETECTIO - [SDR COMA0360273](https://openairdocs.org/sdr/COMA0360273), Jun 11, 2003: MECHANISM. DIRTY. FLIGHT 5258 CABIN DOOR WARNING MESSAGE. FOUND DOOR HANDLE MECHANISM ALL GUMMED UP. CLEANED AND LUBED DOOR MECHANISM. - [SDR COMA0260264](https://openairdocs.org/sdr/COMA0260264), Apr 16, 2002: WEU. FLIGHT 5910 T/O ABORTED AT 95 KTS.C/W RTO INSPECTION - [SDR COMA0260086](https://openairdocs.org/sdr/COMA0260086), Feb 4, 2002: SKIN PANEL. FLIGHT 9461 BIRDSTRIKE ON NOSE OF AIRCRAFT DURING T/O.C/W BIRDSTRIKE INSP - NO DAMAGE FOUND. - [SDR COMA0160323](https://openairdocs.org/sdr/COMA0160323), Mar 18, 2001: FUEL CAP. LOOSE. RT FUEL CAP CAME LOOSE DURING T/O. INSPECTED FUEL CAP AND STRUCTURE. REINSTALLED CAP. - [SDR COMA0160156](https://openairdocs.org/sdr/COMA0160156), Jan 23, 2001: FCU. MALFUNCTIONED. FLAPS FAIL MESSAGE. REPLACED THE FECU. ## STCs that may be installed (OpenAirDocs) (360, 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 (Cessna 310R) - [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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc - [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 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 SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists 310 Series - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [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 SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics - [STC SA111GL](https://openairdocs.org/stc/SA111GL): Install Cleveland conversion kit P/N 199-64. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [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 SA4222SW](https://openairdocs.org/stc/SA4222SW): Mount collision avoidance lights in engine nacelle. Johnson Aviation Products - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc - [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King) - [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King) - [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 SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [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 SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc - [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA1273CE](https://openairdocs.org/stc/SA1273CE): Installation of King KFC 200 2-axis(3 optional) flight control system with a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller. Honeywell International Inc - [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. Honeywell International Inc - [STC SA1555CE-D](https://openairdocs.org/stc/SA1555CE-D): Installation of King Model KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with Flight Director. 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 SA2203WE](https://openairdocs.org/stc/SA2203WE): Installation of air conditioning system. Air Comm Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA00571SE](https://openairdocs.org/stc/SA00571SE): Replacement of certain BF Goodrich pneumatic deicer boots. SMR Technologies Inc - [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 All 360: https://openairdocs.org/aircraft/N427CA/stcs.md ## Related - Other Cessna 310R aircraft: https://openairdocs.org/model/cessna-310r/aircraft.md - The Continental IO-520 series engine: https://openairdocs.org/engine/continental-io-520-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.