# Cessna 310E - Type: Aircraft model (FAA registry) - Registry code: 2074214 - Manufacturer (registry): CESSNA - Model: 310E - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Reciprocating - Seats: 5 - Weight class: Up to 12,499 lb - Cruise speed: 167 mph - Certification: Type certificated - Data sheet: [TCDS 3A10](https://openairdocs.org/tcds/3A10) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 6 - Page: https://openairdocs.org/model/cessna-310e Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [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). 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 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005 - [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 98-25-02](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 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 81-19-04](https://openairdocs.org/ad/81-19-04): Hose Assembly · Rajay Hose Assemblies, 500A, 500B and 87 more. Effective Sep 17, 1981 - [AD 72-14-08 R1](https://openairdocs.org/ad/72-14-08-R1): Flexible Hose Assemblies · Cessna 310, 310A, 310B and 33 more. Effective Sep 4, 1981 - [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 69-15-09](https://openairdocs.org/ad/69-15-09): Fuel Starvation · Cessna 310, 310A, 310B and 6 more. Effective Jul 25, 1969 - [AD 69-12-03](https://openairdocs.org/ad/69-12-03): Fuel Crossfeed Lines · Cessna 310, 310A, 310B and 4 more. Effective Jun 10, 1969 - [AD 57-04-01](https://openairdocs.org/ad/57-04-01): Aileron Hinge · Cessna 310, 310A, 310B and 15 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 ## Information bulletins (advisory) (7) - [SAIB CE-13-27R1](https://openairdocs.org/saib/CE-13-27R1): Flight Controls Frayed Flap Extend Cables. Issued Jan 5, 2022 - [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-14-11](https://openairdocs.org/saib/CE-14-11) (historical): Landing Gear; Nose Landing Gear Trunnions. Issued Feb 25, 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 ACE-99-05](https://openairdocs.org/saib/ACE-99-05): . Issued Nov 17, 1998 ## Registered aircraft (6) - [N47NF](https://openairdocs.org/aircraft/N47NF): [Andrews University](https://openairdocs.org/faa-owner/ANDREWS%20UNIVERSITY), [Berrien Springs, MI](https://openairdocs.org/faa-place/MI/Berrien%20Springs), S/N 60-6047 - [N5076A](https://openairdocs.org/aircraft/N5076A): [Skowbo Rock G](https://openairdocs.org/faa-owner/SKOWBO%20ROCK%20G), [Winchester, VA](https://openairdocs.org/faa-place/VA/Winchester), built 1961, S/N 310M0018 - [N5215G](https://openairdocs.org/aircraft/N5215G): [Maynard Timothy W](https://openairdocs.org/faa-owner/MAYNARD%20TIMOTHY%20W), [Tillamook, OR](https://openairdocs.org/faa-place/OR/Tillamook), built 1961, S/N 310M0023 - [N5244G](https://openairdocs.org/aircraft/N5244G): [Mcmahan William K](https://openairdocs.org/faa-owner/MCMAHAN%20WILLIAM%20K), [Sandy Valley, NV](https://openairdocs.org/faa-place/NV/Sandy%20Valley), built 1961, S/N 310M0026 - [N8136Z](https://openairdocs.org/aircraft/N8136Z): [University Of Alaska Anchorage](https://openairdocs.org/faa-owner/UNIVERSITY%20OF%20ALASKA%20ANCHORAGE), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), S/N 31010004 - [N909SD](https://openairdocs.org/aircraft/N909SD): [Acqua Aviation Inc](https://openairdocs.org/faa-owner/ACQUA%20AVIATION%20INC), [Wayzata, MN](https://openairdocs.org/faa-place/MN/Wayzata), built 1960, S/N 310M0027 ## NTSB investigations (4) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX92LA337](https://openairdocs.org/ntsb/LAX92LA337), Aug 8, 1992: Cessna 310M (N26070), Honolulu, HI, destroyed, 2 fatal. Probable cause: LOSS OF AIRCRAFT CONTROL FOR AN UNDETERMINED REASON AFTER THE PILOT TOOK OFF AT NIGHT AND FLEW THE AIRCRAFT INTO THE AREA OF A THUNDERSTORM AND LIGHTNING. - [NTSB DEN89LA109](https://openairdocs.org/ntsb/DEN89LA109), Apr 17, 1989: Cessna 310E (N4127G), Glenwood Spgs, CO, substantial damage. Probable cause: INADEQUATE COMPENSATION FOR THE WIND CONDITIONS BY THE PILOT, RESULTING IN A LOSS OF CONTROL OF FINAL APPROACH. CONTRIBUTING TO THE ACCIDENT WAS THE DOWNDRAFT. - [NTSB DEN85LA095](https://openairdocs.org/ntsb/DEN85LA095), Mar 14, 1985: Cessna 310 (N5515G), Angel Fire, NM, substantial damage - [NTSB ANC81DA042](https://openairdocs.org/ntsb/ANC81DA042), Apr 10, 1981: Cessna 310E (N5215G), Elmendorf Afb, AK, substantial damage ## FAA accident and incident reports (9) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20210627010979I](https://openairdocs.org/incident/20210627010979I), Jun 27, 2021: Cessna 310E (N5076A), Weyers Cave, VA, Minor damage. The pilot stated that on approach to runway 5 shd, he set up the aircraft for landing, flaps approach and gear down. He stated he checked the gear at least 2… - [Accident 19920808029729A](https://openairdocs.org/incident/19920808029729A), Aug 8, 1992: Cessna 310E (N26070), Honolulu, HI, Destroyed, 2 fatal. Flew into area of thunderstorms at dark night,heavy rain. Disappeared off radar over ocean. Cabin seats in ocean. - [Accident 19890417008299A](https://openairdocs.org/incident/19890417008299A), Apr 17, 1989: Cessna 310E (N4127G), Glenwood Spring, CO, Substantial damage. Landed hard short of runway. Bounced, came back down and broke all three main gears. - [Accident 19850314006879A](https://openairdocs.org/incident/19850314006879A), Mar 14, 1985: Cessna 310E (N5515G), Angel Fire, NM, Substantial damage. Aircraft landed on closed portion of runway. Soft surface caused nose gear collapse. Displaced threshold marked. - [Incident 19831124072899I](https://openairdocs.org/incident/19831124072899I), Nov 24, 1983: Cessna 310E (N5515G), Plano, TX, Minor damage. Veered off the runway into a ditch on the landing rollout. Claimed brake problems. None found. - [Incident 19830619037489I](https://openairdocs.org/incident/19830619037489I), Jun 19, 1983: Cessna 310E (N5515G), Grand Prairie, TX, Minor damage. Nose gear malfunctioned on takeoff. Landed with it partially extended. Flat nose gear strut failed rod idler arm. - [Incident 19820906055009I](https://openairdocs.org/incident/19820906055009I), Sep 6, 1982: Cessna 310E (N5216G), Anchorage, AK, Minor damage. Airplane on first flight after maintenance. Unable to lower nose gear for landing. Gear door not connected. - [Accident 19810410018599A](https://openairdocs.org/incident/19810410018599A), Apr 10, 1981: Cessna 310E (N5215G), Elmendorf Afb, AK, Substantial damage. Nose wheel collapsed during landing roll. Investigation revealed improper maintenance. - [Incident 19781224020969I](https://openairdocs.org/incident/19781224020969I), Dec 24, 1978: Cessna 2105 (N8136Z), Yakima, WA, Minor damage. Passengers on board, pilot pulled prop through before start. Engine started, ended up in a creek bed. ## STCs that may be installed (OpenAirDocs) (241, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA00061LA](https://openairdocs.org/stc/SA00061LA): Installation of JPI digital tachometer. J P Instruments - [STC SA00063LA](https://openairdocs.org/stc/SA00063LA): Installation of Acoustical/Thermal insulation. Luminary Air Group LLC - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics 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 SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc - [STC SA00150SE](https://openairdocs.org/stc/SA00150SE): Installation of TSO shoulder harness assembly with inertia reel and associated mounting brackets in accordance with FAA approved AeroMods Master Drawing List MH010, Rev. B, dated October 13, 1994, or later FAA approved revision. Branson William N - [STC SA00161BO (1 OF 3)](https://openairdocs.org/stc/SA00161BO%20(1%20OF%203)): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. Avidyne Corporation - [STC SA00215NY](https://openairdocs.org/stc/SA00215NY): Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. CAVU Products Limited - [STC SA00228NY](https://openairdocs.org/stc/SA00228NY): Installation of Sky Harbour Aircraft Refinishing Ltd Ice Damage Prevention Plates. Sky Harbour Aircraft Refinishing - [STC SA00243BO (2 OF 5)](https://openairdocs.org/stc/SA00243BO%20(2%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200). Icarus Avionics, LLC - [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation - [STC SA00280NY](https://openairdocs.org/stc/SA00280NY): Installation of .250 inch thick replacement windshield. L P Aero Plastics, Inc - [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation - [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne 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 SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00402SE](https://openairdocs.org/stc/SA00402SE): Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed). Aviation Development Corporation - [STC SA00409DE](https://openairdocs.org/stc/SA00409DE): Installation of an aircraft noise control system. Quiet Flight LLC - [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument. J P Instruments - [STC SA00678SE](https://openairdocs.org/stc/SA00678SE): Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments. J P Instruments - [STC SA00680SE (3 OF 6](https://openairdocs.org/stc/SA00680SE%20(3%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. Electronics International - [STC SA00695SE](https://openairdocs.org/stc/SA00695SE): Replacement of certain Rotomaster and Rayjay scavenge pumps. Machen Inc - [STC SA00709LA](https://openairdocs.org/stc/SA00709LA): Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. Trevor Burward-Hoy - [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 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 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 SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00799CH](https://openairdocs.org/stc/SA00799CH): Installation of Honeywell HC-C2YF-2CUF/FC8468(B)-3 propellers, C-2285-4(P) spinners, A-2476-8 spinner mounting kits and A-2374-1 anti-ice kits. Hartzell Propeller Inc - [STC SA00804SE](https://openairdocs.org/stc/SA00804SE): Installation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'. Advanced Aero Safety Inc - [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments - [STC SA00879CH](https://openairdocs.org/stc/SA00879CH): Installation of McCauley Propeller Model 3AF32C528/82NEA-4 spinner and optional anti-ice/deice. McCauley Propeller Systems - [STC SA00944CH](https://openairdocs.org/stc/SA00944CH): Replace Janitrol combustion heater Model 81D94-X (XX) with C&D Associates combustion heater Model CD25K, CD35K, and CD45K. Hartzell Engine Technologies, LLC - [STC SA01077SE](https://openairdocs.org/stc/SA01077SE): Installation of fluoropolymer film. Columbia Pacific Airlines - [STC SA01085LA](https://openairdocs.org/stc/SA01085LA): Installation of the VNS 1000 Voice Navigation System. VNS Incorporated - [STC SA01105WI-D (1 OF 2)](https://openairdocs.org/stc/SA01105WI-D%20(1%20OF%202)): Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). Honeywell International Inc - [STC SA01114CH](https://openairdocs.org/stc/SA01114CH): Installation of P2 Incorporated 6600 Audio Advisory system. P2 Incorporated - [STC SA01118WI](https://openairdocs.org/stc/SA01118WI): Installation of the Concorde FLA or VRSLA RG series batteries. Concorde Battery Corporation - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Electronics International Inc - [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Aero Enhancements Inc - [STC SA01205WI-D (1 OF 2)](https://openairdocs.org/stc/SA01205WI-D%20(1%20OF%202)): Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. Honeywell International Inc - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA01280CH](https://openairdocs.org/stc/SA01280CH): Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404). D & K Aviation - [STC SA01370SE](https://openairdocs.org/stc/SA01370SE): Installation of BAS, Inc. Shoulder Harness in accordance with BAS, Inc. Drawing List, which includes Installation Instructions, and Instructions for Continued Airworthiness, listed on FAA AML SA01370SE, dated January 26, 2004, or later FAA approved revision. BAS Inc - [STC SA01420WI](https://openairdocs.org/stc/SA01420WI): Installation of Garmin GNS 430A / 530A COMM/NAV/GPS Systems. Data required: (1) Scandinavian Avionics Design GmbH Drawing List 2027438-DL-02, Issue 2; or later EASA approved revisions. (2) Scandinavian Avionics Design GmbH Approved Aircraft Flight Manual Supplement, Doc. 2027438-AM-02A, Issue 1, and Doc. 2027438-AM-02B, Issue 2, both approved by EASA under approval No. EASA.A.S.01389 dated 07-09-2005, or later EASA approved revision. Scandinavian Avionics Design GmbH - [STC SA01436SE (1 OF 2)](https://openairdocs.org/stc/SA01436SE%20(1%20OF%202)): Cockpit sunvisor retrofit kit. Rosen Sunvisor Systems LLC - [STC SA01473SE (2 OF 5)](https://openairdocs.org/stc/SA01473SE%20(2%20OF%205)): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc - [STC SA01487SE (2 OF 5)](https://openairdocs.org/stc/SA01487SE%20(2%20OF%205)): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc All 241: https://openairdocs.org/model/cessna-310e/stcs.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.