# Cessna 320A

- Type: Aircraft model (FAA registry)
- Registry code: 2074506
- Manufacturer (registry): CESSNA
- Model: 320A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 6
- Weight class: Up to 12,499 lb
- Cruise speed: 183 mph
- Certification: Type certificated
- Data sheet: [TCDS 3A25](https://openairdocs.org/tcds/3A25) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 6
- Page: https://openairdocs.org/model/cessna-320a

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 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 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 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 2000-01-16](https://openairdocs.org/ad/2000-01-16): Exhaust System · Cessna 320, 320-1, 320A and 28 more. Effective Feb 15, 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 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 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 75-11-01](https://openairdocs.org/ad/75-11-01): Fuel Lines · Cessna 320, 320-1, 320A and 5 more. Effective Mar 22, 1976
- [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 71-09-01](https://openairdocs.org/ad/71-09-01): Nacelle Electrical Failures · Cessna 320, 320-1, 320A and 5 more. Effective Apr 23, 1971
- [AD 69-14-01](https://openairdocs.org/ad/69-14-01): Fuel Starvation · Cessna 310G, 310H, 310I 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

## 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 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-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-99-06](https://openairdocs.org/saib/ACE-99-06): . Issued Nov 17, 1998
- [SAIB ACE-99-05](https://openairdocs.org/saib/ACE-99-05): . Issued Nov 17, 1998

## Registered aircraft (6)

- [N3008R](https://openairdocs.org/aircraft/N3008R): [Perguson Robert C](https://openairdocs.org/faa-owner/PERGUSON%20ROBERT%20C), [Converse, TX](https://openairdocs.org/faa-place/TX/Converse), built 1962, S/N 320A0008
- [N3020R](https://openairdocs.org/aircraft/N3020R): [Hill James C](https://openairdocs.org/faa-owner/HILL%20JAMES%20C), [Grand Saline, TX](https://openairdocs.org/faa-place/TX/Grand%20Saline), built 1962, S/N 320A0020
- [N3027R](https://openairdocs.org/aircraft/N3027R): [Ledford James](https://openairdocs.org/faa-owner/LEDFORD%20JAMES), [Broad Run, VA](https://openairdocs.org/faa-place/VA/Broad%20Run), built 1962, S/N 320A0027
- [N3040R](https://openairdocs.org/aircraft/N3040R): [Sturgeon Newton Charles](https://openairdocs.org/faa-owner/STURGEON%20NEWTON%20CHARLES), [Midland, TX](https://openairdocs.org/faa-place/TX/Midland), built 1963, S/N 320A-0040
- [N320CR](https://openairdocs.org/aircraft/N320CR): [Bas Part Sales LLC](https://openairdocs.org/faa-owner/BAS%20PART%20SALES%20LLC), [Greeley, CO](https://openairdocs.org/faa-place/CO/Greeley), built 1962, S/N 320A0003
- [N5HS](https://openairdocs.org/aircraft/N5HS): [Rose Raymond P](https://openairdocs.org/faa-owner/ROSE%20RAYMOND%20P), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego), built 1962, S/N 320A0026

## NTSB investigations (16)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW97LA020](https://openairdocs.org/ntsb/FTW97LA020), Oct 18, 1996: Cessna 320A (N430N), Longmont, CO, substantial damage. Probable cause: The partial failure of the fuel control servo, causing an excessive flow/output of fuel to, and flooding of, the right engine.
- [NTSB SEA96FA094](https://openairdocs.org/ntsb/SEA96FA094), May 15, 1996: Cessna 320A (N600JR), Provo, UT, destroyed, 2 fatal. Probable cause: A fuel leak most probably ignited by hot exhaust gases from the leaking right engine manifold exhaust system, the decision by the pilots to operate the aircraft with knowledge of the fuel leak, and…
- [NTSB LAX92LA344](https://openairdocs.org/ntsb/LAX92LA344), Aug 9, 1992: Cessna 320A (N3014R), Novato, CA, substantial damage. Probable cause: THE LOCKED LEFT BRAKE ASSEMBLY DUE TO THE MISSING BRAKE RETAINING CLIPS.
- [NTSB ATL82DA111](https://openairdocs.org/ntsb/ATL82DA111), Apr 21, 1982: Cessna 320A (N600JR), Paintsville, KY, substantial damage
- [NTSB NYC81FA041](https://openairdocs.org/ntsb/NYC81FA041), Apr 20, 1981: Cessna 320 (N5500E), West Mifflin, PA, destroyed, 2 fatal
- [NTSB OAK79FA036](https://openairdocs.org/ntsb/OAK79FA036), Jul 26, 1979: Cessna 320A (N3005R), Monterey, CA, destroyed, 2 fatal
- [NTSB DEN76O0001](https://openairdocs.org/ntsb/DEN76O0001), Oct 18, 1975: Cessna 320 (N3043R), Puerta Valrto, Mexico, destroyed, 4 fatal
- [NTSB OAK74FXQ23](https://openairdocs.org/ntsb/OAK74FXQ23), Feb 24, 1974: Cessna 320A (N3033R), Fallon, NV, substantial damage
- [NTSB CHI74FEE26](https://openairdocs.org/ntsb/CHI74FEE26), Oct 14, 1973: Cessna 320 (N861W), Northbrook, IL, destroyed, 1 fatal
- [NTSB OAK73IP016](https://openairdocs.org/ntsb/OAK73IP016), Dec 12, 1972: Cessna 320A (N3044R), Redding, CA, incident, minor damage
- [NTSB DEN68A0028](https://openairdocs.org/ntsb/DEN68A0028), Dec 30, 1967: Cessna 320A (N3047R), Kanosh, UT, destroyed, 1 fatal
- [NTSB DEN68F0034](https://openairdocs.org/ntsb/DEN68F0034), Jul 23, 1967: Cessna 320A (N3017R), Alamosa, CO, destroyed
- [NTSB OAK67A0080](https://openairdocs.org/ntsb/OAK67A0080), May 18, 1967: Cessna 320A (N3014R), Montello, NV, substantial damage
- [NTSB CHI66F0579](https://openairdocs.org/ntsb/CHI66F0579), Feb 17, 1966: Cessna 320 (N5500E), Saginaw, MI, substantial damage
- [NTSB UNK65X1408](https://openairdocs.org/ntsb/UNK65X1408), Feb 8, 1965: Cessna 320 (N3012R), Rancho Mirage, CA, substantial damage
- [NTSB UNK65X0590](https://openairdocs.org/ntsb/UNK65X0590), Nov 7, 1964: Cessna 320 (N3047R), Norfolk, NE, substantial damage

## FAA accident and incident reports (18)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19980701029429I](https://openairdocs.org/incident/19980701029429I), Jul 1, 1998: Cessna 320A (N3038R), Philadelphia, PA, Minor damage. Upon takeoff from pne, during landing gear retraction, the pilot heard a loud noise and was unable to get a gear up light indication. A visual check revealed…
- [Incident 19980312012909I](https://openairdocs.org/incident/19980312012909I), Mar 12, 1998: Cessna 320A (N3038R), Philadelphia, PA, Minor damage. Narrative: after about 1 hour of flight I heard a bang and felt bump from floor board. I could then see nose tire partially hanging out of gear door via…
- [Incident 19980118002079I](https://openairdocs.org/incident/19980118002079I), Jan 18, 1998: Cessna 320A (N3012R), Twin Bridges, MT, Minor damage. Encountered snow on runway veered left. Unable to return to runway in spite of control inputs. Damage tire wheel.
- [Accident 19961018047039A](https://openairdocs.org/incident/19961018047039A), Oct 18, 1996: Cessna 320A (N430N), Longmont, CO, Substantial damage. (-16) Engine teardown in progress. This report will be updated at a later time.
- [Accident 19960515010679A](https://openairdocs.org/incident/19960515010679A), May 15, 1996: Cessna 320A (N600JR), Provo, UT, Destroyed, 2 fatal. Pilot reported right engine fire. Crashed into a lake. Deteriorated exhaust manifold failed. Fuel leak prior flight.
- [Incident 19931218050689I](https://openairdocs.org/incident/19931218050689I), Dec 18, 1993: Cessna 320A (N3012R), Angleton, TX. Pilot made precautionary landing during a ferry flight. Low fuel and weather was deteriorating.
- [Incident 19930808039619I](https://openairdocs.org/incident/19930808039619I), Aug 8, 1993: Cessna 320A (N3012R), Clinton, MD, Minor damage. Engine rough after takeoff. Returned. Became distracted. Forgot to lower gear, landed gear up.
- [Accident 19920808034739A](https://openairdocs.org/incident/19920808034739A), Aug 8, 1992: Cessna 320A (N3014R), Novato, CA, Substantial damage. Left main wheel locked on landing roll. Left runway into a ditch. Brake clips fell out allowing disc jam in housing
- [Incident 19890929052819I](https://openairdocs.org/incident/19890929052819I), Sep 29, 1989: Cessna 320A (N3020R), Las Vegas, NV, Minor damage. Right gear collapsed on rollout. Veered off runway. Hit runway light. Main gear had not locked. Cause undetermined.
- [Incident 19860713060259I](https://openairdocs.org/incident/19860713060259I), Jul 13, 1986: Cessna 320A (N3019H), College Park, MD, Minor damage. Aircraft overshot landing, unable to stop, ran off side of runway end and struck a ditch.
- [Accident 19821105063179A](https://openairdocs.org/incident/19821105063179A), Nov 5, 1982: Cessna 320A (N3042R), Terrell, TX, Minor damage. Pilot landed with gear up. Failed to use landing check list. No registration on board.
- [Accident 19820421010709A](https://openairdocs.org/incident/19820421010709A), Apr 21, 1982: Cessna 320A (N600JR), Paintsville, KY, Substantial damage. Dropped out on leveloff for landing in gusty crosswind. Level impact with runway bent wing spars. Other damage.
- [Accident 19810420017389A](https://openairdocs.org/incident/19810420017389A), Apr 20, 1981: Cessna 320 (N5500E), West Mifflin, PA, Substantial damage, 1 fatal. Aircraft crashed off end of runway during final approach. Airplane appeared to stall and dive into ground.
- [Accident 19790726037479A](https://openairdocs.org/incident/19790726037479A), Jul 26, 1979: Cessna 320A (N3005R), Monterey, CA, Destroyed, 1 fatal. Acft off course and below minimum altitude on second ILS apch. Hit trees on ridge. First apch also erratic.
- [Incident 19780310014389I](https://openairdocs.org/incident/19780310014389I), Mar 10, 1978: Cessna 320A (N213CW), Buffalo, NY. Pilot returned due to oil loss from an engine. Crank shaft seal leaking, was replaced.
- [Accident 19751018036459A](https://openairdocs.org/incident/19751018036459A), Oct 18, 1975: Cessna 320A (N3043R), Puerta Valrto, Destroyed, 3 fatal. Invest under jurisdiction of govt of Mexico.
- [Accident 19740224004049A](https://openairdocs.org/incident/19740224004049A), Feb 24, 1974: Cessna 320A (N3033R), Fallon, NV, Substantial damage. Plt lndd on 1050 ft long sage brush covered road. Swerved to avoid ditch.
- [Accident 19731014033269A](https://openairdocs.org/incident/19731014033269A), Oct 14, 1973: Cessna 320A (N861W), Northbrook, IL, Destroyed, 1 fatal. Pilot not multi eng rated no medical cert. No record of fly time since last refueling. City area.

## Service difficulty reports (5)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA040830010](https://openairdocs.org/sdr/CA040830010), Aug 12, 2004: PUSHROD. BROKEN. (CAN) PILOT PARKED THE AIRCRAFT BECAUSE OF OIL LEAKING AND RT ENGINE RUNNING ROUGH. THE RT ENGINE NR4 CYLINDER WAS FOUND TO HAVE A BROKEN INTAKE PUSHROD, BROKEN
- [SDR 98ZZZX1549](https://openairdocs.org/sdr/98ZZZX1549), Mar 12, 1998: TORQUE TUBE. FAILED. LANDING GEAR WAS RETRACTED. 40 MINUTES INTO FLIGHT, PILOT HEARD LOUD BANG. AIRCRAFT LANDED WITH MAINS EXTENDED AND LOCKED. NOSE GEAR PARTIALLY RETRACTED. UPON I
- [SDR 98ZZZX1113](https://openairdocs.org/sdr/98ZZZX1113), Mar 9, 1998: FITTING. CORRODED. DURING ANNUAL INSPECTION, FOUND REAR CABIN BULKHEAD SUPPORT (PN 0811075-10) BUCKLED. UPON FURTHER DISASSEMBLY, FOUND FITTING SEVERELY CORRODED.
- [SDR 98ZZZX1112](https://openairdocs.org/sdr/98ZZZX1112), Mar 9, 1998: SUPPORT. BUCKLED. DURING ANNUAL INSPECTION, FOUND REAR CABIN BULKHEAD SUPPORT (PN 0811075-10) BUCKLED. UPON FURTHER DISASSEMBLY, FOUND FITTING SEVERELY CORRODED.
- [SDR 98ZZZX471](https://openairdocs.org/sdr/98ZZZX471), Jan 5, 1998: OIL FILTER. FAILED. FOUND FILTER PLEATS POPPED OUTWARD ALLOWING OIL TO PASS THROUGH UNFILTERED. FOUND AUXILIARY OIL FILTER INSTALLATION HOSES CROSSED REVERSING THE OIL FLOW THROUGH

## STCs that may be installed (OpenAirDocs) (213, 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 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 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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [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 320 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 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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [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 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 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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [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 SA110GL](https://openairdocs.org/stc/SA110GL): Install Cleveland conversion kit P/N 199-64. (320 SERIES S/N'S 0001-D9999 320E0001-F9999). 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 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 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 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 SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. 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 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 SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights. Whelen Aerospace Technologies
- [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 SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [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 SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE 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 SA3822WE](https://openairdocs.org/stc/SA3822WE): Installation of 34-gallon auxiliary fuel tanks in each wing. OCR Aviation
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC

All 213: https://openairdocs.org/model/cessna-320a/stcs.md

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