# Aero Commander 680-E

- Type: Aircraft model (FAA registry)
- Registry code: 0141604
- Manufacturer (registry): AERO COMMANDER
- Model: 680-E
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 7
- Weight class: Up to 12,499 lb
- Cruise speed: 188 mph
- Certification: Type certificated
- Data sheet: [TCDS 2A4](https://openairdocs.org/tcds/2A4) (OpenAirDocs)
- Holder: Twin Commander Aircraft LLC
- Registered aircraft: 4
- Page: https://openairdocs.org/model/aero-commander-680-e

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 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 2000-02-30](https://openairdocs.org/ad/2000-02-30): Airframe Pneumatic Deicing Boots · Twin Commander 680, 680-E, 680-F and 15 more. Effective Mar 24, 2000
- [AD 98-20-34](https://openairdocs.org/ad/98-20-34): Airplane Flight Manuals--Severe Icing Conditions · Twin Commander 500, 500-A, 500-B and 24 more. Effective Nov 3, 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 98-07-17](https://openairdocs.org/ad/98-07-17): Flap System · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 29, 1998
- [AD 98-08-19](https://openairdocs.org/ad/98-08-19): Wing to Fuselage Attachment Brackets and Straps · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 18, 1998
- [AD 94-04-15](https://openairdocs.org/ad/94-04-15): Spar Cap · Twin Commander 500, 560-A, 560-E and 3 more. Effective Apr 12, 1994
- [AD 94-04-13](https://openairdocs.org/ad/94-04-13): Spar Cap · Twin Commander 500, 500-A, 500-B and 17 more. Effective Apr 12, 1994
- [AD 87-21-07 R1](https://openairdocs.org/ad/87-21-07-R1): Fuel Filler Openings · Twin Commander 500, 500-A, 500-B and 16 more. Effective May 5, 1989
- [AD 75-12-09 R2](https://openairdocs.org/ad/75-12-09-R2): Inadvertent Structural Failure · Twin Commander 500, 500-A, 500-B and 12 more. Effective Nov 28, 1981
- [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979
- [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978
- [AD 73-06-02](https://openairdocs.org/ad/73-06-02): Fuel Siphoning · Twin Commander 500, 500-A, 500-B and 13 more. Effective Mar 19, 1973
- [AD 67-28-01](https://openairdocs.org/ad/67-28-01): Lower Front Spar Cap · Twin Commander 560-E, 680, 680-E and 1 more. Effective Oct 10, 1967
- [AD 60-20-01](https://openairdocs.org/ad/60-20-01): Wing Rivet Replacement · Twin Commander 680-E and 720. Effective Oct 28, 1960
- [AD 59-16-01](https://openairdocs.org/ad/59-16-01): Fuel Line Routing · Twin Commander 500, 520, 560 and 5 more
- [AD 59-04-01](https://openairdocs.org/ad/59-04-01): Stabilizer Rivets · Twin Commander 500, 560, 560-A and 4 more

Historical (superseded or no longer in force):

- [AD 94-04-17](https://openairdocs.org/ad/94-04-17) (historical): Flap System Cable · Twin Commander 500, 500-A, 500-B and 27 more. Effective Apr 15, 1994

## Registered aircraft (4)

- [N4278S](https://openairdocs.org/aircraft/N4278S): [Chagnot Catherine J](https://openairdocs.org/faa-owner/CHAGNOT%20CATHERINE%20J), [Athens, OH](https://openairdocs.org/faa-place/OH/Athens), built 1959, S/N 680E-813-60
- [N8445C](https://openairdocs.org/aircraft/N8445C): [Maddox Jody S](https://openairdocs.org/faa-owner/MADDOX%20JODY%20S), [Paterson, WA](https://openairdocs.org/faa-place/WA/Paterson), built 1959, S/N 680E-777-49
- [N8468C](https://openairdocs.org/aircraft/N8468C): [Intravaia Anthony J](https://openairdocs.org/faa-owner/INTRAVAIA%20ANTHONY%20J), [Mountain View, CA](https://openairdocs.org/faa-place/CA/Mountain%20View), built 1959, S/N 680E-802-57
- [N9680E](https://openairdocs.org/aircraft/N9680E): [Mulkey Howard Daniel](https://openairdocs.org/faa-owner/MULKEY%20HOWARD%20DANIEL), [Spanaway, WA](https://openairdocs.org/faa-place/WA/Spanaway), S/N 699-18

## NTSB investigations (34)

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 WPR15LA265](https://openairdocs.org/ntsb/WPR15LA265), Sep 21, 2015: Aero Commander 680 E (N222JS), Boise, ID, substantial damage. Probable cause: The pilot's failure to maintain airplane control following an engine problem for reasons that could not be determined because postaccident examination of both engines and the rudder revealed no…
- [NTSB ERA14CA061](https://openairdocs.org/ntsb/ERA14CA061), Dec 3, 2013: Aero Commander 680E (N71DF), Crescent City, FL, substantial damage. Probable cause: The pilot's failure to maintain directional control during takeoff.
- [NTSB DFW08LA139](https://openairdocs.org/ntsb/DFW08LA139), May 8, 2008: Commander AC-680 (N39BA), Hope, AR, substantial damage. Probable cause: The pilot's failure to maintain control of the twin-engine airplane while landing. Contributing to the accident were the crosswind and partial loss of power on the right engine.
- [NTSB MIA96FA229](https://openairdocs.org/ntsb/MIA96FA229), Sep 10, 1996: Aero Commander 680E (N262X), Lakeland, FL, destroyed, 1 fatal. Probable cause: failure of the pilot to maintain minimum control speed, while returning to the airport for a precautionary landing, following a reported loss of power in one engine, which resulted in a loss of…
- [NTSB MIA91WA162](https://openairdocs.org/ntsb/MIA91WA162), Jun 12, 1991: Aero Commander 680-E (N6266B), Nassau, Bahamas, substantial damage
- [NTSB MIA90FA166](https://openairdocs.org/ntsb/MIA90FA166), Aug 5, 1990: Rockwell 680-E (N599BB), Titusville, FL, destroyed. Probable cause: THE PILOT'S DECISION TO CONTINUE THE FLIGHT WITH A KNOWN UNAIRWORTHY MECHANICAL CONDITION RESULTING IN A SUBSEQUENT LOSS OF ENGINE POWER AND FORCED LANDING.
- [NTSB ATL90LA052](https://openairdocs.org/ntsb/ATL90LA052), Jan 18, 1990: Aero Commander 680E (N612G), Knoxville, TN, substantial damage. Probable cause: THE PILOT'S EXCESSIVE AIRSPEED AND DELAY IN INITIATING A GO-AROUND DURING THE LANDING. FACTORS RELATED TO THE ACCIDENT WERE: THE WET RUNWAY CONDITION, THE PILOT'S FAILURE TO ATTAIN THE PROPER…
- [NTSB MIA85LA110](https://openairdocs.org/ntsb/MIA85LA110), Mar 1, 1985: Rockwell 680E (N709G), Key West, FL, destroyed, 2 fatal
- [NTSB ANC82FA007](https://openairdocs.org/ntsb/ANC82FA007), Nov 7, 1981: Aero Comdr 680E (N6272B), Savoonga, AK, destroyed, 1 fatal
- [NTSB NYC81FA087](https://openairdocs.org/ntsb/NYC81FA087), Sep 16, 1980: Aero Comdr 680E (N1520K), New Windsor, NY, destroyed, 2 fatal
- [NTSB LAX80DUM19](https://openairdocs.org/ntsb/LAX80DUM19), May 6, 1980: Aero Comdr 680 (N8445C), Carlsbad, CA, no damage
- [NTSB SEA79FA020](https://openairdocs.org/ntsb/SEA79FA020), Jan 20, 1979: Aero Comdr 680E (N6872S), Dendelton, OR, destroyed
- [NTSB FTW77FRG16](https://openairdocs.org/ntsb/FTW77FRG16), Dec 9, 1976: Aero Comdr 680E (N344V), Mineral, TX, destroyed
- [NTSB DEN76FQA34](https://openairdocs.org/ntsb/DEN76FQA34), Jan 30, 1976: Aero Comdr 680 (N777MZ), Ft.Sumner, NM, substantial damage
- [NTSB DEN76FQA20](https://openairdocs.org/ntsb/DEN76FQA20), Oct 8, 1975: Aero Comdr 680E (N8490C), Raton, NM, substantial damage
- [NTSB DEN75FTE18](https://openairdocs.org/ntsb/DEN75FTE18), Aug 7, 1974: Aero Comdr 680E (N6888S), Longmont, CO, substantial damage
- [NTSB MIA74AM046](https://openairdocs.org/ntsb/MIA74AM046), Nov 22, 1973: Aero Comdr 680-E (N277LP), Birmingham, AL, destroyed, 1 fatal
- [NTSB ANC73AA036](https://openairdocs.org/ntsb/ANC73AA036), Nov 22, 1972: Aero Comdr 680-E (N8441C), Missing Aircraft, destroyed, 2 fatal
- [NTSB MIA73AM044](https://openairdocs.org/ntsb/MIA73AM044), Oct 12, 1972: Aero Comdr 680-E (N4900), No.Atlantic Ocean (Atlantic Ocean), destroyed, 2 fatal
- [NTSB MIA71FLG34](https://openairdocs.org/ntsb/MIA71FLG34), Jun 25, 1971: Aero Comdr 680E (N8458C), Camden, SC, substantial damage
- [NTSB MIA70F0014](https://openairdocs.org/ntsb/MIA70F0014), Apr 11, 1969: Aero Comdr 680-E (N344V), Jacksonville, FL, substantial damage
- [NTSB ANC69A0031](https://openairdocs.org/ntsb/ANC69A0031), Nov 21, 1968: Aero Comdr 680-E (N3810C), Barrow, AK, destroyed, 7 fatal
- [NTSB MIA68A0090](https://openairdocs.org/ntsb/MIA68A0090), Apr 20, 1968: Aero Comdr 680 (N408EE), San Juan, PR, destroyed, 1 fatal
- [NTSB LAX68A0085](https://openairdocs.org/ntsb/LAX68A0085), Mar 7, 1968: Aero Comdr 680-E (N6243B), Lake Hughes, CA, substantial damage, 1 fatal
- [NTSB MIA68F0307](https://openairdocs.org/ntsb/MIA68F0307), Dec 12, 1967: Aero Comdr 680 (N8302), Decatur, AL, substantial damage
- [NTSB OAK67F0322](https://openairdocs.org/ntsb/OAK67F0322), May 21, 1967: Aero Comdr 680-E (N8439C), Sacramento, CA, substantial damage
- [NTSB DEN67A0065](https://openairdocs.org/ntsb/DEN67A0065), Apr 14, 1967: Aero Comdr 680E (N344V), Denver, CO, substantial damage
- [NTSB MKC67A0038](https://openairdocs.org/ntsb/MKC67A0038), Dec 9, 1966: Aero Comdr 680E (N8496C), Minneapolis, MN, destroyed, 1 fatal
- [NTSB FTW66F0632](https://openairdocs.org/ntsb/FTW66F0632), Apr 25, 1966: Aero Comdr 680-E (N69278), Little Rock, AR, substantial damage
- [NTSB NYC66F0410](https://openairdocs.org/ntsb/NYC66F0410), Dec 3, 1965: Aero Cmdr 680-E (N9375R), Philadelphia, PA, substantial damage
- [NTSB LAX66F0093](https://openairdocs.org/ntsb/LAX66F0093), Aug 2, 1965: Aero Cmdr 680E (N9363R), Reno, NV, substantial damage
- [NTSB NYC65F0191](https://openairdocs.org/ntsb/NYC65F0191), May 18, 1965: Aero Cmdr 680E (N262X), Warminster, PA, substantial damage
- [NTSB UNK65X0804](https://openairdocs.org/ntsb/UNK65X0804), Nov 23, 1964: Aero Cmdr 680 (N6872S), Portland, OR, substantial damage
- [NTSB UNK65X0257](https://openairdocs.org/ntsb/UNK65X0257), Oct 12, 1964: Aero Comm 680E (N6852S), Redding, CA, substantial damage

## FAA accident and incident reports (28)

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.

- [Accident 20150921015559A](https://openairdocs.org/incident/20150921015559A), Sep 21, 2015: Aero Commander 680-E (N222JS), Boise, ID, Destroyed. Aircraft stalled and crashed on approach to boi runway 28L seriously injuring pilot.
- [Accident 20131203025369A](https://openairdocs.org/incident/20131203025369A), Dec 3, 2013: Aero Commander 680-E (N71DF), Cresent City, FL, Destroyed. On December 3, 2013 at approximately 0937 an Aero Commander 680-E, N71DF [privacy data omitted] collided with several trees upon take off from jim finlay farm…
- [Accident 20080508833389A](https://openairdocs.org/incident/20080508833389A), May 8, 2008: Gulstm 680E (N39BA), Hope, AR, Substantial damage. (-23) On may 8,2008, at approximately 1030 CST, N39BA, a GA-680, lost power from the right engine during an approach to landing at Hope, Arkansas (M18). The…
- [Incident 20030809019749I](https://openairdocs.org/incident/20030809019749I), Aug 9, 2003: Gulstm 680E (N8489C), Oakland, CA. (-23) Hydraulic flex line burst on take off spraying hydraulic fluid on the engine causing smoke and hydraulic failure. Aircraft landed without incident,…
- [Incident 19990729018269I](https://openairdocs.org/incident/19990729018269I), Jul 29, 1999: Gulstm 680E (N8489C), Watsonville, CA, Minor damage. (-5)On July 27, 1999, time unknown Mr. Marl alan cribbs, a private pilot certificate # 571064144, with two passengers on board, operated VFR a Gulfstream…
- [Incident 19981030042729I](https://openairdocs.org/incident/19981030042729I), Oct 30, 1998: Gulstm 680E (N3820C), Erwinna, PA, Minor damage. (-5)The pilot had never been into van sant airport, a grass strip where the runway is marked on only one side. The pilot landed on the wrong side of the…
- [Accident 19960909026389A](https://openairdocs.org/incident/19960909026389A), Sep 9, 1996: Gulstm 680E (N262X), Lakeland, FL, Destroyed, 1 fatal. Lost left engine shortly after departing. Feathered same. Stalled circling to land. No anomalies found.
- [Accident 19900805030229A](https://openairdocs.org/incident/19900805030229A), Aug 5, 1990: Gulstm 680E (N599BB), Titusville, FL, Destroyed. Incorrectly leaned mixtures for rough engines. Runaway prop. Crash landed. Prop cable broke. Engine not airworthy.
- [Accident 19900118000729A](https://openairdocs.org/incident/19900118000729A), Jan 18, 1990: Gulstm 680E (N612G), Knoxville, TN, Substantial damage. Landed long and fast on wet runway,hydroplaned. Tried go around but over boosted engines. Ran off end. Cocaine noted
- [Accident 19850301044129A](https://openairdocs.org/incident/19850301044129A), Mar 1, 1985: Gulstm 680E (N709G), Key West, FL, Destroyed, 1 fatal. Ditched, coast guard standing by. Presumed fatal, wreckage not found. Fuel exhaustion at night. Actual dist 240.
- [Accident 19811107072679A](https://openairdocs.org/incident/19811107072679A), Nov 7, 1981: Rkwell 680E (N6272B), Savoonga, AK, Destroyed. Crash occurred during cargo flight in marginal weather conditions.
- [Incident 19810526040479I](https://openairdocs.org/incident/19810526040479I), May 26, 1981: Rkwell 680E (N1863W), Alief, TX. Lost power in right engine during takeoff; tried to return to airport but missed approach and landed in filed.
- [Accident 19800916042629A](https://openairdocs.org/incident/19800916042629A), Sep 16, 1980: Rkwell 680E (N1520K), New Windsor, NY, Destroyed, 1 fatal. Rough engine, loose cowling on takeoff. Feathered same, slowed below VMC. Lost control. Rich mixture fouled plugs.
- [Accident 19800506011649A](https://openairdocs.org/incident/19800506011649A), May 6, 1980: Gulstm 680E (N8445C), Carlsbad, CA. Parked with one engine running on terminal side. Passenger unable to find door. Walked into idling propeller.
- [Incident 19791217046569I](https://openairdocs.org/incident/19791217046569I), Dec 17, 1979: Rkwell 680E (N266X), North Canton, OH, Minor damage. Pilot landed gear up with left prop, HC83X202C1, feathered due to control problem. Pitch change parts failed.
- [Incident 19791020053209I](https://openairdocs.org/incident/19791020053209I), Oct 20, 1979: Rkwell 680E (N3807C), Fruita, CO, Minor damage. Pilot landed long on a short runway, unable to stop.
- [Incident 19790728012819I](https://openairdocs.org/incident/19790728012819I), Jul 28, 1979: Rkwell 680E (N6100L), Downey, ID, Minor damage. Aircraft ran off end of runway after brake failed.
- [Incident 19790305008799I](https://openairdocs.org/incident/19790305008799I), Mar 5, 1979: Rkwell 680E (N3447), Lewiston, ID. Engine lost power without warning, metal found in scavenger oil screen an problem with prop gear reduction area.
- [Accident 19790120001249A](https://openairdocs.org/incident/19790120001249A), Jan 20, 1979: Rkwell 680E (N6872S), Pendleton, OR, Destroyed. Aircraft struck ground 1 mile short of runway during IFR night approach. Freezing rain, low ceiling and visibility
- [Incident 19781018032839I](https://openairdocs.org/incident/19781018032839I), Oct 18, 1978: Rkwell 680E (N9368R), Pullman, WA, Minor damage. Connecting rod bolt failed. Flight attempted to return. Landed at airport en route due to altitude loss
- [Incident 19781002030899I](https://openairdocs.org/incident/19781002030899I), Oct 2, 1978: Rkwell 680 (N9368R), Spokane, WA. Left main retract cylinder broke, all hydraulic fluid lost. Landed safely. Pilot had no brakes.
- [Incident 19780429014589I](https://openairdocs.org/incident/19780429014589I), Apr 29, 1978: Rkwell 680 (N1006S), Philadelphia, PA, Minor damage. While taxiing on ramp left wing tip struck rudder of parked N4954F.
- [Incident 19780201005089I](https://openairdocs.org/incident/19780201005089I), Feb 1, 1978: Rkwell 680E (N3447), Mcminnville, OR. One engine quit, then the other. One restarted and safe landing made. Problem was carburetor icing.
- [Accident 19761209038049A](https://openairdocs.org/incident/19761209038049A), Dec 9, 1976: Rkwell 680E (N344V), Mineral, TX, Destroyed. Illegal drug transportation. Acft believed burned by plt. Injury index presumed.
- [Accident 19760130001699A](https://openairdocs.org/incident/19760130001699A), Jan 30, 1976: Rkwell 680E (N777MZ), Ft.Sumner, NM, Substantial damage. Gusting to 28K,blowing dust. Lnd on road.
- [Accident 19751008039119A](https://openairdocs.org/incident/19751008039119A), Oct 8, 1975: Rkwell 680E (N8490C), Raton, NM, Substantial damage. Nr 6 exhaust stack,r eng,came loose. Hit fence abt 300FT short of rwy. Plt said turb MDT to severe
- [Accident 19740807030119A](https://openairdocs.org/incident/19740807030119A), Aug 7, 1974: Rkwell 680E (N6888S), Longmont, CO, Substantial damage. Lt eng counterweight lobe aft of nr 3 con rod failed thru mounting bushing holes. Ret & lndd ok.
- [Accident 19731122041879A](https://openairdocs.org/incident/19731122041879A), Nov 22, 1973: Rkwell 680E (N277LP), Birmingham, AL, Destroyed. Observed nose high,slow flt condition. Acft last flown 9/8/73.

## Service difficulty reports (5)

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

- [SDR 2005FA0001202](https://openairdocs.org/sdr/2005FA0001202), Aug 17, 2005: STARTER. FAILED. ON START UP FOR SECOND FLIGHT OF THE DAY, AC STARTER WOULD NOT ENGAGE AND TURN ENGINE. SEVERAL ATTEMPS WERE MADE TO START THE ENGINE. STARTER WOULD TURN BUT WOU
- [SDR 2001FA0000140](https://openairdocs.org/sdr/2001FA0000140), Jul 12, 2001: SUMP. CORRODED. MAIN FUEL SUMP REMOVED FROM ACFT. TO FACILITATE MAIN TANK REMOVAL FROM ACFT. VISUAL INSPECTION OF INSIDE OF PART REVEALED CONSIDERABLE CORROSION ON BOTTOM INSID
- [SDR 98ZZZX4555](https://openairdocs.org/sdr/98ZZZX4555), Sep 18, 1998: BUNGEE. BENT. NIGHT CREW HEARD A METALLIC OIL CANNING SOUND IN THE DIRECTION OF AIRCRAFT. THEY INVESTIGATED AND COULD NOT FIND ANYTHING. UPON PULLING AIRPLANE OUT, THE NOSE G
- [SDR 96ZZZX5649](https://openairdocs.org/sdr/96ZZZX5649), Oct 24, 1996: CYLINDER. FAILED. INTERNAL FAILURE OF RT MLG ACTUATOR CAUSED TOTAL HYDRAULIC FLUID DEPLETION WITH SUBSEQUENT EMERGENCY EXTENSION OF LANDING GEAR WITHOUT INCIDENT. ACTUATOR WAS RE
- [SDR 96ZZZX5812](https://openairdocs.org/sdr/96ZZZX5812), Oct 17, 1996: ACTUATOR. FAILED. INTERNAL FAILURE OF RT MLG ACTUATOR CAUSED TOTAL HYDRAULIC FLUID DEPLETION WITH SUBSEQUENT EMERGENCY EXTENSION OF LANDING GEAR WITHOUT INCIDENT. ACTUATOR WAS RE

## STCs that may be installed (OpenAirDocs) (194, 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 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 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 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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists 680 Series
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): 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 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 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 SA1686WE](https://openairdocs.org/stc/SA1686WE): Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. FTG, Inc
- [STC SA1458GL](https://openairdocs.org/stc/SA1458GL): Installation of a Cleveland nose wheel. 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 SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". 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 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 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): 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 SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA09763DS](https://openairdocs.org/stc/SA09763DS): Installation of an S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation
- [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 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 SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): 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 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): 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 SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [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
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA1782WE](https://openairdocs.org/stc/SA1782WE): Installation of drooped ailerons, drooped wing leading edge, stall fence and rudder seal. Sierra Industries Ltd
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [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 SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): 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 SA1847WE](https://openairdocs.org/stc/SA1847WE): Installation of Brittain Up-Command Signal Adapter Kit. Brittain Industries, Inc
- [STC SA1177GL](https://openairdocs.org/stc/SA1177GL): Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 800 in accordance with Installation and Operating Instructions, Form EA 109K, dated April 23, 2001, or later FAA approved revisions. The Medical Oxygen System Kit P/N 807 is an FAA approved option. The Inverter/Pump Kit No. 812 may be installed in accordance with Inverter/Pump Installation Instructions, EA Form 170, dated June 9, 2001, or later FAA approved revisions. Paul/ Lanna Egan LLC

All 194: https://openairdocs.org/model/aero-commander-680-e/stcs.md

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