# N313QS: 2007 Cessna 680

- Status: Valid registration
- Airframe: [Cessna 680](https://openairdocs.org/model/cessna-680) (registry code 2076811, 9 seats)
- Engine: [Pratt & Whitney Canada PW306C](https://openairdocs.org/engine/pratt-whitney-canada-pw306c) (registry code 52169)
- Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (Textron Aviation Inc.), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 680-0140
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 16, 2007
- Certificate issued: July 24, 2020
- Expires: July 31, 2027
- Mode S code: A35365
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=313QS
- Page: https://openairdocs.org/aircraft/N313QS

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 11 in force

### Matched by airframe (Cessna 680)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [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 2018-07-13](https://openairdocs.org/ad/2018-07-13): Landing Gear · Textron 510, 680 and 680A. Effective May 15, 2018
- [AD 2017-06-13](https://openairdocs.org/ad/2017-06-13): Fuselage · Textron 680. Effective May 2, 2017
- [AD 2012-07-04](https://openairdocs.org/ad/2012-07-04): Electrical Power · Cessna 680. Effective May 15, 2012
- [AD 2007-26-16](https://openairdocs.org/ad/2007-26-16): Aft fairing wire bundle assembly · Cessna 680. Effective Jan 18, 2008
- [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 2005-08-03](https://openairdocs.org/ad/2005-08-03): Cockpit display units · Cessna 680. Effective Apr 29, 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 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [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

### Matched by engine (Pratt & Whitney Canada PW306C)

None in force.

## Information bulletins (advisory) (2 in force)

- [SAIB NM-10-45](https://openairdocs.org/saib/NM-10-45): Landing Gear: Nose/Tail Landing Gear Attach Section. Issued Aug 11, 2010
- [SAIB NM-10-12](https://openairdocs.org/saib/NM-10-12): Navigation: Flight Management System. Issued Jan 7, 2010

## NTSB investigations

None matched to N313QS.

## FAA accident and incident reports

None matched to N313QS.

## Reports on N313QS not matched to an aircraft (1)

They name N313QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19920904038439I](https://openairdocs.org/incident/19920904038439I), Sep 4, 1992: Cessna 650 (N313QS), Lincoln, NE. Hydraulic oil quantity dropped. Diverted to Lincoln. Found pinhole in spoiler. Holddown line caused by aileron cable

## Service difficulty reports (54, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR JGVR20260516201](https://openairdocs.org/sdr/JGVR20260516201), May 16, 2026: SKIN. CORRODED. BLENDED MULTIPLE AREAS OF CORROSION ON THE UPPER AND LOWER SKINS OF THE HORIZONTAL STABILIZER, NEAR LT AND RT TIP CAP, LH AND RH IB ELEVATOR HINGE, PERFORMED ND
- [SDR JGVR20260515204](https://openairdocs.org/sdr/JGVR20260515204), May 15, 2026: SKIN. CORRODED. MECHANICALLY REMOVED 1 AREA OF CORROSION ON THE UPPER AFT CORNER OF THE CUT OUT OF THE E-EXIT ON FUSELAGE SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITIO
- [SDR JGVR20260515203](https://openairdocs.org/sdr/JGVR20260515203), May 15, 2026: SPAR. CORRODED. MECHANICALLY REMOVED CORROSION LOCATED ON RH WING AFT SPAR, AFT FACE OF SPAR WEB BELOW SPOILER PANEL #9 AROUND PRESSURE AND RETURN HYDRAULIC LINE CARRY THROUGH 
- [SDR JGVR20260515202](https://openairdocs.org/sdr/JGVR20260515202), May 15, 2026: SPAR CAP. CORRODED. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED INSIDE LH HORIZONTAL STAB ELEVATOR COVE, LOWER SPAR CLIP BETWEEN INBOARD AND MIDDLE ELEVATOR HINGE ATTACHMENTS
- [SDR JGVR20260515001](https://openairdocs.org/sdr/JGVR20260515001), May 15, 2026: SKIN. CORRODED. MECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORT
- [SDR JGVR20260515201](https://openairdocs.org/sdr/JGVR20260515201), May 15, 2026: SKIN. CORRODED. MECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORT
- [SDR 2025FA0000779](https://openairdocs.org/sdr/2025FA0000779), Nov 21, 2025: WING ROOT. CORRODED. CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.
- [SDR 2025FA0000771](https://openairdocs.org/sdr/2025FA0000771), Nov 19, 2025: WING ROOT. CORRODED. CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.
- [SDR 2025FA0000740](https://openairdocs.org/sdr/2025FA0000740), Nov 4, 2025: SKIN. CORRODED. CORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCAT
- [SDR 2025FA0000739](https://openairdocs.org/sdr/2025FA0000739), Nov 4, 2025: SKIN. CORRODED. CORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCAT
- [SDR DXTA2025060603759](https://openairdocs.org/sdr/DXTA2025060603759), Jun 3, 2025: BATTERY PACK. INOPERATIVE. LIGHTS CONNECTED TO THEIR RESPECTIVE EMERGENCY LIGHTING BATTERY PACK FAILED TO OPERATE AFTER TWO 30 MINUTE CHARGING SESSIONS. THE TWO LOWER SIDES OF MAIN CABIN 
- [SDR 2024FA0000757](https://openairdocs.org/sdr/2024FA0000757), Oct 7, 2024: SKIN. CORRODED. REPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER SKINS LOCATED NEAR THE UPPER EDGE AND ONE NEAR THE FORWARD EDGE BY BLENDING, PERFORMING NDT, REPORTING FOR RE
- [SDR DXTA2024090300378](https://openairdocs.org/sdr/DXTA2024090300378), Aug 29, 2024: FUSE. DEFECTIVE. EMERG EXIT SIGN/LIGHT: THE AFT LAV EMERGENCY EXIT SIGN IS INOP. THE AFT DIVIDER OVERHEAD EMERGENCY EXIT SIGN IS INOP. CORRECTIVE ACTION: CHECKED THE EMERGENCY P
- [SDR DXTA2024062512164](https://openairdocs.org/sdr/DXTA2024062512164), Jun 25, 2024: FADEC. FAULTED. DURING DESCENT FROM FL350 WITH ANTI-ICE ON THE ENGINE CONTROL FAULT R AMBER CAS MESSAGE ILLUMINATED. FAULT MESSAGE WAS RESET AFTER PUSHING THE FADEC RESET. REMO
- [SDR DXTA2023082894000](https://openairdocs.org/sdr/DXTA2023082894000), Aug 27, 2023: FUSE. BLOWN. ON PREFLIGHT, ALL EMERGENCY LIGHTS INTERIOR AND EXTERIOR DO NOT ILLUMINATE WITH THE EMER LTS SELECTED ON. IN ARM, AFT EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. M
- [SDR JGVR20230720001](https://openairdocs.org/sdr/JGVR20230720001), Jul 20, 2023: UNKNOWN. UNKNOWN. REPAIRED CRACKED INBOARD END RIB OF THE RH HORIZONTAL STABILIZER, LOWER FLANGE AT RBL 8.8, PER REPAIR -2 OF TEXTRON REPAIR DEFINITION S-680-ATA55/08RD REVISION 
- [SDR DXTA2022112374570](https://openairdocs.org/sdr/DXTA2022112374570), Nov 22, 2022: COALESCER BAG. DIRTY. DEPARTED APF, APU OFF FOR TAKEOFF. LEVELED OFF AT 2000 FT PER CLEARANCE & NOTICED A HOT BURNING OIL ODOR, REDUCED POWER AT 2,000 FT TO KEEP A SLOW AIRSPEED, ODO
- [SDR DXTA2022062764570](https://openairdocs.org/sdr/DXTA2022062764570), Jun 24, 2022: ACM. DEFECTIVE. APU BLEED AIR: COULD NOT CONTROL CABIN TEMP BELOW 80 DEGREES. STARTED APU AND SELECTED BLEED AIR ON. ODOR OF BURNT OIL ENTERED CABIN AND THEN BLEED SELECTED OFF
- [SDR DXTA2022011755260](https://openairdocs.org/sdr/DXTA2022011755260), Jan 15, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTING: WHEN DOING THE EMERGENCY LIGHT CHECK, THE ONLY LIGHTS WORKING ARE THE EXIT LIGHT OVER THE MAIN CABIN DOOR, THE OVERHEAD LIGHT BETWEEN SEATS 
- [SDR DXTA2021123154490](https://openairdocs.org/sdr/DXTA2021123154490), Dec 30, 2021: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: RIGHT SIDE CABIN EMERGENCY LIGHTS INOP. LEFT SIDE OPERATES NORMALLY. // SIGNOFF// RAN APU FOR 1 HOUR TO CHARGE THE EMERGENCY BATTERIES. PREFO
- [SDR DXTA2021121553510](https://openairdocs.org/sdr/DXTA2021121553510), Dec 13, 2021: CONTROLLER. DEFECTIVE. ANTISKID FAIL AMBER CAS: ON CLIMB OUT WE HAD A FLICKERING AMBER ANTISKID FAIL CAS MESSAGE. THE CHECKLIST HAD US TURN IT OFF SINCE THE MESSAGE WOULD NOT CLEAR. W
- [SDR JGVR20210319003](https://openairdocs.org/sdr/JGVR20210319003), Mar 19, 2021: SKIN. CORRODED. BLENDED CORRODED AREAS OF THE LOWER SURFACE OF THE RH LOWER WING SKIN, BELOW THE AFT SPAR CAP NEAR THE MAIN LANDING GEAR WHEEL WELL AREA, PERFORMED NDT AND REPO
- [SDR DXTA022220213833](https://openairdocs.org/sdr/DXTA022220213833), Feb 18, 2021: WHEEL. ICED. RIGHT INBOARD MLG TIRE: BRAKE FROZEN. TIRE DAMAGED. WE FOUND THAT THERE WAS ICE BUILD-UP 0F THE RT INBOARD BRAKE. AFTER REMOVING THE ICE WE WERE ABLE TO TURN TH
- [SDR DXTA021920213833](https://openairdocs.org/sdr/DXTA021920213833), Feb 18, 2021: BRAKE. FROZEN. RIGHT INBOARD MLG TIRE: BRAKE FROZEN. TIRE DAMAGED.
- [SDR JGVR202002192001](https://openairdocs.org/sdr/JGVR202002192001), Feb 20, 2020: SPAR. CORRODED. VERTICAL STAB HAS 1 AREA OF VERIFIED CORROSION ON LH SPAR CLIP BELOW UPPER RUDDER HINGE. FOUND DURING 6 MONTH INSPECTION. REMOVED LEVEL 1 CORROSION FROM VERTICA
- [SDR DXTA2019111403074](https://openairdocs.org/sdr/DXTA2019111403074), Nov 13, 2019: STRUT. STUCK. ALL LANDING GEAR RETRACTION DID NOT RETRACT - WHEN NOSEWHEEL CAME OFF THE GROUND ON TAKEOFF, THE MASTER WARNING LIGHT ILLUMINATED. THE GEAR HANDLE WOULD NOT MOV
- [SDR DXTA2018030800694](https://openairdocs.org/sdr/DXTA2018030800694), Mar 8, 2018: COMPRESSOR. STALLED. DURING CLIMB OUT, AT APPROXIMATELY FL 350 IN MCT THRUST, THERE WERE SEVERAL ENGINE COMPRESSOR STALLS ON THE RT ENGINE. DURING THE STALLS THE ITT EXCEEDED 900. T
- [SDR DXTA2018010400434](https://openairdocs.org/sdr/DXTA2018010400434), Jan 2, 2018: UNKNOWN. SMOKE. SHORTLY AFTER STARTING THE APU AND SELECTING BLEED ON, A GRAYISH SMOKE COULD BE SMELLED AND SEEN THROUGHOUT THE CABIN AND COCKPIT. SMOKE DISSIPATED AFTER APU SH
- [SDR DXTAT2PL6D005MFJN](https://openairdocs.org/sdr/DXTAT2PL6D005MFJN), Dec 27, 2017: BLEED VALVE. DEFECTIVE. AT CRUISE FL340, THE AIRPLANE MADE A LOUD POP, THEN A BANG, FOLLOWED BY A VIBRATION , YAW, AND ITT OVERTEMP/ N1 OVERSPEED ON THE RIGHT ENGINE. BOTH POWER LEVERS
- [SDR JGVR20170823001](https://openairdocs.org/sdr/JGVR20170823001), Aug 23, 2017: DOOR. CORRODED. EMERGENCY EXIT DOOR SKIN HAS SEVERAL AREAS OF CORROSION AROUND PERIPHERY NEAR COMPOSITE RING. FOUND DURING PAINT PROCESS. REMOVED SEAL AND COMPOSITE RINGS AND B
- [SDR 2017F00165](https://openairdocs.org/sdr/2017F00165), Jul 13, 2017: FAIRING. DAMAGED. FAIRING DAMAGE.
- [SDR 2017F00156](https://openairdocs.org/sdr/2017F00156), Jul 12, 2017: SKIN. CORRODED. VERTICAL STABILIZER LEFT AND RIGHT SKIN DAMAGE.
- [SDR 2017F00151](https://openairdocs.org/sdr/2017F00151), Jul 7, 2017: SKIN. CORRODED. HORIZONTAL STABILIZER LEFT AND RIGHT UPPER AND LOWER SKIN DAMAGE.
- [SDR 2017F00149](https://openairdocs.org/sdr/2017F00149), Jul 6, 2017: SPAR. DAMAGED. VERTICAL FIN REAR SPAR DAMAGED.
- [SDR 2017F00147](https://openairdocs.org/sdr/2017F00147), Jul 6, 2017: BULKHEAD. DAMAGED. BULKHEAD BOND ASSY. DAMAGED, DOUBLER CRACKED, NICKED AND DEBONDED.
- [SDR 2017F00146](https://openairdocs.org/sdr/2017F00146), Jul 6, 2017: HINGE BRACKET. CORRODED. RUDDER HINGE BRACKET CORRODED.
- [SDR 2017F00145](https://openairdocs.org/sdr/2017F00145), Jul 6, 2017: ACCESS PANEL. DELAMINATED. VERTICAL STAB LEADING EDGE UPPER LEFT EDGE DELAMINATED.
- [SDR 2017F00144](https://openairdocs.org/sdr/2017F00144), Jul 6, 2017: SKIN. CORRODED. LEFT ELEVATOR SKIN CORRODED.
- [SDR DXTR2016031003](https://openairdocs.org/sdr/DXTR2016031003), Mar 4, 2016: SKIN. CORRODED. CORROSION FOUND AT DISCRETE LOCATIONS ON THE STR AND TAILCONE SKINS. REPAIRED IAW STRUCTURES REPORT S-680-0140/04RD.
- [SDR DXTR2016031002](https://openairdocs.org/sdr/DXTR2016031002), Mar 4, 2016: SKIN. CORRODED. CORROSION FOUND AT MULTIPLE SITES ON THE LT & RT VERTICAL STABILIZER SKINS. REPAIRED IAW STRUCTURES REPORT NR: S-680-014/05RD.
- [SDR DXTR2016031001](https://openairdocs.org/sdr/DXTR2016031001), Mar 4, 2016: SKIN. CORRODED. CORROSION DAMAGE FOUND ON LT UPPER WING SKIN. REPAIRED IAW STRUCTURES REPORT NR: S-680-0140/06RD.
- [SDR DXTA2014080605845](https://openairdocs.org/sdr/DXTA2014080605845), Jul 4, 2014: CONTROL HANDLE. FAULTY. GEAR WOULD NOT RETRACT, GEAR HANDLE COULD NOT BE MOVED. AFTER ACFT WAS JACKED BROUGHT UP CDMS TO LANDING GEAR PAGE. WITH NO HYD TRIED TO PULL GEAR HANDLE BUT HA
- [SDR DXTA2014080605844](https://openairdocs.org/sdr/DXTA2014080605844), Jul 2, 2014: CONTROL HANDLE. FAULTY. GEAR WOULD NOT RETRACT, GEAR HANDLE COULD NOT BE MOVED. REMOVED GEAR HANDLE & BENCH CHECKED SOLENOID OPERATION. APPLIED POWER & GND, HANDLE REMAINS LOCKED DOWN.
- [SDR CWQR20131203049](https://openairdocs.org/sdr/CWQR20131203049), Dec 3, 2013: FILTER ELEMENT. MISMANUFACTURED. DURING A SCHEDULED INSPECTION WE TRIED TO INSTALL A NEW FILTER ELEMENT. THE ELEMENT WOULD NOT SIT INTO THE BOTTOM OF THE FILTER HOUSING BOWL. THE FILTER WAS REJ
- [SDR DXTA2013111205562](https://openairdocs.org/sdr/DXTA2013111205562), Nov 11, 2013: ENGINE. MALFUNCTIONED. APPROXIMATELY 20 MIN INTO FLIGHT AT FL430, CREW NOTICED A HOT SMELL. 5 MINUTES LATER A WHITE GRAY SMOKE ENTERED THE COCKPIT & CABIN. THE PRESS SOURCE SELECT KNO
- [SDR DXTA2013100705531](https://openairdocs.org/sdr/DXTA2013100705531), Oct 7, 2013: ENGINE. ODOR. SMOKE IN CABIN AT FL 430. DURING CLIMBOUT ABOUT 14,000 APU SYS FAIL ANNUNCIATOR CAME ON AND APU SHUTDOWN. APU GEN HAD BEEN OFF, BUT BLEED AIR ON. APPROX 30 MINU
- [SDR DXTA2013053105404](https://openairdocs.org/sdr/DXTA2013053105404), May 30, 2013: BEARING. DIRTY. NOSE GEAR MADE LOUD BANGING NOISE UPON GEAR RETRACTION, SHOOK GLARE SHIELD. NOSE STRUT WITHIN LIMITS RETRACTION GUIDES SEEM TO ALIGNED CORRECTLY. CYCLED GEAR, U
- [SDR DXTA2013051305392](https://openairdocs.org/sdr/DXTA2013051305392), May 12, 2013: COALESCER BAG. DIRTY. GETTING AN INTERMITTENT ACRID "DIRTY SOCK" ODOR IN CABIN DURING FLIGHT WITH APU OFF. R & R THE WATER SEPARATOR COALESCER IAW MM 21-21-03, 21-50-00. THE OPS AND 
- [SDR DXTA2011092304734](https://openairdocs.org/sdr/DXTA2011092304734), Sep 22, 2011: ECU. FAILED. UPON CLIMBING TO CRUISE ALTITUDE, BRIEF ODOR OF "HEAT" WAS NOTED IN THE COCKPIT. FOLLOWED LATER BY THE PASSENGERS WHO ALERTED THE CREW TO WHITE SMOKE COMING FRO
- [SDR 2011FA0000090](https://openairdocs.org/sdr/2011FA0000090), Jan 11, 2011: CONNECTOR. DAMAGED. WHILE PERFORMING THE 2B INTERNAL WING INSP, FOUND THAT THE LT AND RT ELECTRICAL CONNECTOR BLANKING PINS WERE FALLING OUT BECOMING FOD IN THE CTR FUEL TANK. CONN

All 54: https://openairdocs.org/aircraft/N313QS/reports.md

## Service difficulty reports on N313QS not matched to an aircraft (6)

They name N313QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200500803](https://openairdocs.org/sdr/DXTA200500803), Jun 24, 2005: WARNING LIGHT. FALSE ACTIVATION. AFTER TAKEOFF WHEN GEAR WAS RETRACTED RIGHT MAIN LIGHT AND RED GEAR UNSAFE REMAINED ILLUMINATED. RECYCLED GEAR DOWN NORMAL INDICATION AND LANDED A/C. ITEM IS UN
- [SDR DXTA200500789](https://openairdocs.org/sdr/DXTA200500789), Jun 19, 2005: PCB. INOPERATIVE. AFTER TAKEOFF WHEN GEAR WAS RETRACTED, ALL 3 GREEN LIGHTS EXTINGUISHED THE RED GEAR UNSAFE STAYED ILLUMINATED THEN THE RIGHT MAIN LIGHT REAPPEARED. RECYCLED GEA
- [SDR DXTA200500550](https://openairdocs.org/sdr/DXTA200500550), Jan 22, 2005: ENGINE. STOPPED. ON COMPLETION OF THE SPOILER TEST THE LT ENGINE QUITS. OPERATED SPEED BRAKES THRU SEVERAL CYCLES, VERIFIED 85 PERCENT SWITCHES RETRACT THE SPEED BRAKES, PERFORM
- [SDR DXTA200300166](https://openairdocs.org/sdr/DXTA200300166), Nov 19, 2003: BRAKE. MALFUNCTIONED. POWER BRAKE LOW PRESS AND ANTI-SKID INOP LIGHT REMAINED ILLUMINATED ON MASTER CAUTION PANEL AFTER GEAR WAS LOWERED; BRAKES FELT SOFT, HAD TO USE EMERGENCY BRAKE
- [SDR DXTA200300012](https://openairdocs.org/sdr/DXTA200300012), Apr 20, 2003: BRAKE. MALFUNCTIONED. DURING TAXI OUT FOR DEPARTURE CO-PILOT FELT THE BRAKES MOMENTARILY DISENGAGED. PILOT TOOK CONTROL AND HAD SAME EXPERIENCE. AIRCRAFT RETURNED TO BLOCK. PERFORMED
- [SDR 98ZZZX1869](https://openairdocs.org/sdr/98ZZZX1869), Apr 23, 1998: CONNECTION. LOOSE. PILOT REPORTED AFT J-BOX CB ANNUNCIATOR ILLUMINATED IN-FLIGHT. FOUND BAGGAGE HEAT AND APU AUX HYD PUMP CONTROL CB'S LOCATED IN AUX DC J-BOX TRIPPED. USED AN INS

## STCs that may be installed (OpenAirDocs) (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 680)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12082WI](https://openairdocs.org/stc/ST12082WI): Upgrade of AirCell High Speed Internet System to Gogo Business Aviation C1 System. Duncan Aviation Inc
- [STC ST11984SE](https://openairdocs.org/stc/ST11984SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST01141DE](https://openairdocs.org/stc/ST01141DE): Installation of the LifePort Medical Interior. LifePort LLC
- [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST04477CH](https://openairdocs.org/stc/ST04477CH): Installation of a Honeywell RDR-7000 Weather Radar System in accordance with AeroTec STC Master Data List, Doc. # ATEC-077-241-1200, Revision F, dated June 4. 2021, or later FAA-approved revisions. AeroTEC Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04573NY](https://openairdocs.org/stc/ST04573NY): AVIATOR 300 Installation. Amtech Aeronautical Limited
- [STC ST01941WI](https://openairdocs.org/stc/ST01941WI): Installation of Gogo Business Aviation AVANCE L5 Broadband System. Duncan Aviation Inc
- [STC ST01403WI-D](https://openairdocs.org/stc/ST01403WI-D): Installation of alternate part number DU-1080 Display Unit. Honeywell International Inc
- [STC ST01410WI-D](https://openairdocs.org/stc/ST01410WI-D): Installation of alternate part number NI-900 Network Interface Module. Honeywell International Inc
- [STC ST01440WI-D](https://openairdocs.org/stc/ST01440WI-D): Installation of alternate part number EPIC MC-850-2 Multi-Function Control Display Unit. Honeywell International Inc
- [STC ST01448WI-D](https://openairdocs.org/stc/ST01448WI-D): Installation of EPIC Phase 4.1 Software. Honeywell International Inc
- [STC ST01482WI-D](https://openairdocs.org/stc/ST01482WI-D): Installation of EPIC Phase 4.2 Software, alternate part number AGM-200 AFGS and alternate part number TR-865B CMF VDR. Honeywell International Inc
- [STC ST01530WI-D](https://openairdocs.org/stc/ST01530WI-D): Installation of EPIC NIC/PROC, AIOP, AND CMC modules and Pentium M software. Honeywell International Inc
- [STC ST01027DE](https://openairdocs.org/stc/ST01027DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries. MarathonNorco Aerospace Inc
- [STC ST01859WI](https://openairdocs.org/stc/ST01859WI): Installation of Gogo Business Aviation's Gogo Biz 4G Air-to-Ground System. Textron Aviation Inc Wichita Citation Service Center
- [STC ST01840WI](https://openairdocs.org/stc/ST01840WI): Installation of winglets, wing structural reinforcement, and related system changes. Winglet Technology LLC
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST02240LA-D](https://openairdocs.org/stc/ST02240LA-D): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC
- [STC ST02286LA](https://openairdocs.org/stc/ST02286LA): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST04366AT](https://openairdocs.org/stc/ST04366AT): This STC is a replacement of the original equipment nickel cadmium main batteries manufactured by Saft or Marathon with Concorde valve regulated lead acid main batteries. Concorde Battery Corporation
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01399WI](https://openairdocs.org/stc/ST01399WI): Installation of Honeywell DL-950 Data Loader. Textron Aviation Inc
- [STC ST02127LA](https://openairdocs.org/stc/ST02127LA): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Corporation
- [STC ST00717DE](https://openairdocs.org/stc/ST00717DE): Installation of a camera portal as a provision to accommodate a future camera. Sierra Nevada Corporation
- [STC ST01655WI-D](https://openairdocs.org/stc/ST01655WI-D): Installation of a Tenfine Chinese Flight Inspection System. Duncan Aviation Inc
- [STC ST00715DE-D](https://openairdocs.org/stc/ST00715DE-D): Installation of Nose Boom Provisions, Pylons and Antennas. Sierra Nevada Corporation
- [STC ST00718DE](https://openairdocs.org/stc/ST00718DE): Interior installation of, operator seats, equipment racks, power distribution panel, signal junction boxes, inoperative cockpit video display, cabin Inter-Communication System (ICS), ballast boxes and provisions to mount antennas, and baggage compartment installation of, power inverters, alternating current/direct current junction boxes, and a lead-acid mission battery in accordance with Sierra Nevada Corporation Drawing List, Report No. MDL- 0142-25-9309 Revision A, dated June 15, 2011, FAA approved July 25, 2011, or later FAA approved revision. Sierra Nevada Corporation
- [STC ST00720DE](https://openairdocs.org/stc/ST00720DE): Installation of sensors and provisions for future capability to monitor aircraft control surface deflections, existing pilot control input signals, and other aircraft systems in accordance with Sierra Nevada Corporation Drawing List, Report Number MDL-0142-25-9315, Revision B, dated February 24, 2011, FAA approved July 25, 2011, or later FAA approved revision. Sierra Nevada Corporation
- [STC ST00719DE](https://openairdocs.org/stc/ST00719DE): Installation of structural fittings in the wing as provisions to accommodate future external stores in accordance with Sierra Nevada Corporation Drawing List, Report No MDL-0142-25-9316, Revision A, dated February 15, 2011, FAA approved March 29, 2011, or later FAA approved revision. Sierra Nevada Corporation
- [STC ST01608WI-D](https://openairdocs.org/stc/ST01608WI-D): Installation of Aircell High Speed Internet System with Wireless LAN System. Duncan Aviation Inc
- [STC ST02240LA](https://openairdocs.org/stc/ST02240LA): Installation of a Patient Loading and Utility System (PLUS). Lifeport, Inc
- [STC ST02146NY](https://openairdocs.org/stc/ST02146NY): Installation of EMS Technologies Ltd. Cabin Network Xcelerator (CNX). EMS Technologies Canada Ltd
- [STC ST02248NY](https://openairdocs.org/stc/ST02248NY): Installation of EMS HSD-64, HSD-128, HSD-HCM, and HSD-X. EMS Technologies Canada Ltd
- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc
- [STC ST00263BO](https://openairdocs.org/stc/ST00263BO): Installation of Pratt & Whitney Engine Services, Inc. Data Transmission Unit (DTU). Pratt & Whitney Engine Services Inc
- [STC ST02893AT](https://openairdocs.org/stc/ST02893AT): Installation of a Boom Beam Taxi/Landing Light System. Whelen Aerospace Technologies

## Related

- Other Cessna 680 aircraft: https://openairdocs.org/model/cessna-680/aircraft.md
- The Pratt & Whitney Canada PW306C engine: https://openairdocs.org/engine/pratt-whitney-canada-pw306c.md

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