# N359QS: 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: 680-0126
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 22, 2007
- Certificate issued: August 13, 2026
- Expires: August 31, 2033
- Mode S code: A407AB
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=359QS
- Page: https://openairdocs.org/aircraft/N359QS

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 N359QS.

## FAA accident and incident reports

None matched to N359QS.

## Service difficulty reports (42)

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 DXTA2026061808489](https://openairdocs.org/sdr/DXTA2026061808489), Jun 17, 2026: G SWITCH. TRIPPED. ON POST FLIGHT DISCOVERED THE AFT OVER WING EMERGENCY LIGHT, THE BULK HEAD EXIT SIGN, EXIT SIGN, AND LIGHT OVER LAV REMAIN ON WITH THE EMER SWITCH OFF. RESET EM
- [SDR DXTA2026042707766](https://openairdocs.org/sdr/DXTA2026042707766), Apr 24, 2026: BATTERY PACK. DEFECTIVE. WHILE TESTING THE EMERGENCY LIGHTS DURING PRE-FLIGHT, SEVERAL INTERIOR OVERHEAD LIGHTS AND 3 EXTERIOR LIGHTS FAILED TO ILLUMINATE WITH THE EMERGENCY SWITCH IN A
- [SDR DXTA2026042407749](https://openairdocs.org/sdr/DXTA2026042407749), Apr 23, 2026: BATTERY PACK. NO TEST. DURING THE EMERGENCY LIGHT PRE-FLIGHT, SEVERAL INTERIOR OVERHEAD LIGHTS AND EXTERIOR LIGHTS FAILED TO ILLUMINATE. PERFORMED EMERGENCY LIGHTING POWER SUPPLY BATT
- [SDR DXTA2025111005606](https://openairdocs.org/sdr/DXTA2025111005606), Nov 6, 2025: DOOR SEAL. WORN. DOOR SEAL HAS AN AUDIBLE FREQUENCY THAT PRESENTS ON CLIMB STARTING AT FL200 THROUGH FL320 WITH PRESSURE DIFFERENTIALS OF 7.5-9.2 RESPECTIVELY. AIRSPEED IN CLIMB
- [SDR JGVR20251024001](https://openairdocs.org/sdr/JGVR20251024001), Oct 24, 2025: HINGE. CORRODED. FOUND UPPER HINGE UPPER HALF AND CENTER HINGE LOWER HALF ON THE RUDDER CORRODED BEYOND REPAIR. REPLACED PARTS WITH NEW TEXTRON P/N 6931050-46 AND 6931050-52.
- [SDR JGVR20251022002](https://openairdocs.org/sdr/JGVR20251022002), Oct 22, 2025: HINGE BRACKET. CORRODED. REMOVED CORRODE AREAS ON THE LOWER RUDDER HINGE BRACKET AND RUDDER TRIM BRACKET, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED
- [SDR JGVR20251022001](https://openairdocs.org/sdr/JGVR20251022001), Oct 22, 2025: SKIN. CORRODED. REMOVED 10 AREAS OF CORROSION LOCATED ON EMERGENCY EXIT DOOR AROUND CONTOUR RINGS ON OUTER E-EXIT SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEAN
- [SDR DXTA2025012702087](https://openairdocs.org/sdr/DXTA2025012702087), Jan 23, 2025: FUSE. INOPERATIVE. EMERGENCY LIGHTS DO NOT WORK IN THE ARM POSITION WITH ALL POWER SHUT DOWN. ALSO, EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR AND EMERGENCY LIGHT OVER SEAT FOUR DO
- [SDR DXTA2024122401671](https://openairdocs.org/sdr/DXTA2024122401671), Dec 22, 2024: FUSE. BLOWN. POST-FLIGHT - DURING AN EXTERIOR LIGHT INSPECTION (APU ON, EMER LTS-ARM, PAX SAFETY-ON) AFTER FLYING FOR 7 HOURS, NONE OF THE THREE OVER/FRONT WING LIGHTS ILLUM
- [SDR 2024F00255](https://openairdocs.org/sdr/2024F00255), Oct 18, 2024: SPAR SPLICE. CRACKED. CRACK INDICATIONS, CENTER WING, CENTER SPAR SPLICE W.S 37 REF FIELD REPAIR FR680-0126-13812 REV-
- [SDR DXTA2024010810540](https://openairdocs.org/sdr/DXTA2024010810540), Jan 6, 2024: BATTERY. FAULTED. SUSPECT BATTERY PACK 4 FOR CABIN AND OVERWING PAX EMERGENCY LIGHTING CONTROLLING MECH DOES NOT ILLUMINATE LIGHTS OVER SEAT 8 & FWD OVERWING EGRESS LIGHT WITH ON
- [SDR DXTA2023122610435](https://openairdocs.org/sdr/DXTA2023122610435), Dec 25, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS FAILED PREFLIGHT INSPECTION TEST. DURING TEST WE ONLY GOT THREE LIGHTS TOTAL THAT CAME ON, THE EXIT LIGHT ABOVE THE MAIN ENTRY DOOR, THE READIN
- [SDR 2023F00318](https://openairdocs.org/sdr/2023F00318), Oct 29, 2023: SPAR CAP. CORRODED. CORROSION FOUND ON AFT RH OUTBOARD VERTICAL SPAR CAP VFS 168.94. ACCOMPLISHED FIELD REPAIR-CORROSION, VERTICAL STABILIZER, RH VERTICAL SPAR CAP IAW TEXTRON AVIA
- [SDR 2023FA0000675](https://openairdocs.org/sdr/2023FA0000675), Oct 24, 2023: SPAR CAP. CORRODED. CORROSION, VERTICAL STABILIZER, RH VERTICAL SPAR CAP, VFS 168.94: REMOVED CORROSION AND ACCOMPLISHED ULTRASONIC THICKNESS CHECK. VERIFIED NO CRACK INDICATIONS. 
- [SDR DXTA2023092196050](https://openairdocs.org/sdr/DXTA2023092196050), Sep 20, 2023: UNKNOWN. UNKNOWN. UPON CHECKING AIRCRAFT LIGHTS ON POST FLIGHT INSPECTION, WE FOUND THE AFT CABIN EXIT SIGN LIGHT BURNT OUT. REPAIRED BROKEN WIRE FOR AFT LEFT EXIT SIGN ON LAV BU
- [SDR DXTA2023092196070](https://openairdocs.org/sdr/DXTA2023092196070), Sep 20, 2023: UNKNOWN. UNKNOWN. UPON CHECKING AIRCRAFT LIGHTS ON POST FLIGHT INSPECTION, WE FOUND THE AFT CABIN EXIT SIGN LIGHT BURNT OUT. PAIRED BROKEN WIRE FOR AFT LEFT EXIT SIGN ON LAV BULK
- [SDR DXTA2023062689570](https://openairdocs.org/sdr/DXTA2023062689570), Jun 26, 2023: UNKNOWN. UNKNOWN. ON CLIMB OUT THE RT ENG WAS ABOUT 50 DEG HOTTER THAN LT. PASSING FL 380 ENG TEMP SPIKED UP THROUGH AMBER RANGE & TO RED AT 928 DEGREES. PULLED THROTTLE BACK & E
- [SDR JGVR20230531004](https://openairdocs.org/sdr/JGVR20230531004), May 31, 2023: UNKNOWN. UNKNOWN. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON VERTICAL STAB AFT SPAR RUDDER COVE LOCATED JUST ABOVE RUDDER FAIRING PANEL LH SIDE ON SPAR CLIP, PERFORMED 
- [SDR JGVR20230531003](https://openairdocs.org/sdr/JGVR20230531003), May 31, 2023: UNKNOWN. UNKNOWN. MECHANICALLY BLENDED 1 AREA OF CORROSION IN LH GEAR WELL, AFT LOWER SPAR WS 21 TO 23 AND MECHANICALLY BLENDED 1 AREA OF CORROSION IN RH GEAR WELL, AFT LOWER SPA
- [SDR JGVR20230531002](https://openairdocs.org/sdr/JGVR20230531002), May 31, 2023: UNKNOWN. UNKNOWN. MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION APX 3 INCHES IN LENGTH LOCATED ON LH HORIZONTAL STAB, AFT SPAR ELEVATOR COVE, APX 12 INCHES INBD OF STAB TIP UP
- [SDR JGVR20230531001](https://openairdocs.org/sdr/JGVR20230531001), May 31, 2023: UNKNOWN. UNKNOWN. REPLACED THE CORRODED RUDDER TORQUE TUBE WITH NEW TEXTRON P/N 6933025-55 ON RUDDER ASSEMBLY P/N 6933000-20 S/N CE0187 PER CESSNA 680 SRM 55-40-09.
- [SDR DXTA2022101071840](https://openairdocs.org/sdr/DXTA2022101071840), Oct 9, 2022: SWITCH. TRIPPED. EMERGENCY LIGHTS BATTERY: 5G SWITCH TRIPPED ON ONE OF THE EMERGENCY LIGHT BATTERIES. LIGHT OVER SEAT 8 AS WELL AS THE FORWARD OVER-WING LIGHT AND SHARK LIGHT RE
- [SDR DXTA2022081567970](https://openairdocs.org/sdr/DXTA2022081567970), Aug 15, 2022: WATER SEPARATOR. ODOR. APU BLEED AIR: UPON STARTING THE APU AND THE BLEEDS THERE WAS A SMELL OF OIL IN THE AIR//CORRECTIVE ACTION// COMPLETED BORESCOPE INSP OF APU IAW TC-C68-49-1001 
- [SDR DXTA2021112952660](https://openairdocs.org/sdr/DXTA2021112952660), Nov 28, 2021: NONE. NONE. MAIN DOOR HANDLE: THE MAIN DOOR HANDLE IS VERY STIFF AND HARD TO ACTUATE AT THE VERY END OF CLOSING AS WELL AS THE START OF OPENING THE DOOR. // SIGN OFF // REM
- [SDR 2020F00472](https://openairdocs.org/sdr/2020F00472), Nov 24, 2020: SKIN. CORRODED. CORROSION ON WING SKIN. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ11111 DATED NOV 2020.
- [SDR 2020F00455](https://openairdocs.org/sdr/2020F00455), Nov 23, 2020: SKIN. OUT OF ALIGNMENT. MISALIGNED HOLES COMMON TO THE HEATED LEADING EDGE SKIN AND THE REPLACEMENT DIFFUSERS. ACCOMPLISHED TEXTRON AVIATION LETTER DQ27749 DATED NOV 8, 2020; 680-0126,
- [SDR 2020F00454](https://openairdocs.org/sdr/2020F00454), Nov 23, 2020: SPAR CAP. DAMAGED. VERTICAL FIN AFT SPAR CAP (LEFT SIDE) DAMAGE. ACCOMPLISHED TEXTRON AVIATION LETTER DQ27908M1 DATED NOV 19, 2020; 680-0126 (N359QS) VERTICAL FIN AFT SPAR CAP (LE
- [SDR 2020F00453](https://openairdocs.org/sdr/2020F00453), Nov 23, 2020: DOOR. CORRODED. CORROSION ON THE RT LOWER THRUST REVERSER LOWER DOOR ASSEMBLY, PART NUMBER 07ND78004-5. ACCOMPLISHED NORDAM FIELD ENGINEERING DISPOSITION DATED 6 NOV 2020 NTRSD
- [SDR 2020F00447](https://openairdocs.org/sdr/2020F00447), Nov 16, 2020: DOOR. DELAMINATED. REPAIR OF RIGHT ENGINE UPPER COWL DOOR DAMAGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ27776M1 DATED NOV 10, 2020.
- [SDR 2020FA0000495](https://openairdocs.org/sdr/2020FA0000495), Nov 11, 2020: DIFFUSER. ELONGATED. REPAIR TO LEADING EDGE DIFFUSER. TEXTRON AVIATION REPAIR LETTER DQ27749 DATED NOV 8, 2020. 680-0126 N359QS REPAIR RECOMMENDATION.
- [SDR JGVR20190523001](https://openairdocs.org/sdr/JGVR20190523001), May 23, 2019: DOUBLER. DAMAGED. REPAIRED SIX AREAS OF CHAFES /GOUGES IN THE DOUBLER BOND ASSEMBLY OF THE EMERGENCY EXIT OPENING SURROUND P/N 6911166-2 AND FRAME SEGMENT 6911122-3 BETWEEN FS 40
- [SDR DXTA2019031102152](https://openairdocs.org/sdr/DXTA2019031102152), Mar 11, 2019: CONTROLLER. DEFECTIVE. CABIN ALTITUDE AMBER CAS ILLUMINATED - CLIMBING THROUGH FL 180 AMBER CAS CABIN ALTITUDE ILLUMINATED AND CABIN SHOWED 9000 FEET. CABIN ALTITUDE CHECKLIST WAS COM
- [SDR JGVR20171221001](https://openairdocs.org/sdr/JGVR20171221001), Dec 21, 2017: SKIN. CORRODED. REMOVED FIRST LOCK FASTENER COLLAR, JUST ABOVE APU STINGER, ON LT SIDE OF VERTICAL STAB AFT SPAR FACE. MECHANICALLY BLENDED CORROSION APX 3 INCHES ABOVE APU STI
- [SDR DXTA2013061005414](https://openairdocs.org/sdr/DXTA2013061005414), Jun 8, 2013: WARNING LIGHT. FALSE ACTIVATION. IN CRUISE AT FL 410, OBSERVED AN FMS MESSAGE OF "GEAR SPEED LIM 210". OBSERVED RT MAIN GEAR LIGHT ON. GEAR HAD BEEN VERIFIED UP AFTER TAKE OFF. RIGHT GEAR DOWN 
- [SDR CWQR20130321026](https://openairdocs.org/sdr/CWQR20130321026), Mar 21, 2013: RIB. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE RT STABILIZER RIB CLOSE-OUT PANEL CRACKED ON THE UPPER ATTACH FLANGE TO SKIN ATTACH AREA, 4.5" LONG.
- [SDR CWQR20130321025](https://openairdocs.org/sdr/CWQR20130321025), Mar 21, 2013: RIB. CRACKED. DURING A SCHEDULED INSPECTION, WE FOUND THE RT INBD STABALIZER RIB CRACKED ON THE INBD LOWER FLANGE TO SKIN ATTACH AREA IN A ZIZAG PATTERN AND 2.2 INCHES LONG.
- [SDR CWQR20120318022](https://openairdocs.org/sdr/CWQR20120318022), Mar 18, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION, PERFORMED A PRODUCT IMPROVEMENT. REPLACEMENT OF DUCT ASSY 6914070-67. NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD TWO CRACKS A
- [SDR CWQR20120318021](https://openairdocs.org/sdr/CWQR20120318021), Mar 18, 2013: HEAT EXCHANGER. CRACKED. DURING A SCHEDULED INSPECTION, PERFORMED A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD THREE CRACKS
- [SDR DXTA2012021004869](https://openairdocs.org/sdr/DXTA2012021004869), Feb 9, 2012: OIL SYSTEM. OVERSERVICED. WITH APU ON, NON-ELECTRICAL SMOKE STARTED TO FILL CABIN. WITH BLEED AIR TURNED ON, SMOKE INCREASED RAPIDLY. OIL FOUND LEAKING FROM APU COMPARTMENT. FOUND DEICE 
- [SDR DXTA2010102804279](https://openairdocs.org/sdr/DXTA2010102804279), Oct 27, 2010: STRUT. DISCHARGED. ON TAKEOFF, UNABLE TO RAISE GEAR. TAKE OFF + 20 SEC, WOW MISCOMPARE MESSAGE ILLUMINATED. THRUST REVERSERS & NOSEWHEEL STEERING WERE AVAILABLE ON LANDING. TROUBL
- [SDR CWQR.2010.02](https://openairdocs.org/sdr/CWQR.2010.02), Jun 15, 2010: BRACKET. MISINSTALLED. DURING MX THE TECH OPENED THE PILOT'S SIDE WINDOW, AFTER UN-LATCHING THE WINDOW IT SWUNG IN AND FELL OFF IT'S HINGE POINTS. UPON FURTHER INVESTIGATION, FOUND TH
- [SDR DXTA200809123274](https://openairdocs.org/sdr/DXTA200809123274), Sep 12, 2008: CABLE. LOOSE. ACFT HAS AN AIRFRAME FLUTTER- INCREASE W/SPEED ABOVE 250KTS. SOME INDICATIONS W/ AP AND YD ON OR OFF, NOT NOTICED IN RUDDER OR AILERON FLUTTER APPEARS TO BE IN 

## 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

## Earlier aircraft with N359QS

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N359QS before.

- [Cancelled 2003-01-15](https://openairdocs.org/deregistered/N359QS-2003-01-15): Boeing 727-21, S/N 19007, built 1967. Second triennial mailing, no response. Owner: [Emery Worldwide Airlines Inc](https://openairdocs.org/faa-owner/EMERY%20WORLDWIDE%20AIRLINES%20INC), [Palo Alto, CA](https://openairdocs.org/faa-place/CA/Palo%20Alto)

## 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

---
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.