# N929QS: 2023 Textron 680A - Status: Valid registration - Airframe: [Textron 680A](https://openairdocs.org/model/textron-680a) (registry code 2076814, 10 seats) - Engine: [Pratt & Whitney Canada PW306D1](https://openairdocs.org/engine/pratt-whitney-canada-pw306d1) (registry code 51850) - 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: 680A0358 - Year built: 2023 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 31, 2023 - Certificate issued: October 6, 2026 - Expires: October 31, 2033 - Mode S code: ACE108 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=929QS - Page: https://openairdocs.org/aircraft/N929QS 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): 3 in force ### Matched by airframe (Textron 680A) - [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 ### Matched by engine (Pratt & Whitney Canada PW306D1) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N929QS. ## FAA accident and incident reports None matched to N929QS. ## Service difficulty reports (2) 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 DXTA2024091600549](https://openairdocs.org/sdr/DXTA2024091600549), Sep 15, 2024: CONNECTOR. DAMAGED. CABIN EMERG LIGHT: EMERGENCY EXIT SIGN OVER SEAT 7 DOES NOT ILLUMINATE WITH AIRCRAFT POWER OFF AND SWITCH IN ARM POSITION CORRECTIVE ACTION: BENCH CHECKED AFT C - [SDR DXTA2024012310236](https://openairdocs.org/sdr/DXTA2024012310236), Dec 4, 2023: DISC. DISCONNECTED. AILERON CONTROL: WHILE DOING A FLIGHT CONTROL CHECK PRIOR TO TAKEOFF, THE ROLL DISCONNECTED ON ITS OWN WHEN MOVING THE YOKE FOR ROLL. THE PITCH STAYED CONNECTED ## Service difficulty reports on N929QS not matched to an aircraft (20) They name N929QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2016052006243](https://openairdocs.org/sdr/DXTA2016052006243), May 26, 2016: APU. DEFECTIVE. ON GND, APU ONLY, ACFT FILLED WITH SMOKE. REMOVED DEFECTIVE APU & INSTALLED A REPAIRED CUSTOMER SUPPLIED APU. COMPLIED WITH APU OPERATIONAL CHECKS & LEAK CHECKS - [SDR DXTA2015012105965](https://openairdocs.org/sdr/DXTA2015012105965), Jan 20, 2015: ACM. FAILED. AFTER ENGINE START WITH APU OFF, FUMES & SMOKE COULD BE SEEN & SMELLED IN THE CABIN. PERFORMED TROUBLESHOOTING IAW MM 21-52-00 & FOUND ODOR TO BE COMING FROM CO - [SDR DXTA2015011505960](https://openairdocs.org/sdr/DXTA2015011505960), Jan 14, 2015: ACM. FAILED. THERE IS A STRONG ODOR OF BURNING RUBBER WITH A SLIGHT HAZE IN THE CABIN. PERFORMED TROUBLESHOOTING PER MM. 21-52-00 AND FOUND ODOR TO BE COMING FROM COCKPIT AC - [SDR DXTA2014040905724](https://openairdocs.org/sdr/DXTA2014040905724), Apr 4, 2014: STRAP. GOUGED. GOUGED ENG BEAM UPPER CAP STRAP. REPAIRED IAW CESSNA S-750-0129 22RD. - [SDR DXTR20120918001](https://openairdocs.org/sdr/DXTR20120918001), Sep 18, 2012: SKIN. PUNCTURED. DURING PRELIMINARY INSPECTION, FOUND PUNCTURE IN LOWER SKIN OF RT HORIZONTAL STAB. PUNCTURE INCLUDED A DENT .030" DEEP WITH A TEAR AT THE BOTTOM OF THE DENT LOC - [SDR DXTA2012041004947](https://openairdocs.org/sdr/DXTA2012041004947), Apr 9, 2012: CONTROL HANDLE. MALFUNCTIONED. COULD NOT MOVE GEAR HANDLE OUT OF THE DOWN POSITION AFTER TAKEOFF. R & R NLG WIRE HARNESS IAW WDM 32-50-01. R & R MLG CONTROL HANDLE IAW MM 32-30-01. PERFORMED - [SDR DXTA2012032604433](https://openairdocs.org/sdr/DXTA2012032604433), Mar 25, 2012: LANDING GEAR. MALFUNCTIONED. ON DEPARTURE, GEAR HANDLE WAS LOCKED IN THE GEAR DOWN POSITION. UNABLE TO GET GEAR TO RETRACT AND HAD TO HAVE PRIORITY HANDLING BACK TO DEPARTURE. NO EMERGENCY - [SDR DXTA2012030504902](https://openairdocs.org/sdr/DXTA2012030504902), Mar 4, 2012: CAM. INOPERATIVE. AFTER TAKEOFF, UNABLE TO RETRACT GEAR. THE GEAR HANDLE WOULD NOT MOVE. RETRURNED TO AIRPORT. FOUND EXCESSIVE PLAY IN NOSE GEAR SQUAT SWITCH TARGET CAM. REPLACED - [SDR DXTA2012022004878](https://openairdocs.org/sdr/DXTA2012022004878), Feb 19, 2012: SQUAT SWITCH. INOPERATIVE. LANDING GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. LANDING GEAR INDICATIONS REMAINED 3 GREEN AND NO RED. BURNED DOWN FUEL TO MAX LANDING WEIGHT AND LANDED UNE - [SDR DXTA2011020304446](https://openairdocs.org/sdr/DXTA2011020304446), Feb 2, 2011: PDU. FAILED. FLAPS FAILED ON APPROACH. THEY STOPPED AT ABOUT 3 DEGREES AND COULD NOT BE RESET. TROUBLESHOT FLAPS TO FAULTY POWER DRIVE UNIT. R & R FLAP POWER DRIVE UNIT WITH - [SDR DXTA2010072104166](https://openairdocs.org/sdr/DXTA2010072104166), Jul 20, 2010: CONTROLLER. LOCKED. LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. LANDING GEAR HANDLE COULD NOT BE MOVED, AND ALL LANDING GEAR POSITION INDICATOR LIGHTS INDICATED DOWN AND LOCKED. - [SDR DXTA200803203](https://openairdocs.org/sdr/DXTA200803203), Jul 29, 2008: GENERATOR. MALFUNCTIONED. ON TAXI OUT TOWER REPORTED SEEING SMOKE COMING FROM OUR RT ENG. STOPPED ACFT, SHUT BOTH ENG/APU DOWN. INSPECTED LT ENGINE. FOUND DEFECTIVE A/C GENERATOR. REMOVE - [SDR DXTA200702730](https://openairdocs.org/sdr/DXTA200702730), Dec 27, 2007: FLAP SYSTEM. MALFUNCTIONED. WHEN FLAPS SELECTED FOR 15 TO 35. FAILED AROUND 20 DEGREES. DID NOT RESET BUT EVENTUALLY CAME BACK TO FLAPS 15 DEGREES. FLAPS CAME TO 0 DEGREES ON GROUND, FLAP - [SDR DXTA200702566](https://openairdocs.org/sdr/DXTA200702566), Oct 24, 2007: WHEEL. VIBRATES. AT THE BEGINNING OF TAKE-OFF ROLL THE NOSE WHEEL STARTED TO SHIMMY AS THE AIR SPEED INCREASED THE SHIMMY BECAME WORSE. TAKE OFF WAS ABORTED. REMOVED LH NLG WHEE - [SDR DXTA200702450](https://openairdocs.org/sdr/DXTA200702450), Sep 6, 2007: WARNING MESSAGE. ILLUMINATED. DURING TO ROLL (FGC A FAIL), (MACH TRIM OFF), AND (PRI STAB TRIM FAIL) CAS MESSAGES ILLUMINATED. 09-27-07 T/S AND REMOVED AND REPLACED NR 1 IAC AND LOADED SN, A - [SDR DXTA200601769](https://openairdocs.org/sdr/DXTA200601769), Nov 30, 2006: LOGIC CARD. FAILED. DESCENDING TO FL330 AMBER (RUDDER LIMIT FAIL A) MESSAGE DISPLAYED-FIRST 5 SEC, THEN 10 SEC, THEN ABOUT 90 SECONDS, SHOWED 25 PERCENT RUDDER AVAILABLE. REMOVED A - [SDR DXTA200601520](https://openairdocs.org/sdr/DXTA200601520), Jul 27, 2006: STEERING SYS. MALFUNCTIONED. AFTER LANDING TURNING OFF THE RUNWAY ALL CONTROL OF THE NOSEWHEEL STEERING WAS LOST TILLER PLUS PEDALS WERE FROZEN. - [SDR DXTA200500641](https://openairdocs.org/sdr/DXTA200500641), Mar 24, 2005: STRUT. UNDERSERVICED. AFTER TAKEOFF ON GEAR RETRACTION GOT ALL 3 GREEN LIGHTS AND THE RED UNLOCK LIGHT STAYED ON. COULD HEAR THE LOUD AIR NOISE AND THE GEAR CYCLING AT LEAST 4 TIMES. - [SDR DXTA200400321](https://openairdocs.org/sdr/DXTA200400321), Jun 7, 2004: ISOLATION VALVE. FAILED. DURING FLIGHT BAGGAGE SEAL LIGHT CAME ON THEN CABIN ALTITUDE STARTED TO CLIMB. CLOSED BAGGAGE ISOLATION VALVE, CABIN ALTITUDE CONTINUED TO CLIMB. COULD NOT CONT - [SDR DXTA200300107](https://openairdocs.org/sdr/DXTA200300107), Sep 1, 2003: CONTROL UNIT. INOPERATIVE. AMBER (FLAPS FAIL) CAS MESSAGE ILLUMINATED IN FLIGHT WOULD NOT RESET. FLAPS WOULD NOT EXTEND, SLATS OPERATED NORMALLY, DIVERTED INTO JFK AND LANDED SAFELY. ## STCs that may be installed (OpenAirDocs) (16) 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 (Textron 680A) - [STC ST04765NY](https://openairdocs.org/stc/ST04765NY): Unprepared (Grass/Sod) Runway Operations. Textron Aviation Inc - [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 ST122244IB](https://openairdocs.org/stc/ST122244IB): Installation of Gogo Galileo system, including HDX Antenna. Alamo Engineering GmbH - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST11983SE](https://openairdocs.org/stc/ST11983SE): 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 ST02037WI](https://openairdocs.org/stc/ST02037WI): Installation of Gogo Business Aviation AVANCE L5 System with MB 13 Antennas. Duncan Aviation Inc - [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 ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc - [STC ST04367CH](https://openairdocs.org/stc/ST04367CH): Installation of a Medical Interior in accordance with LifePort Master Data List EGR-887-000-001, Revision (B), dated April 18, 2019 or later FAA approved revision and LifePort Master Drawing List MDL-887-00, Revision (D), dated April 11, 2019 or later FAA approved revision.". LifePort LLC - [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 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 ST11168SC](https://openairdocs.org/stc/ST11168SC): Installation of a Pratt & Whitney Flight Data Acquisition, Storage, and Transmission System (FAST). Pratt & Whitney Engine Services Inc ## Related - Other Textron 680A aircraft: https://openairdocs.org/model/textron-680a/aircraft.md - The Pratt & Whitney Canada PW306D1 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw306d1.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.