# N906QS: 2022 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: 680A0320
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 26, 2022
- Certificate issued: July 30, 2026
- Expires: July 31, 2033
- Mode S code: AC86E5
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=906QS
- Page: https://openairdocs.org/aircraft/N906QS

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 N906QS.

## FAA accident and incident reports

None matched to N906QS.

## Service difficulty reports (11)

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 DXTA2026101910227](https://openairdocs.org/sdr/DXTA2026101910227), Oct 17, 2026: EROSION SHIELD. DAMAGED. ON TAKEOFF ACCELERATING THROUGH 90KTS A LARGE BIRD FLEW AT THE AIRCRAFT AND VEERED TO THE LEFT SIDE OF THE NOSE AND UP AND OVER THE TOP OF THE FUSELAGE. ON POST
- [SDR DXTA2026042707769](https://openairdocs.org/sdr/DXTA2026042707769), Apr 24, 2026: PUMP. LEAKING. AT FL430 WE RECEIVED HYD PRESS LOW R CAS MESSAGE. ON HYDRAULIC SYSTEMS PAGE WE COULD SEE THE VOLUME OF FLUID SLOWLY DECREASING. EVENTUALLY CAS MESSAGE HYD VOLUM
- [SDR DXTA2025100905218](https://openairdocs.org/sdr/DXTA2025100905218), Oct 6, 2025: LANDING GEAR. MALFUNCTIONED. DURING APPROACH, THE LEFT MAIN GEAR INDICATED A YELLOW HASH UPON EXTENSION. WE WENT AROUND AND DID THE GEAR DISAGREE LEFT CHECKLIST AND THE LANDING GEAR WILL NO
- [SDR DXTA2025092905090](https://openairdocs.org/sdr/DXTA2025092905090), Sep 25, 2025: ELEC CONNECTOR. DIRTY. DURING INSTRUMENT APPROACH, DURING MLG EXTENSION, LT MLG WAS A YELLOW X & GEAR DISAGREE L CAS MESSEGE APPEARED. DID A MISSED APPROACH, RAISED MLG & CLIMBED TO H
- [SDR DXTA2025040402940](https://openairdocs.org/sdr/DXTA2025040402940), Apr 4, 2025: FLOAT SWITCH. FAULTED. IN FLIGHT FL280 RECEIVED THE FUEL LEVEL LOW R CAS MESSAGE. FOLLOWED QRH AND LANDED SOON AS POSSIBLE. CORRECTIVE ACTION: PERFORMED ARES DOWNLOAD AND SENT FILES T
- [SDR DXTA2025032402779](https://openairdocs.org/sdr/DXTA2025032402779), Mar 22, 2025: DOOR. LACK OF LUBE. MAIN DOOR: WHEN OPENING THE DOOR, IT WILL OPEN ABOUT 2 INCHES AND GETS STUCK. REQUIRES SEVERAL HARD PULLS FROM OUTSIDE OR 2-3 HARD PUSHES INSIDE TO GET IT TO OP
- [SDR DXTA2024111101102](https://openairdocs.org/sdr/DXTA2024111101102), Nov 9, 2024: BATTERY PACK. DISCHARGED. CABIN EMERG LIGHT: READ LIGHT ABOVE SEAT 7 NOT ILLUMINATING DURING THE EMER LTS TEST NOR WHEN THE EMER LTS SWITCH IS IN THE ON POSITION. CORRECTIVE ACTION; POWE
- [SDR DXTA2024052911905](https://openairdocs.org/sdr/DXTA2024052911905), May 28, 2024: DOOR. OUT OF ADJUST. MAIN DOOR: THE MAIN CABIN DOOR DOES NOT OPEN AFTER BEING UNLATCHED UNTIL APPLYING ABOUT 15 TO 20 POUNDS OF PRESSURE INSPECTED MAIN ENTRY DOOR AND FOUND IT OUT O
- [SDR DXTA2024040111370](https://openairdocs.org/sdr/DXTA2024040111370), Mar 31, 2024: RUB STRIP. OUT OF ADJUST. MAIN DOOR: MAIN CABIN ENTRY DOOR REQUIRES SLIGHT PUSH TO OPEN ONCE HANDLE IS MOVED TO OPEN POSITION. CLEANED AND LUBRICATED DOOR HANDLE AND HINGE POINTS ON MED,
- [SDR DXTA2023101697930](https://openairdocs.org/sdr/DXTA2023101697930), Oct 14, 2023: ACTUATOR. DEFECTIVE. GEAR DISAGREE L AMBER CAS: DURING CLIMBOUT AFTER GEAR RETRACTION, GEAR DISAGREE L CAS MESSAGE AND ADC SSEC MISCOMPARE CAS DISPLAYED. RAN CHECKLIST AND DIRECTED 
- [SDR DXTA2023032383050](https://openairdocs.org/sdr/DXTA2023032383050), Mar 22, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR HANDLE WILL NOT MOVE DOWN AFTER DOOR IS CLOSED. REMOVED AND REPLACED BEARING P/N: M81934/2·07V005P AND BOLT P/N: NAS1160-3·12D ON LOW

## Service difficulty reports on N906QS not matched to an aircraft (23)

They name N906QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR JGVR20181130001](https://openairdocs.org/sdr/JGVR20181130001), Nov 30, 2018: ACCESS PANEL. CORRODED. CENTER WING FUEL QUANTITY DIPSTICK PANEL 172BZ HAS LEVEL 2 CORROSION AROUND SEVERAL SCREWS REQUIRING REPLACEMENT OF OUTER PANEL. FOUND WHILE PERFORMING C750 BAS
- [SDR 2016F00208](https://openairdocs.org/sdr/2016F00208), Oct 28, 2016: STRUCTURE. CRACKED. REPAIR OF NOSE DAMAGE, REPORT S-750-0206/16RD REV- DATED 10/25/2016,WITH FAA FORM 8100-9 DATED 10/28/2016.
- [SDR DXTA2014060905799](https://openairdocs.org/sdr/DXTA2014060905799), Jun 8, 2014: APU. ODOR. OILY ODOR COMING FROM AIR SYS. REMOVED APU FROM AIRCRAFT. INSTALLED REPAIRED APU. ALL OPS & LEAK CHECKED GOOD. CLOSED ALL ACCESS. WORK DONE IAW MM 49-10-00. REM
- [SDR DXTA2012122605217](https://openairdocs.org/sdr/DXTA2012122605217), Dec 27, 2012: UNKNOWN. UNKNOWN. SELECTED MLG DOWN, NOSE GEAR WOULD NOT INDICATE GREEN. ABNORMAL PROCEDURES FOLLOWED, INCLUDING NG UPLOCK RING PULLED, RECEIVED THREE GREEN INDICATIONS. LANDED W
- [SDR DXTA2010111804310](https://openairdocs.org/sdr/DXTA2010111804310), Nov 17, 2010: COALESCER BAG. DIRTY. DURING DESCENT THRU 9000 FT, STRONG FUMES WERE SMELLED IN THE PLANE. NO SMOKE WAS SEEN. THE FUMES SMELLED LIKE FROM ACM. REMOVED WATER SEPARATOR. COALESCER SOCK
- [SDR DXTA2010082304203](https://openairdocs.org/sdr/DXTA2010082304203), Aug 20, 2010: COALESCER BAG. ODOR. WITH APU BLEED ON, FEEDING RT PACK, A STRONG, ACRID ODOR WAS NOTED IN CABIN. MAX COOL SWITCH WAS ON AT FIRST THEN SHUT AND ODOR STAYED THE SAME. RAN APU AND TUR
- [SDR 2010FA0000631](https://openairdocs.org/sdr/2010FA0000631), May 25, 2010: FRAME. CRACKED. ((CNQR)) THE PN 6750743-4 FRAME IS PART OF THE AILERON POWER CONTROL UNIT SUPPORT ASSY AND IS APPLICABLE TO ACFT. DURING SCHEDULED INSP, THE FRAME WAS FOUND TO 
- [SDR DXTA2009072303737](https://openairdocs.org/sdr/DXTA2009072303737), Jul 21, 2009: LEAD. FAILED. FIRE COMING FROM APU EXHAUST. AT THE SAME TIME, BANGING NOISE IS COMING FROM LEFT WING. T/S AND FOUND APU IGNITOR LEAD BAD REMOVED AND REPLACED WITH NEW. OPS CH
- [SDR DXTA2009051103646](https://openairdocs.org/sdr/DXTA2009051103646), May 8, 2009: ACM. FAILED. SMOKE IN CABIN AFTER START, TROUBLESHOT TO RT PAC. SMOKE DISAPATES AFTER PAC HAS BEEN TURNED OFF. TROUBLESHOT SYSTEM, FOUND CABIN PAC FAILED. REMOVED AND REPLAC
- [SDR DXTA2009042203613](https://openairdocs.org/sdr/DXTA2009042203613), Apr 21, 2009: COMPUTER. MALFUNCTIONED. DURING TAKEFF ROLL #1 MFD & #1 PFD WENT BLANK MOMENTARILY AND AMBER "IAC TEST INOP 1" ILLUMINATED. REMOVED NR 1 IC-800 INSTALLED SUPPLIED UNIT IAW CE750 M/M CH 
- [SDR DXTA2009042103613](https://openairdocs.org/sdr/DXTA2009042103613), Apr 21, 2009: COMPUTER. MALFUNCTIONED. DURING TAKEOFF ROLL NR 1 MFD & NR 1 PFD WENT BLANK MOMENTARILY AND AMBER "IAC TEST INOP 1" ILLUMINATED. REMOVED NR 1 INTEGRATED COMPUTER & INSTALLED SUPPLIED UN
- [SDR DXTA200803145](https://openairdocs.org/sdr/DXTA200803145), Jun 27, 2008: COALESCER BAG. DIRTY. AT FL410 DETECTED STRONG FUMES IN COCKPIT. COULD DETECT FUMES IN DESCENT AND LANDING. REMOVED AND CLEANED COALECER SOCKS, VERY DIRTY AND ODOROUS. IAW MM 21-90-5
- [SDR DXTA200803101](https://openairdocs.org/sdr/DXTA200803101), Jun 7, 2008: ADC. MALFUNCTIONED. AFTER TAKEOFF THE FOLLOWING MESSAGE ILLUMINATED YAW DAMPER OFF BOTH YAW DAMPERS WERE OFF LINE. REMOVED AND REPLACED NR 1 MADC. PERFORMED OPERATIONAL CHECKS, CHE
- [SDR DXTA200803093](https://openairdocs.org/sdr/DXTA200803093), Jun 3, 2008: PITOT LINE. LEAKING. YAW DAMPER FAILED 3 TIMES BOTH IN A AND B ALSO HAD FGC FAIL MSG WITH EACH OCCURRENCE ALSO A AND B THE LAST FAIL ALSO HAD A FGC ADC MISCOMPARE MSG. REPLACED SOFT
- [SDR DXTA200702721](https://openairdocs.org/sdr/DXTA200702721), Dec 30, 2007: WINDSHIELD. BROKEN. LT WINDSHIELD IS CRACKED. LT WINDSHIELD HEAT INOP ILLUMINATED ON CAS. REMOVED CRACKED L/H WINDSHIELD. INSTALLED NEW WINDSHIELD. OPERATIONAL CHECK GOOD IAW CE750
- [SDR DXTA200702353](https://openairdocs.org/sdr/DXTA200702353), Jul 20, 2007: PACKING. OUT OF TOLERANCE. GEAR WOULD NOT RETRACT AFTER T.O. GEAR HANDLE LOCKED DOWN. HAD BEEN ACTING UP ON PRIOR FLIGHTS, NOT ALLOWING US TO RETRACT IMMEDIATELY. DISASSEMBLED LOWER NOSE 
- [SDR DXTA200702318](https://openairdocs.org/sdr/DXTA200702318), Jul 5, 2007: WHEEL. OUT OF ROUND. EXTREMELY NOTICABLE NOSEWHEEL SHIMMY DURING TAKEOFF ROLL BETWEEN 60-70 KNOTS. FOUND NOSE TIRES OUT OF ROUND REMOVED AND REPLACED NOSE WHEEL/ TIRE ASSY'S WITH AN
- [SDR DXTA200702052](https://openairdocs.org/sdr/DXTA200702052), Mar 27, 2007: ACTUATOR. MALFUNCTIONED. AFTER GEAR DOWN SELECTION, NO NOSE GEAR GREEN LIGHT FOR 20-30 SECONDS. REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR WITH SERVICABLE (INSPECTED) UNIT BY CESSN
- [SDR DXTA200601440](https://openairdocs.org/sdr/DXTA200601440), Jun 15, 2006: UPLOCK SWITCH. OUT OF ADJUST. IN CLIMB, NOSE GEAR UPLOCK RELEASED, GEAR UNLOCK LIGHT ILLUMINATED. ACCOMPLISHED NETJETS GEAR BUMP CHECKLIST, FOUND NOSE GEAR UPLOCK SWITCH ADJUSTED OUT OF SPEC
- [SDR DXTA200501175](https://openairdocs.org/sdr/DXTA200501175), Dec 31, 2005: FADEC. INOPERATIVE. FADEC FAULT CODE CAME ON DURING TAKEOFF, ABORTED TAKEOFF AND RETURNED TO BLOCK. PERFORMED CHECKLIST AND CLEARED FAULT CODE. AIRCRAFT OPS CHECKED GOOD.
- [SDR DXTA200500915](https://openairdocs.org/sdr/DXTA200500915), Aug 22, 2005: PDU. INOPERATIVE. FLAPS FAIL IN FLIGHT, SLATS EXTENDED / FLAPS AT ZERO. ATTEMPTED RESET TO NO AVAIL, DIVERTED. TROUBLESHOT FLAPS WITH TEAM X. TO PDU. REMOVED AND REPLACED PDU WIT
- [SDR DXTA200500828](https://openairdocs.org/sdr/DXTA200500828), Jul 8, 2005: ACTUATOR. FAILED. RUDDER LIMIT FAIL -B- CAS MESSAGE ILLUMINATED DURING FLIGHT. RUDDER LIMIT WAS 28 PERCENT T/S TO BAD ACTUATOR REMOVED AND REPLACED LOWER RUDDER LIMIT ACTUATOR SY
- [SDR 2005FA0000600](https://openairdocs.org/sdr/2005FA0000600), Apr 12, 2005: SKIN. CORRODED. DURING SCHEDULED INSPECTION FOUND SEVERAL SMALL SPOTS OF CORROSION ON BOTH LEFT AND RIGHT LOWER WING SKINS. PN OF THESE WING SKINS ARE: 67221463, 4 , 67221663,4

## 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

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