# N897QS: 2026 Textron 700

- Status: Valid registration
- Airframe: [Textron 700](https://openairdocs.org/model/textron-700) (registry code 2076819, 14 seats)
- Engine: [Honeywell AS907-2-1S](https://openairdocs.org/engine/honeywell-as907-2-1s) (registry code 33403)
- Data sheets: [TCDS T00015WI](https://openairdocs.org/tcds/T00015WI) (Textron Aviation Inc.), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 700-0171
- Year built: 2026
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 13, 2026
- Certificate issued: October 5, 2026
- Expires: October 31, 2033
- Mode S code: AC60C4
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=897QS
- Page: https://openairdocs.org/aircraft/N897QS

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): 2 in force

### Matched by airframe (Textron 700)

- [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

### Matched by engine (Honeywell AS907-2-1S)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N897QS.

## FAA accident and incident reports

None matched to N897QS.

## Reports on N897QS not matched to an aircraft (1)

They name N897QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20171213023719I](https://openairdocs.org/incident/20171213023719I), Dec 13, 2017: Hawker Beechcraft Corp HAWKER 900XP (N897QS), Jacksonville, FL, No damage. EJA897, H25, bdl-jax, reported a bird strike landing runway 26. Aircraft taxied to the ramp. Damage: none. 12/13/2017 2000Z. Verified with maintenance there…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N897QS not matched to an aircraft (19)

They name N897QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2015012605968](https://openairdocs.org/sdr/DXTA2015012605968), Jan 23, 2015: ENGINE. OVERSPEED. NR 2 ENGINE OVERSPEED 105.1 N1. FL400, ISA + 4, MACH.75 THROTTLE DID NOT CONTROL ENGINE. OVERSPEED SELECTED ON NR 2 ENGINE COMPUTER. PILOT MANUALLY SHUTDOWN ENG
- [SDR DXTA2014050505765](https://openairdocs.org/sdr/DXTA2014050505765), May 6, 2014: VALVE. FAILED. DURING RETRACTION GEAR AFTER TAKEOFF, LT MAIN GEAR RED GEAR INDICATOR REMAINED ILLUMINATED. COMPLIED WITH GEAR SPEED LIMITS, EXECUTED ABNORMAL CHECKLIST. GEAR D
- [SDR DXTA2014050505764](https://openairdocs.org/sdr/DXTA2014050505764), May 4, 2014: WARNING SYSTEM. FALSE ACTIVATION. ON DEPARTURE FROM PIT, RIGHT CROSSWIND OF 25 KNOTS TOO, POSITIVE RATE CALLED FOR GEAR UP & THE LT MAIN GEAR RED INDICATOR LIGHT STAYED ON. WHEN WE PICKED UP THE
- [SDR DXTA201405050576](https://openairdocs.org/sdr/DXTA201405050576), May 4, 2014: WARNING SYSTEM. ACTIVATED. ON DEPARTURE FROM PIT, RT CROSSWIND OF 25 KNOTS TOO, POSITIVE RATE CALLED FOR GEAR UP & LT MLG RED INDICATOR LIGHT STAYED ON. WHEN WE PICKED UP THE ACFT ON SATU
- [SDR DXTA2014033005708](https://openairdocs.org/sdr/DXTA2014033005708), Mar 30, 2014: LINK. OUT OF ADJUST. LEFT MLG FAILED TO FULLY RETRACT AFTER TAKEOFF. TOWER REPORTED GEAR APPROXIMATELY 45 DEGREES RETRACTED. RED GEAR UNSAFE LIGHT ILLUMINATED. LOWERED GEAR HANDLE I
- [SDR DXTA2014022105662](https://openairdocs.org/sdr/DXTA2014022105662), Feb 20, 2014: VALVE. OUT OF ADJUST. FOLLOWING REAR RETRACTION, LT MAIN GEAR ILLUMINATED RED & REMAINED ON UNTIL GEAR HANDLE WAS PLACED TO DOWN. NORMAL THREE GREEN INDICATION FOLLOWED. UPON INVESTI
- [SDR DXTA2014020305637](https://openairdocs.org/sdr/DXTA2014020305637), Feb 1, 2014: WARNING SYSTEM. FALSE ACTIVATION. WHEN THE GEAR WAS RETRACTED ON TAKE OFF, LT MLG INTRANSIT LIGHT STAYED ON FOR 5 OR MORE MINUTES. WE ALSO NOTICED A BURNT RUBBER SMELL SHORTLY AFTER RETRACTION. 
- [SDR DXTA2013090305490](https://openairdocs.org/sdr/DXTA2013090305490), Aug 31, 2013: CONDENSER. FAILED. BURNING ODOR IN COCKPIT, NOTICED FROM JUST AFTER TAKEOFF POWER APPLICATION UNTIL DISSIPATION AFTER 8-10 MINUTES. PERFORMED ENGINE MAINTENANCE RUN. RAN EACH ENGI
- [SDR DXTA2013012805262](https://openairdocs.org/sdr/DXTA2013012805262), Jan 27, 2013: SEQUENCE VALVE. FAILED. AFTER TAKEOFF AND GEAR RETRACTION; THE LT MAIN GEAR 'RED' LIGHT REMAINED ILLUMINATED. TOWER CONFIRMED LT MAIN GEAR WAS INDEED DOWN. REPLACED LT GEAR SEQUENCE VA
- [SDR DXTA2013010805238](https://openairdocs.org/sdr/DXTA2013010805238), Jan 7, 2013: UPLOCK SWITCH. OUT OF ADJUST. RED LT MAIN GEAR, RED UNSAFE LIGHT ILLUMINATED IN FLIGHT. JACKED ACFT AND COMPLIED WITH SEVERAL GEAR SWINGS. ALL INDICATIONS WERE NORMAL. PERFORMED VISUAL INSPE
- [SDR DXTA2013010705233](https://openairdocs.org/sdr/DXTA2013010705233), Jan 5, 2013: SWITCH. DIRTY. AFTER T/O THE "RED" LEFT GEAR LIGHT WAS ON. LEVELED OFF AND RECYCLED THE GEAR. RECEIVED THREE GREEN AND PIN, RETRACTED AGAIN AND HAD SAME INDICATION. RETURNED T
- [SDR DXTA2011100304738](https://openairdocs.org/sdr/DXTA2011100304738), Sep 30, 2011: FUEL CONTROL. MALFUNCTIONED. AT CRUISE ALTITUDE, NR 2 ENGINE COMPUTER MM ANNUNCIATOR ILLUMINATED. ENGINE POWER CHANGED ON ITS OWN AT THAT MOMENT. CHECKLIST ITEMS COMPLIED WITH AND NR 2 ENG 
- [SDR DXTA2011061404612](https://openairdocs.org/sdr/DXTA2011061404612), Jun 12, 2011: VALVE. LEAKING. REAR EQUIPMENT BAY OVERHEAT "RED" LIGHT ILLUMINATED AT 8000 FT MSL, DURING CLIMB. APU BLEED SWITCH OFF & APU STOPPED, THROTTLES REDUCED, "RED" LIGHT EXTINGUISHE
- [SDR DXTA2011041104541](https://openairdocs.org/sdr/DXTA2011041104541), Apr 7, 2011: CONTROL PANEL. FAILED. APU FAULT PANEL APPEARS TO HAVE BURNT. FELT HOT TO THE TOUCH. REMOVED APU AND VISUALLY INSPECTED WIRING AND COMPONENTS, NO DEFECTS NOTED. DIDN'T DETECT ANY ELEC
- [SDR DXTA2010072604176](https://openairdocs.org/sdr/DXTA2010072604176), Jul 23, 2010: LEVER. OBSTRUCTED. THE RT THRUST LEVER WILL NOT COME OUT OF THE IDLE POSITION WHEN TRYING TO TAXI. BOTH ENGINES RUNNING CONTROL LOCKS RELEASED. FOUND FCU CONTROL LEVER INTERFERRIN
- [SDR 2010FA0000089](https://openairdocs.org/sdr/2010FA0000089), Feb 4, 2010: TRIM SYSTEM. MALFUNCTIONED. CLIMBING ON DEPARTURE FROM PSP WITH AUTOPILOT ENGAGED, AUTOPILOT WAS DISCONNECTED MANUALLY BECAUSE IT WAS GOING TO GO THROUGH THE LEVEL OFF ALTITUDE, THE TRIM W
- [SDR 2009FA0000765](https://openairdocs.org/sdr/2009FA0000765), Apr 5, 2009: BEARING. DAMAGED. THE SUBJECT ENGINE WAS REMOVED FOLLOWING A COMMANDED INFLIGHT SHUTDOWN ON APRIL 5TH, 2009. SHUTDOWN DETAILS: AT APPROX 39K, CREW NOTED NR 1 ENGINE THUMP AND VIB
- [SDR DXTA2009040603584](https://openairdocs.org/sdr/DXTA2009040603584), Apr 5, 2009: ENGINE. FAILED. AT FL380, .76M, A THUMP WAS FELT IN THE AIRFRAME WITH A CONSTANT VIBRATION. LT NR 1 OIL PRESS TURNED RED AND COMPLETED THE LOW OIL PRESS MEM ITEMS AND SHUT THE 
- [SDR 2008FA0000265](https://openairdocs.org/sdr/2008FA0000265), Mar 22, 2008: COMPRESSOR. SEPARATED. ON CLIMB THROUGH FL140 CREW HEARD BANG FROM RT ENGINE WITH VIBRATION. RT ITT INCREASED 150C BUT NO OVER TEMP. REDUCED POWER, THEN BROUGHT POWER BACK UP, WITH SA

## STCs that may be installed (OpenAirDocs) (11)

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 700)

- [STC ST12145SE](https://openairdocs.org/stc/ST12145SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC
- [STC ST00415BO](https://openairdocs.org/stc/ST00415BO): Installation of an NVIS/NVG compatible lighting system and infrared capable exterior lighting. ATI Engineering Services LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST02812LA](https://openairdocs.org/stc/ST02812LA): Installation of the Honeywell EDG-100 Connected Engine Data Access System. Honeywell International Inc
- [STC ST04572CH](https://openairdocs.org/stc/ST04572CH): Installation of an Airborne Terminal System and a Ka Radome. StandardAero Business Aviation Services LLC
- [STC ST02746SE](https://openairdocs.org/stc/ST02746SE): Installation of external aerodynamic modifications, interior furnishings and equipment, including provisions for additional non-essential systems. Textron Aviation Inc
- [STC ST02694SE](https://openairdocs.org/stc/ST02694SE): Group Reduced Vertical Separation Minimum (RVSM) airworthiness approval. AeroMech Incorporated
- [STC ST04211NY](https://openairdocs.org/stc/ST04211NY): Installation of of NSM UNIFIS 3000 G2 Flight Inspection System. Aerospace Design & Compliance LLC
- [STC ST01971WI](https://openairdocs.org/stc/ST01971WI): Installation of the Garmin G5000 Software Changes & GH-3900 Standby Configuration Updates. Textron Aviation 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

## Related

- Other Textron 700 aircraft: https://openairdocs.org/model/textron-700/aircraft.md
- The Honeywell AS907-2-1S engine: https://openairdocs.org/engine/honeywell-as907-2-1s.md

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