# N825QS: 2022 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: 700-0066 - Year built: 2022 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 15, 2022 - Certificate issued: April 24, 2026 - Expires: April 30, 2033 - Mode S code: AB44DD - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=825QS - Page: https://openairdocs.org/aircraft/N825QS 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 N825QS. ## FAA accident and incident reports None matched to N825QS. ## Service difficulty reports (7) 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 DXTA2025061603895](https://openairdocs.org/sdr/DXTA2025061603895), Jun 14, 2025: LINK ASSY. BENT. MAIN DOOR HARDWARE: AS I WAS CLOSING THE DOOR FROM THE INSIDE OF THE CABIN, I HEARD A SNAP AND THE DOOR OPENED BACK UP. THE CONNECTION PIN ON THE INTERIOR ARM A - [SDR DXTA2025022602467](https://openairdocs.org/sdr/DXTA2025022602467), Feb 22, 2025: BATTERY. FAULTY. WHEN ACCOMPLISHING THE POWER ON CHECKLIST (BATTERIES CONNECTED, AND BATTERY SWITCHES OFF) THE EMERGENCY LIGHTS BOTH EXTERIOR/INTERIOR FAILED TO ILLUMINATE IN TH - [SDR DXTA2025022502455](https://openairdocs.org/sdr/DXTA2025022502455), Feb 21, 2025: UNKNOWN. UNKNOWN. AFTER CHARGING EMERGENCY LIGHT BATTERIES FOR 60 MINUTES, THE EMERGENCY LIGHTS FAIL PREFLIGHT TEST. WHEN BATTERIES ARE OFF AND EMERGENCY LIGHTS ARE IN ARMED, NO - [SDR DXTA2024052911902](https://openairdocs.org/sdr/DXTA2024052911902), May 28, 2024: HANDLE. BINDING. MAIN ENTRANCE DOOR WHEN RAISING THE HANDLE TO OPEN POSITION THE HANDLE BINDING ON HALFWAY UP MAKING DIFFICULT TO OPEN THE DOOR. REQUIRING EXCESSIVE FORCE TO LIF - [SDR DXTA2023052486990](https://openairdocs.org/sdr/DXTA2023052486990), May 24, 2023: BATTERY PACK. DEFECTIVE. EMERG LIGHT SWITCH: EMER LIGHTS DO NOT ILLUMINATE WITH SWITCH IN ARM AND BATTERIES OFF. RECEIVED REPAIRED BATTERY CHARGER SYSTEM (EMER BATTERY) P/N: CBS28-1 S/N - [SDR DXTA2023050985670](https://openairdocs.org/sdr/DXTA2023050985670), May 8, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: ON PREFLIGHT, WITH BATTERIES IN OFF POSITION AND EMERGENCY LIGHTS PLACED IN ARM, NONE OF THE EMERGENCY LIGHTS ILLUMINATE. WITH EMERGENCY LIGH - [SDR DXTA2022051962140](https://openairdocs.org/sdr/DXTA2022051962140), May 17, 2022: NONE. DEFECTIVE. LEFT FUEL TRANSFER: DURING LEVEL FLIGHT, FUEL TRANSFER SWITCH SELECTED TO RIGHT TANK, AT WHICH TIME AMBER FUEL TRANSFER FAIL CAS MESSAGE DISPLAYED. SWITCH WAS R ## Service difficulty reports on N825QS not matched to an aircraft (19) They name N825QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR JGVR201609060001](https://openairdocs.org/sdr/JGVR201609060001), Sep 2, 2016: THRESHOLD. CRACKED. CRACKED MAIN ENTRY DOOR LOWER INNER THRESHOLD AND OUTER THRESHOLD. INSTALLED NEW INNER THRESHOLD, AND NEW OUTER THRESHOLD IAW SRM AND MM. - [SDR DXTA2015100106097](https://openairdocs.org/sdr/DXTA2015100106097), Sep 30, 2015: FAN. ODOR. ELECTRICAL ODOR NOTICED IN THE FLIGHT COMPARTMENT AFTER DEFOG FAN SET TO HIGH. INSTALLED NEW DEFOG BLOWER ASSEMBLY FAN. PERFORMED SATISFACTORY OPERATIONS CHECK - [SDR DXTA2013011405245](https://openairdocs.org/sdr/DXTA2013011405245), Jan 12, 2013: UPLOCK SWITCH. MALFUNCTIONED. RED "GEAR UNLOCKED" INDICATION AFTER GEAR RETRACTION DURING TAKEOFF. GEAR WAS MOVED TO THE DOWN POSITION AND 3 GREEN LIGHTS WERE OBSERVED WITH THE RED "GEAR UNL - [SDR DXTA2012080605079](https://openairdocs.org/sdr/DXTA2012080605079), Aug 6, 2012: OUTFLOW VALVE. FAILED. IN CRUISE FLIGHT (FL450) CABIN BEGAN TO LOSE PRESSURE. EXECUTED RAPID DESCENT, CABIN BUMPED A COUPLE OF TIMES, CABIN DESCENT STOPPED BRIEFLY, THEN CONTINUED. MA - [SDR CWQR20120210004](https://openairdocs.org/sdr/CWQR20120210004), Feb 10, 2012: SEAT. CRACKED. DURING AN INSPECTION, THE CO-PILOT SEAT BASE WAS FOUND TO BE CRACKED 1.13" ON THE SUPPORT ANGLE TO BASE AREA. THE SEAT BASE DOES NOT APPEAR TO BE DAMAGED AND TH - [SDR DXTA2009041703604](https://openairdocs.org/sdr/DXTA2009041703604), Apr 17, 2009: ENGINE. UNDAMAGED. DURING POST FLIGHT, FOUND EVIDENCE OF BIRD STRIKE INTO RT ENGINE. COMPLIED WITH BIRD STRIKE INSPECTION ON AIRFRAME IAW M.M. CH 5-10-00, NO DAMAGE FOUND. COMPLIE - [SDR DXTA2009010403460](https://openairdocs.org/sdr/DXTA2009010403460), Jan 4, 2009: ACTUATOR. INOPERATIVE. UPON ARRIVAL, GEAR SELECTED DOWN, UNLOCK LITE REMAINED ON AND ONLY NOSE AND RMLG INDICATORS WERE GREEN. COMPLETED CK LIST AND BLEW GEAR DOWN W/NO LT GEAR DOWN I - [SDR DXTA2009010503460](https://openairdocs.org/sdr/DXTA2009010503460), Jan 4, 2009: WARNING LIGHT. ILLUMINATED. SELECTED GEAR DOWN, UNLOCK LIGHT REMAINED ON AND ONLY NOSE AND RMLG INDICATORS WERE GREEN. - [SDR DXTA2008121903409](https://openairdocs.org/sdr/DXTA2008121903409), Dec 19, 2008: BULB. BURNED OUT. ON APPCH, EXTENDED LANDING GEAR- NO GREEN LITE ON LT MAIN GEAR. CHECKED LITE BULB WITH ROTARY TEST: INC FAILED BULB. FOLLOWED PROCEDURE FOR GEAR FAIL TO DEPLOY - [SDR DXTA2008122203409](https://openairdocs.org/sdr/DXTA2008122203409), Dec 19, 2008: INDICATOR. INOPERATIVE. EXTENDED LANDING GEAR- NO GREEN LIGHT ON LT MAIN GEAR. - [SDR DXTA2008120203383](https://openairdocs.org/sdr/DXTA2008120203383), Dec 2, 2008: ACTUATOR. LEAKING. GEAR UNLOCKED LIGHT AND HYD PRESS LIGHT REMAINED ON AFTER GEAR RETRACTION. REMOVED AND REPLACED LEAKING LT OLEO. - [SDR DXTA2008120303383](https://openairdocs.org/sdr/DXTA2008120303383), Dec 2, 2008: INDICATOR. MALFUNCTIONED. GEAR UNLOCKED LIGHT REMAINED ON AFTER GEAR RETRACTION. - [SDR DXTA200803204](https://openairdocs.org/sdr/DXTA200803204), Jul 29, 2008: PROBE. FAILED. DURING TAKEOFF ROLL "L FUEL GAUGE" LIGHT ILLUMINATED PASSING 60 KTS. ABORTED TAKEOFF. REMOVED AND REPLACED LT WING NR 4 FUEL PROBE DUE TO INTERNAL FAILURE IAW M - [SDR DXTA200803045](https://openairdocs.org/sdr/DXTA200803045), May 5, 2008: CONTROLLER. FAILED. AT FL300 THE CABIN RATE STARTED CLIMBING ABNORMALLY TILL IT REACHED 6000 FT IAW MINT THE 10,000 FT CABIN ENUNCIATORS ILLUMINATED AND THE EMER PRESS CAME ON. OXY - [SDR DXTA200701879](https://openairdocs.org/sdr/DXTA200701879), Jan 25, 2007: WARNING SYSTEM. UNKNOWN. DURING TAKEOFF ROLL , AMBER (IAS) COMPARATOR MESSAGE APPEARED ON PFD. TAKEOFF WAS ABORTED IAW CHECKLIST PROCEDURES. (IAS) MESSAGE EXTINGUISHED AND DID NOT REAPP - [SDR DXTA200601300](https://openairdocs.org/sdr/DXTA200601300), Mar 14, 2006: ACTUATOR. MALFUNCTIONED. DURING APPROACH TO LANDING LOWERED GEAR AND HAD LEFT MAIN GEAR LIGHT NOT ILLUMINATE WITH A RED GEAR UNLOCK ANNUNICATOR. NOSE AND RIGHT MAIN WERE GREEN. PERFORME - [SDR DXTA200500891](https://openairdocs.org/sdr/DXTA200500891), Aug 8, 2005: PIPE. CHAFED. PERFORM VISUAL INSPECTION OF THE RT LINE ASSY P/N 6516311-19 (REFUEL/DEFUEL FLOW) FOR SIGNS OF CHAFFING BY FLAP CROSS OVER CABLE BEHIND PANEL 172BB. (CHAPT. 6 A - [SDR DXTA200500729](https://openairdocs.org/sdr/DXTA200500729), May 18, 2005: TRIM SYSTEM. MALFUNCTIONED. AILERON TRIM APPEARS TO BE FREEZING UP IN FLIGHT AT FL 380 AT -28 C RAT. THE ROLL TRIM ANNUNCIATOR ILLUMINATED, WAS UNABLE TO MOVE THE AILERON TRIM KNOB UNTIL T - [SDR DXTA200400350](https://openairdocs.org/sdr/DXTA200400350), Aug 1, 2004: LANDING GEAR. MALFUNCTIONED. DURING APPROACH NOSE GEAR WOULD GO TO DOWN AND LOCK ON TWO TRIES. BLEW GEAR DOWN AND PROCEEDED TO LAND. JACKED AIRPLANE, CYCLED GEAR 15 TIMES TO BLEED SYSTEM RE ## 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 --- 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.