- Owner type
- Co-owned
- Serial number
- 700-0060
- Year built
- 2021
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 4, 2021
- Certificate issued
- December 8, 2021
- Expires
- December 31, 2028
- Mode S code
- AB39B8
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 2
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2023 | 1 |
|---|---|
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N822QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Textron 700 aircraft
FAA incident reports
No FAA accident or incident reports matched to N822QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Textron 700 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026060108265Wire Harness · malfunctionedON DEPARTURE OUT OF KTEB AFTER CALLING FOR "GEAR UP" THE FO TRIED TO RETRACT THE GEAR. THE HANDLE SEEM LIKE IT WAS LOCKED INTO PLACE AND WOULD NOT MOVE FROM THE GEAR SELECTED DOWN POSITION. COMPLIED WITH SB700-32-07 (LANDING GEAR - REPLACED THE LEFT AND RIGSDR DXTA2025102105355Transducer · faultedRED CAS HYD O' TEMP B MESSAGE CAME ON IN FLIGHT CORRECTIVE ACTION: REMOVED FAULTY HYDRAULIC TEMPERATURE TRANSDUCER ON SYSTEM B RESERVOIR AND REPLACED WITH A CUSTOMER SUPPLIED NEW UNIT. OPS CHECKS AND LEAK CHECKS ARE GOOD AT THIS TIME. ALL WORK DONE IN REFERENCSDR DXTA2025042503196Squat Switch · faultedAFTER POSITIVE RATE PM ATTEMPTED TO RETRACT GEAR. HE COULD NOT GET THE HANDLE TO MOVE. SHORTLY AFTER RECEIVED AN AMBER GROUND DETECT FAULT. THE GEAR WAS NEVER RETRACTED AND STAYED DOWN WITH A THREE GREEN INDICATION AND WAS NEVER RETRACTED. THE 18,000 AND 230 KSDR 2024F00171Access Door · corrodedRH APU ACCESS PANEL (331CR) HAS LEVEL 2 CORROSION AND CRACK AT FASTENER HOLESDR DXTA2023060587880Unknown · unknownON TAKE OFF, UNABLE TO RETRACT THE LANDING GEAR. SEQUENTIALLY "GROUND DETECT FAULT " CAS APPEARED. FERRIED THE AIRPLANE WITH THE GEAR DOWN. USING ARES VIEW TO TROUBLESHOOT THE PROBLEM WITH THE LANDING GEAR NOT RETRACTING ON AIR. FOUND WOW GEAR DISAGREE, LSDR DXTA2023060187590Unknown · unknownMAIN DOOR: CLIMBING THROUGH 13K GOT AMB CABIN ALT. DECENDING TO 13K GOT RED CABIN ALT AND AMBER CHECK DOORS AND CABIN DOOR OPEN. DIVERTED AND LANDED UNEVENTFUL. // SIGNOFF// REVIEWED ARES DATA ON A MAY31ST FLIGHT. VERIFIED DISCREPANCY INFLIGHT AND NOTED AT SDR DXTA2023052687090Unknown · unknownWE HAD TO RESET DOOR 2X, ALSO STIFF TO CLOSE AND STIFF TO OPEN SOMETIMES. PERFORMED CLEANING OF THE INTERIOR DOOR ANDLE RELEASE SWITCH AND MODEL 700 MAINTENANCE MANUAL (REV 9) 52-10-00 (ORIGINAL ISSUE) CABIN DOOR - ADJUSTMENT/TEST, THEN PERFOMRED CABIN DOOR LSDR DXTA2023041183990Unknown · unknownMAIN DOOR HANDLE: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRES INORDINATE STRENGTH TO OPEN IT FROM THE INSIDE AND OUTSIDE OF THE CABIN. TROUBLE SHOT DOOR ISSUE TO DOOR ROTARY SOLENOID INOP GAINED ACCESS TO DOOR HANDLE ASSY. REMOVED AND REPLACED ROTASDR DXTA2023020679960Not Reported · not reportedEMERGENCY LIGHTING: ON PREFLIGHT NONE OF THE EMERGENCY LIGHTS WORK. //SIGNOFF// CHARGED BATTERIES FOR 2 HRS WAITED 1/2 HR AND OPS CHECK LIGHTS WITH GOOD RESULTS, WAITED ANOTHER 1 HR AND HALF AND CHECK LIGHTS WITH GOOD RESULTS. ALL WORK DONE PER CE-700 AMM 33-5SDR DXTA2022120675610Connector · damagedWHEN CLOSING MAIN CABIN DOOR FROM INSIDE AIRCRAFT, HANDLE DOES NOT POSITIVE DETENT AND CABIN DOOR DOOR OPEN AND CHECK DOOR CAS MESSAGES REMAIN DISPLAYED. CHECKLIST ALTERNATE DOOR CLOSING METHOD IS REQUIRED TO PROPERLY CLOSE DOOR. REMOVED CONNECTOR JC027 & NOSDR DXTA2022030357800Wire Harness · damagedCABIN DOOR OPEN AMBER CAS: DEPARTING KAPF-KPTK CLIMBING THEOUGH 2000' WE GOT A AMBER: CABIN DOOR OPEN CASA FOLLOWED BY A CHECK DOORS AMBER CAS. WE STOPPED THE CLIMB AT 5000' AND SLOWED DOWN. CONPLETEE QRH AMBER MESSAGES 21C, 22C. CABIN PRESSURE WAS INCREASINSDR DXTA2021122754120None · noneCABIN EMERG LIGHT: OVERHEAD CABIN EMERGENCY LIGHTS ARE INOP. // SIGNOFF// PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTS AND IS GOOD IRW CE-700 AMM 33-50-00.
Reports on N822QS not matched to an aircraft · 12
They name N822QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTR2014070901Skin · dentedFOUND TWO DENTS IN FUSELAGE SKIN INBD AND FWD OF LT LOWER WING AND CRACK AT DOME NUT. ONE AT BS 254.35, PROTRUDING OUT 0.025" DEEP, 0.35" LONG, 0.20" WIDE, AND THE OTHER AT BS 257.85 DENTED INWARD, 0.025" DEEP, 1.4" LONG, 1.45" WIDE. REPAIR IAW ERO-588981.SDR DXTA2014071405818Rib · crackedRIGHT WING HAS CRACKED RIB IN THE OTBD FLAP WELL WS 133.07. COMPLIED WITH THE RT WING RIB REPAIR IAW THE ERO-555540QC. ACCOMPLISHED EDDY CURRENT INSPECTION OF RT WING TE RIB AT WS 133.07 IAW NDI MANUAL PART-6-20-00-02 IAW ERO-585141-1. NO ADDITIONAL DEFECTSSDR DXTA2014071405817Rib · crackedLEFT WING HAS CRACKED RIB IN THE INBD FLAP WELL WS 79.06. REPAIRED LT WING RIB IN THE INBD FLAP WELL AT WS 79.06 IAW ERO-585141-2 INSPECTED 6. ACCOMPLISHED EDDY CURRENT INSPECTION OF LT WING TE RIB AT WS 79.06 IAW NDI MANUAL PART-6-20-00-02 IAW ERO-585141-2
STCs that may be installed · 11
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 700
STC ST12145SEInstallation of Starlink Aviation SystemSTC ST04736NYTrue Blue TS28 Emergency Battery Power Supply ReplacementSTC ST00415BOInstallation of an NVIS/NVG compatible lighting system and infrared capable exterior lightingSTC ST04575ATInstallation of the Rockwell Collins ALT-1000+/ -4000+ with 5G FilteringSTC ST02812LAInstallation of the Honeywell EDG-100 Connected Engine Data Access SystemSTC ST04572CHInstallation of an Airborne Terminal System and a Ka RadomeSTC ST02746SEInstallation of external aerodynamic modifications, interior furnishings and equipment, including provisions for additional non-essential systemsSTC ST02694SEGroup Reduced Vertical Separation Minimum (RVSM) airworthiness approvalSTC ST04211NYInstallation of of NSM UNIFIS 3000 G2 Flight Inspection SystemSTC ST01971WIInstallation of the Garmin G5000 Software Changes & GH-3900 Standby Configuration UpdatesSTC ST01027DEInstallation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries