- Owner type
- Co-owned, fractional ownership
- Serial number
- 9480
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 21, 2012
- Certificate issued
- October 18, 2023
- Expires
- October 31, 2030
- Mode S code
- A00623
Bombardier BD-700-1A11TCDS T00003NYAirframe · Bombardier BD-700-1A11TCDS E00057ENEngine · Rolls-Royce Deutschland BR700-710A220
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 71
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1999 | 1 |
|---|---|
| 2001 | 2 |
| 2003 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 4 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 6 |
| 2017 | 4 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 5 |
| 2022 | 4 |
| 2023 | 10 |
| 2024 | 4 |
| 2025 | 7 |
| 2026 | 6 |
Airframe · Bombardier BD-700-1A11
AD 2026-15-09Landing GearAD 2026-11-07Equipment/furnishingsAD 2026-13-02NavigationInformation bulletins that may apply · 3
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N100QSMatched 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 Bombardier BD-700-1A11 aircraft
FAA incident reports
No FAA accident or incident reports matched to N100QSMatched 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 Bombardier BD-700-1A11 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026060408300Fmu · failedWHILE DESCENDING, AT APROX FL340 THE CREW OBSERVED 2 LARGE BANGS SOUNDED LIKE COMPRESSOR STALLS. FLT ATTENDANT NOTED BANGS LOUDER IN BACK THAN WHAT PERCEIVED IN FRONT. AFTER LOUD BANGS, RT FADEC FAIL MESSAGE WAS ILLUMINATED. FOLLOWED THAT CHECKLIST WHILE TUSDR DXTA2025061003800Tire · explodedMLG: LEFT OUTBOARD MAIN TIRE #1 EXPLODED DURING TAXI INTO RAMP. REPLACED BOTH LH IB AND LH OB MLG WHEEL/TIRE ASSEMBLIES IAW BOMBARDIER GL-5000 GVFD AMM 32-41-01.SDR DXTA2025011301901Door · out of alignmentMAIN DOOR: UPON CLOSING MAIN CABIN DOOR CREW NOTICED HANDLE ALINGMENT RED STRIPES NOT ALIGNED, AND SOLENOID TYPE NOISE ACTUATING ABNORMALLY LATE, NO CAS MESSAGES RELATED TO THE MAIN CABIN DOOR. INSTALLED PLACARD. OPS CHECK GOOD. IAW GL5000 MM 52-11-00.SDR DXTA2024102100895Actuator · defectiveNLG: NOSE STEER FAIL CAS MESSAGE CAME ON AFTER LANDING GEAR EXTENSION. ECL CHECKLIST PROCEDURE ACCOMPLISHED BUT MESSAGE PERSISTED, SYSTEM TURNED OFF FOR LANDING. ATEMPTED A RESET ON GROUND AFTER VACATING RUNWAY BUT STILL NO STEERING. HARD FAIL. CORRECTIVE ACTSDR DXTA2024073000028Door · malfunctionedWITH APU RUNNING. WHEN MAIN CABIN DOOR IS BEING CLOSED IT STARTS TO RAISE AND THEN QUITS AND GOES BACK DOWN. THIS HAPPENED MULTIPLE TIMES BEFORE FINALLY CLOSING. FEELS LIKE THE MOTOR IS GETTING WEAK .SDR DXTA2023082994150Seal · defectiveEMERG EXIT DOOR: REPEAT WRITE UP. AFTER TAKEOFF DURING INITIAL CLIMB, EMERGENCY EXIT MADE LOUD HISSING, BUZZING, HORN SOUNDING NOISES. NOISE WENT AWAY AFTER WE CLIMBED THROUGH ABOUT 15,000 FEET. GAINED ACCESS LO OVER-WING EMERGENCY EXIT DOOR LO LUBRICATE THE SDR DXTA2021011104583Switch · defectiveMAIN ENTRY DOOR AUTO SWITCH INSIDE AND OUT WORKS INTERMITTENTLY. MANUAL SWITCH ON OUTSIDE WORKS FINE. POWERED UP AIRCRAFT AND DUPLICATED SQUAWK, CHECKED GALLEY TOUCHSCREEN CONTROLLER AND FOUND ACTIVE FAULT "RDE 1 FAILED OR FAILED WIRING" RESET RDE 1 BREAKERSDR DXTR2020012001Hydraulic Line · chafedNR 1 HYD PRESS LINE IS LOOSE AND WORN WERE IT PASSES THRU BRACKET COMING FROM ENGINE IN AFT SERVICE BAY. REMOVED NR 1 HYDRAULIC PRESSURE LINE P/N GD478-1102-11 AND NR 1 CASE DRAIN HYDRAULIC LINE P/N GD478-1103-5 SPM 20-22-00. REMOVED THE LT BRACKET ASSEMBLY P/SDR JGVR2018101900000Windshield · crackedWITHIN 24 HOURS AFTER REPAIR OF THE RIGHT WINDSHIELD "HUMP SEAL" IN ACCORDANCE WITH MAINTENANCE MANUAL PROCEDURE, THE WINDSHIELD CRACKED. THE CRACK SLOWLY PROPAGATED ACROSS THE WINDSHIELD.SDR DXTA2018032400770Warning Message · false activationRIGHT MAIN INBOARD TIRE BLEW ON LANDING. 'UNCOMMANDED BRAKE' MESSAGE FOLLOWED BY ' BRAKE 50%DEGRADED' MESSAGE. TROUBLESHOT THE RT MLG NR 3 BRAKE MESSAGE IAW QMS IAW AMM 45-47-00. A GENERAL VISUAL INSPECTION WAS COMPLIED WITH IAW AMM 05-51-06. NO DEFECTS WHERSDR WVER835K060720151Skin · dentedDENT ON LT NOSE FUSELAGE SKIN LOCATED BETWEEN FS 185.00 & FS 193.00, 2" BELOW STRINGER 23. DENT IS .026"D X 2.75"L X 1.25"W.
STCs that may be installed · 141
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 141 STCs