- Owner type
- Co-owned
- Serial number
- 21122
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- July 23, 2026
- Expires
- July 31, 2033
- Mode S code
- A988A1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 54
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2006 | 1 |
|---|---|
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 5 |
| 2018 | 3 |
| 2019 | 3 |
| 2020 | 3 |
| 2021 | 6 |
| 2022 | 5 |
| 2023 | 9 |
| 2024 | 8 |
| 2025 | 1 |
| 2026 | 3 |
Airframe · Bombardier BD-100-1A10
AD 2026-13-02NavigationAD 2026-02-06Flight controlsAD 2026-01-07Time Limits/Maintenance ChecksInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Bombardier BD-100-1A10
SAIB AIR-22-02R1Pitot/Static Anti-Ice SystemSAIB NM-18-32R1Electrical Power - Direct Current Power CenterNTSB investigations
No NTSB investigations matched to N713QSMatched 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-100-1A10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N713QSMatched 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-100-1A10 aircraft
Service difficulty reports · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
Reports on N713QS not matched to an aircraft · 9
They name N713QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200702072Engine · malfunctionedLEFT ENG ROLLED BACK TO 91% N1 ON T/O ROLL (APROX 80 KNOTS). T/O ABORTED. INSP EEC FOR FAULTS NONE NOTED. RAN A/C AT ALL POWER SETTINGS IN AUTO & MANUAL MODES. NO ROLL BACK NOTED SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME ALL WORK DONE IAW CE 650 M/M 76-10-0SDR DXTA200601245Gearbox · frozenFLAPS INOP, WOULD NOT EXTEND. FLAP INOP LIGHT ILLUM, WOULD NOT RESET. CHK`D FLAP CONTROLLER. NONE FOUND GAINED ACCESS TO FLAP PDU. DISCONNECTED RT FLAP DRIVE CABLE FROM PDU. UPON REMOVAL, DRIVESHAFT OF FLEX CABLE REMAINED IN PDU & CABLE SEPARATED FROM PDU.SDR DXTA200500713Indicator · inoperativeLT GEAR ANNUNCIATOR FAILED TO LIGHT DURING GEAR EXTENSION (OR ROTORY TEST) BLEW GEAR DOWN USING CHECK LIST PROCEDURE. DURING ROLL OUT (L) SIDE GEAR BEGAN SMOKING. FOUND LT LANDING GEAR INDICATOR PULLED LOOSE IN ITS SOCKET. RESET INDICATOR AND PERFORMED LAND
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