- Owner type
- Co-owned, fractional ownership
- Serial number
- 20801
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 26, 2019
- Certificate issued
- July 23, 2026
- Expires
- July 31, 2033
- Mode S code
- A95D6B
Bombardier BD-100-1A10TCDS T00005NYAirframe · Bombardier BD-100-1A10TCDS E00010LAEngine · Honeywell AS907-2-1A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
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 | 4 |
| 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 N702QSMatched 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 N702QSMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025112605823Cable · failedMAIN DOOR CABLE HAS SNAPPED. MAIN DOOR UNABLE TO BE CLOSED USING EITHER THE ELECTRIC MOTOR OR STANDBY PULL HANDLE AT TOP OF STAIRS. REMOVED BROKEN MAIN CABIN DOOR CABLE AND INSTALLED AS RECEIVED NEW MAIN CABIN DOOR CABLE. OPS CHECKS GOOD WITH NO OTHER DEFECTSDR DXTA2025021902419Handle · failedMAIN DOOR HANDLE: WHEN THE MAIN DOOR IS IN THE OPEN POSITION AND WEIGHT IS APPLIED ON THE STEPS, THE DOOR MOVES DOWN FARTHER AND BOTTOMS OUT AND HITS AND RESTS ON THE FUSELAGE. DUE TO DOOR CATCH FAILURE DOOR OVER EXTENDED AND CAME IN CONTACT WITH FUSELAGE REQUSDR DXTA2023102398500Door Latch · faultedMAIN CABIN DOOR WILL NOT COME ALL THE WAY DOWN TO THE BOTTOM OF ITS ALLOWABLE TRAVEL. AFTER OPENING THE DOOR, AND GETTING TO THE BOTTOM OF THE STEPS, THE DOOR HAS A LOUD AUDIBLE POP, AND THE DOOR SETTLES THE REST OF THE WAY, ABRUPTLY, CAUSING THE BOTTOM OF THESDR DXTA2023070390270Actuator · defectiveMAIN CABIN DOOR WILL NOT CLOSE USING MOTOR. JERKS & SHIMMIES, AND WHEN IT WILL BEGIN TO CLOSE IT GETS TO ABOUT 3/4 CLOSED AND MOTOR CAN NO LONGER RAISE DOOR. BEGAN REMOVAL OF LH CLOSET BY REMOVING TRIM AND DOOR ENTRY HEADLINER, IAW S.M.M. 25-24-05. R & R PASDR DXTA2022041960660None · leakingBLEED AIR: CABIN AIR HAS A VERY STRONG MUSTY SMELL, PARTICULARLY IN HUMID CONDITIONS. /// CORRECTIVE ACTION /// BORESCOPE INSPECTED APU COMPRESSOR SEAL. FOUND VERY SOOTY AND EVIDENANCE OF OIL LEAKING. REMOVED AND REPLACED APU. OPS AND LEAKS CHECKS GOOD, NO DEF
Reports on N702QS not matched to an aircraft · 15
They name N702QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2014100605906Engine · leakingDURING LANDING & FLIGHT IDLE HAD AN ODOR IN THE COCKPIT. TOWER ADVISED THE RT ENGINE WAS SMOKING. THE SMOKE DISSIPATED INSIDE & WAS NO LONGER VISIBLE TO THE TOWER. REPLACED THE RT ENGINE DUE TO INTERNAL OIL LEAK & SMOKE IN THE CABIN. PERFORMED SATISFACTOSDR DXTA2012062805021Eec · inoperativeIN FLIGHT, RECEIVED FADEC FAULTY ICAS MESSAGE AND EICAS COMPARITOR FAIL WITH YELLOW DASH LINES IN ITT. ABOUT 5 MINUTES LATER, FELT A LIGHT SHUTTER ASSOCIATED WITH THE ENGINE ROLLING BACK AND FAILED. AFTER ABOUT 30 SECONDS, ENGINE AUTO LIGHTED. NO ABNORMAL VSDR DXTA2011051004575Brake Assy · defectiveDURING APPROACH, PBI BRAKES APPLIED BY LT SEAT PILOT, & ON TOUCHDOWN BRAKES DID NOT SEEMS TO CATCH. FEEL THAT WAY AT TIMES AS THRUST REVERSERS ARE DEPLOYING ON THIS TYPE ACFT, AT ABOUT 70 KNOTS LT SEAT ASKED RT SEAT TO APPLY BRAKES, DIDN'T SEEM TO CATCH. P
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