- Owner type
- Co-owned, fractional ownership
- Serial number
- 20655
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 23, 2016
- Certificate issued
- June 2, 2026
- Expires
- June 30, 2033
- Mode S code
- AAD72C
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 N798QSMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2025FA0000200Skin Panel · corrodedCORROSION FOUND AT FS 779 THAT WAS CLASSIFIED AS LEVEL 2 AND A REPAIR WAS REQUIRED.SDR 2025FA0000199Skin Panel · corrodedCORROSION FOUND AT FS 779 THAT WAS CLASSIFIED AS LEVEL 2 AND A REPAIR WAS REQUIRED.SDR 2025FA0000161Support Bracket · corrodedFUSELAGE FAIRING SUPPORT AND STRAP HAVE CORROSION PRESENT IN MULTIPLE LOCATIONS OF VARYING THICKNESSES.SDR 2025FA0000159Support Strap · corrodedCORROSION FOUND ON THE BOTTOM OF THE LOWER STRAP FOR THE LOWER FUSELAGE FAIRING AT FS 707SDR DXTA2023111510058Unknown · unknownMAIN DOOR HANDLE: MAIN PAX DOOR HANDLE, ON THE INSIDE VERY DIFFICULT TO OPEN. ITS BINDING UP ENOUGH SOME PEOPLE CANNOT FULLY PUSH THE HANDLE UP. //SIGNOFF// CLEANED AND LUBRICATED CABIN DOOR LINKAGE AND OPEN LOCK LEVER IAW CL-350 A.M.M. 12-22-00 . DOOR OPERATESDR DXTA2023070390220Unknown · unknownMAIN DOOR: MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN AND CLOSE FROM INSIDE AND OUTSIDE OF THE AIRCRAFT.//CORRECTIVE ACTION//OPERATED MAIN CABIN DOOR AND DUPLICATED DISCREPANCY. INSPECTED DOOR AND SURROUNDING AREA. FOUND THE MAIN CABIN DOOR CURTAIN INCORRECTLTY
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