- Owner type
- Co-owned, fractional ownership
- Serial number
- 20534
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 19, 2014
- Certificate issued
- August 11, 2026
- Expires
- August 31, 2033
- Mode S code
- AA60AF
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 N768QSMatched 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 N768QSMatched 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 DXTA2025060403725Unknown · odorAFTER STARTING THE APU THE CABIN AND COCKPIT HAD A VERY STRONG ODOR OF WET SOCKS. ARRIVED AT THE AIRCRAFT AND APPLIED APU POWER, ALLOWING THE SYSTEMS TO FULLY BOOT UP. AFTER APPLYING APU BLEED, WE WERE ABLE TO CONFIRM THE REPORTED ODOR DISCREPANCY IN BOTH THSDR DXTA2023092796530Unknown · unknownBAGGAGE DOOR HANDLE: CARGO DOOR HANDLE NEEDS EVALUATION. AMBER CARGO DOOR OPEN CAS ILLUMINATED APPROXIMATELY 700 AGL ON APPROACH. DOOR HANDLE AND PRESSURE DOOR WERE IN OPEN POSITION AFTER SHUTDOWN. //SIGNOFF// CONDUCTED A VISUAL INSPECTION OF THE BAGGAGE DOOR SDR DXTA2023021380360Unknown · unknownPROX SYS FAULT CYAN CAS: CYAN PROX SYS FAULT ILLUMINATED PRIOR TO ENGINE START B3-007472 MAIN CABIN DOOR WILL NOT FULLY OPEN OR CLOSE. //SIGNOFF// PERFORMED GVI OF DOOR NOTING WHEN THE INNER DOOR HANDLE WAS MOVED, IT FELL FURTHER TOWARDS THE OPEN POSITION ABOUSDR DXTA2016092406307Door Seal · crackedLOST COMPLETE CABIN PRESSURE AT FL430. REPACKED ALL CREW AND CABIN O2 MASK IAW MM 35-21-01. PERFORMED PRESSURIZATION CHECK OF AIRCRAFT ON GROUND TO 7.3 PSID. NO ABNORMALITIES NOTED. REMOVED OLD CABIN DOOR SEAL IAW MM 52-11-09. INSTALLED NEW CABIN DOOR SEAL IAWSDR DXTA2016010406150Wheel · failedONE HOUR INTO THE FLIGHT AT FL 400, THE CYAN, LT HYD ENG PUMP FAIL, CAS MSG ILLUMINATED. THE HYD SYNOPTIC SHOWED 0% FLUID LEVEL. 10 MINS LATER THE AMBER, LT HYD PRESS LOW, CAS MSG ILLUMINATED, FOLLOWED BY THE AMBER, SPOILER FAULT & CYAN LT ENG FAULT. WE FOL
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