- Owner type
- Co-owned, fractional ownership
- Serial number
- 20554
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 28, 2015
- Certificate issued
- December 1, 2025
- Expires
- December 31, 2032
- Mode S code
- AA7952
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 N774QSMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025111105649Bolt · brokenAS US CUSTOMS AGENT WALKED DOWN THE AIRSTAIR, THE FORWARD AIRSTAIR DOOR GAS STRUT BROKE OFF THE ATTACH POINT OF THE DOOR. IT APPEARS THE BOLTS SHEERED OFF. EXTRACTED BROKEN HARDWARE AND VERIFIED NO FURTIIER DAMAGE NOTED. INSTALLED NEW HARDWARE AND OPS CHECKED SDR DXTA2025032502781Structure · no discrepancyWHILE IN CRUISE FLIGHT WITH FLAPS RETRACTED AND GEAR RETRACTED, IN SMOOTH AIR, WE EXPERIENCED SEVERE MOUNTAIN WAVE. WITH THROTTLES AT IDLE & SPEED BRAKES FULLY DEPLOYED WE ACCELERATED BEYOND MMO (.83) TO MACH .86 AND CLIMBED OVER 500' IAW AMM 05-51-09-210-8SDR DXTA2024112001174Bolt · damagedENTRANCE STAIR GAS STRUT: LEFT SIDE ENTRANCE STAIR FORWARD STRUT HAS SHEARED OFF AT THE TOP HINGE POINT ARRIVED AT AC. CONFIRMED DISCREPANCY. PREPPED AC FOR MAINTENANCE. REMOVED SHEARED BOLT AS REQUIRED. INSPECTED FUSELAGE TELESCOPING STRUT, FUSELAGE ANCHOR POSDR DXTA2024052811894Acm · smokeAFTER LANDING WE SMELLED AN UNUSUAL SMOKE SMELL BUT THOUGHT IT WAS FROM OUTSIDE. AFTER STARTING APU AND SELECTING AIR SOURCE ON, NOTICED UNUSUAL SOUND AND SMOKE BOTH IN COCKPIT AND CABIN. SOON AFTER, CAUTION PACK TEMP HIGH CAS MESSAGE DISPLAYED. WE COMPLIED SDR DXTA2021090348120Engine · damagedRIGHT ENGINE ENGINE COMPRESSOR STALL: ON ROTATION FOR TAKEOFF A SCRAPING SOUND WAS HEARD FROM THE RIGHT SIDE OF THE AIRCRAFT. IT WASN'T A SOUND I HAD HEARD BEFORE IN THIS AIRPLANE. AFTER THE FACT, THE OWNER COMMENTED SHE HEARD TWO DISTINCT POPS AT THAT TIME. I
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