- Owner type
- Corporation
- Serial number
- 20595
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 19, 2015
- Certificate issued
- May 4, 2026
- Expires
- May 31, 2033
- Mode S code
- AAABF6
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 N787QSMatched 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 N787QSMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2024091600529A/C Pack · failedACM: OM LANDING WHEN THE APU WAS TURNED ON WE NOTICED A SMELL, THEN A HAZE DEVELOPE IN THE CABIN. ALSO THERE WAS A LOUD SQEAL COMINF FRON THE AC VENTS. THEN WE RECEIVED THE AMBER "PACK TEMP HIGH" MESSAGE. CORRECTIVE ACTION: REMOVED AND REPLACED ACM. REFERENCE SDR DXTA2023080792310Apu · defectiveAFTER LANDING THE APU WAS STARTED, SHORTLY AFTER THE BLEEDS WERE CONFIGURED FOR APU AIR USE (AS WE PULLED ONTO THE PARKING AREA) THE COCKPIT AND CABIN FILLED WITH SMOKE (FROM THE GASPER VENTS). THERE WAS NO ASSOCIATED APU FIRE INDICATION. REMOVED AND REPLACEDSDR DXTA2023071791020Unknown · unknownWHILE IN CRUISE AT FL230 IN CRUISE POWER SETTING, ICE DETECTED CAS MESSAGE DISPLAYED. AFTER TURNING ON ANTI-ICE, GOT RED WING ANTI-ICE LEAK CAS MESSAGE. FOLLOWED BY AMBER L(R) WING ANTI-ICE FAIL CAS MESSAGES & CYAN L(R) ENG THRUST FAULT CAS MESSAGES. QRH DIRECSDR DXTA2016011806166Rvdt · failedAT 43000' THERE WAS A PRONOUNCED DUTCH ROLLING. ALSO YOKE KEPT GOING LEFT - RIGHT. DESCENDED TO 38000, STILL ROLLING. DESCENDED TO 31000, STILL OCCURRING. THRU 33000 YAW & ROLL PRONOUNCED. DIDN'T SETTLE UNTIL MID-TEENS. WHEN YOU HIT ANY TURBULENCE IT WOU
Reports on N787QS not matched to an aircraft · 5
They name N787QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200601615Link · wornAFTER TAKEOFF GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CHECKED SYSTEM FOR PROPER OPERATION, COULD NOT DUPLICATE. CHECKED NOSE SQUAT SWITCH FOUND NOSE CENTERING LINK ASSY NOT GRABBING CENTERING SWITCH TO ACTUATE PROPERLY. REMOVED AND REPLACED NOSE CENTSDR DXTA200501018Control Panel · hotBURNT WIRING SMELL WAS NOTICED AFTER ENGINE SHUTDOWN. HEADING AD SELECTION CONTROL PANEL WAS EXTREMELY HOT SO COMPLETE SHUTDOWN WAS INITIATED. - TROUBLESHOT TO BAD REMOTE INSTRUMENT CONTROLLER, REPLACED BAD R.I.C. IAJ CE 650MM CH 34-21-00 + OPS CHECK GOOD.SDR DXTA200400224Line · contaminatedDURING TAKEOFF WITH MAX TAKEOFF POWER APPLIED, THE RIGHT RUDDER PEDAL WENT FULL FORWARD POSITION, TAKEOFF WAS ABORTED. TROUBLESHOT AND FOUND LINE GOING TO RUDDER BIAS ACTUATOR HAD FROZEN MOISTURE IN IT. REMOVED LINE AND PURGED MOISTURE, REINSTALLED LINE, OPS
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