- Owner type
- Co-owned, fractional ownership
- Serial number
- 20663
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 20, 2016
- Certificate issued
- July 21, 2025
- Expires
- July 31, 2032
- Mode S code
- A9B78E
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 N725QSMatched 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 N725QSMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025063004060Warning Light · false activationDURING CLIMB OUT, THE GEAR WARNING HORN ACTIVATED WITH THE ASSOCIATED RED GEAR INDICATOR LIGHTS. THE GEAR INDICATION DID NOT EXTINGUISH. WE CYCLED THE GEAR AND THE GEAR INDICATION AND HORN EXTINGUISHED. CORRECTIVE ACTION; PERFORMED GEAR SWING OF THE LANDING SDR DXTA2025032602797Skin · dentedFOUND A SMALL DENT ON THE LH LOWER PYLON TRAILING EDGE SKIN. THE DENTS DEPTH IS MEASURED AT -.031. MAX ALLOWABLE LIMIT IS -.100.SDR 2025FA0000114Skin · corrodedDURING AN INSPECTION FOUND CORROSION AROUND FASTENER HOLES ON THE LOWER FUSELAGE AFT SECTION AT FS 779 LH STRINGER 21L AND AT FS 779 AT THE CHIN FAIRING FASTENER HOLE.SDR DXTA2024111501150Trim System · faultedPRI STAB TRIM FAIL AMBER CAS: IN LEVEL FLIGHT WITH AUTO PILOT ENGAGED WE GOT AN AMBER PRIMARY STAB TRIM FAIL CORRECTIVE ACTION; ARRIVED AT AC, APPLIED POWER AND ALLOWED SYSTEMS TO POWER UP. GAINED ACCESS TO MDC AND CONFIRMED HORIZONTAL STAB TRIM FAULT IN FAULTSDR DXTA2024092200593Flow Valve · corrodedBLEED LOOP FAULT CYAN CAS: AT 43000FT CYAN BLEED LOOP FAULT CAS MESSAGE FOLLOWED SHORTLY AFTER WITH A RED PACK LEAK MESSAGE. FOLLOWING CHECKLIST WE DESCENDED AND AT AROUND 30000FT RED CABIN ALTITUDE ILLUMINED CAUSING PAX O2 MASKS TO DEPLOY. CORRECTIVE ACTION:SDR DXTA2024032811325Valve · defectiveDUE TO INBRD BRAKE FAIL AMBER CAS ILLUMINATING, R & R INBD BCV IAW AMM 32-43-09. OPS/LEAK CHECKED GOOD. DUE TO INBRD BRAKE FAIL AMBER CAS ILLUMINATING, R & R LT INBD BRAKE PRESSURE TRANSDUCER IAW AMM 53-63-09. OPS/LEAK CHECKED GOOD. DUE TO FIRE SYS FAULT ILLUSDR DXTA2023052587050Unknown · unknownDURING CRUISE, AT FL410 AMBER ELECTRICAL FAULT EICAS ILLUMINATED W/BOTH BATTERIES & BOTH GENS SHOWING FAILED & OFFLINE. FAILURE LASTED FOR MINUTES THEN EXTINGUISHED & RETURNED TO NORMAL. OCCURED AT LEAST 3 TIMES IN FLT & AGAIN DURING LANDING. CREW FOLLOWED U
Reports on N725QS not matched to an aircraft · 12
They name N725QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2014012805628Structure · damagedTHE MAIN ENTRANCE DOOR AFT LOWER CORNER IS BENT INWARD & SOME PAINT & PRIMER APPEARS TO BE CRACKED OR MISSING. THE DOOR IS 0.168 OUT OF CONTOUR AT THE DEEPEST POINT. ACCOMPLISHED REPAIR TO LOWER AFT CORNER OF MAIN ENTRANCE DOOR. PERFORMED OPERATIONAL & PRESSDR DXTA2013101405542Strut · failedALL PROBE HEAT INOPERATIVE, COMES ON WHEN OVERRIDE IS SELECTED. TROUBLESHOT TO A FAULTY NOSE GEAR STRUT NOT FULLY EXTENDING. REMOVED AND REPLACED NOSE LANDING GEAR SHOCK STRUT ASSEMBLY IAW CMP 322016, 322002. OPS AND LEAK CHECKED GOOD.SDR DXTA2013022805300Receptacle · failedCABIN MONITORS CIRCUIT BREAKER POPPED. LIGHT ACRID ODOR WAS NOTED IN CABIN. CABIN MONITORS CIRCUIT BREAKER WILL NOT RESET. REMOVED DEFECTIVE LT NR 2 CABIN SEAT MONITOR BASE RECEPTICLE. INSTALLED REPAIRED RECEPTICLE. PERFORMED OPS CHECK AND TESTED NORMAL. NO
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