- Owner type
- Co-owned
- Serial number
- 20666
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 23, 2017
- Certificate issued
- September 29, 2026
- Expires
- September 30, 2033
- Mode S code
- A9C2B3
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 N728QSMatched 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 N728QSMatched 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 DXTA2025071604240Door · bindingCOMPLETED A FLIGHT AND WHILE OPENING THE MAIN CABIN DOOR NOTICED HANDLE WAS LIGHLY STIFF & THEN LIGHTLY POPPED UP AND WAS WORKING. THOUGHT IT WAS PERHAPS "USER ERROR". WE THEN VERIFIED BY OPENING AND CLOSING THE DOOR A FEW TIMES TO SEE IF IT COULD BE DUPLICASDR DXTA2025063004069Trim System · faultedLEFT BASE, FLAPS 20, RECEIVED AMBER AP STAB TRIM FAIL. PER QRH TURNED AUTOPILOT OFF & FLEW APPROACH TO LAND. DID HAVE TROUBLE PUSHING PLANE NOSE DOWN AFTER ADDING FLAPS 30 AND ALL THE WAY TO LANDING. PLANE HAS HAD RECENT WRITE UP FOR PRIMARY FLIGHT CONTROLS ISDR DXTA2024110401018Electronic Unit · defectiveFLT SPOILERS FAULT AMBER CAS: CLIMB INF THROUGH FL330 AT 270 KNOTS WITH THE AUTOPILOT ENGAGED, A MOMENTARY ROLL MOVEMENT OCCURRED, FOLLOWED BY A YELLOW SPOILERS FAULT, CYAN STAB TRIM FAULT CAS MESSAGES, AS WELL AS SPOILER PANELS 2&7 YELLOW ON THE FLIGHT CONTROSDR DXTA2023110399620Pump · brokenAT ALTITUDE, HEARD A GRINDING NOISE WHICH LASTED FOR ABOUT 5 SECONDS COMING FROM BACK OF AIRPLANE. WAS FOLLOWED WITH A LT, HYD PUMP, FAIL, CASS MESSAGE. PULLED UP SCHEMATIC & COULD SEE THE FLUID WAS DRAINING FROM LT HYDC SYS WHEN FLUID REACHED 0 GOT A AMBER LTSDR DXTA2023031482550Unknown · unknownEMERGENCY EXIT DOORS: DURING FLIGHT THE EMERGENCY EXIT LIGHTED PYRAMID SIGN CAME OFF AND A PAX REPLACED IT UPSIDE DOWN RESOLUTION: REMOVED EMERGENCY EXIT SIGN AND FLIPPED IT UP RIGHT AND THEN RESECURED SIGN TO WALL. WORK DONE IN REF TO CL350 AMM 33-51-00SDR DXTA2022062464540None · noneMAIN DOOR: MAIN CABIN DOOR WILL NOT CLOSE. WHEN IT GETS TO THE TOP IT SEEMS TO BIND. // SIGNOFF// DISCONNECTED CABLE AND SPERATED ACTUATOR AND CABLE REEL. FOUND CABLE REEL TO BE EXTREMELY DIRTY. CLEANED
UP CABLE REEL, REATTACHED DOOR CABLE REEL AND CABLE AND SDR DXTA2022060163110None · noneEMERGENCY LIGHTS WILL NOT TURN OFF
Reports on N728QS not matched to an aircraft · 15
They name N728QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2013042905364Uplock Switch · failedAFTER SELECTING GEAR UP THE LT GEAR INDICATION SHOWED RED HASH LINES. THE ACFT DID FEEL LIKE THE GEAR WAS DOWN. NO DRAG OR PULL TO ONE SIDE. WE CYCLED THE GEAR 3X DID NOT FIX THE PROBLEM. JACKED A/C AND SWUNG GEAR SEVERAL TIMES. VERIFIED DISCREPANCY. DISCONSDR DXTA2011110304771Power Unit · malfunctionedDURING APPROACH, SELECTED FLAPS 12 & SLATS DOWN. SLATS & KRUEGERS CAME DOWN NORMALLY BUT FLAPS DID NOT & RECEIVED A SLAT/FLAP MAINT EICAS MESSAGE. AFTER LANDING, FLAPS/SLATS AND KREUGERS ALL RECTRACTED NORMALLY. TROUBLESHOT FLAP SYS TO PDU. REMOVED FLAP PDSDR DXTA2011060204601Windscreen · crackedRIGHT WINDSCREEN OUTER PANE CRACKED IN A SPIDER WEB FASHION WHILE FLYING AT FL 400. R & R RT WINDSCREEN IAW MM 56-10-05. OPS AND LEAK CHECKED GOOD.
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