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N726QS

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2016 Bombardier BD-100-1A10 · Honeywell AS907-2-1A

Open in FAA registry

Owner type
Co-owned, fractional ownership
Serial number
20659
Year built
2016
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
December 13, 2016
Certificate issued
June 17, 2026
Expires
June 30, 2033
Mode S code
A9BB45
Bombardier BD-100-1A10Airframe model · 8 seats · 2 engines · 874 registeredTCDS 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.

2006In forceSuperseded2026
See all 61 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

Historical bulletins · 2
SAIB AIR-22-02Pitot/Static Anti-Ice SystemIssued Feb 25, 2022SAIB NM-18-32Electrical Power - Direct Current Power CenterIssued Dec 3, 2018

NTSB investigations

No NTSB investigations matched to N726QSMatched 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.

Incident 20211110022202ITaxi · Albany, NYWhile taxing to runway 01, the left wing of EJA726 (N726QS) struck N333WC while in the non-movement area causing damage to the left wingtip on N726QS and a scrape just below the APU exhaust on N333WC. N333WC was parked on the non-movement area with no one in…Nov 10, 2021 · Minor damage

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR DXTA2026041307591Outflow Valve · defectiveIN CRUISE AT FL410, WE GOT A "AUTO PRES FAIL" EICAS MESSAGE. IMMEDIATELY STARTED A DECENT TO A LOWER ALTITUDE AND RAN CHECKLIST BUT THE CABIN PRESSURE WOULD NOT RESPOND TO MANUAL INPUTS. THE CABIN WAS CLIMBING AT ABOUT 4400FPM AT THIS POINT SO WE WENT ON O2 Apr 9, 2026 · N726QS · Bombdr BD1001A10 · Pressure Regulator/Outflow ValveSDR DXTA2025013002160Connector · disconnectedEMERG EXIT SIGN/LIGHT: SIDEWALL MOUNTED EMERGENCY EXIT LIGHT JUST FORWARD OF EMERGENCY EXIT IS NOT ILLUMINATING. CORRECTIVE ACTION: RESECURED CONNECTION OF LIGHT ASSY. OPS CHECK GOOD. IAW CL-350 SMM 33-50-01Jan 29, 2025 · N726QS · Bombdr BD1001A10 · Light System WiringSDR DXTA2022120775760Line · leakingGEAR DISAGREE AMBER CAS: ON TAKEOFF, GEAR WAS SELECTED UP AND GEAR DISAGREE AMBER CAS MESSAGE ILLUMINATED. GEAR REMAINED INDICATED 3 GREEN W/ NO ASSOCIATED IN TRANSIT OR RED WARNINGS. CREW RAN QRH, EXTENDED GEAR NORMALLY. REMOVED LEAKING RT MLG SIDE STAY HYDDec 7, 2022 · N726QS · Bombdr BD1001A10 · Hydraulic System, MainSDR DXTA2022120675650Handle · faultedENTRANCE STAIR: MAIN DOOR WHEN STEP ON TO THE STAIRS THE RED HANDLE RETRACTS TO THE MID POSITION CAUSING THE DOOR TO DROP. UNSTABLE CONDITION. THE MAIN CABIN DOOR WILL NOT CLOSE WITH THE HANDLE IN THAT POSITION . YOU WOULD HAVE TO PUSH THE HANDLE FWD TO CLOSE Dec 6, 2022 · N726QS · Bombdr BD1001A10 · Passenger/Crew DoorsSDR DXTA2020123004535Strut · defectiveAFTER BLOCK IN, WITH DELTA P AT 0 (ZERO), MAIN CABIN DOOR WOULD NOT OPEN. TOP OF DOOR STARTS TO SEPARATE FROM AIRFRAME. APPLIED SOMEWHAT MORE FORCE THAN NORMAL WITHOUT DOOR CONTINUING TO OPEN. WE WERE ABLE TO SAFELY OPEN THE MAIN CABIN DOOR AND DUPLICATED TDec 29, 2020 · N726QS · Bombdr BD1001A10 · Passenger/Crew Doors
Reports on N726QS not matched to an aircraft · 7

They name N726QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR DXTA2012110105126Oil System · leakingCLIMBING THRU 38,000 FEET TO 39,000, RECEIVED A RT ENGINE LOW OIL PRESSURE INDICATION. RAN CHECK LIST AND SHUTDOWN THE ENGINE IAW CHECK LIST. CHECKED ENGINE OIL PRESSURE IT WAS 0. LANDING WAS UNEVENTFUL ON POST FLIGHT NOTICED OIL LEAKING FROM THE ENGINE COOct 31, 2012 · N726QS · Gulstm 200 · Turbine Engine Oil SystemSDR DXTA2012031404919Receptacle · damagedON THE GROUND WITH APU RUNNING, POWERED UP THE PERSONAL VIDEO MONITORS TO DISPLAY THE AIRSHOW. AFTER ABOUT 3 TO 5 MINUTES, NOTICED THE MONITOR AT SEAT NR 2 POSITION FLICKERED, THEN WENT BLANK AND IT BEGAN TO EMANATE AN ELECTRICAL BURNING ODOR FROM CONNECTIONMar 13, 2012 · N726QS · Gulstm 200 · Communications System WiringSDR DXTA2010101804263Rudder Control · malfunctionedUNCOMMANDED RUDDER TRIM MOVEMENT IN FLIGHT. RUDDER MOVES FROM 1 UNIT RT TO 1 UNIT LT WITH A CORRESPONDING CHANGE IN ACFT COORDINATION.Oct 15, 2010 · N726QS · Gulstm 200 · Rudder Control System

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