- Owner type
- Co-owned, fractional ownership
- Serial number
- 20607
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 26, 2016
- Certificate issued
- June 18, 2026
- Expires
- June 30, 2033
- Mode S code
- AAAFAD
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 N788QSMatched 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 N788QSMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026081209211Acm · faultedON CLIMB OUT, NOTICED A WHISTLING NOISE, FOLLOWED BY A UNDESCRIBABLE ODOR. FOLLOWED BY HOT AIR COMING OUT OF THE AIR-CONDITIONING. ON THE ECS PAGE THE ONLY ABNORMALITY WAS THE SUPPLY LINES WERE 61 AND 65 DEGREES. REMOVED FAULTY ACM P/N OFF 3471A020000 S/N OFFSDR DXTA2025060403729Acm · failedAFTER LANDING DURING ROLL OUT WE SMELLED AN ODOR THAT SMELLED LIKE SMOKE & HAD A DIRTY SOCK SMELL. WE HAD VISIBLE SMOKE IN CABIN. APU WAS NOT ON AT THIS TIME. DURING TAXI WHILE APU WAS BEING STARTED RECEIVED AN AMBER PACK TEMP HIGH MSG. ARRIVED AIRCRAFT &SDR DXTA2025013102148Oil System · lowR ENG OIL PRESS LOW CAS: ON CLIMBOUT, RIGHT ENGINE OIL PRESSURE LOW RED CAS ILLUMINATED WITH AN ASSOCIATED OIL PRESSURE INDICATION OF 41 PSI. FOLLOWED QRH AND PERFORMED PRECAUTIONARY SHUT-DOWN OF RIGHT ENGINE DUE TO CONTINUED DECREASE IN OIL PRESSURE. LANDED SDR DXTA2024101800876Ecs · contaminatedAFTER ENGINES STARTUP HAD BURNT ACIDIC SMELL COMING OUT OF ECS. OPS NORMAL RUNNING WITH APU. SMELL DECREASED BIT WAS STILL PRESENT AFTER ABOUT 5 MINUTES. RETURNED TO MAINTENANCE DUE TO OIL BYPASS ISSUE. AFTER SHUTDOWN BAGGAGE COMPARTMENT HAD STRONG BURNING SMESDR DXTA2024082300299Hose · damagedCOCKPIT ODOR OBSERVED IN COCKPIT DURING CLIMB AND DESCENT AND TAXI. ODOR NOT OBSERVED AT LEVEL CRUISE IN THE HIGHER FLIGHT LEVELS. ODOR WAS CERTAINLY COMING FROM COCKPIT VENT WHEN THEY WERE FULLY OPEN. ODOR COULD BE DESCRIBED AS A SKUNK. VERY STRONG. ALSOSDR DXTA2024071212339None · noneBIRD STRIKE ON TAKEOFF FROM KRKD, AFTER LANDING INSPECTION SHOWED LEFT PITOT TUBE WAS STRUCK AND POSSIBLE ENGINE INGESTION. COMPLIED WITH AMM 05-51-45 GVI AFTER BIRD STRIKE. FOUND BIRD REMAINS ON LT PITOT PROBE & IN TIP OF PROBE. CLEANED PROBE FULLY & DIDN`TSDR DXTA2024052811895Warning Light · illuminatedAMBER CAS EMERGENCY ON TAKE OFF B3-648394. REMOVED EMERGENCY EXIT DOOR TO CHECK FOR PROPER RIGGING, EMERGENCY DOOR LATCH BOLTS DISTANCE IS CORRECT ACCORDING TO AMM. NO ADJUSTMENTS OR RIGGING REQUIRED. REINSTALLED EMERGENCY DOOR. NO EMERGENCY EXIT DOOR MSG PRESDR DXTA2022112874820Sign · inoperativeEMERGENCY EXIT SIGN TO THE LEFT OF EMERGENCY EXIT DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT SIGN IAW CL350 AMM 33-51-01 OPS CHECK GOODSDR DXTA2021080646490Warning Message · false activationAMBER EMERGENCY EXIT CAS MESSAGE ILLUMINATED JUST AFTER TAKEOFF. WHILE RUNNING THE CHECKLIST THE LIGHT EXTINGUISHED AND DID NOT REILLUMINATE. WE RETURNED FOR LANDING WITHOUT INCIDENT. POWERED AIRCRAFT ON AND PERFORMED VISUAL INSPCETION OF EMERGENCY EXIT DOORSDR DXTA2021042841340Accumulator · lowOUTBD BRAKE PRESS LO AMBER CAS: AFTER LANDING IN IAH WE HAD TO GET TOWED INTO THE RAMP FROM THE TAXIWAY. WE SHUT DOWN THE ENGINES OPENED THE DOOR AND GAVE THE LINEMAN THE GEAR PINS. I THEN PRESSED THE BRAKES TO RELEASE THE PARK BRAKE AND WE GOT AN AMBER OUTBOASDR DXTA2020101704224Door · lack of lubeMAIN CABIN DOOR WILL NOT CLOSE PROPERLY FROM THE OUTSIDE. WHEN THE DOOR IS AT THE END OF THE POWER ASSIST CYCLE, THE DOOR HANDLE CANNOT BE MOVED TO THE CLOSED POSITION. IN SEVERAL ATTEMPTS TO CLOSE THE DOOR WE WERE SUCCESFUL ONLY ONCE, BUT WITH STRONG UPWARDSDR DXTA2019022542074Cap · missingRIGHT ENGINE ENGINE OIL - DURING FLIGHT CLIMBING OUT OF 10,000 FEET WE GOT THE LOW OIL PRESS RIGHT SIDE RED WARNING CAS MESSAGE. WE FOLLOWED THE CHECKLIST. WE HAD TO SECURE THE ENGINE AND RETURN FOR A LANDING AFTER DECLARING AN EMERGENCY. AFTER SHUT DOWN WE F
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