N146QS

BOMBARDIER INC BD-700-1A10 · 2014 · Valid Registration

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
NETJETS AVIATION, INC. (DXTA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

N · 2026-03-08 Matched by certificate designator
ATA 3260

AFTER TAKEOFF GEAR WOULD NOT RETRACT. CYCLED ONCE STILL WOULD NOT RETRACT. WHEN GEAR HANDLE WAS UP WE GOT AN AMBER CAS GEAR DISAGREE. PUT GEAR HANDLE DOWN AND CONTINUED SHORT FLIGHT. REVIEWED PREVIOUS STEPS AND PROCEEDED WITH THE FOLLOWING; GAINED ACCESS TO SELECTOR VALVE AND REMOVED AND REPLACED SELECTOR VALVE IAW GL-6000 AMM 32-33-15. PERFORMED OPS AND LEAK CHECKS. OPS AND LEAK CHECKS GOOD. BLED HYDRAULIC SYSTEM 3 AS REQUIRED. SWUNG GEARS SEVERAL TIMES AND ALL GEAR SWINGS SUCCESSFUL. DURING CLOSE UP OF WHEEL BINS, ONE OF THE RECEPTCALES BROKE OFF. REMOVED BROKEN RECPTCALE AND INSTALLED NEW ONE. CLOSED OUT ACCESS TO VALVE AND RETURNED AIRCRAFT TO ORIGNAL CONFIGURATION. AS PER PREVIOUS STEP, PERFORMED OPS CHECKS OF SPC. PERFORMED OPS CHKD & OPS CHKD GOOD. REMOVED MLG DOOR. SELECTOR VALVE NEED OK TO INSTALL NEW CONTROL VALVE. INSTALLED LANDING GEAR DOOR SELECTOR VALVE IAW TO MM 32-31-17. TECH CR RII SR OPS TEST REQUIRED. TECO-PERFORMED OPS TEST & VERIFY RIG/ ADJ IAW MM CA 32-30-00. TECH CR RII SR OPS TEST SAT. PERFORMED OPS TEST OF STALL PROTECTION COMPUTER IAW MM 27-32-00. OPS TESTED SAT.

Source: SDR DXTA2026031107170 · FAA SDRS
O · 2024-12-08 Matched by certificate designator
ATA 5210

ENTRANCE STAIR HAND RAIL: HAND RAIL HAS COME APART AT TOP OF THE STAIR. LEFT HAND SIDE ENTERING AIRCRAFT. THERE IS A SCREW MISSING EXTRACTED BROKEN SCREW FROM CABIN DOOR HANDLE EXTENSION. INSTALLED SCREW AS REQUIRED. P/N: MS24693-C23. OPS CHECKED GOOD. REF GL6000 SMM 52-12-52

Source: SDR DXTA2024121101446 · FAA SDRS
J · 2018-02-06 Matched by certificate designator
ATA 3240

AFTER GEAR SELECTED DOWN, A BRAKE FAULT CAS MESSAGE AND AUTOBRAKE FAIL CAS MESSAGE ILLUMINATED. ON TOUCHDOWN THE LEFT BRAKE DRAGGED AND SHIMMIED. RIGHT BRAKE WAS USED TO STOP PLANE. REMOVED AND REPLACED THE LT OTBD BRAKE CONTROL VALVE AND BCU. OPS AND LEAKS CHECKED SATISFACTORY. WORK PERFORMED IAW AMM 32-43-09, & 32-43-13.

Source: SDR DXTA2018020700560 · FAA SDRS