N762QS
Registered owner: TEXTRON AVIATION INC, KS (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NETJETS AVIATION, INC. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
WHEN DEPLANING AND STEPPING ON THE BOTTOM STEP, THE DOOR HANDLE CAME OUT OF THE DOWN LOCKED POSITION AND THE DOOR DROPPED TO WHERE THE BOTTOM OF THE DOOR STRUCK THE FUSELAGE. REMOVED DEBRIS FROM HINGE LOCK ASSEMBLY AND VERIFIED THAT THE HINGE LOCK ASSEMBLY OPERATES SMOOTHLY.
ON APPROACH INTO BED THE APU START COMMANDED ON ABOUT A 4-5 MI FINAL AT ABOUT 1500FT AGL. AT 300-400FT AGL A RED APU FIRE CAS ILLUMINATED & AURAL WARNING WAS OVERHEARD. APU FIRE & FIRE EXT 2 SWITCHES PRESSED. APU FIRE CAS EXTINGUISHED & APU WAS OBSERVED WITH DECREASING RPM. A NORMAL LANDING & TAXI OCCURRED, NO OUTSIDE OBSERVERS REPORTED ANYTHING, NO EMERGENCY DECLARED. INFLIGHT APU FIRE QRC & QRH COMPLETED. FOUND EXIT/EXHAUST DUCT COLLAPSED. PERFORMED A GVI OF APU WITH NO FINDINGS APU LOOKS NORMAL R & R NR 2 FIRE BOTTLE. INSTALLED NEW SQUIBS IAW AMM 26-21-01, 26-21-05. PERFORMED OPS TEST OF ENG & APU FIRE EXTINGUISHING SYS IAW AMM 26â¢11-00. R & R MUFFLER ASSY IAW AMM 49·81-01 .RAN APU, NO FAULTS NOTED.
NWS FAIL AMBER CAS: UPON LANDING AND THE NOSE GEAR TOUCHING DOWN, WE RECEIVED THE AMBER NWS FAIL CAS MESSAGE. WE STOPPED ON THE RUNWAY, RAN THE QRH, TRIED RE-ENGAGING THE NWS AND IMMEDIATELY GOT THE NWS FAIL MESSAGE AGAIN HAD TO BE TOWED OFF THE RUNWAY. EMSV MANIFOLD REPLACED AND BOTH NOSE WOWF PROX SENSORS ADJUSTED UNDER WO# 29602582. PERFORMED REMAINING OPERATIONAL CHECKS I/A/W CL-350 AMM 32-61-00-820-801 (17)(18)(23) AND CLOSEOUT AS REQUIRED. ALL OPERATIONAL CHECKS SATISFACTORY. RETURNED AIRCRAFT TO NORMAL CONFIGURATION.
DURING CRUISE AT FL410 A TCAS IN STBY DIDPLAYED ON THE MFD AND A WHITE XPDR IN STBY CAS MESSAGE DISPLAYED. TRANSPONDER WAS IN A/RA BUT TRANSPONDER CODE WAS YELLOW ALONG WITH FLIGHT ID. ATC NOT ABLE TO GET ANYTHING BUT A PRIMARY RETURN, REGARDLESS OF WHICH TRANSPONDER SELECTED. PERFORMED THE OPS CHECKS OF THE TRANSPONDER WITH SATISFACTORY RESULTS REF CL 350 AMM 34-54-01. PERFORMED THE FOLLOW ON CHECKS AFTER RERACKING THE JB4 WITH SATISFACTORY RESULTS UP TO THE RETRACTION FUNCTIONAL CHECKS IAW AMM 24-63-13. JACKED AIRCRAFT & PERFORMED MULTIPLE OPS MLG SWINGS, NO DEFECTS NOTED IAW AMM 32-30-00. RETURNED TO ITS ORIGINAL CONFIGURATION.
FLAPS FAULT AMBER CAS ILLUMINATED - "FLAPS FAULT" AMBER CAS MESSAGE. FOLLOWED QRH. FLAPS FAULT STAYED ON. ACCOMPLISHED FLAP FAIL PROCEDURE. LANDED NO FLAP. MX HISTORY FLAP FAULT CODE: A124 FLAP JAM. SIGNOFF TROUBLESHOT FLAP FAIL AMBER CAS AND DETERMINED RT FLAP POSITION SENSOR TO HAVE LOW RESISTANCE ACROSS PINS 9F AND 9E AT FCU CONNECTOR A124BP1. REMOVED RT FLAP POSITION SENSOR AND INSTALLED NEW SENSOR IAW MM TASKS 27-52-17-000-802 AND 27-52-17-400-802 FUNCTION TEST OF FLAP SYSTEM GOOD.
WOW FAIL AMBER CAS ILLUMINATED. FLIGHT AT FL 430 AMBER WOW FAIL AND GEAR DISAGREE CAS ILLUMINATED. R&R PSEU.
AMBER, HYD PTU FAIL, MSG CAME ON WHEN FLAPS 10 SELECTED DURING LANDING APPROACH. TROUBLESHOT ANF FOUND FLAP ADU TO BE LEAKING INTERNALLY CAUSING HYD FLUID TRANSFER FROM THE LEFT HYD SYSTEM TO BE RIGHT WHICH CAUSED THE PTU FAIL LIGHT TO COME ON MOMENTARILY. REMOVED AND REPLACED FLAP PTU WITH A REPAIRED UNIT IAW BD-100. AIRCRAFT MAINTENANCE MANUAL CH 27-52-33. -PERFORMED SATISFACTORY LEAK TEST OF FLAP PDU IAW TASK 27-52-33-790-801. PERFORMED SATISFACTORY FUNCTIONAL TEST IAW TASK 27-52-00-720-801. PARTS: PUMP, HYDRAULIC, VARIABLE DELIVERY (PN: 51160-06, SN: K1008) PUMP, DC MOTOR, BRUSHLESS (PN: 53110-02, SN: K0153) UNIT, FLAP POWER (PN: 1751A0000-04, SN: 00585).