N489TM
Registered owner: JERSEY AVIATION LLC, CT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Wheels Up Private Jets LLC (CVGA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
11 reports on file, 2018-07-10 – 2023-09-14.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 7,660 hrs · 6,165 cycles
LEFT THRUST REVERSER DEPLOY IN FLIGHT. FOUND THRUST REVERSER LH DEACTIVATION PROCEDURE PERFORMED ON 9/13/2023 WAS INCOMPLETE. CONNECTORS P427 AND P429 WERE STILL CONNECTED. DISCONNECTED P427 AND P429 REMOVING POWER FROM THE ISOLATION AND CONTROL VALVES. WORK PERFORMED IAW BE400 AMM 78-30-00.
Part: SWITCH — FAILED (LEFT ENGINE) · airframe 7,660 hrs · 6,166 cycles
SUDDEN LEFT YAW AND LEFT THROTTLE UN-COMMAND REDUCED TO IDLE. THE LEFT THRUST REVERSER HAD BEEN PREVIOUSLY PLACED ON MEL. CLEARED THE MEL ITEM BY REPLACING THE LH T/R STOW SWITCHES. CYCLED T/R SEVERAL TIMES. T/R OPERATION WAS SMOOTH AND CONSISTENT. ENSURED T/R BUCKETS WERE LOCKED TIGHTLY AND FLUSH WITH COWLING. INSPECTED T/R FEEDBACK CABLE FOR PROPER OPERATION AND ROUTING. NO DEFECTS NOTED.
Part: SKIN — CRACKED (RT ELEVATOR) · airframe 6,004 hrs · 4,836 cycles
SUPPLEMENTAL INFORMATION, RT ELEVATOR OUTBOARD COVER HAS A CRACK. INSTALLED NEW ACCESS PANEL, IAW BEECHJET 400XP AMM CH 27-30-00.
Part: BRACKET — CRACKED · airframe 6,004 hrs · 4,836 cycles
RT/PYLON, AFT UPPER PANEL TWO BRACKETS CRACKED.
Part: BRACKET — CRACKED (RT NACELLE) · airframe 6,004 hrs · 4,836 cycles
SUPPLEMETAL INFORMATION, RT PYLON, AFT UPPER PANEL TWO BRACKETS CRACKED. STOP DRILLED CRACKS, FABRICATED BACKING PLATE DOUBLER AND INSTALLED USING MS20410AD-4 RIVETS, IAW BEECHJET 400/400A SRM CH 51-50-21.
Part: SKIN — DAMAGED (RUDDER) · airframe 6,004 hrs · 4,836 cycles
RUDDER TOP TRAILING EDGE DAMAGED. INSTALLED RUDDER P/N 45A24001-211 S/N RK-576 FROM AIRCRAFT 475TM. PERFORMED FUNCTIONAL TEST AND CONFIRMED SERVICEABILITY, IAW HAWKER 400XP AMM 27-20-00.
Part: RUDDER — DENTED · airframe 6,004 hrs · 4,836 cycles
RUDDER TOP TRAILING EDGE DAMAGED
Part: STIFFENER — CRACKED (NLG SPADE DOOR) · airframe 6,004 hrs · 4,836 cycles
NLG SPADE DOOR I/B STIFFENER CRACKED
Part: STIFFENER — CRACKED (NLG DOOR) · airframe 6,004 hrs · 4,836 cycles
SUPPLEMETAL INFORMATION, NLG SPADE DOOR INBOARD STIFFENER CRACKED. STOP DRILLED CRACKS & FABRICATED REPAIR ANGLE DOUBLERS & INSTALLED, IAW BEECHJET 400/400A SRM CH 51-50-45.
Part: RIB — CRACKED (HORIZ STAB) · airframe 4,444 hrs · 3,657 cycles
HORIZONTAL RIBS AT STATION 110 FOUND CRACKED DURING BOROSCOPE INSPECTION. REPAIRED CRACKS IN LT AND RT HORIZONTAL STABILIZER RIBS BY INSTALLING NEW RIB KIT IAW KIT DRAWING 128-6200 REV 4.
Part: INLET — CRACKED (RT ENGINE) · airframe 4,444 hrs · 3,657 cycles
RT ENGINE INLET LINER FOUND CRACKED DURING SCHEDULED INSPECTION. REPAIRED RIGHT ENGINE INLET LINER BY FABRICATING DOUBLER FROM .016 347 STAINLESS STEEL SHEET AND INSTALLING IAW SRM CHAPTER 51-40-01 AND 51-50-00. SANDED, PRIMED, AND REFINISHED INLET.