N450TM
Registered owner: WHEELS UP PARTNERS LLC, NY (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.
9 reports on file, 2017-12-04 – 2020-05-12.
Part: AIR DUCT — DAMAGED (BLEED AIR SYS) · airframe 6,829 hrs · 5,578 cycles
R/H BLEED AIR DUCT METAL FLEX BRAIDS FOUND BROKEN DURING INSPECTION (Y-DUCT FUESLAGE) P/N 45A63502-0022. MX REMOVED AND REPLACED WITH A SERVICEABLE UNIT.
Part: AIR DUCT — DAMAGED (BLEED AIR SYS) · airframe 6,829 hrs · 5,578 cycles
L/H ENGINE BLEED AIR DUCT FLEX BRAIDS FOUND BROKEN DURING INSPECTION P/N 45A40304-021. MX REMOVED AND REPLACED THE DUCT WITH A SERVICEABLE UNIT.
Part: AIR DUCT — CRACKED (BLEED AIR SYS) · airframe 6,829 hrs · 5,578 cycles
R/H BLEED AIR DUCT TUBE FOUND CRACKED DURING INSPECTION P/N 45A40301-11. MX REPLACED THE BLEED DUCT WITH A SERVICEABLE UNIT
Part: SKIN — CRACKED (THRUST REVERSER) · airframe 5,873 hrs · 4,845 cycles
LH AND RH UPPER THRUST REVERSER DOORS SKIN HAS CRACKS.
Part: SUPPORT BRACKET — CRACKED (LT NACELLE) · airframe 5,873 hrs · 4,845 cycles
LEFT HAND PYLON MID SUPPORT BRACKET CRACKED. CORRECTIVE ACTION: REMOVED LH PYLON MID SUPPORT BRACKET, FABRICATED A NEW SUPPORT BRACKET FROM .032 2024 T3 ALCLAD ALUMINUM. INSTALLED BRACKET ON LH PYLON. ALL WORK ACCOMPLISHED IAW BEECHJET 400/400A SRM 51-41-00.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 5,873 hrs · 4,845 cycles
HORIZONTAL STABILIZER RH RIB AT STATION 11.81 HAS CRACKS AND LH RIB AT STATION 11.81 HAS CRACKS.
Part: DOOR — CRACKED (NLG SPADE) · airframe 5,873 hrs · 4,845 cycles
NLG SPADE DOOR CRACKED.
Part: DOOR — CRACKED (THRUST REVERSER) · airframe 3,467 hrs · 4,504 cycles
BOTH LT AND RT UPPER THRUST REVERSER DOOR SKINS FOUND TO HAVE CRACKS ACROSS THE RIVETS. BOTH THRUST REVERSER DOORS WERE REMOVED AND REPLACED.
Part: TRANSDUCER — DEFECTIVE (HYD PRESSURE) · airframe 5,154 hrs · 4,266 cycles
ON INITIAL DECENT INTO PSN CREW NOTED HYDRAULIC PRESSURE WAS HIGH AT 1750-1800 PSI, NORMAL RANGE 1500 PSI. COMPLETED ABNORMAL CHECKLIST AND REQUESTED DIVERSION TO DFW FOR A LONGER RUNWAY. CREW LANDED WITHOUT INCIDENT AND WAS ABLE TO UTILIZE HYDRAULICS UNTIL COMPLETION OF FLIGHT. MX TROUBLESHOT THE PROBLEM TO A DEFECTIVE HYDRAULIC PRESSURE TRANSDUCER AND ATTACHING CANNON PLUG.