N453TM
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.
5 reports on file, 2019-01-03 – 2026-02-13.
Part: STRUT — OVERSERVICED (ZONE 700) · airframe 10,525 hrs · 8,145 cycles
ON LANDING, REVERSERS WOULD NOT DEPLOY. BELOW 60 K LOST BRAKES. USED EMERGENCY BRAKES TO STOP ACFT. AFTER TAXIING OFF RUNWAY, PLACED BRAKES IN ANTI SKID OFF POSITION. BRAKES WERE RESTORED. AIRSPEED INDICATOR SPEED LOW BAR WAS VISUAL. AFTER ACFT PARKED MAIN WHEEL STRUTS WERE ABNORMALLY HIGH. FOUND LT & RT MLG STRUTS TO BE OVERSERVICED WITH NITROGEN. SERVICED LT & RT MLG STRUTS IAW WITH AMM 12-00-00. GROUND RAN ACFT OPS CHECKED T/R'S. OPS CHKD NORMAL. BLED LT & RT BRAKES IAW AMM 32-40-00. FOUND LT & RT STRUTS TO BE OVERSERVICED WITH NITROGEN, NOT ALLOWING SQUAT SWITCHES TO CLOSE. T/R OPS CHK PERFORMED IAW MM 78-30-00. PERFORMED BRAKE FUNCTIONAL CHK IAW AMM 32-40-00, OPS CHKD NORMAL. NO AIRSPEED INDICATOR LOW SPEED NOTED.
Part: INLET — CRACKED (RT ENGINE) · airframe 7,172 hrs · 5,405 cycles
DURING SCHEDULED MX FOUND RT ENGINE INLET AT 9 O'CLOCK POSITON CRACKED. INSTALLED SERVICABLE R/H ENGINE INLET DUCTL
Part: STIFFENER — CRACKED (THRUST REVERSER) · airframe 4,058 hrs · 5,321 cycles
MAINTENANCE FOUND THE LEFT HAND UPPER TRUST REVERSER STIFFENER CRACKED. MX REMOVED AND REPLACED THE STIFFENER WITH A NEW UNIT. IAW CMM REPAIR #7 78-30-07
Part: BEAM — CRACKED (RT MLG) · airframe 7,058 hrs · 5,321 cycles
MAINTENANCE FOUND THE RIGHT HAND MAIN LANDING GEAR CRACKED AT THE FORWARD BEAM. MAINTENANCE REMOVED AND REPLACED THE FORWARD BEAM WITH A NEW PART IAW BEECHCRAFT 400A SRM 51-41-00 AND 51-43-00
Part: SKIN — CORRODED (HORIZ STAB) · airframe 6,207 hrs · 4,673 cycles
LT AND RT HORIZONTAL STABILIZER LEADING EDGES FOUND TO BE CORRODED BEYOND SRM LIMITATIONS.