N482TM
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.
10 reports on file, 2015-02-20 – 2020-07-10.
Part: INTAKE — CRACKED (NR 2 NACELLE) · airframe 5,245 hrs · 4,216 cycles
MX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEAD.MX FABRICATED A DOUBLER AND INSTALLED WE. IAW BEECHJET 400A SRM 54-00-01 AND 54-10-01
Part: MOUNT — CRACKED (NR 2 ENGINE) · airframe 5,245 hrs · 4,216 cycles
MX FOUND A CRACK ON THE #2 ENGINE VERTICAL MOUNT BRACKET. MX STOPPED DRILLED CRACK AND INSTALLED A DOUBLER IAW SRM 51-50-45
Part: BRACKET — CRACKED · airframe 5,245 hrs · 4,216 cycles
MX FOUND A CRACKED BRACKET UNDER THE STARTER GENERATOR DUCT ON THE #2 ENGINE INTAKE COWL ANTI ICE DUCT. MX REMOVED BRACKET FROM ENGINE COWL. REMOVED AND REPLACED DUCT ASSEMBLY WITH A NEW ASSEMBLY AND HOSE. LEAK AND OPS CHECKS GOOD. IAW BEECHJET 400A MM 30-20-00
Part: BRACKET — CRACKED (ANTI ICE DUCT) · airframe 5,245 hrs · 4,216 cycles
MX FOUND A CRACKED BRACKET UNDER THE STARTER GENERATOR DUCT ON THE #2 ENGINE INTAKE COWL ANTI ICE DUCT.
Part: INTAKE — CRACKED (NR 2 ENGINE) · airframe 5,245 hrs · 4,216 cycles
MX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEAD
Part: ATTACH BRACKET — CRACKED (NLG DOOR) · airframe 5,245 hrs · 4,216 cycles
NOSE LANDING GEAR DOOR END ATTACH BRACKETS CRACKED AT END RIVETS
Part: INTAKE — CRACKED (LEFT) · airframe 5,245 hrs · 4,216 cycles
MX DISCOVERED MULTIPLE CRACKS ON THE LH INTAKE OUTER SKIN LOOKING THRU THE STARTER GENERATOR DUCT HOLE
Part: INTAKE DUCT — CRACKED (RIGHT) · airframe 5,245 hrs · 4,216 cycles
MX FOUND THE RH INTAKE FORWARD BULKHEAD CRACKED WHEN LOOKING THRU THE STARTED GENERATOR DUCT HOLE. MX STOP DRILLED THE CRACK AND INSTALLED A DOUBLER IAW BEECHJET 400A SRM 51-43-01,51-50-01 AND 51-50-15
Part: ACTUATOR — DEFECTIVE (ZONE 500) · airframe 2,862 hrs · 2,355 cycles
DURING CLIMB, FLIGHT CREW NOTICED UNCOMMANDED ROLL TRIM DEFLECTION. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTURE AIRPORT. MAINTENANCE DETERMINED LEFT ROLL TRIM ACTUATOR DEFECTIVE. REPLACED LEFT ROLL TRIM ACTUATOR AND OPERATION CHECKED GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,846 hrs · 1,527 cycles
WHEN THE LG WAS SELECTED DOWN FOR LANDING THE RT MAIN GEAR LIGHT FAILED TO ILLUMINATE & RED GEAR HANDLE LIGHT REMAINED ON. THE ALTERNATE GEAR EXTENSION WAS ATTEMPTED IAW THE CHECKLIST. THE RT MAIN LIGHT & RED HANDLE LIGHT REMAINED ILLUMINATED. EMER PROCEDURES FOLLOWED & THE ACFT LANDED NORMALLY. INSPECTED LG FOR OBVIOUS DEFECTS WITH NONE FOUND. 3 POINT JACKED ACFT IAW 400 & 400A MM 07-10-00. COMPLIED WITH EMER DOOR CLOSE SYS BLEEDING IAW 32-30-00. COMPLIED WITH LG OPERATIONS TEST IAW 32-00-00 WITH NO DEFECTS NOTED.