N482TM

HAWKER BEECHCRAFT CORP 400A · 2007 · Valid Registration

Registered owner: JERSEY AVIATION LLC, CT (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
WHEELS UP PRIVATE JETS LLC (CVGA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2020-07-10 Matched by certificate designator
ATA 7160

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

Source: SDR T17A2020072710025 · FAA SDRS
O · 2020-07-10 Matched by certificate designator
ATA 5415

MX FOUND A CRACKED BRACKET UNDER THE STARTER GENERATOR DUCT ON THE #2 ENGINE INTAKE COWL ANTI ICE DUCT.

Source: SDR T17A20200710025 · FAA SDRS
O · 2020-07-10 Matched by certificate designator
ATA 5280

NOSE LANDING GEAR DOOR END ATTACH BRACKETS CRACKED AT END RIVETS

Source: SDR T17A20200710026 · FAA SDRS
O · 2020-07-10 Matched by certificate designator
ATA 7120

MX FOUND A CRACK ON THE #2 ENGINE VERTICAL MOUNT BRACKET. MX STOPPED DRILLED CRACK AND INSTALLED A DOUBLER IAW SRM 51-50-45

Source: SDR T17A20200710027 · FAA SDRS
O · 2020-07-10 Matched by certificate designator
ATA 5340

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

Source: SDR T17A2020072210028 · FAA SDRS
O · 2020-07-10 Matched by certificate designator
ATA 7160

MX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEAD

Source: SDR T17A202007100025 · FAA SDRS
O · 2020-06-24 Matched by certificate designator
ATA 7160

MX DISCOVERED MULTIPLE CRACKS ON THE LH INTAKE OUTER SKIN LOOKING THRU THE STARTER GENERATOR DUCT HOLE

Source: SDR T17A20200624021 · FAA SDRS
O · 2020-06-24 Matched by certificate designator
ATA 7160

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

Source: SDR T17A20200624022 · FAA SDRS
F · 2016-09-29 Unresolved
ATA 2711

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.

Source: SDR T17A201610034016 · FAA SDRS
N · 2015-02-20 Unresolved
ATA 3260

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.

Source: SDR T17A201502234007 · FAA SDRS