N233XL

CESSNA 560XL · 2002 · Fixed-wing multi-engine · 2 engines · 13 seats · Valid Registration

Registered owner: VANGUARD JET LLC, TX (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
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.

4 reports on file, 2017-12-30 – 2021-04-18.

WARNING INDICATION · 2021-04-18 Matched by certificate designator
ATA 2740

Part: WARNING MESSAGE — ILLUMINATED (STAB CONTROL SYS) · airframe 6,299 hrs · 4,370 cycles

AFTER TAKEOFF WE HAD A "STAB MISC" LIGHT ILLUMINATE. WE STAYED BELOW 200KTS AND CONTINUED OUR CLIMB BUT THE LIGHT ON HYD LIGHT WENT OUT. AT ALT, WE FOLLOWED THE CHECKLIST TO NO AVIAL. TRIED FLAPS 7 DEGREES TO 15 DEGREES WITH NO CHANGE.

Source: SDR CVGA20210422001
OTHER · 2019-01-16 Matched by certificate designator
ATA 2730

Part: TORQUE TUBE — CORRODED (RT ELEVATOR) · airframe 4,551 hrs · 3,147 cycles

FOUND RT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED RT ELEVATOR TORQUE TUBE IAW SRM 51-40-03, 51-40-06 AND 55-20-01.

Source: SDR CVGA20190119001
OTHER · 2019-01-16 Matched by certificate designator
ATA 2730

Part: TORQUE TUBE — CORRODED (LT ELEVATOR) · airframe 4,551 hrs · 3,147 cycles

FOUND LT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED LT ELEVATOR TORQUE TUBE IAW SRM 51-40-03, 51-40-06 AND 55-20-01.

Source: SDR CVGA20190119002
VIBRATION/BUFFET · 2017-12-30 Matched by certificate designator
ATA 7830

Part: THRUST REVERSER — PARTIAL DEPLOY · airframe 3,654 hrs · 2,511 cycles

AIRPLANE HAD SHALLOW VIBRATION INFLIGHT. VIBRATION INCREASED WITH AIRSPEED. AN EMERGENCY WAS DECLARED AS A PRECAUTION. LANDING WAS UNEVENTFUL. DURING POST FLIGHT, FOUND BOTTOM PORTION OF RIGHT THRUST REVERSER TO BE DEPLOYED APPROXIMATELY A 1/2 INCH.

Source: SDR CVGA20180103001