N47HF

CESSNA 560XL · 2003 · Valid Registration

Registered owner: CITATION MSN 560-5153 LLC, DE (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

B · 2022-10-10 Matched by certificate designator
ATA 4930

STRONG ODOR OF FUEL IN COCKPIT DURING DESCENT. ON POST FLIGHT FOUND STRONG ODOR OF FUEL IN HELL HOLE.

Source: SDR CVGA20221014001 · FAA SDRS
J · 2022-01-21 Matched by certificate designator
ATA 3241

ANTI-SKID ANNUNCIATOR STEADY ON WITH GEAR DOOR, CIRCUIT BREAKER POPPED. CHECKLIST DIRECTED RESET, CIRCUIT BREAKER POPPED A SECOND TIME.

Source: SDR CVGA20220124001 · FAA SDRS
J · 2018-01-01 Matched by certificate designator
ATA 7930

MASTER WARNING INFLIGHT FOR LOW OIL PRESSURE ON RIGHT ENGINE. ZERO OIL PRESSURE NOTED ON PRESSURE GAUGE. OIL TEMP 60 DEG CELSIUS. PERFORMED ENGINE SHUTDOWN PER EMERGENCY CHECKLIST. FOLLOWING UNEVENTFUL LANDING, WIRING WAS CHECKED VISUALLY FOR SECURITY WITH NO DEFECTS NOTED. OIL PRESSURE TRANSMITTERS WERE SWAPPED.

Source: SDR CVGA20180105001 · FAA SDRS
O · 2015-07-10 Matched by certificate designator
ATA 5610

THE RT FORWARD SIDE WINDOW CRACKED ON THE INNER PANE DURING A FLIGHT AT 41,000 FT CAUSING THE CREW TO MAKE AN UNSCHEDULED LANDING. SPOKE WITH ACFT MFG AND THEY CONFIRMED THAT THAT THE INNER CRACKING IS UNCOMMON. UPON INSPECTION THERE WAS NO OVER VOLTAGE DAMAGE OR OVER TORQUING OF THE FRAME SCREWS.

Source: SDR W9BA20150710001 · FAA SDRS
K B · 2015-04-14 Unresolved
ATA 4990

COCKPIT FILLED WITH SMOKE ON UPWIND CLIMB - NOTED THAT THE APU OIL QUANTITY WAS LOW. SERVICED APU OIL TO FULL, PERFORMED GROUND POWER RUNS WITH ACM (PACK)- ON, INSPECT WATER SEPARATOR SOCK FOR OIL CONTAMINATION. PERFORMED APU / ENGINE GROUND RUNS UTILIZING DIFFERENT BLEED AIR SOURCES, THEN MEL APU FOR MAINTENANCE FLIGHT. INSPECT APU COMPRESSOR (BORESCOPE)- NO AMORALITIES NOTED. CONTINUE "NORMAL OPERATIONS" PER HONEYWELL APU SUPPORT.

Source: SDR 2015F00058 · FAA SDRS
O · 2015-01-21 Unresolved
ATA 2720

UPON PERFORMING INSPECTION DOCUMENT 9 TASK RUDDER AND TRIM CONTROL SYSTEM FUNCTIONAL CHECKS, THE RUDDER AUTO PILOT SERVO CABLE WAS FOUND COMPLETELY BROKEN WITH NO EVIDENCE OF COMING IN CONTACT OF ANY PART OF THE AIRCRAFT AIRFRAME. THE RUDDER SERVO ASSY, PN 4006719910, SN 3028094, SERVO CABLE PN 6660001-81.

Source: SDR W9BR2015031900099 · FAA SDRS
J · 2010-12-26 Unresolved
ATA 2731

PILOT REPORTS ON CLIMB OUT ABOUT 41K FT RECEIVED A TRIM MISCOMPARE. ELECTRIC AND MANUAL TRIM INOP. ON DESCENT AT ABOUT 20K FT TRIM BEGAN TO WORK AGAIN.

Source: SDR CNQ82011001 · FAA SDRS