N47HF
Registered owner: CITATION MSN 560-5153 LLC, DE (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.
7 reports on file, 2010-12-26 – 2022-10-10.
Part: SEALANT — DETERIORATED (APU) · airframe 12,200 hrs · 10,072 cycles
STRONG ODOR OF FUEL IN COCKPIT DURING DESCENT. ON POST FLIGHT FOUND STRONG ODOR OF FUEL IN HELL HOLE.
Part: POWERPACK — FAILED (ZONE 700) · airframe 11,825 hrs · 9,824 cycles
ANTI-SKID ANNUNCIATOR STEADY ON WITH GEAR DOOR, CIRCUIT BREAKER POPPED. CHECKLIST DIRECTED RESET, CIRCUIT BREAKER POPPED A SECOND TIME.
Part: TRANSMITTER — MALFUNCTIONED (OIL PRESSURE) · airframe 8,645 hrs · 7,583 cycles
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.
Part: WINDOW — CRACKED (COCKPIT) · airframe 7,378 hrs · 6,430 cycles
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.
Part: APU — SMOKE (ZONE 200) · airframe 7,294 hrs · 6,348 cycles
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.
Part: CABLE — FAILED (AUTOPILOT RUDDER)
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.
Part: ACTUATOR — FROZEN (TRIM SYSTEM) · airframe 4,991 hrs · 4,352 cycles
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.