N500FZ
Registered owner: DB N941JP LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
6 reports on file, 2009-10-06 – 2017-07-12.
Part: OIL CAP — CRACKED (LEFT ENGINE) · airframe 9,153 hrs · 9,085 cycles
DURING THE DEPARTURE, CLIMBING THROUGH FL240, WHEN THE OIL PRESSURE ON THE LEFT ENGINE STARTED DROPPING. THE MASTER WARNING LIGHT AND THE LOW OIL PRESSURE ANNUNCIATION LIGHT ILLUMINATED, CONFIRMING THE OIL PRESSURE GAUGE INDICATION. THE ENGINE WAS SHUTDOWN . THE CREW FOLLOWED UP WITH THE CHECK LIST AND RETURNED TO DEPARTURE WITHOUT INCIDENT. FOUND THE OIL CAP CRACKED
Part: BRAKE SYS — PRESSURE LOSS (ZONE 700) · airframe 8,813 hrs · 8,768 cycles
AFTER INITIAL START UP. DURING TAXI OUT THE CREW NOTED RT BRAKE PEDAL WENT TO THE FLOOR. THE PIC RETURNED TO THE PARKING SPACE AND EXECUTED A NORMAL SHUTDOWN.
Part: AIR DUCT — BLOWN (ZONE 100) · airframe 8,693 hrs · 8,653 cycles
ENROUTE, APPROX 35 MINS FROM KINT, WE HEARD A LOUD POP & PRESSURIZATION ROC WENT TO 4,000 FPM UP, INITIATED A DECENT. DECLARED EMER, INITIATED & COMPLETED EMER PROCEDURES & DIVERTED. CABIN PRESS STABILIZED APPROX 13,000' CABIN ALTITUDE.
Part: CONTROL HANDLE — BROKEN (COCKPIT) · airframe 8,364 hrs · 8,308 cycles
EMERGENCY GEAR EXTENSION T HANDLE BROKE OFF DURING A TEST OF THE EMER GEAR EXTENSION SYS DURING ROUTINE MX.
Part: SKIN — BULGED (ZONE 100) · airframe 7,789 hrs · 7,768 cycles
A SMALL 3 BY 5 INCH BULGING SECTION OF THE BELLY SKIN WAS NOTED DURING INSPECTION. SKIN BULGE WAS LOCATED IN THE CENTER WING SECTION ON THE BELLY OF THE ACFT. TWO RIVETS HAD PULLED THROUGH AND THREE ARE PRESENTLY STRESSED. REMOVED ADF ANTENNA AND A BORESCOPE INSPECTION DID NOT REVEAL ANY USEFUL INFORMATION. AN EDDY CURRENT INSPECTION REVEALED NO CRACKS IN THE SKIN PANEL. AN ULTRASONIC THICKNESS INSPECTION WAS PERFORMED, ALSO WITH NO USEFUL FINDINGS. THE SKIN PANEL WILL BE REMOVED FOR FURTHER INSPECTION AND REPAIR OF THE UNDER LYING STRUCTURE. OPEN
Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 6,815 hrs · 6,988 cycles
DURING GEAR EXTENSION, LANDING GEAR INDICATORS SHOWED BOTH MAIN GEAR DOWN AND LOCKED, HOWEVER, THE NOSE GEAR INDICATOR DID NOT ILLUMINATE. THE CREW FOLLOWED THE CHECKLIST FOR ALTERNATE GEAR EXTENSION.