N337FX
Registered owner: GABBERT JOHN, OH (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, 2010-03-12 – 2014-08-05.
Part: LINE — CHAFED (HYDRAULIC SYS) · airframe 7,453 hrs · 4,019 cycles
THE ACFT EXPERIENCED A HIGH TEMP NR 1 HYDRAULIC SYSTEM LEADING TO A LOSS OF HYDRAULIC FLUID RESULTING IN A DECLARED EMERGENCY LANDING. AFTER INVESTIGATING THE CAUSE OF THE FLUID LOSS WE DISCOVERED THE NR 1 HYDRAULIC SYSTEM PRESSURE LINE, PN 604-75238-3 WAS CHAFED THROUGH RESULTING IN LOSS OF PRESSURE. THE PRESSURE LINE CLAMP WAS MISSING THE RUBBER ANTI-CHAFE RUBBER. ADDITIONALLY SINCE THE ENGINE DRIVEN PUMP WAS OPERATED AT A HIGH TEMPERATURE AND EXCEEDING THE MM REQUIREMENTS THE LT ENGINE DRIVEN HYDRAULIC PUMP WAS CHANGED.
Part: CLAMP — FAILED (BLEED AIR SYS) · airframe 6,774 hrs · 3,645 cycles
LEFT 14TH STAGE DUCT FAIL LIGHT ILLUMINATED & BLEED AIR DUCT RED CAS MESSAGE. LANDING & TAXI WERE UNEVENTFUL. REPLACED BLEED AIR CLAMPS WITH NEW. THE FLIGHT WAS ON A PART RELEASE NUMBER 135-1118.
Part: SWITCH — FAILED (PITCH TRIM) · airframe 6,385 hrs · 3,447 cycles
PILOT STATED BOTH CAS MESSAGES POSTED. TURNED OFF AUTOPILOT AND STAB TRIM CHANNELS 1 AND 1 WERE OFF LINE AND WOULD NOT RESET. DECLARED AN EMERGENCY AND MADE A UNEVENTFUL LANDING. AMBER ICAS (STAB TRIM) AND (MACH TRIM) POST DURING DECENT TO LAND. CREW TRIED TO ENGAGE PITCH TRIM CHANNEL 1 AND 2, DID NOT COME BACK ON LINE DURING FLIGHT. WHILE ON GROUND STAB CHANNELS WOULD RESET. DURING TROUBLESHOOTING, FOUND PITCH TRIM DISCONNECT SWITCH LOCATED IN PILOTS CONTROL WHEEL DEFECTIVE. REPLACED WITH NEW PART, OP'S CHECK OK.
Part: FLAP SYSTEM — FAILED
FLAPS FAILED AT ZERO DEGREES. AIR TURN BACK.
Part: FLAP SYSTEM — FAILED (TE FLAPS)
AT FL 400, FLAPS FAILED AT ZERO DEGREES.
Part: PSEU — FAILED (MLG) · airframe 3,490 hrs · 1,903 cycles
CREW REPORTED WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION THE NOSE GEAR DID NOT GO UP. IT INDICATED GREEN AND DOWN ON THE DISPLAY AND THE MAINS SHOW UP. THE RED ICAS (NOSE DOOR OPEN) & (GEAR DISAGREE) WERE POSTED ALSO. WHEN THE GEAR HANDLE IS PLACED IN THE DOWN POSTING ALL 3 GEAR SHOW GREEN AND ALL CAS MESSAGES CLEAR. MX FOUND ONLY 11.1 VDC AT THE NLG SELECTOR VALVE CONNECTOR P4GA PIN A. SHOULD BE 28VDC. RINGOUTS DONE: NLG SELECTOR VALVE CONN P4GA PIN A = 11 VDC. JB-15 CONN P83 PINS 78 AND 79 (POWER FROM PSEU) = 11 VDC. P160 FLOOR DISCONNECT AT STA 273R PINS 68 AND 69 (FEED THRU CONN BETWEEN PSEU AND JB-15) = 11 VDC. R & R THE PSEU, OPS CHECKED GOOD. OPS CHECKED GOOD. R & R THE NR 2 WOW AND CENTERING PROXIMITY WIRING HARNESS, OPS CHECKED GOOD. PERFORMED SEVERAL GEAR RETRACTION, NO DEFECTS NOTED.