N407BH
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.
17 reports on file, 1995-05-18 – 2002-06-13.
Part: SQUIB — DAMAGED (CARGO BAY)
WHILE INVESTIGATING REASON FOR CARGO SMOKE WARNING IT WAS FOUND THAT THE CARGO FIRE EXTINGUISHER BOTTLE WAS NOT FIRED. CREW REPORTED THAT THE BOTTLE WAS FIRED IAW EMERGENCY PROCEDURES. THE CARGO BOTTLE SQUIB WAS FOUND TO HAVE BENT ELECTRICAL PINS. SQUIB WAS REPLACED THE THE SYSTEM WAS OPERATIONALLY TESTED.
Earlier reports · 1995–2000 · 16 reports
2000
Part: PANEL — BURNED (COCKPIT)
LEFT AND RIGHT PUSHER DISARM, L+R PUSH 1+2, L+R DRIVE XFER, AND ALL 4 GPWS LIGHT CAME ON SIMUTANIOUSLY ILLUMINATED IN CRUISE AND REMAINED ON FOR ENTIRE FLIGHT. ALSO, HAD L+R PROP DE-ICE STATUS LIGHTS, IGNITION STATUS LIGHTS ILLUMINATED. L+R MODE SELECT PANEL DIGIT LIGHTS ILLUMINATED BRIGHTLY AND COULD NOT BE CONTROLLED BY DIGITS RHEOSTAT. STRONG ELECTRICAL FUMES FOR REMAINDER OF FLIGHT FOLLOWED ALL OF THIS. FOUND LEFT MODE SELECT PANEL BURNED, AND REPLACED. RIGHT MODE SELECT PANEL WAS ALSO REPLACED DUE TO BEING INOPERATIVE. (M)
1999
Part: SWIVEL — LEAKING (MLG)
AFTER TAKEOFF PILOT REPORTED LOSS OF HYDRAULIC PRESSURE AND QUANTITY AFTER GEAR CAME UP. AN EMERGENCY EXTENSION OF THE LANDING GEAR WAS PERFORMED. MAIN LANDING GEAR HYDRAULIC SWIVEL LEAKING. REMOVED AND REPLACED HYDRAULIC SWIVEL. PERFORMED OPERATIONAL AND FUNCTIONAL CHECK OF THE LANDING GEAR SYSTEM. AIRCRAFT RETURNED TO SERVICE. (M)
1998
Part: LOAD MONITOR — FAILED (LT ENGINE)
LEFT INTAKE LIGHT COMES ON CONTINUOUSLY DURING FLIGHT. REMOVED AND REPLACED LOAD MONITOR. (X)
Part: TAILPIPE — DIRTY (RT ENGINE)
RIGHT ENGINE TAIL PIPE HOT LIGHT ON IN FLIGHT. REMOVED RIGHT TAILPIPE ASSY. INSPECTED, CLEANED, AND SEALED CONNECTORS. REINSTALED GROUND RUN CHECKS GOOD. (M)
Part: EFIS TUBE — INOPERATIVE (RIGHT)
RIGHT EFIS INOP. REMOVED AND REPLACED UPPER EFIS TUBE F/O'S SIDE. OPS CHECK GOOD. (M)
Part: AIRSPEED IND — FAILED (LT COCKPIT)
CAPTAINS AIRSPEED INDICATOR INOP. REMOVED AND REPLACED CAPTAINS AIRSPEED INDICATOR. (M)
Part: OVERHEAT SENSOR — CONTAMINATED (RT ENGINE)
RIGHT HAND TAIL PIPE HOT LIGHT IN-FLIGHT. CLEANED MOISTURE FROM TAILPIPE OVER HEAT SENSOR. CREW RAN A/C SYSTEM. OPS CHECKED GOOD. (X)
1997
Part: PLUG — MISINSTALLED (LEFT PROP)
LEFT PROP OIL PRESSURE 0 PSI 40 DEGREES CELSIUS, CWP WARNING CAME ON. INSTALLED AND LOCK WIRED PROP RIG PIN PLUG. GROUND RUN AND OPS CHECK GOOD. (M)
Part: WEU — INOP (LEFT)
LEFT ENGINE BLEED LIGHT CAME ON IN FLT (ENGINE WAS SHUT DOWN). REMOVED AND REPLACED WEU. (M)
Part: BLEED AIR — LEAK (RIGHT)
RIGHT BLEED LEAK IN FLIGHT. GROUND RAN COULD NOT DUPLICATE DISCREPANCY. INSPECTED 'Y' CONNECTIONS IN WING ROOT, PERISEALS IN FLAP COVE, ASSOCATED PIPING. NO LEAKS NOTED AT THIS TIME. (M)
Part: OIL TEMP GAUGE — FAILED (LT ENGINE)
LEFT OIL TEMP REACHED HIGH TEMP LIMIT. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE TEMP GAUGE. (M)
Part: PRESSURIZATION — MALFUNCTIONED (CABIN)
PRESSURE ERRACTIC SHORTLY AFTER TAKEOFF. DEFERRED PRESSURIZATION PER MEL. (M)
Part: STRUT — REQ'D SERVICE (LT MLG)
AFTER TAKEOFF AND GEAR UP CONFIG WARNING CAME ON, AIRCRAFT RETURNED FOR UNEVENTFUL LANDING. SERVICED LT MLG STRUT. (M)
Part: ENGINE — LOW OIL (LEFT)
LEFT ENGINE OIL PRESSURE IN YELLOW ARC. STATION MAINTENANCE SERVICED LEFT ENGINE OIL. (M)
1996
Part: COWLING — BENT (RT NACELLE)
AFTER TAKEOFF RIGHT COWLING DOOR CAME OPEN IN FLIGHT, AIR RETURN. REMOVED AND REPLACED FORWARD AND AFT COWLINGS. (M)
1995
Part: EEL WIRE — FAILED (CABIN)
EMERGENCY LIGHT NR 7 CIRCUIT BREAKER OUT, WON'T RESET. REPAIRED WIRE TO RAYCHEM CONNECTOR AND RESET NR 7 CIRCUIT BREAKER, CHECKED SYSTEM IAW AMM. (Z)