N406BH
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.
16 reports on file, 1995-05-19 – 1999-09-27.
Part: SENSOR LOOP — FAILED (LT WING)
PILOT REPORTED LEFT BLEED LEAK, LIGHT REMAINED ON AND MADE INFLIGHT SHUTDOWN. REMOVED AND REPLACED LEFT WING BLEED AIR SENSOR LOOP IAW AMM 36-23-10. CHECK GOOD IAW AMM 36-23-00. (M)
Part: SWIVEL — INOPERATIVE (RT MLG)
AIRCRAFT LOST ALL HYDRAULIC FLUID. FLUID CAME FROM HYDRAULIC SWIVEL ON RIGHT GEAR. REMOVED AND REPLACED HYDRAULIC SWIVEL ON RIGHT MAIN GEAR. REMOVED AND REPLACED EXPLOSION BOLTS. (M)
Earlier reports · 1995–1998 · 14 reports
1998
Part: ACTUATOR — FAILED (NLG STEERING)
DURING TAXI STEERING TILLER BECAME DIFFICULT TO TURN. NOSE WHEEL WAS UNCONTROLLABLE. HYD PUMP RAN NORMALLY WHEN DEPRESSED AND HYD WAS OK. AFTER EXCERSIZING TILLER IT BEGAN WORKING FOR A SHORT TIME. REMOVED AND REPLACED NOSE WHEEL STEERING SERVO ACTUATOR IAW 32-50-25. OPS CHECK GOOD. (M)
Part: ECU — SURGE (RT ENGINE)
RIGHT ENGINE HAD A ITT SURGE ON TAKEOFF. REMOVED AND REPLACED RIGHT ENGINE ECU. (M)
Part: TR UNIT — FAILED (FWD FUSELAGE)
RADAR PAINTING FALSE ECHOS. REMOVED AND REPLACED RADAR TRANSCEIVER. OPS CHECK GOOD. (M)
Part: ENGINE — FAILED (LEFT)
LOUD SQUEAL LT ENGINE. REMOVED AND REPLACED LT ENGINE. (X)
Part: PROP GEAR BOX — FAILED (LT ENGINE)
CREW SHUT DOWN LEFT ENGINE, NO OIL PRESSURE. COULD NOT FEATHER LEFT PROP. REMOVED AND REPLACED LEFT PROP GEARBOX. (M)
1997
Part: RT UNIT — FAILED (FWD FUSELAGE)
LOST WEATHER RADAR DURING CLIMB-OUT. GOT FAULT FLAG IN ALL RANGES AND MODES. RESET BREAKER STILL THE SAME. REMOVED AND REPLACED RADAR RT. GROUND CHECKS GOOD. (M)
Part: INDICATOR — MALFUNCTIONED (YAW TRIM)
YAW TRIM INDICATOR UNCONTROLLABLE. DEFERRED. (X)
Part: CONNECTOR — LOOSE (RT ENGINE)
RIGHT INTAKE HEAT FAILED EN ROUTE. CLEANED AND RESECURED LOAD MONITOR AND THERMAL CONTROLLER CANNON PLUGS. (X)
Part: HOT LIGHT — ILLUMINATED (LT TAIL PIPE)
TAIL PIPE HOT CAME ON DURING TAKEOFF, WENT OUT 30 SECONDS AFTER REDUCING TO FLIGHT IDLE. PERFORMED OPS TEST OF RT AND LT ENGINE FIRE AND TAIL PIPE HOT DETECTORS SYSTEM TESTS NORMAL. (M)
Part: BATTERY — DISCHARGED (CABIN)
LEFT AFT CENTER AND EXTERNAL 'L' EMERGENCY LIGHTS OUT. REMOVED AND REPLACED EMERGENCY BATTERY AT 21LN. CHECK GOOD. OK FOR SERVICE. REFERENCE OPERATOR CONTROL NR 97ZZZX950. (X)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
LEFT AFT CENTER AND EXTERNAL 'L' EMERGENCY LIGHTS OUT. REMOVED AND REPLACED POWER SUPPLY UNIT AT 24LN. CHECK GOOD. OK CONTINUE SERVICE. REFERENCE OPERATOR CONTROL NR REXA97010.
1996
Part: TRANSDUCER — FAILED (RT ENGINE)
PERFORMED A PRECAUTIONARY SHUTDOWN ON RIGHT ENGINE, OIL PRESSURE AND GAUGE. REMOVED AND REPLACED RIGHT PGB OIL TRANSDUCER IAW GEMM. GROUND RUNS GOOD. OK FOR SERVICE. (M)
1995
Part: EEL — INOP (CABIN)
EMERGENCY OVERHEAD LIGHT INOP 2A. REMOVED AND REPLACED EMERGENCY OVERHEAD LIGHT, OPS CHECK GOOD. (M)
Part: ENGINE — MALFUNCTIONED (RIGHT)
LOST RIGHT ENGINE OIL PRESSURE, CWP VERIFIED BY GAUGE, SHUTENGINE DOWN. INSPECTED ENGINE FOUND TO BE WITHIN OVER SERVICE LIMIT TABLE 206 GE MM OK FOR SERVICE OR 10 ADDITIONAL FLIGHT HOURS. (M)