N402BH
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.
14 reports on file, 1995-12-18 – 1999-12-03.
Part: VALVE — INOPERATIVE (MLG)
DURING LANDING PHASE OF FLT, CREW SELECTED L/G GEAR DOWN AND L/G FAILED TO EXTEND. TRANSIT LIGHT WAS ILLUMINATED AND HYD PUMP CONTINUED TO RUN WITH NORMAL ACCUMULATOR PRESSURE AND HYD FLUID QTY. CREW ATTEMPTED TO HAND PUMP THE GEAR DOWN WITH NEGATIVE RESULTS. EMERGENCY GEAR EXTENSION HANDLE WAS PULLED AND LANDING GEAR EXTENDED WITH GEAR INDICATING DOWN AND LOCKED. AFTER A NORMAL LANDING, IT WAS DISCOVERED THAT THE NOSE WHEEL STEERING WAS INOPERATIVE. DIFFERENTIAL POWER WAS UTILIZED FOR TAXI TO THE GATE. LANDING CONTROL VALVE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE AND LEFT/RIGHT SEPARATION BOLTS. PERFORMED FUNCTIONAL/OPERATIONAL TEST OF LANDING GEAR SYSTEM WITH NO F
Part: ENGINE — FAILED (RIGHT)
CHIPS LIGHT WARNING WITH ASSOCIATED RISE IN OIL TEMPERATURE ON RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE. (M)
Part: CONNECTOR — FAILED (ROW 3A)
SPARK AND SMOKE CAME FROM WINDOW LIGHT OVER SEAT 3A. REMOVED AND REPLACED TWO BULB CONNECTORS. (M)
Earlier reports · 1995–1998 · 11 reports
1998
Part: SEAL — FAILED (LT ENGINE)
LEFT ENGINE LOST OIL PRESSURE. REMOVED AND REPLACED LEFT BB AXIS SEAL AND RUNNER. REF: OPERATOR CONTROL NR 98ZZZX2425. (X)
Part: RUNNER — FAILED (LT ENGINE)
LEFT ENGINE LOST OIL PRESSURE. REMOVED AND REPLACED LEFT BB AXIS SEAL AND RUNNER. REF: OPERATOR CONTROL NR REXA98096.
Part: TRANSDUCER — INOP (LT MLG)
ANTI-SKID INOP. REMOVED AND REPLACED LHOB WHEEL SPEED TRANSDUCER. (M)
1997
Part: FCU — FAILED (RT ENGINE)
RT ITT FLUCTUATES FROM 150 DEGREES-900 DEGREES DURING POWER CHANGES AND SMALLER FLUCTUATES WHEN POWER STEADY. REMOVED AND REPLACED RT FCU. (M)
Part: ITT INDICATOR — FAILED (RT ENGINE)
RIGHT ENGINE ITT FLUX. REMOVED AND REPLACED RIGHT ITT INDICATOR. (M)
Part: 4.5 BIAS TRIMMER — FAILED (RT ENGINE)
RIGHT ITT GAUGE FLUCTUATES FROM 850 DEGREES CELCIUS TO 600 DEGREES CELSIUS ON CLIMB-OUT. REMOVED AND REPLACED T4.5 BIAS TRIMMER. (M)
Part: PUMP — INOPERATIVE (HYD SYSTEM)
HYDRAULIC PUMP FAILED IN-FLIGHT. REMOVED AND REPLACED HYDRAULIC PUMP. (X)
Part: NAV RECEIVER — INOPERATIVE (NR 1 NAV)
CAPTAINS NR 1 NAV RADIO INOP. REMOVED AND REPLACED NAV CONTROL UNIT AND NAV RECEIVER. (M)
Part: SWIVEL — SHEARED (RT MLG)
EMERGENCY LANDING DUE TO LOSS OF HYD FLUID OR PRESSURE. REMOVED AND REPLACED DOWNLOCK SWIVEL ON RIGHT HYD MAIN LANDING GEAR. (M)
1996
Part: SMOKE DETECTOR — ILLUMINATED (LAVATORY)
LAVATORY SMOKE ILLUMINATED ON TAKEOFF ROLL, ABORTED TAKEOFF. DEFERRED PER MEL 26-13-01. (M)
1995
Part: PWR DISTR UNIT — FAILED (RIGHT)
LOST RT MAIN BUS AND ALL ASSOCIATE FLEET EQUIPMENT ON APPROACH. REMOVED AND REPLACED SHORTED WIRE AC225. REMOVED AND REPLACED LT AND RT PDU'S AND TIME DELAY RELAY PC12. SYSTEM OPERATION CHECKED GOOD. ACFT OK FOR CONTINUED SERVICE. (X)