N59805
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.
103 reports on file, 1997-04-23 – 2002-06-07.
Part: MONITOR — MALFUNCTIONED (OIL COOLER) · airframe 5,698 hrs
SWITCH WILL NOT EXTINGUISH OIL COOLER LIGHT ON A/C UNLESS THE UNIT IS TAPPED ON WHILE A/C IS OPERATING IN THE PROPER RANGE.
Part: INDICATOR — FAILED (COCKPIT) · airframe 5,698 hrs
INDICATOR BEARING POINTER STAYS STOWED.
Earlier reports · 1997–2001 · 101 reports
2001
Part: BATTERY — DISCHARGED (MAIN)
WON'T START AIRCRAFT. REPLACED WITH SERVICEABE BATTERY.
Part: BATTERY — DISCHARGED (MAIN)
WON'T START AIRCRAFT.
Part: BATTERY — DISCHARGED (MAIN)
WON'T START AIRCRAFT. REPLACED WITH SERVICEABE BATTERY.
Part: RECEIVER — FAILED (COCKPIT) · airframe 5,565 hrs
SQUELCH STAYS ON. ALIGNED RECEIVER SEVERAL TIMES. SWAPPED Q317 AND Q319 TRANSISTORS. REALIGNED RECEIVER BOARD. REPLACED Q304, Q305, Q306, Q307, Q308, Q317, Q318, Q319, Q320 AND Q321 TRANSISTORS AND I301 IC CHIP. ALSO REPLACED BROKEN NAMEPLATE. ADJUSTED VCO VOLTAGE AND REALIGNED RECEIVER. REPLACED RECEIVER BOARD. BENCH CHECK GOOD.
1999
Part: INVERTER — INOPERATIVE (AC SYSTEM)
INVERTER INOPERATIVE; TRIPPING CIRCUIT BREAKER.
Part: AMPLIFIER — INOPERATIVE (SCAS)
AMPLIFIER INOPERATIVE.
Part: INDICATOR — FAILED (RADAR)
INDICATOR HAD NO DISPLAY.
Part: RADAR UNIT — FAILED (COCKPIT)
SEARCH 1 AND 2 RADAR SCREEN IS BLANK AND R/T FAULT ON SCREEN.
Part: DRIVE ASSY — INOPERATIVE (RADAR ANTENNA)
STABILIZATION INOPERATIVE.
Part: DRIVE ASSY — FAILED (RADAR ANTENNA)
RADAR WILL NOT PAINT TARGETS.
Part: INDICATOR — FAILED (COCKPIT)
INDICATOR WILL NOT SPIN UP.
Part: BAG — LEAKING (FLOAT)
FLOAT BAG LEAKING.
Part: MOTOR — MALFUNCTIONED (BLOWER)
OIL COOLER LIGHT STAYS ON.
Part: TRANSPONDER — INOPERATIVE (COCKPIT)
TRANSPONDER INOPERATIVE. SMELLS BURNT. PERFORMED PRELIMINARY INSPECTION. FOUND EXCESSIVE CORROSION AND POWER SUPPLY BAD.
Part: TRANSCEIVER — FAILED (COCKPIT)
TRANSERVER DISPLAYS R/T FAULT IN 1 AND 2 MODES WHEN IN SEARCH.
Part: RETAINER ASSY — PITTED (M/R DRIVE)
RETAINER ASSY HAD EXCESSIVE PITTING. REPLACED WITH SERVICEABLE PART.
Part: AMPLIFIER — FAILED (AUTOFLIGHT)
PITCH CHANNEL DROPS OFF WHEN BEEPING FORE AND AFT. ATTEMPTED ALIGNMENT. DID NOT CURE PROBLEM.
Part: DRIVE ASSY — INOPERATIVE (RADAR ANNTENA)
TILT INOPERATIVE.
Part: STARTER — FAILED (ENGINE)
STARTER WILL NOT DISENGAGE.
Part: CAUTION PANEL — MALFUNCTIONED (COCKPIT)
CAUTION PANEL HAS INTERNAL SHORT. NR 1 FUEL PRESSURE LIGHT STAYS ON.
Part: BATTERY CHARGER — MALFUNCTIONED (DC SYSTEM)
NR 2 BATTERY CHARGER MONITOR TRIPS OFF.
Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)
RADAR SKIPPING.
Part: DRIVE ASSY — LOOSE (RADAR ANTENNA)
ALLEN SCREWS LOOSE AND SHOCK MOUNTS NEED TO BE REPLACED.
Part: TRANSCEIVER — INTERMITTENT (COCKPIT)
TRANSCEIVER RECEIVE IS NOISY AND INTERMITTENT, SUSPECT SQUELCH CIRCUIT. PERFORMED PRELIMINARY INSPECTION AND FOUND TRANSMIT POWER SLOWLY DROPS.
Part: TRANSCEIVER — NOISY (COCKPIT)
TRANSCEIVER RECEIVES NOISY.
Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)
EXCESS CLUTTER ON HIGH RANGES.
Part: STARTER — MALFUNCTIONED (START/GENERATOR)
NR 1 ENGINE WILL NOT GO INTO CROSS START FOR 20 SECONDS AND START.
Part: STARTER — FAILED (ENGINE)
STARTER WOULD NOT START AIRCRAFT.
Part: AMPLIFIER — MALFUNCTIONED (FBW ELEVATOR)
AMPLIFIER WILL NOT STAY ON LINE.
Part: ACTUATOR — MALFUNCTIONED (MAIN ROTOR)
ACTUATOR WILL NOT MONITOR TEST AND KICKS OFF.
Part: SENSOR — ERRATIC (AFCS)
ALTITUDE SENSOR ERRATIC ABOVE 1,000 FEET.
Part: INDICATOR — READS LOW (COCKPIT)
INDICATOR INDICATES 10 KNOTS LOW OVER 100 KNOTS AIRSPEED.
Part: COMPUTER — FAILED (AUTOFLIGHT)
COMPUTER FAILED 2.1 ON SST BENCH.
Part: ACTUATOR — INOPERATIVE (YAW CHANNEL)
ACTUATOR INOPERATIVE.
Part: SENSOR — MALFUNCTIONED (SCAS SYSTEM)
SCAS PITCH TRIPS IN-FLIGHT.
1998
Part: TRANSPONDER — MALFUNCTIONED (ATC)
ATC TRANSPONDER REPORTED AS NOT SQUAWKING. PERFORMED PRELIMINARY INSPECTION. REPLACED TRANSISTOR Q104, Q502, AND TWO EACH SPACERS, REPAIRED. BEGAN BENCH CHECK AND FOUND WEAK TRANSMIT POWER. ALIGNED TRANSMITTER AND GOT 100 WATTS OUT.
Part: SENSOR — FAILED (SCAS SYSTEM)
SCAS PITCH PROBLEM.
Part: ACTUATOR — FAILED (TAIL ROTOR)
ACTUATOR KICKS AFCS PITCH OFFLINE.
Part: PUMP — NOISY (HYDRAULIC SYSTEM)
HYDRAULIC PUMP NOISY.
Part: GENERATOR — FAILED (DC SYSTEM)
GENERATOR HAS NO OUTPUT.
Part: STARTER — FAILED (ENGINE)
DURING 250 HOUR INSPECTION, FAILED CLUTCH SLIPPAGE TORQUE TEST. BREAKAWAY WAS AT AROUND 450 INCH/POUNDS, LIMITS ARE 325 TO 375 INCH/POUNDS.
Part: ACTUATOR ASSY — FAILED (ELEVATOR SYS)
ACTUATOR ASSY WILL NOT MONITOR TEST AND KEEPS KICKING OFF-LINE.
Part: TRANSCEIVER — FAILED (COCKPIT DME)
TRANSCEIVER HAS BURNED COMPONENTS INTERNALLY.
Part: BAG — LEAKING (FLOAT)
FLOAT BAG LEAKS.
Part: HOSE — LOOSE (SERVO)
EXPERIENCED NR 2 HYDRAULIC SYSTEM PRESSURE DROP AND ILLUMINATION OF CAUTION LIGHT IN-FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HOSE LOOSE AT SERVO FITTING, TIGHTENED SAME. REF: 214ST IPC, CHAPTER 29-99-00, FIGURE 29-5, ITEM 23.
Part: INDICATOR — FAILED (COCKPIT)
ATTITUDE INDICATOR SLOW TO ERECT AND FALLS OFF-LINE AFTER 10 MINUTES.
Part: STROBE — INOPERATIVE (EXTERNAL LIGHTS)
STROBE LIGHT INOPERATIVE.
Part: PROBE — INACCURATE (FUEL QUANTITY)
TRANSMITS INACCURATE READINGS.
Part: SENSOR — MALFUNCTIONED (SCAS SYSTEM)
SCAS WILL NOT STAY ENGAGED.
Part: AMPLIFIER — FAILED (FBWE)
WILL NOT MOTION TEST NOR WILL ELEVATORS STAY EMERGED.
Part: ACTUATOR ASSY — FAILED (ELEVATOR SYS)
ACTUATOR ASSY ELEVATOR WILL NOT STAY ON-LINE.
Part: AMPLIFIER — FAILED (FBWE)
ELEVATOR WILL NOT STAY ENGAGED.
Part: DRIVE ASSY — INOPERATIVE (RADAR ANNTENA)
TILT INOPERATIVE.
Part: DRIVE ASSY — INOPERATIVE (RADAR ANNTENA)
DRIVE ASSY INOPERATIVE.
Part: TRANSCEIVER — FAILED (COCKPIT)
NO DISPLAY, ELECTRICAL BURNING SMELL WHEN TURNED ON.
Part: DRIVE ASSY — INOPERATIVE (RADAR ANNTENA)
TILT CONTROL HAS NO EFFECT ON ANTENNA.
Part: TRIPLEX BEARING — SPALLED (SWASHPLATE)
RECEIVED INPUT QUILL ASSEMBLY P/N 214-040-019-101 INTO OVERHAUL SHOP DUE TO METAL. FOUND TRIPLEX BEARING SET TO BE SPALLING, CAUSING METAL IN OIL.
Part: STARTER — MALFUNCTIONED (START/GEN)
STARTER PREMATURELY DISENGAGES.
Part: SHAFT — FAILED (BLOWER ASSY)
BLOWER SHAFT SHEARED.
Part: AMPLIFIER — FAILED (AFCS)
AMP WILL NOT STAY ON LINE. TIME SINCE REPAIR 0:00.
Part: INDICATOR — READS LOW (OIL SYSTEM)
INDICATOR READING LOW PRESSURE, INDICATOR FAILED COMMON MODE TEST.
Part: RATE GYRO — FAILED (COCKPIT)
NEEDLE DEFLECTS RIGHT ON RATE GYRO.
Part: ADF — INOPERATIVE (COCKPIT)
POINTER ON ADF RECEIVER INOPERATIVE.
Part: TRANSCEIVER — FAILED (COCKPIT)
RT FAULT DISPLAYED AND DOES NOT TRANSMIT. PERFORMED PRELIMINARY INSPECTION.
Part: LINE — BROKEN (NR 2 ENGINE)
NR 2 ENGINE SPOOLED DOWN IN-FLIGHT. SECURED ENGINE AND CONTINUED ON TO LAND BASE. MADE SINGLE ENGINE LANDING WITHOUT INCIDENT. MAINTENANCE FOUND AIR LINE BROKEN. REF: GENERAL ELECTRIC CT7 IPC, CHAPTER 72-00-00, FIGURE 1, ITEM 10.
Part: MOTOR — FAILED (BLOWER)
HYDRAULIC MOTOR SLOW TURNING; WILL NOT TURN OUT OIL COOLER CAUTION LIGHT AT GROUND IDLE.
Part: INDICATOR — FAILED (COCKPIT)
INDICATOR CANNOT MATCH TORQUES ON ENGINE.
Part: STARTER — FAILED (START/GEN)
STARTER/GENERATOR BURNT.
Part: AFCS — MALFUNCTIONED (COCKPIT)
AFCS LIGHT WILL NOT COME ON.
Part: ACTUATOR — INOPERATIVE (M/R)
STEP MOTOR IS INOPERATIVE.
Part: AFCS — MALFUNCTIONED (COCKPIT)
AFCS WILL NOT COME ON.
Part: COMPUTER — MALFUNCTIONED (AUTO FLIGHT)
AUTOFLIGHT COMPUTER PRODUCES 5 ERRORS ON CDI WHEN CAP TO GPS OR VOR.
Part: TRANSDUCER — FAILED (COCKPIT)
TRANSDUCER CAUSES FAIL 6 ON ADC.
Part: INDICATOR — INOPERATIVE (TRIPLE TACH)
COPILOT TRIPLE TACH PEGS OUT OCCASIONALLY.
Part: REGULATOR — MALFUNCTIONED (AC SYSTEM)
GENERATOR WOULD NOT STAY ON LINE.
Part: REGULATOR — FAILED (DC SYSTEM)
GENERATOR WOULD NOT STAY ON LINE.
Part: CAUTION PANEL — DEFECTIVE (COCKPIT)
ANTI-ICE LIGHT WILL NOT COME ON FOR NR 1 ENGINE.
Part: INDICATOR — INTERMITTENT (TRIPLE TACH)
INDICATOR INTERMITTENT.
Part: INDICATOR — FAILED (COCKPIT HIS)
POINTER IS OFF BY 13 WHEN DIGITS ARE AT ZERO.
Part: RESTRAIN SYS — MALFUNCTION (COCKPIT)
RESTRAIN SYS WILL NOT LOCK PROPERLY.
Part: STARTER — FAILED (ENGINE)
STARTER DISENGAGES AFTER 3 SECONDS.
Part: CARTRIDGE — DEFECTIVE (BOOST PUMP)
A/C STUD BROKEN OFF.
Part: INDICATOR — FAILED (ELEV POSITION)
ELEV POSITION INDICATOR INOPERATIVE.
Part: INDICATOR — FAILED (ENG OIL)
PRESSURE NEEDLE FLUCTUATES WHEN VIBRATED.
Part: LIFE RAFT — DEFECTIVE (EMERG EQUIP)
WILL NOT FIT IN THE AIRCRAFT.
Part: PROBE — FAILED (FUEL SYS)
PROBE WILL NOT TEST.
Part: INDICATOR — FAILED (TRIPLE TACH)
TRIPLE TACH INDICATOR INTERMITTENT.
Part: PROBE — FAILED (FUEL SYS)
PROBE WILL NOT TEST.
Part: AFCS — INTERMITTENT (ANNUN PANEL)
AFCS ENGAGE INTERMITTENT.
Part: NAV UNIT — FAILED (COCKPIT)
NAV UNIT DOES NOT DRIVE POINTER.
Part: AMPLIFIER — FAILED (AUTO FLIGHT)
AMPLIFIER FAILED MONITOR TEST.
Part: AMPLIFIER — FAILED (AUTOFLIGHT)
AMPLIFIER FAILED MONITOR TEST.
Part: TRANSMITTER — FAILED (FLUX VALVE)
TRANSMITTER EXCESSIVE READINGS.
Part: TRANSMITTER — FAILED (FLUX VALVE)
TRANSMITTER READS LOW OUT OF TOLERANCE.
Part: INDICATOR — DEFECTIVE (VERT SPEED)
INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79.
Part: INDICATOR — DEFECTIVE (COCKPIT)
INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79.
1997
Part: INDICATOR — STICKS (COCKPIT)
AIRSPEED INDICATOR STICKS AT ZERO.
Part: ALTIMETER — FAILED (COCKPIT)
ALTIMETER HAS EXCESSIVE FRICTION ERROR AND ENCODER IS OUT OF TOLERANCE.
Part: TORSION ARM — TORN (M/R XMSN)
TORSION ARM BEARINGS TORN.
Part: SEAT — CORRODED (ROTOR SHAFT)
CORROSION AT CENTER BORE (SEAT) WHERE BEARING P/N 214-030-602-3 IS INSTALLED. REPLACED WITH NEW SUPPORT.
Part: BLADE — CRACKED (M/R)
M/R BLADE LOWER PRIMARY GRIP PAD CRACKED.