N5010F
Registered owner: NORTON COLE R, IA (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.
42 reports on file, 1995-08-31 – 2001-04-19.
Part: INDICATOR — FAILED (RADAR) · airframe 14,347 hrs
DOES NOT PAINT TARGETS. FOUND UNIT HAS NO NOISE, ADJUSTED AUTOMATIC NOISE CONTROL. TROUBLESHOT VIDEO BOARD AND REPLACED R1450 RESISTOR. REPAIRED. BENCH CHECK GOOD.
Earlier reports · 1995–1999 · 41 reports
1999
Part: VALVE — INOPERATIVE (CROSSFEED)
VALVE INOPERATIVE.
Part: INDICATOR — INTERMITTENT (FUEL PRESSURE)
FUEL PRESSURE INDICATOR INTERMITTENTLY STICKS AT ZERO.
Part: INDICATOR — ERRATIC (FUEL PRESSURE)
FUEL PRESSURE INDICATOR HAD UNRELIABLE ERRATIC READINGS.
Part: INDICATOR — READS HIGH (DUAL AMMETER)
AMMETER READS 50 AMPS HIGHER.
Part: GYRO — FAILED (COCKPIT)
NO TURN INDICATIONS DISPLAY ON GYRO.
Part: INDICATOR — INTERMITTENT (ATTITUDE)
INDICATOR OPERATES INTERMITTENTLY.
Part: BRAKE ASSY — MALFUNCTIONED (MAIN ROTOR)
WHEN ROTOR BRAKE CALIPERS WERE INSTALLED, INBOARD MICROSWITCH CONTACTS ROTOR BRAKE QUILL HOUSING. INBOARD MICROSWITCH WAS INSTALLED DIFFERENT ON THIS CALIPER ASSY THAN THE ONE REMOVED. SCRAPPED SWITCH ASSY ON INBOARD SIDE OF ROTOR BRAKE CALIPER.
Part: TARSYN — FAILED (COCKPIT)
UNIT DOES NOT SLAVE IN MAGNETIC COMPASS MODE. UNIT FUNCTION GOOD ON SST BENCH.
Part: INDICATOR — STICKING (TORQUE METER)
TORQUE METER INDICATOR'S NR 1 NEEDLE STICKS.
1998
Part: GYRO — INOPERATIVE (COCKPIT)
GYRO INOPERATIVE.
Part: TRANSPONDER — MALFUNCTIONED (COCKPIT)
TRANSPONDER HAS LOW POWER. TIME SINCE REPAIR 0:00 HOURS.
Part: CONTROL UNIT — FAILED (DC CONTROL)
CONTROL UNIT WILL NOT COME ON LINE.
Part: TRANSPONDER — FAILED (COCKPIT)
NO CODE TRANSMITTER. NO REPLY LIGHT. NO TEST LIGHT. TIME SINCE REPAIR 0:00 HOURS.
Part: TARSYN — FAILED (AUTOFLIGHT)
TARSYN FAILS TEST 8.5 ON SST.
Part: INDICATOR — FAILED (COCKPIT HSI)
NO ADF POINTER INFO DISPLAYED.
Part: INDICATOR — STICKING (COCKPIT ITT)
ITT INDICATOR STICKS AT 580 DEGREES.
Part: INVERTER — MALFUNCTIONED (AC SYSTEM)
INVERTER TRIPS CIRCUIT BREAKER.
Part: TARSYN — FAILED (AUTOFLIGHT)
TARSYN - PIN C OF BOTTOM CONNECTOR HAS PINS BACKING OUT OF CONNECTOR.
Part: INDICATOR — FAILED (HYDRAULIC SYS)
HYDRAULIC PRESSURE NEEDLE WILL NOT RETURN TO ZERO.
Part: INVERTER — FAILED (AC SYSTEM)
INVERTER WOULD NOT COME ON LINE AT INITIAL INSTALLATION FROM STOCK.
Part: VALVE — INCORRECT (COMPASS)
COMPASS HAS INCORRECT HEADINGS, OUTPUT UNRELIABLE.
Part: CONTROL — MALFUNCTIONED (COCKPIT HF)
LEDS LIGHT UP, DISPLAY BAD.
Part: GYRO — FAILED (COCKPIT)
RT FLAG ON ADI NOT PULLED.
Part: INDICATOR — FAILED (COCKPIT HSI)
GS FLAG WILL NOT PULL.
Part: FLUX VALVE — INACCURATE (COMPASS)
READING IS OFF 80 DEGREES.
Part: INDICATOR — STICKING (COCKPIT HSI)
HSI INDICATOR'S TO/FROM FLAG STICKS, NR 2 BEARING POINTER RATCHETS.
Part: EJECTOR — CRACKED (EXHAUST)
LEFT EJECTOR ASSEMBLY'S WELDS ARE CRACKED AND HAS LOOSE RIVETS.
Part: TARSYN — FAILED (COCKPIT)
DIRECTIONAL GYRO HAS NO SYNCHRO HEADING OUTPUT. TIME SINCE REPAIR, 7:15 HOURS.
1997
Part: LINK ASSY — WORN (M/R)
LINK ASSY HAS EXCESSIVE PLAY.
Part: INDICATOR — FAILED (ALTIMETER)
INDICATES 3000 FEET AT FIELD ELEVATION
1996
Part: VALVE — INTERMITTENT (FUEL SYS)
INOPERATIVE, CYCLES INTERMITTENT.
Part: TRANSCEIVER — MALFUNCTION (COCKPIT)
FREQUENCY DOES NOT SHOW TILL 20 OR 30 MINUTES.
Part: INDICATOR — FAILED (COCKPIT)
INDICATOR CAUSES R/T NOT TO TRANSMIT.
Part: TRANSCEIVER — FAULTY (COCKPIT VHF)
AFTER UNIT HEATS UP, MODULATION BEGINS TO BREAK UP.
Part: BEARING — FAILED (T/R DRIVE)
DUST SHIELD SPINNING. REPLACEMENT PART PURCHASED AS PER ASB212-95-95 REV. B.
Part: BEARING — FAILED (T/R DRIVE)
DUST SHIELD SPINNING.
Part: BEARING — FAILED (T/R DRIVE)
DUST SHIELD SPINNING. REPLACEMENT PART PURCHASED AS PER ASB212-95-95 REV. B.
Part: TRANSCEIVER — MALFUNCTION (COCKPIT VHF)
TRANSCEIVER WILL NOT TUNE.
Part: VALVE — MALFUNCTION (FUEL SYS)
VALVE INOPERATIVE. CYCLES CONSTANTLY.
1995
Part: BLADE — DENTED (T/R)
TR BLADE HAS DENT ON TRAILING EDGE.
Part: CONTROL UNIT — FAILED (NR 1 GENERATOR)
#1 GENERATOR FAILS TO COME ON LINE. RELAY 212-075-199-1 BLOWS IT OUT. REPLACED Q4 TRANSISTOR P/N 05-990044. BENCH CHECK OK.