N2758N
Registered owner: LOWE JERRY W, VA (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.
27 reports on file, 1995-05-24 – 1999-08-09.
Part: VOLT REGULATOR — FAILED (DC SYSTEM)
GENERATOR WILL NOT COME ON-LINE.
Part: INDICATOR — INOPERATIVE (TOT)
TOT INDICATOR INOPERATIVE.
Part: VOLT REGULATOR — MALFUNCTIONED (DC SYSTEM)
AMMETER SPIKES WHEN RADIO MIKE KEYED ON VOLTAGE REGULATOR.
Part: INDICATOR — INOPERATIVE (COCKPIT)
INDICATOR'S PRESSURE NEEDLE INOPERATIVE.
Part: INDICATOR — READS LOW (FUEL QUANTITY)
FUEL QUANTITY INDICATOR HAS A CRACKED GLASS AND READS LOW AT 400 POUNDS AND ABOVE.
Part: FITTING — WRONG PART (ENGINE OIL)
WRONG TYPE FITTING INSTALLED ON HOSE ASSEMBLY.
Part: SKIN — DENTED (HORIZ STAB)
FIN ASSEMBLY HAS HOLE IN LEADING EDGE, DENTED, AND SEPARATED.
Earlier reports · 1995–1998 · 20 reports
1998
Part: INDICATOR — MALFUNCTIONED (COCKPIT)
TOT NEEDLE STICKS ON START-UP.
Part: INDICATOR — READS HIGH (COCKPIT)
TOT INDICATOR READS 10 PERCENT HIGH ABOVE 500 AFTER UNIT IS WARM.
Part: IMPELLER — CORRODED (BLOWER)
BLOWER IMPELLER EXCESSIVELY CORRODED. SCRAPPED ASSY AND REPLACED WITH NEW ASSY.
Part: PANEL — MISMANUFACTURED (FUSELAGE)
PANEL ASSEMBLY MISMANUFACTURED. PANEL WAS TRIMMED .1250 INCH TOO SMALL, COULD NOT GET GOOD EDGE DISTANCE FOR SCREW HOLES.
Part: DOOR — CORRODED (FUSELAGE)
DOOR ASSEMBLY CORRODED AND SEPARATED BEYOND REPAIR AT THIS STATION.
Part: CROSSTUBE — CORRODED (MLG)
CORROSION AND PITTING DAMAGE AT SKID TUBE MOUNTING POINT EXCEEDING LIMITS. SCRAPPED CROSSTUBE.
Part: BELLCRANK — CHAFED (TAIL ROTOR)
BELLCRANK CHAFED BEYOND LIMITS. SCRAPPED BELLCRANK AND REPLACED WITH SERVICEABLE PART.
Part: DISC SET — CORRODED (TAIL ROTOR)
DISC CORRODED AND PITTED. REPLACED WITH SERVICEABLE PARTS.
Part: SUPPORT — CORRODED (COCKPIT)
SUPPORT HAS CORROSION AND PITTED BEYOND LIMITS. REPLACED WITH SERVICEABLE SUPPORT.
Part: INDICATOR — CRACKED (COCKPIT TOT)
TOT INDICATOR INTERMITTENT AND GLASS FACE CRACKED.
Part: INDICATOR — INTERMITTENT (COCKPIT TOT)
TOT INDICATOR INTERMITTENT.
Part: COOLER — FAILED (ENGINE OIL)
INSTALLED OIL COOLER FROM STOCK AND RAN AIRCRAFT. ENGINE OIL TEMP WAS HIGH.
Part: ACTUATOR — FAILED (M/R)
ACTUATOR INOPERATIVE.
1997
Part: TRANS RESTRAINT — WORN (M/R)
WORN BEARINGS AND UNSTAKED.
Part: INDICATOR — FAILED (ENG OIL)
INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DID NOT WORK. SCRAPPED INDICATOR AND REPLACED WITH SERVICEABLE PART.
Part: ELT — MALFUNCTION (COCKPIT)
ELT STAYS ON AND WILL NOT SHUT OFF.
Part: NOZZLE — CRACKED (NR 2)
ENGINE REMOVED DUE TO HIGH T.O.T. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON #2 NOZZLE FWD INNER BAND, AFT INNER BAND WELDMENT SEPARATING AND CRACK VANES. INSTALLED A NEW #2 NOZZLE.
Part: SHROUD HOUSING — OVER SPECS (ENGINE)
RECEIVING INSPECTION REVEALED: MEASURED .005 TO .007 OVER SPECS (10.199 - 10.200) ON SHROUD HOUSING AFT PILOT. INSTALLED A DALLAS AIRMOTIVE OVERHAULED SHROUD HOUSING.
1995
Part: BATTERY — WEAK (DC SYS)
BATTERY HOT LIGHT. INSPECTED BY ACCESSORY SHOP: VOLTAGE READING TAKEN AS RECEIVED. FOUND BATTERY WEAK.
Part: WHEEL — SULFIDATION (1ST STAGE BLADES)
ENGINE REMOVED DUE TO TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: SULFIDATION ON ALL 1ST STAGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL.