N5742H
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.
17 reports on file, 1995-05-23 – 1998-08-20.
Part: NOZZLE — DAMAGED (ENGINE)
ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE VANES AND OUTER SHROUD.
Part: NOZZLE — DAMAGED (ENGINE)
ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED: COATING LIFTING FROM NR 2 NOZZLE 1ST AND 2ND STAGE TIP PATH.
Part: STARTER — FAILED (START/GEN)
STARTER/GENERATOR ARCHING AND GENERATOR WILL NOT COME ON LINE. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN AND COMMUTATOR BURNED AND PITTED.
Earlier reports · 1995–1997 · 14 reports
1997
Part: ENGINE — FAILED (OIL SYSTEM)
IN-FLIGHT, ENGINE OIL PRESSURE AND TORQUE PRESSURE BEGAN TO FLUCTUATE. LANDED ON OFFSHORE PLATFORM WITHOUT INCIDENT. MAINTENANCE FOUND OIL TANK LEVEL SEVERAL QUARTS LOW. REPLACED ENGINE ASSY.
Part: INDICATOR — INOPERATIVE (TOT)
TOT INDICATOR FAILED. NEEDLE STICKS
Part: FIN ASSY — SEPARATED (VERT FIN)
FIN ASSY CORRODED AND SEPARATED BEYOND REPAIR.
Part: TRANSPONDER — INOPERATIVE (COCKPIT ATC)
TRANSPONDER UNIT INOPERATIVE. TEST LIGHT WILL NOT COME ON.
Part: TACH GEN — MALFUNCTION (M/R)
TACH GEN SUSPECT BEARING OIL SOAKED.
Part: OIL COOLER — DEFECTIVE (ENG OIL)
HIGH ENGINE OIL TEMPERATURE. ENG OIL COOLER MALFUNCTION.
Part: NOZZLE — DEFECTIVE (NR 2)
RECEIVED PART FROM MACHINE SHOP. INSPECTION REVEALED; TIP PATH LIFTING ON #2 NOZZLE #2 TIP AS MARKED. INSTALLED A STANDARD AERO OVERHAULED #2 NOZZLE.
Part: INDICATOR — ERROR (GAS PRODUCER)
GAS PRODUCER INDICATOR EXCESSIVE FRICTION ERROR.
Part: ACTUATOR — BEARING FROZEN (M/R CONTROL)
ACTUATOR BEARING FROZEN.
1996
Part: SENSOR — DEFECTIVE (ROTOR RPM)
SENSOR DEFECTIVE. LOW ROTOR LIGHT WILL NOT COME ON. REPLACED WITH SERVICEABLE SENSOR.
Part: NOZZLE — CRACKED (NR 1 NOZ VANE)
ENGINE REMOVED DUE TO HIGH OIL CONSUMPTION. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED AND BOWED BEYOND SERVICEABLE LIMITS ON #1 NOZZLE VANES. REPLACED DISCREPANT PART.
Part: RESTRAINT — WORN EXCESS (TRANSMISSION)
RESTRAINT IS WORN EXCESSIVELY. (BEARING WORN)
1995
Part: BATTERY — WEAK (DC SYS)
BATTERY WEAK. INSPECTED BY ACCESSORY SHOP. THIS BATTERY HAS BEEN LEAD TESTED AND FOUND TO BE WEAK AS RECEIVED. FURTHER INSPECTION FOUND ELECTROLYTE DISCOLORED AND BATTERY FAILED TO COME UP TO REQUIRED 1.55 VOLTS AT END OF CHARGE.
Part: SUPPORT — REQ REPLACEMENT (SWASHPLATE)
AS PER ASB 206L-93-89 REV. B (REPLACEMENT OF -109 SUPPORT WITH -113 SUPPORT)