N104PH
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.
18 reports on file, 1995-08-02 – 1999-02-23.
Part: INDICATOR — STICKS (FUEL QUANTITY)
FUEL QUANTITY INDICATOR'S NEEDLE STICKS LOW AND HIGH ENDS OF SCALE INACCURATE.
Part: ACTUATOR — INOPERATIVE (MAIN ROTOR)
ACTUATOR HAS NO MOVEMENT OR ACTIVATION.
Part: PUMP — CORRODED (OIL SYSTEM)
STUDS CORRODED ON PUMP ASSEMBLY.
Earlier reports · 1995–1998 · 15 reports
1998
Part: ACTUATOR — MALFUNCTIONED (MAIN ROTOR)
ACTUATOR INTERMITTENTLY STICKS IN EXTENDED POSITION.
Part: BEACON — FAILED (LOCATOR)
BEACON WOULD NOT TEST WHEN INSTALLED IN MOUNT.
Part: RECEIVER — INOPERATIVE (GPS)
GPS RECEIVER WILL NOT COME ON. PERFORMED PRELIMINARY INSPECTION AND FOUND BURNED COMPONENT ON IOP/POWER SUPPLY BOARD.
Part: COUPLING — WORN (ENGINE N1)
ENGINE REMOVED DUE TO TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED: N1 COUPLING FAILED NO-GO GAUGE. INSTALLED A NEW N1 COUPLING.
Part: TRANSCEIVER — FAILED (COCKPIT)
RADIO POWERS OFF BY ITSELF. (NO DISPLAY) VERIFIED COMPLAINT. PERFORMED PRELIMINARY INSPECTION AND FOUND UNIT TO HAVE NO DISPLAY DUE TO BURNT SPOT ON DISPLAY BOARD.
Part: TRANSCEIVER — FAILED (COCKPIT)
TRANSPONDER INOPERATIVE.
1997
Part: INDICATOR — FAILED (ENG TOT)
READS HIGH OUT OF TOLERANCE. NEEDLE STICKS AT 800 DEGREES. SENT TO MASCO FOR INSPECTION AND REPAIR.
Part: TRANSPONDER — MALFUNCTION (COCKPIT ATC)
TRANSMITS DIFFERENT CODE NUMBERS THAN SELECTED CODE. PERFORMED PRELIMARY INSPECTION, CLEANED WAFER SWITCHES. REPAIRED. REPLACED C401 AND C402 CAPACITORS. REPAIRED. BENCH CHECK GOOD.
Part: ACTUATOR — INOPERATIVE (ENGINE)
ENGINE LINEAR ACTUATOR INOPERATIVE.
Part: GPS 150 — FAILED (COCKPIT GPS)
GPS 150 WOULD NOT PICK UP SATELLITES.
Part: ALTIMETER — STICKS (COCKPIT)
ALTIMETER 100 FEET OFF; NEEDLE STICKS THROUGHOUT SCALE.
1996
Part: WHEEL — DEFECTIVE (1ST STAGE)
TURBINE REMOVED DUE TO 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: MINOR SULFIDATION ON ALL 1ST STAGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL.
Part: GP SUPPORT — DEFECTIVE (NR 8 BEARING)
RECEIVING INSPECTION REVEALED: .0015 OVERSIZED ON GP SUPPORT #8 BEARING BORE I.D. B/P SPECS. (1.7050 - 1.7060) REQUESTING 100% WARRANTY REPAIR PER DAVID MENARD AND ROB HALDEMAN. THIS UNIT OVERHAULED ON DALLAS AIRMOTIVE W/O LF0828.
Part: GPS 150 — INOPERATIVE (COCKPIT GPS)
INOPERATIVE AND KNOB ALSO MISSING. TIME SINCE REPAIR 0:00.
1995
Part: GPS 150 — MALFUNCTION (COCKPIT)
UNIT GOES FROM SELF-TEST TO OPERATE TO SELF-TEST, ETC. CONTINUOUSLY. SENT TO GARMIN INTERNATIONAL FOR WARRANTY REPAIR.