N5416F
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.
6 reports on file, 1995-05-29 – 2001-08-03.
Part: TURBINE WHEEL — BROKEN (ENGINE)
TURBINE RECEIVED FROM FIELD, REMOVED COMB CASE FOUND SULPHADATION ON NR 1 WHEEL. WHEEL HAS BROKEN BLADES DUE TO SULPHADATION. (M)
Part: WIRE — BROKEN (FIRE DETECTION) · airframe 8,364 hrs
WHILE HOVERING TO REFUELING POINT, WIRE BROKEN OFF AT A TERMINAL END FOR THE NR 1 LOWER SENSOR.
Part: FIRE DETECTOR — SHORTED (NR 1 ENGINE)
DURING PRESTART CHECK. AFT PROBE SHORTED TO ELBOW ON ENGINE AIR SYSTEM.
Part: HYDRAULIC PACK — FAILED (NR 2 HYD)
AIRCRAFT AT HOVER. DURING HOVER, HYDRAULIC BLOCK LIGHT ILLUMINATED. NR 2 HYDRAULIC ENGAGED LIGHT ILLUMINATED AND COLLECTIVE DROPPED TO LOW STOP. AIRCRAFT RECOVERED PRIOR TO IMPACT. HYDRAULIC PACK CHANGED, AIRCRAFT CHECK FLOWN AND RETURNED TO SERVICE. (X)
Part: HOUSING — CRACKED (RT MOUNT STUD)
DAILY INSPECTION FOUND TAIL ROTOR GEAR BOX CASE CRACKED AT RIGHT MOUNTING STUD.
Part: LAMINATED PACK — CORRODED (INNER SLEEVE)
UPON INSPECTION OF PARTS FOR REPAIR OF TAIL ROTOR ASSEMBLY, FOUND CORROSION BEYOND LIMITS ON CENTER SECTION OF LAMINATED PACK DUE TO SALT ATMOSPHERE IN WHICH THE AIRCRAFT FLIES. PART WAS SCRAPPED DUE TO CORROSION BEYOND LIMITS.