N41299
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.
3 reports on file, 2013-10-06 – 2017-09-25.
Part: TAIL ROTOR — CRACKED · airframe 4,395 hrs · 13,862 cycles
DURING THE TAIL ROTOR 600HR/24 MONTH AIRFRAME INSPECTION (A 1660) FOUND 2EA "SPLITS" ON SLOPE. NOTE: ONLY 1 DAMAGE AREA PER SLOPE SHALL BE PERMITTED PER AMM. INSPECTION WAS CARRIED IAW AMM 64-10-00, 6-3. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION DUE TO OTHER SCHEDULED MAINTENANCE REQUIREMENTS.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 3,795 hrs · 11,741 cycles
DURING THE INITIAL INSPECTION OF BOTTOM STRUCTURE, CORROSION LOCATED ON RT MAIN BEAM DOUBLER & AFT CTR CROSS BEAM, INTERSECTING AT RT JACK PAD, AS SEEN IN SRM 53-10-02,02. CTR RT BEAM Y398.5 DETAIL B, IT 21 INTERSECTING AT LT & RT SIDE & CTR CROSS BEAMS X2325 DETAIL I, IT 37A.
Part: CONTROLLER — BINDING (MAIN ROTOR) · airframe 3,144 hrs · 9,622 cycles
PILOT FELT RESISTANCE IN THE FORE AND AFT CYCLIC PITCH CONTROL ON APPROACH. TROUBLESHOOTING AND TALKING TO TECH REP, DETERMINED THAT THE PITCH MAIN ROTOR SERVO IS FAILING INTERNALLY. THIS SERVO CONTROL WAS R & R, WITH THE SUBSEQUENT OPERATIONAL GROUND AND FLIGHT CHECKED GOOD. NO DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.