N911RC
Registered owner: SHAMO SHELENA, UT (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.
17 reports on file, 1999-05-28 – 2004-04-01.
Part: STARTER GEN — FAILED (NR 2) · airframe 3,211 hrs
DURING CRUISE FLIGHT, NR 2 DC GENERATOR LIGHT ILLUMINATED. PILOT FOLLOWED AIRCRAFT EMERGENCY CHECKLIST FOR SINGLE DC GENERATOR FAILURE AND LANDED AIRCRAFT. MAINTENANCE REPLACED NR 2 STARTER GENERATOR.
Earlier reports · 1999–2003 · 16 reports
2003
Part: CONNECTOR — CONTAMINATED (NR2 OVRSPD CONT) · airframe 3,000 hrs
DURING FLIGHT, NR2 ENGINE OVERSPEED LIGHT ILLUMINATED. MAINTENANCE CLEANED OIL CONTAMINATION FROM THE CONNECTOR TO THE NR 2 ENGINE OVERSPEED CONTROL.
Part: ISOLATION MOUNT — DAMAGED (AUTOFLIGHT) · airframe 2,765 hrs
SEPERATION BETWEEN ELASTOMER AND CENTER PORTION OF MOUNT.
Part: TRANSPONDER — INTERMITTENT (ATC) · airframe 2,677 hrs
ATC TRANSPONDER FOUND FAULTY. INTERMITTENT OPERTION. CONTROL HEAD WILL DISPLAY "FAIL". IN SHOP REPAIR.
Part: SEARCH LIGHT — MALFUNCTIONED (EXTERIOR) · airframe 2,491 hrs
SEARCH LIGHT DOES NOT RETRACT ALL THE TIME.
Part: COUPLING — LEAKING (MAIN ROTOR)
COUPLING LEAKING GREASE. REPLACED OUTER COUPLING DUE TO PITTING IN RETAINER GROOVE. REPAIRED.
2002
Part: GEARBOX — SHORTED (SEARCH LIGHT) · airframe 2,369 hrs
SEARCH LIGHT HAS AN ELECTRICAL SHORT LOCATED IN THE ROTATION AXIS GEARBOX.
Part: COMPUTER — DAMAGED (AUTO PILOT) · airframe 2,162 hrs
FOUND PROBLEM TO BE IN THE "FORCE TRIM CB ON" LOGIC. PREFLIGHT TEST IS NORMAL HOWEVER AUTOPILOT WILL NOT ENGAGE. ENTERED DIAGNOSTIC MODE AND INTO THE DISCRETE I/O SCREEN. FOUND BIT NR 13 OF PORT 1 IN THE DISCRETE INPUTS TO BE "1" WITH THE FORCE TRIM CB IN. CYLCED THE CB REPEATEDLY AND THE INPUT RESPONSE WAS INTERMITTENT. CHECKED FOR PROPER VOLTAGE AND GENERAL CONDITION OF PIN 56 IN RACK CONNECTOR 9A1P2 AND CHECKED OK.
Part: BRUSHES — WORN (STARTER GEN)
STARTER GEN HAS WORN BRUSHES.
Part: COMPUTER — FAILED (AUTO PILOT) · airframe 1,786 hrs
COMPUTER WILL NOT ENGAGE AUTO PILOT WHEN AP BUTTON IS DEPRESSED.
Part: BRUSHES — WORN (STARTER GEN)
STARTER GEN BRUSHES EXCESSIVELY WORN.
Part: INDICATOR — MALFUNCTIONED (ENGINE NG) · airframe 2,059 hrs
ENGINE NG INDICATOR HAS A FLUCTUATING NEEDLE.
Part: GYRO — FAILED (COCKPIT) · airframe 1,715 hrs
INOPERATIVE WITH ATTITUDE FAIL DISPLAYED ON EADI. SENT TO GREATLAKES AVIONICS FOR INSPECTION AND REPAIR.
2001
Part: BEARING — DELAMINATED (MAIN ROTOR) · airframe 1,715 hrs
DELAMINATION. PENDING VENDOR REPAIR.
Part: INDICATOR — PRECESSES (ATTITUDE) · airframe 1,690 hrs
INTERMITTENT PROBLEM OF PRECESSING 30 DEGREES. REPLACED WITH SERVICEABLE PART.
1999
Part: PITCH CONTROL — MALFUNCTIONED (MAIN ROTOR)
BRAKE WILL NOT ENGAGE WHEN AUTOPILOT IS TURNED OFF, BUT WILL ENGAGE WHEN TAPPED ON.
Part: LIGHT — INOPERATIVE (FUSELAGE)
INOPERATIVE, NO MOVEMENT BUT LIGHT WORKS.