N911BY
Registered owner: AMERICAN HONOR FOUNDATION INC, FL (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.
87 reports on file, 1995-03-31 – 2008-09-13.
Part: COMPUTER — FAULTED (YAW)
WHILE RETURNING TO BASE, CREW NOTICED AN INCREASING STRONG ELECTRICAL ODOR AS THE ACFT TURNED FINAL. CONTINUED TO THE LANDING AREA AND PUT THE ACFT OUT OF SERVICE. CREW SAW NO SMOKE BUT ONLY THE ODOR. MAINTENANCE FOUND YAW COMPUTER TO BE FAULTY AND REPLACED IT. NO CIRCUIT BREAKERS WERE DISPLACED AND LOAD METERS READ NORMAL THROUGHOUT THE EVENT. THERE WERE NO OTHER ABNORMALITIES OR DAMAGES. (K)
Earlier reports · 1995–2001 · 86 reports
2001
Part: SHROUD — WORN (GAS PRODUCER)
EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
2000
Part: NOZZLE — CRACKED (FUEL INJECTOR)
CRACKED BEYOND SERVICEABLE (NOT REPAIRABLE) LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: HARNESS — SHORTED (ENGINE)
INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL RING — WORN (TURBINE SHROUD)
WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM.
Part: SHROUD — DAMAGED (TURBINE ROTOR)
EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — WARPED (GAS PRODUCER)
EXCESSIVE WARPAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SPRING — WORN (SEAL RING)
WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM.
Part: BEARING — DAMAGED (ENGINE)
EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: LIGHT — WORN (TAIL)
CLEAR TAIL LIGHT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: BEARING — WORN (TAIL ROTOR)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH2 EACH NEW UNITS, CORRECTED PROBLEM. (X)
Part: SEAL — LEAKING (CSD) · airframe 6,863 hrs
LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: DIFFUSER — CRACKED (ENGINE)
DIFFUSER ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SEAL — WORN (1ST TURBINE) · airframe 6,863 hrs
SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: CURL — BURNED (COMBUSTION CHAMB) · airframe 6,863 hrs
EXCESSIVE BURN IN SOME AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SEAL — LEAKING (NR 3 BEARING) · airframe 6,863 hrs
LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SHROUD — DAMAGED (GAS PRODUCER) · airframe 6,863 hrs
EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SEAL — LEAKING (NR 2 BEARING) · airframe 6,863 hrs
LEAKING BYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SEAL — WORN (WORN)
WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
1999
Part: BLADE — WORN (GAS PRODUCER)
EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SEAL — WORN (TURBINE SHOUD)
SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SEAL — LEAKING (NR 2 BEARING)
SEAL, NR 2 BEARING, LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SEAL — MELTED (NR 3 BEARING)
SEAL, NR 3 BEARING, LEAKING BEYOND SERVICE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: GUIDE — WORN (LEFT DOOR)
WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: CATCHER — WORN (LEFT DOOR)
CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: CATCHER — WORN (RT DOOR)
CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — LEAKING (NR 2 BEARING)
SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: MANIFOLD — MALFUNCTIONED (FUEL SYSTEM)
IMPROPER NOZZLE SPRAY PATTERN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SHROUD — DAMAGED (GAS PRODUCER)
SHROUD HAD EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (TAIL ROTOR)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: LEAD — WORN (IGNITION SYSTEM)
LEAD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (TAIL ROTOR)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (TAIL ROTOR)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
1998
Part: BEARING — WORN (TAIL ROTOR)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: ROTOR ASSY — DAMAGED (POWER TURBINE)
FAILED SB LT101-72-10-0153 (Q-ROTOR INSPECTION). EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TC: 3,518.5.
Part: EXCITER — FAILED (ENGINE)
EXCITER INOPERATIVE. IGNITERS WILL NOT SPARK (NOT VERY EXCITABLE). REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — WORN (TURBINE SHROUD)
SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TC: 6,926.0.
Part: TUBE ASSY — LEAKING (PT SCAVENGE)
TUBE ASSY LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — CORRODED (ENGINE)
BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: ROTOR ASSY — FAILED (TURBINE)
FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 4,571.4.
Part: BEARING — CORRODED (ACCESSORY DOOR)
BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — LEAKING (ENGINE)
SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — LEAKING (ENGINE)
SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SHAFT — CORRODED (COMPRESSOR)
SHAFT HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 1,661.3.
Part: NOZZLE ASSY — MALFUNCTIONED (GAS PRODUCER)
UNABLE TO GET CORRECT FLOW WHICH RESULTED IN ENGINE LOW POWER WITH HIGH EGT. -08 WEFA NEEDS TO BE BETWEEN 3.592 AND 3.600. WEFA FOR DISCREPANT UNIT IS 3.692 WHICH IS TOO HIGH FOR FLEET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BLADE — DEFECTIVE (T/R)
T/R BLADE PAINT BEGINNING TO PEEL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BLADE — DEFECTIVE (T/R)
T/R BLADE PAINT BEGINNING TO PEEL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (T/R)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
1997
Part: BEARING — WORN (T/R)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: BLADE — CRACKED (M/R)
FAILED BLADE INSPECTION. EXCESSIVE SKINS CRACKS AND BUILDING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BLADE — CRACKED (M/R)
FAILED BLADE INSPECTION. EXCESSIVE SKINS CRACKS AND BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BLADE — CRACKED (M/R)
M/R BLADE FAILED BLADE INSPECTION. EXCESSIVE SKIN BULGING AND CRACKS.
Part: BLADE — CRACKED (M/R)
M/R BLADE FAILED BLADE INSPECTION. EXCESSIVE SKIN BULGING AND CRACKS.
Part: ROTOR ASSY — BLADE SHIFT (POWER TURBINE)
ENGINE H275G5-001 FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT Q-ROTOR 9.93 GMIN2. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 5,956.8.
Part: BEARING — WORN (T/R)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R)
BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R)
BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: SWITCH — INTERMITTENT (START)
SWITCH UNIT OPERATED INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
1996
Part: LIGHT — INTERMITTENT (TAIL)
TAIL LIGHT UNIT OPERATES INTERMITTENTLY BECAUSE OF WORN SOCKET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: FITTED BOLT — WORN (T/R HEAD)
FITTED BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM.
Part: BELLOWS — TORN (M/R MAST)
BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (T/R HEAD)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R BLADE)
BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R BLADE)
BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH, 2 EACH NEW UNITS CORRECTED PROBLEM.
Part: BEARING — FAILED (RT ENG NR 2)
BEARING HAS EXCESSIVE SCORING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: ROTOR — WORN (COMPRESSOR)
COMPRESSOR AXIAL ROTOR WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 104,663.
Part: SEAL — LEAKING (CSD LIP)
CSD LIP SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — LEAKING (ALTERNATOR)
ALTERNATOR AFT SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — LEAKING (GOVERNOR)
GOVERNOR/STARTER/FCU SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM.
Part: SEAL — LEAKING (ALTERNATOR)
ALTERNATOR FORWARD SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: LIGHT SOCKET — WORN (TAIL)
LAMP WILL NOT REMAIN ILLUMINATED BECAUSE SOCKET IS WORN. SOCKET IS TOO LOOSE TO GET PROPER CONTACT WITH LAMP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BOLT — WORN (T/R)
BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (T/R)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: SEAL — LEAKING (RT ENG NR 2)
RIGHT ENGINE NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. ACTUAL P/N INSTALLED, 4-141-45-02, SN 390.
Part: SEAL — LEAKING (RT ENGINE NR 3)
RIGHT ENGINE NR 5 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — PITTED (ENGINE COMPR)
COMPRESSOR BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
1995
Part: ROTOR ASSY — BLADE SHIFT (POWER TURBINE)
FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 2 PLUS 0.013 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 979.4.
Part: SEAL — LEAKING (NR 3 BEARING)
SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R)
TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R)
TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM.
Part: ROTOR ASSY — BLADE SHIFT (POWER TURBINE)
ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (T/R)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
Part: BELLOWS — TORN (MAST)
BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BELLOWS — TORN (M/R MAST)
BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. ABOVE DATE IS OCCURRENCE DATE. REMOVAL DATE 1/10/95. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.
Part: BEARING — WORN (T/R)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.
Part: BEARING — WORN (T/R)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNIT(S) CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R BLADE)
BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNIT(S) CORRECTED PROBLEM.