N31079
Registered owner: TOP FLIGHT AVIATION OF MISSISSIPPI LLC, MS (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.
14 reports on file, 1999-04-22 – 2013-07-10.
Part: COMPRESSOR — STALLED (ENGINE) · airframe 12,259 hrs
DURING CLIMB OUT, WHILE PASSING THROUGH 200 FT, THE HELICOPTER EXPERIENCED A COMPRESSOR STALL. TORQUE READINGS WERE MAXED OUT AND THE ACFT EXPERIENCED A RT THEN LT YAW.
Earlier reports · 1999–2011 · 13 reports
2011
Part: CONTROLLER — SMOKE (TCAS) · airframe 16,070 hrs
FIRST FLIGHT OF THE DAY, STARTED THE HELICOPTER AND ALL AS NORMAL UNTIL TURNED ON THE AVIONICS MASTER. ABOUT 45 SECONDS AFTER THAT, RT AFTER TURNING ON THE TCAS AND GETTING A "FAILED" MESSAGE, STARTED TO SMELL SMOKE. THE PASSENGER IN THE FRONT SEAT CONFIRMED THE SMOKE AND POINTED OUT WERE IT WAS COMING FROM - THE TCAS ENCLOSURE.
2007
Part: BATTERY — DISCHARGED (MASTER) · airframe 13,795 hrs
PILOT WORE BATTERY DOWN TRYING TO START AIRCRAFT
2004
Part: BLADE — DAMAGED (TAIL ROTOR) · airframe 11,951 hrs
AVERAGE SKIN THICKNESS .00684 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPPED BLADE. REQUEST WARRANTY.
Part: BLADE — DAMAGED (TAIL ROTOR) · airframe 11,951 hrs
AVERAGE SKIN THICKNESS .00673 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPPED BLADE. REQUEST WARRANTY.
Part: BATTERY — WEAK (MASTER) · airframe 11,950 hrs
BATTERY IS WEAK. BATTERY FAILED 1ST CAPACITY CHECK AFTER 28 MINUTES. CHARGED BATTERY WITH C 1/10 CONDITIONING CHARGE. BATTERY FAILED 2ND CHECK AFTER 33 MINUTES. SUBMITTED FOR WARRANTY CONSIDERATION.
2001
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 8,883 hrs
STIFFENER IS CRACKED. REPLACED WITH NEW PART.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 8,883 hrs
STIFFENER IS CRACKED. REPLACED WITH NEW PART.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 8,883 hrs
PART IS CRACKED. REPLACED WITH NEW PART.
Part: CROSSTUBE — CORRODED (LANDING GEAR) · airframe 8,572 hrs
PART HAS INTERGRANULAR CORROSION SEVERAL PLACES ON TUBE. THIS FORWARD CROSSTUBE HAD ONLY 602 HOURS SINCE INSTALLATION, THE CORROSION WAS EXTENSIVE AND BEYOND LIMITS. REPLACED CROSSTUBE WITH NEW PART.
Part: EXHAUST STACK — CRACKED (ENGINE) · airframe 8,267 hrs
CRACKED.
2000
Part: EXHAUST PIPE — CRACKED (ENGINE)
EXHAUST ASSY CRACKED. REMOVED AND REPLACED DUCT. (X)
Part: EXHAUST PIPE — CRACKED (ENGINE)
EXHAUST ASSY IS CRACKED. REPLACED WITH NEW PART. (X)
1999
Part: EXHAUST PIPE — CRACKED (ENGINE)
EXHAUST ASSEMBLY IS CRACKED. REPLACED PART. (X)