N805MH

EUROCOPTER EC 130 B4 · 2004 · Valid Registration

Registered owner: AIRSTAR LEASING LLC, NV (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
ALEXAIR INC. (X33A)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

K · 2008-06-12 Matched by certificate designator
ATA 7261

DURING ROUTINE INSP EXCESSIVE OIL LEAKAGE WAS NOTED AT THE MODULE 5 OUTPUT MAGNETIC SEAL. CLOSE INSP OF REMOVED SEAL REVEALED NO OBVIOUS DEFECT. A NEW SEAL WAS INSTALLED WITH NO FURTHER LEAKAGE NOTED. (K)

Source: SDR M7K2008F00035 · FAA SDRS
O · 2007-10-10 Matched by certificate designator
ATA 7400

AT END OF FLIGHT, PILOT SELECTED IDLE POSITION AND ENGINE REMAINED IN THE FLIGHT POSITION AND WAS SHUTDOWN FROM FLIGHT POSITION. A FAULT CODE WAS GENERATED THA THE START STOP SWITCH WAS DEFECTIVE IN SOME MANNER. A NEW ENGINE START STOP/ON OFF SWITCH WAS INSTALLED AND THE PROBLEM WAS CORRECTED. RECORDS INDICATED ATH 11 SWITCHES OF THIS TYPE HAVE BEEN REPLACED IN OUR FLEET WHICH HAS FLOWN NEARLY 50,000 HOURS TO DATE. (K)

Source: SDR M7K2008F00055 · FAA SDRS
O · 2007-10-10 Matched by certificate designator
ATA 6700

A FAULT CODE WAS GENERATED AT ENGINE SHUTDOWN INDICATING A DEFECT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS INSTALLED. THIS HAS BECOME A VERY COMMON PROBLEM WITH THE LATEST REPLACEMENT PART THAT THEY LAST MUCH LESS THAN THE 2000 HOUR SERVICE LIFE LIMIT. THE SAME POTENTIOMETERS ORIGINALLY INSTALLED LASTED AS LONG AS 4000 HOURS WITHOUT FAILING. SHORTLY AFT THE REQUIREMENT TO REPLACE THESE PART AT A 2000 HOUR INTERVAL IT SEEMS THAT THE QUALITY OF THESE PARTS DRAMATICALLY DECREASED. ENGINE ANTICIPATOR CONTROL CIRCUIT SIGNAL OF COLLECTIVE POSITION IS GENERATED BY THIS POTENTIOMETER TO CONTROL DECU SIGNAL TO THE ENGINE. (K)

Source: SDR M7K2008F00140 · FAA SDRS
O · 2007-09-19 Matched by certificate designator
ATA 5302

FITTING FOUND CRACKED DURING POST FLIGHT INSP. A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AC AND NEVER ON OTHERS FOR REASONS UNKNOWN. SOME SHIMMING IS SOMETIMES REQUIRED AND IF DONE POORLY THIS MAY AGGRAVATE THE CRACK DEVELOPMENT. (K)

Source: SDR M7K2008F00051 · FAA SDRS
O · 2007-09-19 Matched by certificate designator
ATA 5100

FITTING FOUND CRACKED DURING INSP. A NEW FITTING INSTALLED. (K)

Source: SDR M7K2008F00049 · FAA SDRS