N848MH

EUROCOPTER EC 130 B4 · 2007 · Rotorcraft · 1 engine · 6 seats · Valid Registration

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

Operators of this aircraft

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

OperatorRolePeriodBasis
MAVERICK AIRSTAR, LLC (Q2KA)Certificate holderMatched by certificate designator
MAVERICK HELICOPTERS, INC (M7KA)Certificate holderMatched by certificate designator

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.

5 reports on file, 2008-03-24 – 2008-09-01.

OTHER · 2008-09-01 Matched by certificate designator
ATA 7310

Part: PRESSURE SWITCH — OUT OF TOLERANCE (FUEL FILTER)

DURING ROUTINE 600 HOUR INSPECTION THE FUEL FILTER PREBLOCKAGE PRESSURE SENSOR WAS FOUND OUT OF TOLERANCE IAW MM DATA. A NEW SWITCH WAS INSTALLED. THIS IS A RARE FAILURE FOR THIS PART. (K)

Source: SDR M7KA0729084290
WARNING INDICATION · 2008-08-04 Matched by certificate designator
ATA 7532

Part: BLEED VALVE — MALFUNCTIONED (ENGINE)

DURING FLIGHT OPERATIONS BLEED VALVE WAS CLOSING LATE AND OPENING TOO EARLY. A SERVICEABLE BLEED VALVE WAS INSTALLED. NO FURTHER DEFECT NOTED. SUSPECT ANEROID BELLOWS LOST CALIBRATION. THIS IS A RARE FAILURE FOR THIS PART. (K)

Source: SDR M7KA0718084290
OTHER · 2008-08-04 Matched by certificate designator
ATA 6220

Part: BUSHING — LOOSE (STARFLEX)

DURING ROUTINE INSPECTION A STAR ARM END BUSHING WAS FOUND LOOSE. STARFLEX REMOVED FOR REPAIR AND SERVICEABLE STARFLEX INSTALLED. THIS IS A VERY COMMON FAILURE RECENTLY FOR THIS PART. SUSPECT THAT AN ADHESIVE FAILURE IS THE PROBLEM THAT MAY BE HEAT RELATED. (K)

Source: SDR M7KA0708084290
OTHER · 2008-03-24 Matched by certificate designator
ATA 6210

Part: TUNING UNIT — CRACKED (BLADE)

ROUTINE 100 HOUR INSPECTION REVEALED THAT HAMMER BLADE HAD CRACKED. AS THIS BLADE IS NORMALLY UNDER A 1200 FLEX PER MINUTE OPERATION IT IS EXPECTED TO WORK HARDEN OR FATIGUE OVER TIME. SUSPECT A METAL DEFECT OF SOME NATURE AS MOST OF THESE BLADES LAST MUCH LONGER IN SERVICE. (K)

Source: SDR M7K2008F00092
OTHER · 2008-03-24 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (MAIN ROTOR)

PREFLIGHT INSPECTION REVEALED THAT HAMMER BLADE HAD CRACKED IN TWO AND THE WEIGHTS AND BLADE WERE CAPTURED BY THE CONTAINMENT BOX ASSY. AS THIS BLADE IS NORMALLY UNDER A 1200 FLEX PER MINUTE OPERATION IT IS EXPECTED TO WORK HARDEN OR FATIGUE OVER TIME. THIS BLADE FAILED AFTER A VERY SHORT TIME SPAN, HOWEVER, AS COMPARED TO NORMAL. SUSPECT A METAL DEFECT OF SOME NATURE. (K)

Source: SDR M7K2008F00093