Registered owner
Airstar Leasing LLC
Owner type
LLC
Serial number
4020
Type
Rotorcraft
Engine
Turbo-shaft
Certificate issued
September 11, 2008
Expires
April 30, 2028
Mode S code
AB1953

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 50

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2002In forceSuperseded2026
ADs by the year they took effect: 64 ADs
20021
20031
20042
20051
20061
20083
20103
20112
20121
20134
20143
20151
20161
20173
20181
20192
20205
20219
20223
20232
20241
20257
20267
See all 65 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N814MHMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter EC 130 B4 aircraft

FAA incident reports

No FAA accident or incident reports matched to N814MHMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter EC 130 B4 aircraft

Service difficulty reports · 6

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR M7KA0709084020Bushing · looseDURING 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. (KAug 4, 2008 · N814MH · Urocop EC130B4 · Main Rotor HeadSDR M7K2008F00029Potentiometer · failedA FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FURTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODEL HELICOPTER. SUGGEMay 12, 2008 · N814MH · Urocop EC130B4 · Tail Rotor Control SystemSDR M7K2008F00129Magnetic Seal · leakingSEAL LEAKAGE WAS NOTED TO BE INCREASING OVER TIME AND SEAL WAS CHANGED WHEN OIL BEGAN ACCUMULATING ON THE ENGINE DECK FOLLOWING A DAYS WORTH OF FLIGHTS. THIS SEAL WAS A HISTORY OF LEAK DEVELOPMENT AND USUALLY WILL BE CHANGED SEVERAL TIMES BEFORE ENGINE REACHEOct 30, 2007 · N814MH · Urocop EC130B4 · Turbine Engine Oil SystemSDR M7K2008F00058Fan · failedFAN ASSY HAD 3 BLADES MISSING CORNERS WITH 1 BLADE MISSING 40 PERCENT OF ITS DIMENSIONS. NEW FAN ASSY INSTALLED. INITIAL BLADE FAILURE SEEMED TO BE A MATERIAL FAILURE NOT CAUSED BY AN IMPACT. THIS TYPE DEFECT IS PRETTY RARE. (K)Oct 30, 2007 · N814MH · Urocop EC130B4 · Engine Oil CoolerSDR M7K2008F00135Blade · failedIB SURFACE ADJACENT TO PITCH HORN WORN BEYOND LIMITS DUE TO "TT" STRAP FAILURE, OB LAMINATE OF 20/21 PLATES BREAKS. THIS PROBLEM OCCURS WHEN STRAPS BREAK INTO 2 PIECES AND BROKEN ENDS VIBRATES LIKE A REED, BEYOND THE HEAT SHRINK. SUGGEST MFG THICKENS OB PLATESep 19, 2007 · N814MH · Urocop EC130B4 · Tail Rotor BladesSDR 0720064020Pulley · wornON INSP, QUITE A BIT OF DARK DUST HAD ACCUMULATED UNDER HYD PUMP DRV ASSY MOUNTING, THOUGHT TO BE ROTOR BRAKE DUST ACCUMULATION. DRV PULLEY APPEARED TO BE CORRECTLY ALIGNED, UPON LOOSENING, PULLEY WAS FOUND TO WOBBLE LIKE A U-JOINT. UPON TEARDOWN, FOUND CTR Jul 21, 2006 · N814MH · Urocop EC130B4 · Hydraulic Pump (Electric/Engine), Main

STCs that may be installed · 134

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 134 STCs