Registered owner
Mustang Leasing LLC
Owner type
LLC
Serial number
4248
Year built
2007
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
July 24, 2007
Certificate issued
August 23, 2007
Expires
January 31, 2028
Mode S code
AB973E

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 64

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: 89 ADs
20021
20032
20042
20052
20062
20074
20083
20092
20107
20113
20124
20134
20146
20152
20162
20174
20182
20192
20205
202110
20223
20232
20241
20257
20267
See all 90 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N846MHMatched 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 N846MHMatched 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 M7KA1109084125Hinge · crackedHINGE ATTACHMENT BORE HAD A 1` LONG CRACK RADIATING.Nov 17, 2008 · N846MH · Urocop EC130B4 · Fuselage, Door HingeSDR M7KA1028084248Latch · wornDURING ROUTINE INSPECTION LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. HINGE ATTACHMENT BORE HAD A 1` LONG CRACK RADIATING. INSTALLED NEW LATCHES AS REQUIRED.Nov 17, 2008 · N846MH · Urocop EC130B4 · Aerodynamic FairingsSDR M7KA0625084248ABleed Valve · interferenceDURING FLIGHT OPERATIONS BLEED VALVE WAS STICKING OPEN INTERMITTENTLY. A SERVICEABLE BLEED VALVE WAS INSTALLED. NO FURTHER DEFECT NOTED. SUSPECT ANEROID BELLOWS LOST PRESSURE. THIS IS A REAR FAILURE FOR THIS PART. (K)Aug 4, 2008 · N846MH · Urocop EC130B4 · Compressor Bleed ValveSDR M7KA0625084248Bearing · failedPILOT REPORTED THAT ON PREFLIGHT INSPECTION THE OIL COOLER FAN IMPELLOR WOULD NOT TURN BY HAND. BEARINGS WERE SEIZED. INSTALLED SERVICEABLE BLOWER ASSY. THIS PART IS FAILURE PRONE, SUSPECT ALTERNATIVE ARMATURE BEARINGS OR GREASE BE CONSIDERED. (K)Aug 4, 2008 · N846MH · Urocop EC130B4 · Engine Oil CoolerSDR M7K2008F00015Starflex · crackedDURING ROUTINE INSP ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATION UTILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING AND STAR ARM END. WITH ROTOR HUB SLEEVES REMOVED, BUSHING COULD BE MOVED MANUAMay 12, 2008 · N846MH · Urocop EC130B4 · Main Rotor HeadSDR M7K2008F00111Potentiometer · defectiveFAILURE CODE AT SHUTDOWN INDICATED A FAULT WITH THE COLLECTIVE POTENTIOMETER. INSTALLED NEW POTENTIOMETER AND NO FURTHER PROBLEM NOTED. THIS IS A VERY COMMON FAULT FOR THIS PART THAT EFFECTS THE DISPATCH RELIABILITY FOR THIS MODEL AIRCRAFT. (K)Mar 24, 2008 · N846MH · Urocop EC130B4 · Rotorcraft Flight Control

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