Registered owner
Mustang Leasing LLC
Owner type
LLC
Serial number
4290
Year built
2007
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
October 31, 2007
Certificate issued
October 2, 2008
Expires
July 31, 2028
Mode S code
AB9EAC

From the FAA registry file of October 24, 2026.

On this page

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 N848MHMatched 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 N848MHMatched 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 · 5

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

SDR M7KA0729084290Pressure Switch · out of toleranceDURING 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)Sep 1, 2008 · N848MH · Urocop EC130B4 · Engine Fuel DistributionSDR M7KA0708084290Bushing · 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 · N848MH · Urocop EC130B4 · Main Rotor HeadSDR M7KA0718084290Bleed Valve · malfunctionedDURING 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)Aug 4, 2008 · N848MH · Urocop EC130B4 · Compressor Bleed ValveSDR M7K2008F00093Blade · crackedPREFLIGHT 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 Mar 24, 2008 · N848MH · Urocop EC130B4 · Main Rotor BladesSDR M7K2008F00092Tuning Unit · crackedROUTINE 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 LMar 24, 2008 · N848MH · Urocop EC130B4 · Main Rotor Blades

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