Registered owner
Mustang Leasing LLC
Owner type
LLC
Serial number
4158
Year built
2006
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
February 16, 2007
Certificate issued
October 2, 2008
Expires
July 31, 2028
Mode S code
AB3D1B

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 N823MHMatched 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 N823MHMatched 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 M7K2008F00047Freq Adapter · crackedDURING ROUTINE INSP A CRACK WAS FOUND IN ELASTOMER SURFACE OF BLUE CODED FREQUENCY ADAPTER THAT HAD REACHED MM LIMITATION OF 10MM. ALL (3) ADAPTERS WERE REPLACED AS A KIT IAE MFG RECOMMENDATIONS. SUGGEST MFG ALTER ELASTOMER FORMULATION TO IMPROVE SERVICE LIFJun 23, 2008 · N823MH · Urocop EC130B4 · Main Rotor HeadSDR M7K2008F00033Fitting · crackedDURING ROUTINE INSP, FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO FLANGE EDGE. NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR THIS PART. BORE HOLES MUST BE MATCH DRILLED AND ALIGNED PERFECTLY. SUGGEST A MORE DURABLE MATERIAL BE USEDMay 28, 2008 · N823MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00024Potentiometer · 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 · N823MH · Urocop EC130B4 · Main Rotor ControlSDR M7K2008F00011Starflex · cracked(REF 1212074158) DURING ROUTINE INSP, THE ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATION UTILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING & STAR ARM END. WITH ROTOR HUB SLEEVES REMOVED BUSHING CMay 12, 2008 · N823MH · Urocop EC130B4 · Main Rotor HeadSDR M7K2008F00134Bracket · crackedFOUND CRACKED DURING AIRFRAME 100/200/500 HOUR INSPECTION, BRACKET SUPPORTS, AIR INLET COOLING DUCT WHICH IS SUBJECT TO RAM AIR AND LIKELY VIBRATES CAUSING METAL OF BRACKET TO COLD WORK. THIS IS A COMMON PROBLEM WHICH OCCURS EVERY 200-300 HOURS FOR THIS COMPOSep 19, 2007 · N823MH · Urocop EC130B4 · Starter-Generator

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