Owner type Corporation
Year built 2011
Type Rotorcraft
Engine Turbo-shaft
Airworthiness Standard, normal
Airworthiness date April 16, 2012
Certificate issued January 24, 2023
Expires January 31, 2030 From the FAA registry file of October 24, 2026.
On this page Registration Potential ADs 64 Information bulletins 5 NTSB investigations 0 FAA incident reports 0 Difficulty reports 9 Potential STCs 134 Related links 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.
2002 In force Superseded2026 ADs by the year they took effect: 89 ADs 2002 1 2003 2 2004 2 2005 2 2006 2 2007 4 2008 3 2009 2 2010 7 2011 3 2012 4 2013 4 2014 6 2015 2 2016 2 2017 4 2018 2 2019 2 2020 5 2021 10 2022 3 2023 2 2024 1 2025 7 2026 7
See all 90 ADs Information bulletins that may apply · 5 Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations No NTSB investigations matched to N425AM Matched 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 Investigations on N425AM not matched to an aircraft · 1 They name N425AM, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.
FAA incident reports No FAA accident or incident reports matched to N425AM Matched 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 Reports on N425AM not matched to an aircraft · 2 They name N425AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 9 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2024091120112 Unknown · odor DURING CLIMB OUT MED CREW ADVISED THEY DETECTED AN ELECTRICAL ODOR COMING FROM THE OXYGEN QTY DISPLAY PANEL, NO VISIBLE SMOKE OR HEAT DETECTED FROM PANEL. PERFORMED INSPECTION OF WIRES ON BACK PANEL, MGB COMPARTMENT AND ENGINE. PERFORMED GROUND RUN, NO DEFECTS Sep 10, 2024 · N425AM · Urocop EC130B4 · Air Distribution System SDR QMLA2023062020049 Pitot Tube · clogged G500 AIRSPEED INDICATION WAS LAGGING BEHIND PERCEIVED AIRSPEED ON CLIMB OUT FROM AIRPORT REPOSITIONING TO BASE. ONCE AT TRAFFIC PATTERN ALTITUDE, BEGAN TO TRY AND DIAGNOSE WHAT THE G500 AIRSPEED INDICATION WAS SHOWING. IT MAXED OUT AT 50KIAS AT WHAT I PERCE Jun 17, 2023 · N425AM · Urocop EC130B4 · Pitot/Static System SDR QMLA2023050920038 Hose · unknown AFTER TAKE OFF WITH AIR CONDITIONING FAN ON AND DEMIST 1 TURN OPEN COCKPIT HAD BURNING SMELL AND SMOKE HAZE. AIRCRAFT RETURNED TO DEPARTURE LOCATION WITHOUT INCIDENT. INSPECTED HEAT AND DEMIST DIFFUSERS FOR DEBRIS WITH NONE FOUND. HEAT AND DEMIST VALVES OPER May 8, 2023 · N425AM · Urocop EC130B4 · Air Conditioning System SDR 2A6D20200603001 Deck Plate · elongated HAS AN ELONGATED HOLE ON THE RT SIDE OF THE TRANSMISSION DECK THAT IS UTILIZED IN THE AFT AC EVAPORATOR PN EC130-6204-2 INSTALLATION DWG EC130-622 AS THE MOST INBOARD AFT HOLE UTILIZING AN AN3-4A BOLT. AT THE HOLES WIDEST POINT IT MEASURES AT .35 BY .26. THE Jun 3, 2020 · N425AM · Urocop EC130B4 · Fuselage Main, Plate/Skin SDR 2A6D2020052001402 Frame · chafed CHAFES TO THE AFT FUSELAGE AFT FRAME (PN: 350A21-1242.20). THE CHAFES ARE FOUND ON
THE FREE EDGES OF THE INBOARD STIFFENING FLANGES ON THE LH AND RH SIDES OF THE FRAME. THE LH SIDE CHAFES
WERE MEASURED TO BE 7MM X 12MM (0.276” X 0.472”) AND 0.014” DEEP; AND May 20, 2020 · N425AM · Urocop EC130B4 · Fuselage Main, Frame SDR 2A6D2020051301401 Bulkhead · cracked CRACK DAMAGE WAS NOTED ON THE 22 DEGREE BULKHEAD WEB May 13, 2020 · N425AM · Urocop EC130B4 · Fuselage Main, Bulkhead SDR QMLA2018022618020 Doubler · cracked DURING A PREFLIGHT AIRWORTHINESS CHECK, FOUND CRACK IN THE UPPER AFT CORNER OF DOUBLER AROUND THE OPENING OF THE BATTERY COMPARTMENT IN THE TAILBOOM. CRACK MEASURED 1 3/8 INCHES IN LENGTH Feb 26, 2018 · N425AM · Urocop EC130B4 · Rotorcraft Tail Boom SDR QMLA2017101417111 Mount · cracked CRACK FOUND ON THE NR 1 TAIL ROTOR DRIVE SHAFT BEARING MOUNT BRACKET, FOUND DURING A SHCEDULED MAINTENANCE BEARING CHANGE. Oct 14, 2017 · N425AM · Urocop EC130B4 · Tail Rotor Drive Shaft SDR QMLA2014013114013 Search Light · inoperative THE PILOT REPORTED THAT HE & THE MEDICAL CREW WERE ON CLIMB OUT JUST FOLLOWING A REFUEL OF THE ACFT WHEN THEY EXPERIENCED AN ELEC SMELL COME THROUGH THE CABIN. THE PILOT IMMEDIATELY PERFORMED AN EMERGENCY LANDING INTO A VACANT PARKING LOT. THE MECHANIC DID A Jan 31, 2014 · N425AM · Urocop EC130B4 · Exterior Lighting Reports on N425AM not matched to an aircraft · 33 They name N425AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
See all 33 unmatched reports 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.
Airframe · Eurocopter EC 130 B4 See all 134 STCs