- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4658
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- December 8, 2009
- Certificate issued
- February 20, 2015
- Expires
- February 29, 2028
- Mode S code
- A39D49
Eurocopter EC 130 B4TCDS H9EUAirframe · Eurocopter EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
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.
| 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 |
Airframe · Eurocopter EC 130 B4
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N332AMMatched 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 N332AMMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2026042175104Frame · dentedA LARGE DENT WAS DISCOVERED ON THE TRANSMISSION DECK SKIN AND CENTER BEAM PN: 355A21-2109-21. THE DAMAGE TO THE DECK SKIN IS APPROXIMATELY 0.060” DEEP AND 3.5” WIDE BY 2.5” LONG. THE DAMAGE TO THE CENTER BEAM HAS AN AREA OF 2.0” WIDE AND 1.3” HIGH ON THE VERTISDR 2A6R2026110375103Frame · dentedA DENT WAS DISCOVERED ON THE TRANSMISSION DECK SKIN ON THE LH SIDE. THE DAMAGE IS APPROXIMATELY 0.038” DEEP AND 0.5” IN DIAMETER. AN APPROXIMATE LOCATION OF THE DAMAGE IS AT F.S. 3661MM, W.L. -1765MM, AND L.B.L. -450MM. A DETAILED DESCRIPTION OF THE TYPICAL DASDR 2A6R2026110375102Frame · corrodedDAMAGE TO THE RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OUTBOARD FACE OF THE FRAME. THE RH EDGE FRAME WAS PARTIALLY REPLACED AND SPLICED INTO THE REMAINING SERVICEABLE FRAME. A DETAILED DESCRIPTION OF THE APPROVED REPASDR 2A6R2026110375101Frame · corrodedDAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ACROSS THE ENTIRE LENGTH OF THE OUTBOARD FACE OF THE FRAME. THE LH EDGE FRAME REQUIRED FULL REPLACEMENT; THEREFORE, CUTS OR SPLICING DOUBLERS WERE NOT REQUIRED. A DETAILSDR QMLA2023110220099Unknown · unknownAFTER AMBER AND RED GOV LIGHT ILLUMINATED, MYSELF AND THE CREW COULD SMELL AN ELECTRICAL SMOKE ODOR. AFTER LANDING AND SHUTDOWN. ARRIVED AT AIRCRAFT, CLEANED ELECTRICAL CONNECTORS ON FADEC AND NF SENSOR. GOV LIGHT WENT OUT.SDR QMLA2023060420043Unknown · unknownUPON DEPARTURE FROM KPDK, ENG CHIP LIGHT ILLUMINATED ON THE WARNING PANEL. IT WENT OUT AFTER A FEW SECONDS. LANDED AS SOON AS POSSIBLE BACK TO KPDK AND SHUT DOWN ENGINE, CHECKED THE CHIP PLUGS AND THERE WAS NOTHING ON THEM. GROUND RUN THE AIRCRAFT WITH NO LISDR QMLA2015102015100Mount Bracket · crackedDURING A SCHEDULED MX EVENT FOR AAIP INSPECTION, A1040 300 HOUR / 12 MONTH INSPECTION, THE HORIZONTAL STABILIZER WAS PULLED. THE INSPECTION WAS PERFORMED ON THE INTERIOR OF THE TAIL BOOM & THE MOUNTING BRACKETS FOR THE HORIZONTAL STABILIZER. THE UPPER RT MOUSDR QMLA2015101015095Knob · inoperativeDEPARTED BASE, APPROX 5 NM FROM HOSPITAL NOTICED THAT THE BACK LIGHTING FOR ALL THE INSTRUMENTS WAS DIMMING. TRIED TO INCREASE THE LIGHTING BUT WAS UNABLE. THE NEXT THING TO HAPPEN WAS THE RADAR ALT. WAS INDICATING 0 FEET & WARNING LIGHT ILLUMINATING, WAS AISDR QMLA2015022315011Doubler · crackedDURING INSPECTION FOR CRACKS IAW AD 2014-12-51, A CRACK WAS FOUND IN THE LOWER RT DOUBLER PLATE FOR THE HORIZONTAL STABILIZER ON THE INTERIOR OF THE TAIL BOOM. THE INSPECTION OF THIS AREA DOES NOT FALL WITHIN THE SCOPE OF THE APPLICABLE AD. THE CRACK IS APPR
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