- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 7022
- Year built
- 2010
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 23, 2010
- Certificate issued
- January 11, 2021
- Expires
- January 31, 2028
- Mode S code
- A40291
Eurocopter EC 130 B4TCDS H9EUAirframe · Eurocopter EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 22, 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 N358AMMatched 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 N358AMMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2025121774403Frame · chafedDURING 600-HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED AT THE CENTER OF THE LH AND RH X-FRAME. THE MAX DEPTH OF DAMAGE ON THE LH SIDE IS 0.018” WITH AN AREA OF 0.040” BY 0.035” THE MAX DEPTH OF DAMAGE ON THE RH SIDE IS 0.013” WITH AN AREA OF 0.020” BY 0.010”.SDR 2A6R2025121074402Frame · corrodedDAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22) AND RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAMES. BOTH LH AND RH EDGE FRAMES REQUIRED FULL REPLACEMENT. THESDR 2A6R2025121074401Stringer · crackedDURING 600 HOUR INSPECTION, A CRACK APPROXIMATELY 0.9” LONG WAS DISCOVERED DURING ROUTINE INSPECTION ON THE TAIL BOOM STRINGER JUST BELOW THE BATTERY DOOR FRAME. THE LOCATION OF THIS DAMAGE IS LOCATED APPROXIMATELY AT F.S. 7,272MM, W.L. 2,110MM, AND B.L.-160.SDR QMLA2024121720150Button · damagedPILOT DISCREPANCY: BURNING SMELL IN COCKPIT. MECHANIC FINDINGS: FOUND STROBE LT PUSHBUTTON LIGHT REMAINING ON IN BOTH ON AND OFF POSITIONS IN 30 ALPHA PANEL, ALSO NOTICED BELLY STROBE LIGHT NOT FLASHING CONSISTENTLY. REMOVED COVER FROM 30 ALPHA PANEL AND FUMESSDR QMLA2024062920078Inverter · odorCREW REPORTED BURNING SMELL IN THE CABIN AREA DURING CRUISE FLIGHT. MECHANIC FOUND INVERTER INOPERATIVE.SDR QMLA2024062720075Outlet · failedCREW REPORTED "SMELL OF BURNING PLASTIC IN CABIN" AND RETURNED TO BASE. MECHANIC FOUND FAULTY GFCI OUTLET (LH MED WALL) READING ABNORMAL VOLTAGE BETWEEN UPPER AND LOWER RECEPTACLE SUSPECTING SHORT IN GFCI ITSELF. REMOVED AND REPLACED IAW REF. SUBSEQUENT OPERASDR QMLA2024061720064Unknown · odorDURING FLIGHT AND RETURN TO BASE FROM FLIGHT, CREW NOTIFIED PILOT THAT THEY SMELLED A ELECTRICAL BURNING AROUND THE BACK CABIN WALL. IT WAS DARK INSIDE THE CABIN SO VISUAL IDENTIFICATION WAS DIFFICULT. PILOT AND CREW INSPECTED THE AREA BUT COULD NOT IDENTIFY TSDR QMLA2023040420024Fire Detector · unknownENG FIRE LIGHT ILLUMINATED DURING FLIGHT WHEN NO FIRE WAS PRESENT. SUSPECT MOISTURE IN A CONNECTOR.SDR QMLA2018040118037Shelf · crackedDURING INSPECTION, FOUND THE BATTERY SHELF CRACKED AFT OF TB FRAME 2285.8 STARTING AT 4 INCHES AND IS APPROXIMATELY 1.75 INCHES LONG, ANOTHER CRACK 3 INCHES AFT OF THAT, APPX 4.5 INCHES LONG WITH MULTIPLE CRACKS AND MISSING MATERIAL.SDR QMLA2017122117141Friction Lock · out of adjustPRIOR TO TAKEOFF, PILOT FELT EXTREME FORCE IN COLLECTIVE WITH NO ASSOCIATED WARNING OR CAUTION LIGHTS ILLUMINATED. PILOT CHECKED TO MAKE SURE THAT THE COLLECTIVE LOCK WAS RELEASED AND THAT THE COLLECTIVE FRICTION WAS SET TO THE MINIMUM SETTING, BUT THE EXTREMSDR QMLA2016111016125Sleeve · deterioratedCREW REPORTED SMOKE COMING FROM DEMISTER SYSTEM WHEN ACTIVATED. AIRCRAFT RAN UP AND VERIFIED ON GROUND. NO SMOKE COMING FROM HEATER SYSTEM WHICH IS IN PARALLEL TO DEMISTER VALVE. INSPECTED SLEEVE ASSEMBLY FOR DEMISTER AND FOUND HOSES TO BE DETERIORATED. REPLA
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