- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 7571
- Year built
- 2013
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- June 27, 2013
- Certificate issued
- September 27, 2021
- Expires
- September 30, 2028
- Mode S code
- A02A66
Eurocopter EC 130 T2TCDS H9EUAirframe · Eurocopter EC 130 T2TCDS E00054ENEngine · Turbomeca ARRIEL-2D
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 33
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2013 | 2 |
|---|---|
| 2014 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 3 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 4 |
| 2021 | 11 |
| 2022 | 6 |
| 2023 | 5 |
| 2024 | 1 |
| 2025 | 6 |
| 2026 | 6 |
Airframe · Eurocopter EC 130 T2
AD 2026-19-02Main rotor bladesAD 2026-16-10Tail rotor drive shaftAD 2026-16-01Main rotor driveInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Eurocopter EC 130 T2
SAIB SW-15-20Air Conditioning System WiringNTSB investigations
No NTSB investigations matched to N11FQMatched 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 T2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N11FQMatched 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 T2 aircraft
Service difficulty reports · 22
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6D20240614001Attach Angle · crackedDAMAGE TO THE BAGGAGE COMPARTMENT LH FWD LOWER ANGLE (P/N: 350A210053.28) IN THE FORM OF GOUGE/CRACK. THE GOUGE/CRACK DAMAGE MEASURED TO BE APPROXIMATELY 0.13” IN DIAMETER.SDR 2A6D20240528001Frame · corrodedDAMAGE TO THE AFT UPPER FRAME (P/N: 350A21-1242.35) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS ON THE UPPER FLANGE OF FRAME AT LH AND RH BOTTOM SIDE NEAR THE AFT LOWER FRAME. THE LH SIDE CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 0.71: X 2.05” AND THSDR 2A6D20240509003Floorbeam · corrodedDAMAGE IS ON THE LH CABIN FLOOR EDGE FITTING (P/N: 350A214753.20) IN THE FORM OF CORROSION AND CRACKS. THE LH FITTING PLATE IS EXCESSIVELY CORRODED AND THE CRACK DAMAGES AT TWO FASTENER HOLES TO EOP WHICH RESULTS IN REPLACEMENT OF LH FITTING.
See all 22 reportsReports on N11FQ not matched to an aircraft · 14
They name N11FQ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR A4J2003F00003Module · shortedDURING (A) CHECK PIE MAINTENANCE FOUND FLOOR EMERGENCY LIGHT AT ROW 17 WHITE LIGHT NOT WORKING. REMOVED AND REPLACED LAMP MODULE IAW MD80 MM 33-53-01. OPERATIONAL CHECK GOOD.SDR 2003F00510Cover · looseFLOOR PATH LIGHTING LOOSE. REMOVED AND REPLACED SECTIONS OF FLOOR PATH LIGHTING COVERS THAT WOULD NOT STAY IN PLACE IAW MD-80 MM 33-53-01. OPERATIONAL CHECK GOOD. (M)SDR 2003F00040Battery · dischargedFORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT INOPERATIVE. PROBLEM WAS DETERMINED TO BE BATTERIES. REMOVED AND REPLACED BATTERIES IAW 25-60-00 MM. OPERATIONAL CHECK GOOD. (M)
STCs that may be installed · 78
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 78 STCs