- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0625
- Year built
- 2007
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- May 2, 2008
- Certificate issued
- July 20, 2012
- Expires
- July 31, 2028
- Mode S code
- AC1099
Eurocopter Deutschland EC 135 T2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 T2+TCDS E34NEEngine · Turbomeca ARRIUS-2B1A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 17
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2003 | 1 |
|---|---|
| 2005 | 1 |
| 2007 | 1 |
| 2008 | 2 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2019 | 3 |
| 2021 | 1 |
| 2022 | 1 |
| 2024 | 3 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland EC 135 T2+
AD 2026-20-06Main rotor gearboxAD 2026-17-05Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N877CRMatched 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 Deutschland EC 135 T2+ aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2025010672306Angle · crackedDURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK ROOF ANGLE (PN: L533M1017266). THE CRACK WAS LESS THAN 3.25” IN LENGTH AND FIT THE CRITERIA AND APPLICABILITY FOR THE GENERIC AIRBUS REPAIR DESIGN APPROVAL SHEET AHI-135-53-061SDR 2A6R2025010672305Frame · crackedDURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE LH UPPER AND RH LOWER FRAME 5 MEDICAL INTERIOR MOUNT LOCATIONS. THE CRACKS WERE LESS THAN 1.5” IN LENGTH AND FIT THE CRITERIA AND APPLICABILITY FOR THE GENERIC AIRBUS REPAIR DESIGN APPROVAL SHEETSDR 2A6R2025010672304Frame · chafedDURING 1000 HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED ON THE FRAME 4 INNER SKIN PANEL (PN: L533M1407205). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-366SDR 2A6R2025010672302Floor Panel · dentedDURING 1000 HOUR INSPECTION, FOUND SEVERAL AREAS OF DENT / DEBOND DAMAGE WERE DISCOVERED ON THE CABIN FLOOR (PN: L533M1016237). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDASDR 2A6R2025010672301Attach Angle · corrodedDURING 1000 HOUR INSPECTION, CORROSION DAMAGE WAS DISCOVERED ON THE LOWER RH AND AFT ‘BROOM CLOSET’ ATTACHMENT ANGLES (PN: L533M1052317 & L533M1052318). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIR METHODS ENGINEERSDR QMLA2021102720054Arm · damagedSTRAIGHT & LEVEL FLIGHT, 2300’ MSL, APPROX. 1700’ AGL, NIGHT, PILOT UNDER GOGGLES. A LOUD THUMP WAS HEARD WITH A SIMULTANEOUS IMPACT IN THE AIRFRAME FELT BY ALL 3 CREW MEMBERS. A QUICK SCAN OF ALL INSTRUMENTS SHOWED NO MALFUNCTIONS, ALL SYSTEMS WITHIN NORMAL PSDR QMLA2019112319088Chip Detector · false activationRETURNING FROM HOSPITAL (NO PATIENT TRANSPORT) AT CRUISE FLIGHT. THE #1 ENGINE CHIP LIGHT ILLUMINATED. ALERTED CREW AND CALLED AIRCOM. TRIED TO BURN THE CHIP NO SUCCESS. TOLD AIRCOM THAT I WAS DIVERTING TO THE GREEN BAY AIRPORT. PLACED THE AFFECTED ENGINE TO ISDR QMLA2018071718083Fcu · crackedDURING A COMPRESSOR WASH, WE NOTICED WHAT APPEARED TO BE SMOKE COMING FROM NR 2 ENGINE. DURING INVESTIGATION WE FOUND IT WAS FUEL LEAKING FROM THE FUEL CONTROL UNIT. MORE IMPORTANTLY, IT APPEARS TO BE FROM A CRACK IN THE HOUSING.SDR QMLA2013032013041Magnetic Seal · wornDURING FLIGHT, NOTICED THE NR 1 ENGINE CHIP LIGHT. RESET THE MASTER CAUTION AND BURNED CHIP. CHIP LIGHT WENT OUT. NR 1 ENGINE CHIP CAUTION RETURNED. RESET MASTER CAUTION AND BURNED CHIP. CHIP LIGHT WENT OUT. RETURNED TO BASE. NR 1 ENGINE CHIP RETURNED SDR QMLA2012031812044Hmu · leakingWHEN REFUELING ACFT, PILOT NOTICED FUEL DRIPPING FROM DRAIN TUBE AND ON SIDE OF ACFT. MECHANIC VERIFIED IT WAS FUEL LEAKING FROM THE HMU AND IT WAS NOT LEAKING FROM ONE OF THE PIPES ON THE HMU WHEN PRIME PUMPS TURNED ON. REMOVED HMU FIRE SHIELDS & LEAK WAS SDR QMLA2011042411050Compressor · contaminatedIN CRUISE FLIGHT, UPON TURNING THE HEATER ON, SMOKE & FUMES FILLED COCKPIT AND CABIN. THE PROBLEM WAS SOME LT OVER RESIDUE FROM THE COMPRESSOR WASH. MECHANIC VERIFIED THE SYS INTEGRITY THEN RAN THE ACFT WITH THE HEAT ON AND DOORS OPEN TO VENTILATE SYS. RAN FSDR QMLA09031909010Windshield · brokenAT APPROX 1300 HOURS, THE ACFT HIT A BIRD THAT PUT A LARGE HOLE IN THE RT WINDSCREEN. THE BIRD ENTERED THE COCKPIT STRIKING THE PILOT ON HIS RT SHOULDER. PILOT WAS WEARING A HELMET WITH FACE SHIELD LOWERED. UPON THE POST FLIGHT INSP, FOUND THAT THE RT ENDPLAT
STCs that may be installed · 71
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.