Registered owner
Air Methods LLC
Owner type
LLC
Serial number
7651
Year built
2013
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
November 26, 2013
Certificate issued
May 14, 2019
Expires
May 31, 2029
Mode S code
A1C63F

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.

2013In forceSuperseded2026
ADs by the year they took effect: 51 ADs
20132
20141
20152
20162
20173
20181
20191
20204
202111
20226
20235
20241
20256
20266
See all 51 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N213SHMatched 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 N213SHMatched 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 · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR QMLA 202608272006Main Rotor · fodJUST PRIOR TO LANDING, A SMALL PLASTIC BAG FLOATED UP AND INTO THE MAIN ROTOR SYSTEM. IT BLEW OUT ALMOST IMMEDIATELY AFTER THE FACT. A NORMAL LANDING AND SHUTDOWN WERE PERFORMED.Aug 27, 2026 · N213SH · Urocop EC130T2 · Main Rotor HeadSDR 2A6R2025050272901Skid · corrodedDURING 600 HOUR / AAIP INSPECTIONS, FOUND OEM LH SKID TUBE PN 350A41-6002-0001 CORRODED NEAR RIVETS IN ZONE C2 (AMM32-11-00,6-6). REMOVED THE AIRBUS LEFT LANDING GEAR SKID TUBE PN 350A41-6002-0001 AND INSTALLED A NEW DART SKID TUBE (PN: D130-1048-011) IN ACCORMay 2, 2025 · N213SH · Urocop EC130B4 · Wheel/Ski/FloatSDR 2A6D20200430002Bulkhead · chafedFORWARD L/H SIDE BAGGAGE AREA FORWARD BULKHEAD HAS MULTIPLE CHAFF MARKS. 31 IN TOTAL; THE TOTAL SIZE OF THE AREA IS 10.5 IN X 11 IN. THE DEEPEST CHAFF MEASURES OUT AT .008 IN.Apr 30, 2020 · N213SH · Urocop EC130T2 · Fuselage Main, BulkheadSDR 2A6D20200430001Deck Plate · chafedR/H SIDE TRANSMISSION DECK INBOARD OF ENGINE OIL TANK AT THE EDGE OF TRANSMISSION DOUBLER. THE CHAFF DAMAGE MEASURES .009 IN. DEEP AND .2955 IN WIDE X .5335 LONG. LOCATED AT STATION IS 3440.58 WL 15.18, BL/R 373.13.Apr 30, 2020 · N213SH · Urocop EC130T2 · Fuselage Miscellaneous StructureSDR 2A6D20200423001Door Frame · crackedFOUND A CRACK UNDER THE FORWARD LOWER R/H SIDE DOOR LATCH, THE CRACK MEASURES 5.7345 IN. LONG AND HAVE 2 EA. SPIDERS CRACKS EMITTING FROM MAIN CRACK. STA.1633.6 WL 2544.9 BL/R 863.6Apr 23, 2020 · N213SH · Urocop EC130T2 · Passenger/Crew Doors

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

Earlier aircraft with this N-number · 1

This aircraft carried N213SH before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.