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N436CM

Open the Markdown

2009 Eurocopter Deutschland EC 135 P2+ · Pratt & Whitney Canada PW206B2

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Registered owners
Carolinas Healthcare System DBAMedcenter Air
Location
Charlotte, NC
Owner type
Corporation
Serial number
0800
Year built
2009
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
September 16, 2009
Certificate issued
October 2, 2009
Expires
December 31, 2028
Mode S code
A539A6
Eurocopter Deutschland EC 135 P2+Airframe model · 7 seats · 2 engines · 166 registeredTCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B2

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 50

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2000In forceSuperseded2026
See all 65 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N436CMMatched 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 P2+ aircraft

FAA incident reports

No FAA accident or incident reports matched to N436CMMatched 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 Deutschland EC 135 P2+ aircraft

Service difficulty reports · 4

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

SDR QMLA2022031020017Frame · crackedDURING 1000-HOUR AIRFRAME INSPECTION FOUND TWO RIVETS MISSING FROM LH FRAME 4 WEBBING APPROX. 39” FROM FLOOR AND WEB DISTORTED IN THE AREA. ON RH SIDE SAME HIGHT 39” ABOVE FLOOR A 6.5-INCH CRACK IN THE WEBBING AT FRAME 4. WHEN DISASSEMBLY FOR REPAIR ON 6.5 -INMar 10, 2022 · N436CM · Urocop EC135P2 · Fuselage Structure (General)SDR QMLA2018012418007Angle · crackedDURING A 400 HOUR INSPECTION, FOUND A CRACK APPROXIMATELY 1.5 INCHES LONG ON THE RT FORWARD MAIN GEARBOX DECK AT THE TRANSITION TO THE CABIN ROOF ABOVE THE NR 4 BULKHEAD. REPAIRED IAW SRM 51-71-53,8-7.Jan 24, 2018 · N436CM · Urocop EC135P2 · Fuselage Main, StructureSDR RMXA1126201008001Connector · dirtyAPPROX 10 MINUTES INTO FLIGHT (LEVEL) EXPERIENCED A FADEC MINOR CAUTION ON THE CAD. CONFIRMED THE NR2 TWIST GRIP WAS IN THE NUETRAL POSITION. THE FADEC MINOR THEN BECAME A FADEC FAIL AND RAN THROUGH THAT CHECKLIST AND PERFORMED A SHALLOW APPROACH. VEMD FAILUNov 25, 2010 · N436CM · Urocop EC135P2 · Engine Fuel System WiringSDR RMXA051520100800Transducer · unserviceableDURING FLIGHT, THE MAIN TRANSMISSION OIL PRESSURE INDICATION FLUXUATED. PILOT PERFORMED A PRECAUTIONARY LANDING SHORT OF BASE. TECH DETERMINED THE TRANSMISSION OIL PRESSURE TRANSDUCER WAS DEFECTIVE. REPLACEMENT PART ORDERED.May 15, 2010 · N436CM · Urocop EC135P2 · Main Rotor Indicating System

STCs that may be installed · 74

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 74 STCs