Aircraft record

N102HN2000 Eurocopter Deutschland Gmbh EC135P1

Registration validNot yet verified by ownerSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 198218 ADs may apply21 service difficulty reports

Registration: Valid; expires Nov 30, 2028
Based in: Greenwood Village, CO; owner city / state
Engine: PW206B SERIES · 431 hp; P&W Canada
Owners: 1; since 2018
NTSB events: None; since 1982
ADs may apply: 18; confirm with A&P
Service reports: 21; since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026

Registered owner: Air Methods LLC
Owner type: LLC
City, state: Greenwood Village, CO
Certificate issued: Nov 26, 2018
Expires: Nov 30, 2028
Airworthiness: Standard · Normal
Airworthiness date: Jan 12, 2001

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer: Eurocopter Deutschland Gmbh
Model: EC135P1
Year: 2000
Serial number: 0159
Aircraft type: Rotorcraft
Category: Land
Certification: Type Certificated
Seats: 7
Engines: 2
Max takeoff weight: Up to 12,499 lb
Type certificate data sheet: H88EU
Mode S code: A00CDE

Engine

Make and model: P&W Canada Pw206b Series
Type: Turbo-shaft
Power: 431 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records

2018 – nowAir Methods LLCGreenwood Village, CO · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (18)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

AD	Subject	Effective	Applies to
2014-05-06 R1	Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by…	Jan 22, 2019	Airframe (EC135P1)Certain serial numbers: EC135 P1 0005–00829; EC135 P2 0005–00829; EC135 P2+ 0005–00829; EC135 T1 0005–00829; EC135 T2 0005–00829; EC135 T2+ 0005–00829; …. Only with: EC135: tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117C-2: tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed.
2018-07-01	Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…	May 3, 2018	Airframe (EC135P1)Serial numbers per Table 1 of Airbus Helicopters Alert Service Bulletin EC135-63A-017, Revision 2, dated December 5, 2016. Only with: Main transmission FS108 housing upper part P/N 4649 301 034, 4649 301 067, or 4649 301 088 installed, with a serial number listed in Table 1 of ASB EC135-63A-017.
2017-03-01	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters	Mar 31, 2017	Airframe (EC135P1)Certain serial numbers: EC135 0005–00829; MBB-BK 117 C-2 9004–9310. Only with: EC135: with tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117 C-2: with tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed.
2016-11-21	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…	Jul 11, 2016	Airframe (EC135P1)
2015-12-09 R1	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…	Feb 25, 2016	Airframe (EC135P1)

Show all 18 ADs

AD	Subject	Effective	Applies to
2014-16-24	Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus…	Sep 25, 2014	Airframe (EC135P1)Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed.
2014-13-09	Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…	Jul 30, 2014	Airframe (EC135P1)Only with: Mounting ring frame X9227 P/N L535H2120301, L535H2120303, or L535H2120304 installed, except those with frame reinforcement P/N L535H2100201 installed.
2014-05-01	Eurocopter Deutschland GmbH Helicopters	Apr 14, 2014	Airframe (EC135P1)Only with: Main gearbox (MGB) P/N 4649 010 003, 4649 010 005, 4649 010 006, 4649 010 006X, 4649 010 008, 4649 010 008X, 4649 001 007, 4649 010 010, or 4649 010 013 installed.
2013-21-06	Eurocopter Deutschland GmbH Helicopters	Jan 31, 2014	Airframe (EC135P1)Only with: Goodrich external mounted hoist with boom support assembly P/N 44301-500, 44307-500, or 44307-500-1 installed (EC135); boom P/N 44307-500 installed (MBB-BK 117 C-2).
2013-21-05	Eurocopter Deutschland GmbH Helicopters	Dec 5, 2013	Airframe (EC135P1)Only with: With bearing P/N LN9367GE6N2, rod P/N L671M5040205, lever P/N L671M5040101, and floor P/N L533M1014101 through L533M1014106 installed.
2013-18-05	Eurocopter Deutschland GmbH Helicopters	Oct 18, 2013	Airframe (EC135P1)Only with: Fire extinguishing system P/N L262M1808101, L262M1812101, or L262M1812102 installed.
2013-11-15	Eurocopter Deutschland GmbH Helicopters	Jul 26, 2013	Airframe (EC135P1)Certain serial numbers: EC135 P1 0005–0699; EC135 P2 0005–0699; EC135 P2+ 0005–0699; EC135 T1 0005–0699; EC135 T2 0005–0699; EC135 T2+ 0005–0699; …. Only with: BO-105A/C/S/LS A-1 with cantilever assembly P/N 105-40132 or 105-40139; BO 105 LS A-3 with cantilever assembly P/N 105-40139; EC135 (excluding S/Ns 0076, 0093, 0098, 0099, 0102, 0104, 0106, 0108, 0110, 0111, 0113, 0114, 0116, 0117, 0119) with cyclic stick locking device P/N L670M1045101/-102/-104/-105/-106/-107 and pin P/N L311M1038205 or L311M1099205; MBB-BK117 A-1 through C-1 with cyclic stick holder assembly P/N 117-41140-01, 117-41230-01 or 117-41230-03; MBB-BK117 C-2 with cyclic stick locking device P/N B856M1011101 and pin P/N L311M1038205 or L311M1099205 installed.
2013-03-21	Pratt & Whitney Canada Corp. Turboshaft Engines	Mar 26, 2013	Engine (PW206B SERIES)
2009-03-05	Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and…	Mar 27, 2009	Engine (PW206B SERIES)
2004-22-11	Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 Helicopters	Dec 7, 2004	Airframe (EC135P1)Only with: Main rotor drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed.
2004-14-22	Pratt & Whitney Canada PW206B, PW206C, PW206E, PW207D, and PW207E Turboshaft Engines	Aug 3, 2004	Engine (PW206B SERIES)Only with: PW206B engines only if PWC Service Bulletin No. 28119 has been incorporated.
2000-26-12	Eurocopter Deutschland GmbH Model EC135 P1 and EC135 T1 Helicopters	Feb 6, 2001	Airframe (EC135P1)Certain serial numbers: 0005–0094. Only with: Hydraulic line shielding hose DN 56, P/N L290M20X1 001, installed.
99-22-01	Eurocopter Deutschland GmbH Model EC135 P1 and T1 Helicopters	Dec 17, 1999	Airframe (EC135P1)Certain serial numbers: 0005–0120

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (21)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

Fuselage · deck plate · crackedSep 16, 2026
DURING INSPECTIONS THE MGB DECK WAS FOUND TO BE CRACKED FROM THE ELECTRICAL CONNECTOR AFT TO THE FIREWALL AND FORWARD OF THE ELECTRICAL CONNECTOR APPROX. 2 INCHES
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · web · crackedSep 15, 2026
NR 2 WEB UNDER FLOOR CABLE CHANNEL CRACKED
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · bracket · crackedSep 14, 2026
CRACK FOUND ON REINFORCEMENT BRACKET AND ON MGB DECK
From FAA Service Difficulty Reports; matched by N-number and serial number.

Show all 10 reports

Fuselage · web · crackedSep 14, 2026
DURING INSPECTIONS FOUND A RIB ON NR 1 SIDE UNDER FLOOR CABLE CHANNEL COVER CRACKED
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuel · cartridge · inoperativeDec 1, 2025
AFT FUEL PUMP MEL'D. REMAINING FUEL PUMP FAILED TO MAINTAIN THE NR 2 SUPPLY TANK FULL. FUEL LEVEL FLUCTUATED BETWEEN 15 (FULL) AND 12 SEVERAL TIMES AND THEN DROPPED TO 12 AND STAYED THERE THE REMAINDER OF THE FLIGHT. REPLACED PUMP CARTRIDGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Engine · bypass valve · faultedSep 29, 2025
THE NUMBER ONE ENGINE OIL TEMPERATURE EXCEEDED THE LIMIT DURING FLIGHT, INDICATING A READING OF 131 DEGREES CELSIUS. FOLLOWED THE EMERGENCY PROCEDURE AND ATTEMPTED TO INCREASE THE AIRSPEED, BUT DID NOT BRING ENGINE TEMPERATURE DOWN TO NORMAL LIMITS. PLACED ENGINE IN IDLE, & THE TEMPERATURE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuel · pump · faultedApr 8, 2025
DURING AIRCRAFT STARTUP PROCEDURES, THE FWD FUEL PUMP CAUTION REMAINED ON WHEN THE FUEL PUMP SWITCH WAS PLACED TO ON. SHUT THE AIRCRAFT DOWN, CONTACTED MAINTENANCE PERSONNEL AND ENTERED THE DISCREPANCY INTO THE AIRCRAFT LOGBOOK. CLEARED THE DISCREPANCY IAW THE AIRCRAFT MEL AND RETURNED TO BASE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Tail rotor · cotter pin · missingFeb 10, 2025
YAW SERVO ACTUATOR BRACE HAD A MISSING COTTER PIN ON POST FLIGHT INSPECTION. VERIFIED TORQUE ON T/R NUT. INSTALLED COTTER PIN. ALL MAINTENANCE COMPLETED. AIRCRAFT RELEASED TO REVENUE SERVICE. #MEC-005650
From FAA Service Difficulty Reports; matched by N-number and serial number.
Electrical power · o-ring · leakingFeb 5, 2025
ON POST FLIGHT INSPECTION OIL LEAK WAS DISCOVERED. TIGHTENED LOOSE LINE ON ACCESSORY GEARBOX, INSTALLED O-RING ON STARTER/GENERATOR DRIVE SPLINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Engine · line · leakingFeb 5, 2025
LEAK FROM #1 ENGINE DISCOVERED ON POST FLIGHT INSPECTION UPON LANDING AT HOSPITAL. TIGHTENED LOOSE LINE,
From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 21 reports.

Sources

FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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