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Aircraft record

N305PH2005 Eurocopter Deutschland Gmbh EC 135 P2

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 198217 ADs may apply3 service difficulty reports

Registration
Valid
expires Jan 31, 2030
Based in
Tempe, AZ
owner city / state
Engine
PW206B SERIES · 431 hp
P&W Canada
Owners
1
since 2017
NTSB events
None
since 1982
ADs may apply
17
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Phi Health LLC
Owner type
LLC
City, state
Tempe, AZ
Certificate issued
Jan 3, 2017
Expires
Jan 31, 2030
Airworthiness
Standard · Normal
Airworthiness date
Jul 6, 2005

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
EC 135 P2
Year
2005
Serial number
0395
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
A33332

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
  1. 2017 – nowPhi Health LLCTempe, AZ · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (17)

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.

ADSubjectEffectiveApplies to
2014-05-06 R1Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by…Jan 22, 2019Airframe (EC 135 P2)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.
2018-07-01Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…May 3, 2018Airframe (EC 135 P2)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.
2017-03-01Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) HelicoptersMar 31, 2017Airframe (EC 135 P2)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.
2016-11-21Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…Jul 11, 2016Airframe (EC 135 P2)
2015-12-09 R1Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus…Feb 25, 2016Airframe (EC 135 P2)
Show all 17 ADs
ADSubjectEffectiveApplies to
2014-16-24Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus…Sep 25, 2014Airframe (EC 135 P2)Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed.
2014-13-09Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter…Jul 30, 2014Airframe (EC 135 P2)Only with: Mounting ring frame X9227 P/N L535H2120301, L535H2120303, or L535H2120304 installed, except those with frame reinforcement P/N L535H2100201 installed.
2014-05-01Eurocopter Deutschland GmbH HelicoptersApr 14, 2014Airframe (EC 135 P2)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.
2014-01-02Eurocopter Deutschland GmbH HelicoptersMar 3, 2014Airframe (EC 135 P2)Certain serial numbers: 870; 872; 873; 879; 883; 884; …. Only with: Mechanical air conditioning system compressor bearing block upper bearing P/N L210M1872105 installed.
2013-21-06Eurocopter Deutschland GmbH HelicoptersJan 31, 2014Airframe (EC 135 P2)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).
2013-21-05Eurocopter Deutschland GmbH HelicoptersDec 5, 2013Airframe (EC 135 P2)Only with: With bearing P/N LN9367GE6N2, rod P/N L671M5040205, lever P/N L671M5040101, and floor P/N L533M1014101 through L533M1014106 installed.
2013-18-05Eurocopter Deutschland GmbH HelicoptersOct 18, 2013Airframe (EC 135 P2)Only with: Fire extinguishing system P/N L262M1808101, L262M1812101, or L262M1812102 installed.
2013-11-15Eurocopter Deutschland GmbH HelicoptersJul 26, 2013Airframe (EC 135 P2)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.
2013-03-21Pratt & Whitney Canada Corp. Turboshaft EnginesMar 26, 2013Engine (PW206B SERIES)
2009-03-05Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and…Mar 27, 2009Engine (PW206B SERIES)
2004-22-11Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 HelicoptersDec 7, 2004Airframe (EC 135 P2)Only with: Main rotor drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed.
2004-14-22Pratt & Whitney Canada PW206B, PW206C, PW206E, PW207D, and PW207E Turboshaft EnginesAug 3, 2004Engine (PW206B SERIES)Only with: PW206B engines only if PWC Service Bulletin No. 28119 has been incorporated.

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

Service Difficulty Reports (3)

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.

  • Communications · radio · overheatedJul 26, 2016

    SHORTLY AFTER TAKE OFF, CREW NOTICED FAINT BURNING ELECTRICAL ODOR IN THE CABIN. COULD NOT IDENTIFY WHERE THE BURNING ODOR WAS COMING FROM, AND NO INDICATIONS WERE PRESENT ON THE CAD & VOLTAGE METER PLUS NO CIRCUIT BREAKERS WERE POPPED. NOTIFIED OPS OF THE SITUATION, CANCELED THE FLIGHT AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · transducer · malfunctionedSep 25, 2006

    LOST GB OIL PRESSURE ON VEMD GAUGE AND COULD NOT CONFIRM WITH MRGB OIL PRESSURE LIGHT ON WARNING PANEL. MAINTENANCE REPLACED THE TRANSMISSION OIL PRESSURE TRANSDUCER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · electrical box · inoperativeFeb 16, 2006

    WHILE IN CRUISE FLIGHT THE GEN DISCON WARNING WAS DISPLAYED WITH LOSS OF NR 1 BUS SYSTEM. PERFORMED EMERGENCY PROCEDURE IAW PHI POLICY AND LANDED AS SOON AS PRACTICAL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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