- Serial number
- 0670
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- May 12, 2008
- Certificate issued
- September 15, 2016
- Expires
- September 30, 2029
- Mode S code
- A46F2A
- Registered owner
- Phi Health LLC
- Location
- Tempe, AZ
- Owner type
- LLC
Eurocopter Deutschland EC 135 P2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B2
From the FAA registry file of October 20, 2026.
On this page
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. Not a compliance determination.
| 2000 | 1 |
|---|---|
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 7 |
| 2024 | 4 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland EC 135 P2+
AD 2026-20-06Main rotor gearboxAD 2026-17-05Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory. Matched the same way as ADs.
NTSB investigations
No NTSB investigations matched to N385PHMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter Deutschland EC 135 P2+ aircraft
Investigations on N385PH not matched to an aircraft · 2
They name N385PH, but no registry record covers the event date, or the aircraft registered then was built later.
NTSB SEA95IA082Incident · No injuriesIncident investigationFinal reportFairchild SA-227 · Pasco, WAImproper installation of the rudder trim actuator rod by company maintenance personnel which resulted in binding and fracture of the rod.NTSB SEA91LA040Accident · No injuriesLimited investigationFinal reportSwearingen SA-227 · Kalispell, MTThe flight crew's inablity to maintain directional control after landing in snow-depth conditions that had been erroneously reported as being within operating limitations.
FAA incident reports
No FAA accident or incident reports matched to N385PHMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter Deutschland EC 135 P2+ aircraft
Reports on N385PH not matched to an aircraft · 4
They name N385PH, but no registry record covers the event date, or the aircraft registered then was built later.
Incident 19950416011329ISwrngn SA227AC · Pasco, WANarrative: during takeoff phase of flight, crew experienced vibration through-out aircraft. Aircraft returned to point of departure without further incident. Inspection of the aircraft found rudder trim tab actuator to rudder trim tab link rod had failed. It…Incident 19910402012569ISwrngn SA227AC · Missoula, MTStruck a pheasant while on approach to airport. Landed safely.Accident 19901231061889ASwrngn SA227AC · Kalispell, MTLanded on runway in deep snow. Hit drifts and veered off runway. Pilot had received report runway had 1 inch snow.Incident 19890404020569ISwrngn SA227AC · Missoula, MTAircraft veered right when reverse thrust applied. Left runway. Thrust uneven and no nose steering. Cause not given
Service difficulty reports · 4
SDR QXEA9600141Air Distr · odorNUMBER TWO BLEED AIR HAS NOXIOUS ODOR. INSPECTED AND PLACED ON MEL 21-4.SDR QXEA9600022Cooling Turbine · failedSMOKE IN THE CABIN ON FINAL APPROACH. SMOKE ISOLATED TO NR 2 BLEED. AIRCRAFT LANDED IN BZN WITHOUT FURTHER PROBLEM. NR 2 COOLING TURBINE REPLACED IAW MAINT MANUAL, OPS CHECKED GOOD ON GROUND RUN.SDR QXEA9500207Indicator-Ldg · failedPDX: DURING APPROACH TO PDX, GEAR CAME DOWN AND LOCKED. ON TOUCHDOWN, THE LEFT MAIN GREEN INDICATOR LIGHT EXTINGUISHED THEN CAME BACK ON AGAIN. THE LIGHT EXTINGUISHED AGAIN DURING BRAKING AND REVERSE AND REMAINED OUT. INDICATOR WAS REPLACED AND GROUND OPERSDR QXEA9500122Link Rod · brokenPSC - RUDDER VIBRATION AFTER ROTATION. VIBRATION CONTINUED IN FLIGHT, AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. RUDDER TRIM TAB TO TAB ACTUATOR ROD WAS BROKEN. REPLACED ROD AND RIGGED TRIM TAB I/A/W MM. THE ROD BROKE BECAUSE THE TAB AC