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Eurocopter, EC-135T2, 2004, Turbomeca Arrius 2B2 Engines, Dual Pilot IFR Avionics

Eurocopter, EC-135T2, 2004, Turbomeca Arrius 2B2 Engines, Dual Pilot IFR Avionics

Description

  1. Registration And Identification
    1. Registration: PH-EMS
    2. Year of manufacture: 2004
    3. Basic color: RAL 1016
  2. Airframe And Engine Times
    1. Total time: 1888:38
    2. Total landings: 10193
    3. Engines: Turbomeca Arrius 2B2
    4. Engine 1 serial number: 32168
    5. Engine 2 serial number: 32169
    6. Engine 1 total time: 1678:33
    7. Engine 2 total time: 1519:13
  3. Standard Configuration
    1. EC 135 standard aircraft according to technical data 135.03.101.02E.
  4. Eurocopter Options
    1. Sliding window in copilot door
    2. Height adjustable pilot seat instead of standard pilot seat
    3. Dual controls, copilot (removable)
    4. Sliding door fastener, max position LH
    5. One hand latching system for clam-shell doors
    6. Strobe lights (white flash lights)
    7. Search and landing light 450 W
    8. IFR pitch/roll SAS
    9. Enhanced sound proofing kit
    10. Cockpit / cabin separation curtain
    11. Dual AC system
    12. Mast moment indication
    13. Rotor brake system
    14. Starter/generator (2x200 A, 28 V DC) instead of standard starter/generator
    15. Engine compressor washing device
    16. Fuzz burner for engines
    17. Bleed air heating system: EMS version
    18. Windshield wiper system
    19. Lengthened skids
    20. Lashing points (wind speeds up to 40 kts)
    21. Landing and searchlight, 450 W
    22. Engine fire extinguishing system
    23. Copilot pitot static system (electrically heated)
    24. Battery type Varta, 40 Ah, 24 V instead of standard battery
    25. Settling protectors
  5. Avionics
    1. The avionics package is the Eurocopter “Dual Pilot IFR” (DPIFR) version. This includes (but not limited to):
    2. Radar altimeter KRA 405B, KNI 416
    3. ELT C406-2HM Artex (incl. antenna)
    4. 2nd directional gyro 205 1BL Goodrich
    5. 4" artificial horizon GH 14-391
    6. Gyro magnetic heading sys. with HSI C14D
    7. Horizontal situation indicator KPI552
    8. VHF NAV/COM/GPS (pilot) with I-panel annunciation switch unit GNS 430 (Garmin) MD41 (Midcontinent)
    9. VHF NAV/COM/GPS (copilot) with I-panel annunciation switch unit GNS 430 (Garmin) MD41 (Midcontinent), (dual Garmin)
    10. CDI 1 (KI206)
    11. RMI (KI229)
    12. Marker beacon KR 21
    13. Audio/com control system pilot + intercom select panel (ICS mode selector) AS-3100-12 (low impedance)
    14. Audio/com control system co-pilot AS-3100-12 (low impedance)
    15. IC amplifier IC-3100-4 (low impedance)
    16. DME equipment KN63
    17. KDI 572
    18. Transponder (mode S) GTX 330 (Garmin)
    19. 2" standby horizon AI 804 DC (Goodrich), incl. emergency battery
    20. 4" artificial horizon GH 14-391, 2nd system
    21. 3" airspeed indicator, 2nd system (copilot)
    22. 3" altimeter (encoding), 2nd system (copilot)
    23. 3" vertical speed indicator, 2nd system (copilot)
  6. EASA STC Options
    1. TAS, traffic advisory system, Avidyne TAS 600 series
    2. Track and trace locator (RAM locator)
    3. GPS USB output signal (from the Garmin), for navigation tablet
  7. Medical Equipment
    1. The helicopter is equipped and delivered with the Bucher medical interior, EC135-AC61. The numbers in the drawing are linked with the numbers mentioned below. This is just a basic overview of the installed options.
    2. 1 medical attendant seat (swivel)
    3. 2 medical attendant seat (fix)
    4. 3 oxygen bottle retainer assy
    5. 4 rear door stowage unit
    6. 5 integral floor
    7. 6 Bucher side load stretcher assy
    8. 7 medical equipment wall assy
    9. 8A suction unit
    10. 9 Bucher side loading device
    11. 10 seat rail extension (copilot seat)
    12. 11 EMS GPU connector
    13. 12 center lighting assy
    14. 13 rear area light assy
    15. 14 power supply 12/28 V DC (not shown)
    16. 15 roof rail plate
    17. 16 infusion hook
    18. 17 fwd light inst.
    19. 18 electr. system center console
    20. 19 fwd 12 V outlet
    21. 20 attachment plate
    22. 21 Zarges box
    23. 22 LSU retainer
    24. 23 center cabinet
    25. 24 side cabinet RH (not installed)
    26. 25 stop assy
    27. 26 stop assy
    28. 27 shroud installation
  8. Maintenance Data
    1. The overview below gives information about the maintenance status of the helicopter. The helicopter is in flyable condition (with EASA airworthiness review certificate) and is used as spare helicopter for ANWB MAA operations.
    2. 400 FH inspection Eurocopter MSM: 378:42 time remaining (h:min)
    3. 800 FH inspection Eurocopter MSM: 778:42 time remaining (h:min)
    4. 800 FH inspection engine 1 Turbomeca MM: 513:09 time remaining (h:min)
    5. 800 FH inspection engine 2 Turbomeca MM: 513:09 time remaining (h:min)
    6. Main transmission time since overhaul: 1032:24 TT, 2967:36
    7. Main rotor blade 1622 life limit 12400:00 FH: 9491:10 remaining
    8. Main rotor blade 1120 life limit 12400:00 FH: 8854:21 remaining
    9. Main rotor blade 127 life limit 12400:00 FH: 8116:22 remaining
    10. Main rotor blade 747 life limit 12400:00 FH: 7335:43 remaining
    11. Tail rotor gearbox 3000 FH tail rotor gearbox inspection: 1111:22 remaining