- Year
- 2016
- Serial
- PCE-BP0029
Specifications
Airframe
- MSN ·
- PCE-BP0029
- Registry ·
- United Kingdom
Performance (across variants)
- Cruise ·
- 100 kt
- Service ceiling ·
- 15,000 ft
- MTOW ·
- 4,500 kg
- Passengers ·
- Up to 12
Avionics equipment
- Rockwell Collins
Avionics
Rockwell Collins
Description
Details Additional Equipment Additional Baseline Equipment Steps for cockpit / cabin access Rotor brake system Second radar altimeter One solid state Cockpit and Voice Flight Data Recorder with provision for image recording and 90 days ULB battery (as per AIR OPS) One Emergency Locator Transmitter (ELT – 3 frequencies) (fixed) Kit First Aid (Bulkhead compatible) Additional navigation and fleet management systems ADS-B Out (Automatic Dependent Surveillance – Broadcast) Health and Usage Monitoring System (HUMS) Flight Data Monitoring system (FDM) Helicopter Terrain Avoidance and Warning System (HTAWS) Satcom Skytrac (EDCU Control) FP Additional Equipment Cabin and Avionic Cabin VIP /passenger transport interior VIP Liners Electric Pax Footstep LH & RH Air Conditioning Heating Passenger cabin ambient LED lights, PSU with reading lights and ventilation/AC outlets, emergency lights, emergency exit signs, passenger advisory lights (safety belt chimes) and Passenger Addressing Loudspeakers. I CS Configuration ”008″ Utility socket 10A VIP Internal PA Speakers USB interseat consol socket Comprises 7 passengers headset plugs. Kit Life jacket 4+3 Cockpit Co-pilot hinged window (storm window) Chart Holder Avionics Equipment EVS MaxViz1500 Camera Weather Radar Rockwell Collins RTA-4112 External video camera FP Interior Completion VIP : 07 Pax (4 + 3 Pax) DIAMOND Interior completion (4+3 seats) Seats in Mid Blue Leather Crashworthy seat in the rear cabin bay (Qty.3) Crashworthy seat in the front cabin bay (Qty.4) Baggage compartment rear tail separation Baggage compartment (one door-access from left hand side) Baggage compartment cargo tie–down fittings Lockable baggage compartment door Avionic Package: Single Pilot Configuration Night VFR/ IFR (EASA/FAA) Cockpit Display System (CDS) Three Rockwell Collins Display Units 10” X 8” colour AMLCD with LED backlight and NVIS compatibility: 2 Primary Flight Displays (PFD) and 1 Multi-Function Display (MFD) One Integrated Standby Instrument System (ISIS) Two Display Control Panels (DCP) Two Cursor Control devices (CCD) One Reversionary Control Panel (RCP) One Display Dimming Panel Two Master Caution Lights (MCL) Two Master Warning Lights (MWL) Two Avionics Full Duplex Ethernet (AFDX) switches Aircraft Monitoring and Management System (AMMS) Two Aircraft Monitoring & Management Computers (AMMC) One Data Transfer Device (DTD) Two touch screen control panels 4-Axis Automatic Flight Control System (AFCS) Flight Control Computer (FCC) One Flight Control System (FCS) Control Panel Radio Comm and Navigation System Two VHF -AM radios Two NAV (VOR/ILS/MB) receivers One DME One Transponder with Enhanced Surveillance Mode (Mode S) First SBAS GNSS (GPS) Second SBAS GNSS (GPS) TCAS II Interphone Communication System Two Audio Control Panels (Pilot and Co-pilot stations) One Audio Management Unit interfacing external transceivers One Passenger Intercom Amplifier Primary Flight Instruments Two Flux Valves Two Air Data and Altitude Heading Reference Systems One Radar Altimeter Pilot Clock integrated in the display Co-Pilot Clock integrated in the display One Standby Magnetic Compass Painting Customized painting scheme 2 metallic colors from Company paint selection Dark Blue and White Standard painting and finishing









