2018 Leonardo AW109 Trekker Helicopter Specifications
LEONARDO AW109 TREKKER · Systems Description
Overview
The document provides detailed specifications and systems information for the 2018 Leonardo AW109 Trekker Helicopter, a twin-engine light utility helicopter. It covers general characteristics, rotor systems, powerplant details, electrical systems, avionics, safety features, and interior configurations.
- Type: Twin-engine light utility helicopter
- Crew capacity: 1-2, with up to 6 passengers
- Powered by two Pratt & Whitney Canada PW207C engines
- Features a titanium main rotor system with composite blades
- Equipped with dual independent hydraulic systems
- Fuel capacity: 177 US gallons
- Includes advanced avionics and safety systems
- Crash-resistant design with reinforced structure
Document
Source
Originally published by amazonaws.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Systems Description
- Year ·
- 2018
- File size ·
- 1.9 MB
- Publisher ·
- amazonaws.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Max passenger capacity ·
- 6
- Fuel capacity us gallons ·
- 177
What is the 2018 Leonardo AW109 Trekker Helicopter Specifications?
The 2018 Leonardo AW109 Trekker Helicopter Specifications is a systems description for the LEONARDO AW109 TREKKER, dated 2018.
Where does the 2018 Leonardo AW109 Trekker Helicopter Specifications come from?
This copy of the 2018 Leonardo AW109 Trekker Helicopter Specifications was originally published by amazonaws.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the 2018 Leonardo AW109 Trekker Helicopter Specifications published?
The 2018 Leonardo AW109 Trekker Helicopter Specifications — the LEONARDO AW109 TREKKER systems description on file — is dated 2018.
Most owners only have the POH. Here's the essential set for the LEONARDO AW109 TREKKER.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
In this document
General Information
The AW109 Trekker is a state-of-the-art twin-engine helicopter with a total flight time of 170 hours since new.
Rotor System
The main rotor features a titanium hub with four composite blades, while the tail rotor has a steel hub with two composite blades.
Powerplant and Fuel System
It is powered by two PW207C engines with a dual independent fuel system and a crash-resistant three-cell fuel system.
Electrical System
The helicopter has a 24 V DC battery, two 200 A generators, and multiple electrical buses for various functions.
Avionics
Includes a 3-axis autopilot, dual displays for flight data, and various navigation and communication systems.
Safety and Warning Systems
Features master warning lights, aural alerts, engine fire detection, and an Emergency Locator Transmitter.
Safety notes
- Ensure proper operation of dual hydraulic systems.
- Monitor engine parameters for safe operation.
- Check fuel system integrity before flight.
- Use caution with crash-resistant features during maintenance.
- Follow emergency procedures for fire detection alerts.
Full document text
California Aviation Services, Inc 6791 Airport Dr. STE A, Riverside, California 92504, USA Leo Bell 1(951)354-5274 AIRCRAFT SPECIFICATION 2018 Leonardo AW109 Trekker Helicopter Specifications General Information The 2018 Leonardo AW109 Trekker Helicopter, is a state-of-the-art, twin-engine light utility helicopter. It is currently registered as TBD and has accrued a total flight time of 170 hours since new (SNEW). The helicopter is powered by PW207C engines, with serial numbers PCE-BH0903 and PCE-BH0889. California Aviation Services, Inc 6791 Airport Dr. STE A, Riverside, California 92504, USA Leo Bell 1(951)354-5274 AIRCRAFT SPECIFICATION General Characteristics • Type: Twin-engine light utility helicopter • Crew: 1–2 (single-pilot VFR standard; dual-pilot IFR optional) • Passenger Capacity: Up to 6 passengers • Airframe: Constructed with an aluminum alloy fuselage featuring bonded panels, a semi- monocoque aluminum alloy tail boom, and reinforced skid-type landing gear. The aircraft is equipped with hinged crew doors on both left and right sides, sliding passenger doors with jettisonable windows, and a separate baggage compartment with a hinged door. Rotor System The AW109 Trekker's main rotor system features a titanium, fully articulated hub with four composite blades that have swept tips. The blades are fitted with elastomeric bearings and dampers, and each grip can be replaced individually. The tail rotor has a steel, semi-rigid delta-hinged hub with two composite blades, which are also individually interchangeable. Controls • Dual independent hydraulic systems • Force trim and artificial feel for enhanced flying comfort • Adjustable friction devices on cyclic and collective controls • Adjustable directional pedals • Flapping and droop restraint mechanism Powerplant and Fuel System • Engines: Two Pratt & Whitney Canada PW207C turboshaft engines • Engine Control: Dual FADEC with auto-start, supporting normal, emergency, and training modes • Integrated Assemblies: Engine-mounted fuel pump/filter and oil pump/filter for each engine • Lubrication: Engine lubrication and cooling, equipped with two oil chip detectors • Fuel Architecture: Dual independent systems with cross-feed capability, submerged boost pumps, airframe-mounted fuel filter, right-hand refueling point, and ground fuel drains • Fuel Capacity: 177 US gallons, crash-resistant three-cell fuel system (upgraded from 152 US gallons) Transmission, Drive, and Hydraulics • Main Transmission: Rated at 960 shp for takeoff and 900 shp continuous • Design: Three-stage transmission with dual freewheeling units California Aviation Services, Inc 6791 Airport Dr. STE A, Riverside, California 92504, USA Leo Bell 1(951)354-5274 AIRCRAFT SPECIFICATION • Hydraulic Systems: Dual independent, redundant systems with transmission-mounted pumps and separate reservoir • Cooling and Lubrication: Internal dry sump with pressure/scavenge pumps and oil filter, transmission oil chip detectors (two units) • Tail Rotor Gearbox: Single-stage 90° bevel gearbox with sight glass and chip detector • Transmission Shafts: Included in the configuration Electrical System • Battery: 24 V DC, 33 Ah Ni-Cd battery with temperature probe • Generators: Two 200 A self-cooled starter-generators • Power Control: Two voltage regulators, battery and interconnecting bus relays, external power relay and receptacle • Buses: One battery, two essential, two emergency, two main, and two auxiliary buses • Exterior Lighting: NVG-friendly position lights (green/red/white), two anti-collision lights, right- hand taxi and left-hand landing lights • Cockpit Lighting: Two utility lights and instrument lights with dimming capability • Radio Master: Equipped with ground function California Aviation Services, Inc 6791 Airport Dr. STE A, Riverside, California 92504, USA Leo Bell 1(951)354-5274 AIRCRAFT SPECIFICATION Avionics • AFCS 3-axis duplex SP-711 Honeywell • Radar altimeter Single Pilot VFR Standard Package • Two 6" × 8" displays for Primary Flight Display (PFD) and Multi-Function Display (MFD) with Synthetic Vision System (SVS), Highway in the Sky (HITS), Helicopter Terrain Awareness and Warning System (HTAWS), Flight Management System (FMS), and radio tuning • Dual Data Acquisition Units (DAU) and dual Air Data Attitude Heading Reference Systems (ADAHRS) • Navigation and Communication: VHF/AM, VOR/ILS, GPS, Mode-S transponder • Pilot Intercom System (ICS) and magnetic direction indicator Upgraded – Dual Pilot IFR Avionic Package • Dual controls for both pilot and co- pilot • Co-pilot PFD with SVS, HITS, HTAWS, FMS, and radio tuning • Additional radios: Second VHF/AM, second VOR/ILS, and second GPS • Navigation Aids: Automatic Direction Finder (ADF), Distance Measuring Equipment (DME), Marker Beacon • Flight Instrumentation: Flight Director, Electronic Standby Indicator, second magnetic compass, and digital clock • Co-pilot Intercom System (ICS) California Aviation Services, Inc 6791 Airport Dr. STE A, Riverside, California 92504, USA Leo Bell 1(951)354-5274 AIRCRAFT SPECIFICATION Systems Data Display • Engine parameters: Dual Inter-Turbine Temperature (ITT in °C), torque (TQ%), N1 (compressor %), N2 (turbine %) • Rotor speed (NR %) • Transmission: Oil pressure (PSI) and temperature (°C) • Engine oil: Pressure (PSI) and temperature (°C) • Fuel: Pressure (PSI) and quantity (kg) • Hydraulic: Dual system pressure (PSI) • Electrical: Dual DC voltmeter (VDC) and ammeter (Amp) • Environmental: Outside air temperature (°C) Safety and Warning Systems • Master warning and master caution lights • Aural alerts and warning/caution/advisory messages • Engine fire detection and two engine compartment extinguishers • Pulsed chip detectors for monitoring • Emergency Locator Transmitter (ELT) installed Interior and Cabin Cockpit • Crash-resistant pilot and co-pilot seats, adjustable fore/aft, equipped with lap belts and headrests
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• Shoulder harnesses with inertial reels for both pilot and co-pilot • Standard cockpit interior with anti-reflection instrument panel • Portable Fire Extinguisher California Aviation Services, Inc 6791 Airport Dr. STE A, Riverside, California 92504, USA Leo Bell 1(951)354-5274 AIRCRAFT SPECIFICATION (Customize Corporate Seating Available) California Aviation Services, Inc 6791 Airport Dr. STE A, Riverside, California 92504, USA Leo Bell 1(951)354-5274 AIRCRAFT SPECIFICATION Passenger Cabin • Passenger intercommunication system and two cabin loudspeakers • Reading and emergency lights • Upper and lower air vents, along with ventilation ram air inlets • Acrylic windshield and side/overhead windows Environmental and Utility Equipment • Air conditioning ECU • Installed windshield wiper and rotor brake • Provision for external hoist with a capacity of 272 kg (600 lb)