P68 Observer 2 STAND

Product catalog summary

Introduction
This document provides a general description of the standard equipment for the Vulcanair P68 Observer 2 aircraft. It is not a technical document and should be used solely for understanding the aircraft's standard equipment.

Powerplant and Propeller
The aircraft is equipped with two Textron Lycoming IO-360-A1B6 engines, each producing 200HP at 2,700 RPM. These are four-cylinder, direct-drive, normally aspirated, fuel-injected engines with air cooling and internal piston cooling. The propellers are Hartzell two-blade, constant speed, full feathering types with hydraulic governors.

Flight Instruments and Indicators
The aircraft features a digital primary display and multifunction display by Garmin GDU 1040. Additional instruments include a magnetic compass, a digital standby attitude module, a heated pitot system, and various indicators for fuel quantity, engine hours, and more.

Cockpit, Flight, and Ground Controls
The cockpit includes dual primary flight controls, a fixed tricycle landing gear, and an automatic emergency locator transmitter. Engine controls are pedestal-mounted with adjustable friction, and flight trim controls are available for rudder and stabilator. The aircraft also features a heavy-duty brake system and a stall warning system.

Electrical Systems
The electrical system includes a 24-volt battery, two 130 A alternators, voltage regulators, and resettable circuit breakers. External power supply receptacles and static discharge wicks are also included.

Fuel System
The aircraft has two fuel tanks with a total capacity of 142 gallons, of which 138 gallons are usable. The system includes auxiliary electric pumps, quick drains, strainers, filters, and gascolators.

Lighting Systems
Exterior lighting includes LED navigation lights, recognition lights, strobe lights, taxi lights, and an ice inspection light. Interior lighting features map swivel lights, courtesy lights, and cabin reading lights.

Cabin Comfort System
The cabin is equipped with a heating system, fan heater/windshield defrost, fresh air vents, and soundproofing. It also includes a cabin door, rear cargo door, and emergency escape window.

External Features
The aircraft has a standard paint scheme, full chemical corrosion protection, and various external features like a tow bar, tie-down rings, and control surface lock kit.

Cockpit and Cabin Appointments
The cockpit and cabin include reclining seats, luggage compartments, seat belts, carpeting, storm windows, sun visors, and various power sockets. Safety equipment includes an emergency torch, first aid kit, and fire extinguisher.

Product Support Documents
Support documents include a flight manual, parts catalogue, maintenance manual, and log books for the aircraft and engines.

New Generation Avionics Package
The avionics package features an autopilot system, Garmin G950 integrated cockpit system, and various Garmin units for communication, navigation, and data management.

Catalog excerpts

STANDARD EQUIPMENT LIST IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for the purpose of generally describing the aircraft standard equipment. Vulcanair S.A. and Vulcanair S.p.A. reserve the right to make changes in specifications, materials, equipment or prices at anytime without prior notice or to discontinue models as required. It is the responsibility of the pilot to conduct all operations in accordance with the approved Pilot’s Operating Handbook, which is the only official source of data. Vulcanair S.p.A. Copyright © 1996-2016 All Rights Reserved.

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POWERPLANT AND PROPELLER Engines: Two Textron Lycoming IO-360-A1B6 200HP @ 2,700 RPM, 4 Cylinders, Direct Drive, Normally Aspirated, Fuel Injected (Bendix Type) Tuned Induction, Horizontal Opposed, Air-cooled with incorporated oil jets for internal piston cooling. Engine Mounts: Dynafocal Type, Two Engine shock absorber, Two Oil System: Oil Filters Cartridge Type, Two Oil Coolers Full Flow, Two Air Intake System: Air Filter Foam Type, Two Alternate source w/Manual Control, Two Geared Starter: Two Propeller: Hartzell, Two Blade, Constant Speed Full Feathering Propellers, Two Polished Propeller...

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vulcanair H aircraft Hi COCKPIT, FLIGHT AND GROUND CONTROLS Dual primary Flight Controls Landing Gear, Fixed Tricycle Automatic Emergency Locator Transmitter ELT 406 MHZ Engine Control Pedestal mounted with adjustable friction: Throttle, Two Propellers, Two Mixture, Two Flight Trim Controls: Rudder: Mechanic wheel on Pedestal with Indicator Stabilator: Mechanic wheel on Pedestal with Indicator Stabilator: Electric switch on control Wheel Alternate Source Engine Air Inlet Control Alternate Instrument static Source and Control Heavy Duty Brake System: Pilot Toe Brake Cylinders Co-pilot Toe Brake...

Open the catalog to page 3

vulcanair H aircraft Hi LH Switches Panel Landing Light Navigation Lights Stall Heated detector Pitot Heat Strobe Light Taxi Light Ice Inspection Light RH Switches Panel A/P Master A/P Elect. Trim ELECTRICAL SYSTEMS 24 Volt, 19 Amp/Hour Battery (Concorde RG24-20) 130 A Alternator 28Vdc, Two Voltage Regulators, Two Resettable Circuit Breakers External Power Supply Receptacle Static Discharge Wicks FUEL SYSTEM Two Fuel Tanks with 142 Gallons (538 litres)Total Capacity; 138Gallons Usable (520 Litres) Auxiliary Electric Pump, Two Individual Fuel Tank Quick Drain, Two Fuel Strainer, Two Fuel Filter,...

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vulcanair ■ aircraft Hi INTERIOR LIGHTING: Map swivel light with touch sensing control, Two (LED) Under-wing Courtesy Light, One (left side) Cabin Reading Lights, Four Internally Lighted Rocker Switches CABIN COMFORT SYSTEM Cabin Air heating system Fan Heater/Windshield Defrost Cabin Fresh Air Vent with Ventilation Fan Overhead Cabin Fresh Air Distribution Vents, Two Cabin Door Rear Cargo Door Emergency Escape Window Soundproofing EXTERNAL FEATURES Standard paint scheme Full Chemical Corrosion Protection Tow Bar Tie-Down Rings, Three Jack Pads Control Surface Lock Kit (Tail + Aileron) Locks with...

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vulcanair ■ aircraft Hi COCKPIT AND CABIN APPOINTMENTS Speaker Luggage Compartment (24 Cu.Ft., 400Lbs) Pilot and Co-Pilot Seats reclining fore/aft and vertical adj., with magazine storage pockets on back; Rear Passenger seat with reclining feature and fore/aft adjustable (2nd Row), Two. Rear Passenger Seat (3rd Row), Two. Three Point Seat Belts and Inertial Reel, Six Lightweight Carpeting Pilot and Co-pilot Storm Windows Sunvisor, Two 24 Volt, 5 Amp Auxiliary Power Socket, Three Map Pockets, Two Emergency Torch First Aid Kit Manual Fire Extinguisher Pitot Tube Cover Fuel Stick Gauge PRODUCT SUPPORT...

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NEW GENERATION AVIONICS PACKAGE AUTOPILOT TWO AXIS S-TEC SYSTEM 55X GARMIN G950 INTEGRATED COCKPIT SYSTEM: DIGITALPRIMARY DISPLAY GARMIN GDU 1040, CONTROL/DISPLAY UNIT, ONE DIGITAL MULTIFUNCTION DISPLAY GARMIN GDU 1040, CONTROL/DISPLAY UNIT, ONE AHRS GARMIN GRS 77/GMU 44, ONE TRANSPONDER GARMIN GTX 33 MODE S AUDIO PANEL WITH MARKER BEACON AND INTERCOM GMA 1347 GIA63W COMM/NAV/GS/GPS INTEGRATED AVIONIC UNITS, TWO AIR DATA COMPUTER GARMIN GDC74A ENGINE INTERFACE UNIT GARMIN GEA71, TWO Note: Cockpit shown with some optional equipment Vulcanair S.A. and Vulcanair S.p.A. reserve the right to make...

Open the catalog to page 7

P68 Observer 2 STAND

P68 Observer 2 STAND

Catalog excerpts

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