P68C

P68C

P68C

Product catalog summary
Overview: This document provides a general description of the standard equipment for the Vulcanair P68C aircraft. It is not a technical document and should be used only for general informational purposes. Vulcanair reserves the right to make changes to specifications, materials, equipment, or prices without prior notice.
Powerplant and Propeller: The aircraft is equipped with two Textron Lycoming IO-360-A1B6 engines, each providing 200HP at 2,700 RPM. The engines are air-cooled, fuel-injected, and feature a direct drive system. The propellers are Hartzell two-blade, constant speed, full feathering types with hydraulic governors.
Flight Instruments and Indicators: The aircraft includes a Garmin GDU 1040 digital primary display and multifunction display, a magnetic compass, a digital standby attitude module, and various other indicators such as fuel quantity and engine hour-meter.
Cockpit, Flight, and Ground Controls: Features include dual primary flight controls, a fixed tricycle landing gear, an automatic emergency locator transmitter, and various engine and flight trim controls. The cockpit is equipped with a heavy-duty brake system, stall warning system, and a variety of switches and controls for flight operations.
Electrical Systems: The aircraft uses a 24-volt electrical system with a 19 amp/hour battery and two 130 A alternators. It includes voltage regulators, resettable circuit breakers, and static discharge wicks.
Fuel System: The aircraft has two fuel tanks with a total capacity of 142 gallons, of which 138 gallons are usable. It includes auxiliary electric pumps, fuel strainers, and filters.
Lighting Systems: Exterior lighting includes LED navigation lights, recognition lights, strobe lights, and landing lights. Interior lighting features map swivel lights, cabin reading lights, and internally lighted rocker switches.
Cabin Comfort System: The cabin is equipped with a heating system, fresh air vents, and soundproofing. It includes a pilot door, 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 such as tow bars and tie-down rings.
Cockpit and Cabin Appointments: The cockpit includes a speaker, luggage compartment, adjustable seats, seat belts, carpeting, and various other amenities for comfort and safety.
Product Support Documents: The aircraft comes with a flight manual, parts catalogue, maintenance manual, and various warranties and logbooks.
New Generation Avionics Package: The avionics package includes an S-TEC System 55X autopilot, Garmin G950 integrated cockpit system, and various Garmin components for communication, navigation, and data management.
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Catalog excerpts

P68C-1

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.

 Open the catalog to page 1
P68C-2

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...

 Open the catalog to page 2
P68C-3

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
P68C-4

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,...

 Open the catalog to page 4
P68C-5

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 Pilot Door ( rh side of aircraft) 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...

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P68C-6

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...

 Open the catalog to page 6
P68C-7

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

All VULCANAIR S.p.A. catalogs and technical brochures

  1. P68C-TC

    7  Pages

  2. Vulcanair

    16  Pages

  3. Vr (P68R)

    7  Pages

  4. V1.0

    2  Pages

*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.