Pilatus PC-6 Porter 107in Wingspan ARF

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Overview

The Pilatus PC-6 Porter is a single-engined Short Take-Off and Landing (STOL) utility aircraft designed by lt Pilatus Aircraft of Switzerland.

First flown in 1959, the PC-6 continues in production at Pilatus Flugzeugwerke in Stans, Switzerland. It has been built in both piston engine and turboprop powered versions and was produced for a time by Fairchild Hiller in the United States . Total Number build is 581.

Features

All Balsa and lite-ply construction
Fully covered in weathered detail
Fibreglass cowling
Control surfaces pre-hinged and installed
Two piece wing with aluminium wing joiner
Pilot door and rear door can open-close
Big battery hatch for Electric version

Includes:

Assembly instructions with stage-by-stage illustrations - [ Download ]
Plywood seat
Fibreglass cowling
Aluminium landing gear and Wheels
Landing Struts
Aluminium wing joiner
Wing struts
Engine mounts
Spinner
Fuel tank
Decals and all hardware

Required Hardware (Not Supplied)

Transmitter, Motor, Propeller, Servos, Battery, Extension Leads, Glue, Tools and Silicone Fuel Line (For GP).

Recommended Hardware (Not Supplied)

Engine: DLE30 (30cc) 2-Stroke Petrol Engine
Electric Motor & ESC - Dualsky GA3000.7 V2 270KV 585g 3000W X-Motor | Dualsky Summit 100HV Brushless ESC
Servos - 8 (7 for electric) x MacGregor MG5921HV 20.3Kg.cm/0.12s High Voltage Digital Servo

Specifications:

Wingspan:	107in (2720mm)
Fuselage Length:	78.7in (2000mm)
Weight (Ready to fly):	6.5kg - 7.0kg
Engine:	26cc - 30cc (2-stroke)
Radio:	6 channels with 8 servos (7 for electric)
Electric Motor:	Dualsky GA3000.7 V2 270KV 585g 3000W X-Motor