Technical data

Document N° :
F2-1.0/R80/F/EU
Pioneer 200
Flight Manual
Section: 1
General
REVISION : 0
Dated: 20-04-2002
Sect : 1 -Page: 4 of 6
1.2. TECHNICAL DATA
1.2.1. ENGINE
Manufacturer: ROTAX GmbH
Aircraft Engine
Type: 912 UL Series liquid cooled
1.2.2. PROPELLER
Manufacturer: TONINI
Type: Fixed Pitch Wooden
GT 166X142
Diameter: 166 cm
Pitch: 142 cm
1.2.3. APPROVED FUEL TYPES AND GRADES
-UNLEADED MOGAS (98 Octane or greater - 90 RON or greater)
-100 LL or 100/130 grade aviation gasoline
(only for short utilization time, with carbon level inspection)
1.2.4. FUEL CAPACITY
Total: 54 Litres
Useable 50 Litres