EasyManua.ls Logo

Extra 300S - Fuel System Specifications

Extra 300S
226 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
Page Date: 20. April 2002 1 - 5
Pilot´s Operating Handbook
EXTRA 300S
Section 1
General
1.4 ENGINE
Manufacturer Textron-Lycoming Williamsport Plant PA 17701 USA.
a) Type Lycoming AEIO-540-L1B5
b) Type Lycoming AEIO-540-L1B5D
Rated power: 300HP @ 2700RPM, 270HP @ 2400RPM
1.5 PROPELLER
Manufacturer MT-Propeller Entwicklung GmbH, Federal Republic of Germany.
a)Type MTV-9-B-C/C 200-15 3-blade constant speed.
b)Type MTV-14-B-C/C 190-17 4-blade constant speed.
1.5.1 Exhaust Systems (Optional)
Manufacturer Gomolzig Flugzeug- und Maschinenbau GmbH, Federal Republic of Germany
Exhaust Silencer for standard system: PN: EA 300 NSD, GO3-606500.
Complete 6 in 1 System with integrated Silencer: PN: EA 300-606000
1.6 FUEL
Fuel type AVGAS 100/100 LL (for alternate fuel grades see later issues of Textron Lyc. S.I.
No 1070)
Minimum 100/130 octane. Maximum 115/145 octane
Total fuel volume 171 litres (45,1 US Gallon)
- Wingtanks (2 x 60 l) 120 litres (31.7 US Gallon)
- Center tank 42 litres (11,1 US Gallon)
- Acro tank 9 litres (2,3 US Gallon)
Usable fuel in the system 169 litres (44,6 US Gallon)
Usable fuel for acrobatic (acro and center tank) 49 litres (12.9 US Gallon)
1.7 OIL
Maximum sump capacity: 16 qts.
Minimum sump capacity: -Acrobatics: 12 qts.
-Normal: 9 qts.
Average ambient air Mil-L6082 Mil-22851
temperature grades ashless dispersant grades
All temperatures ---- SAE 15W50 or 20W50
> 27°C (80°F) SAE 60 SAE 60
> 16°C (60°F) SAE 50 SAE 40 or 60
- 1°C til 32°C SAE 40 SAE 40
(30°F - 90°F)
Page Date: 31. January 2006

Table of Contents

Related product manuals