Page Date: 19. February 2014 1 - 5
Section 1
General
Pilot´s Operating Handbook US
EXTRA 330LX
1.4 ENGINE
Manufacturer: Textron-Lycoming Williamsport Plant PA 17701 USA.
Type: Lycoming AEIO-580-B1A
Rated power: 315 HP/235 kW @ 2700 RPM
303 HP/226 kW @ 2600 RPM
286 HP/213 kW @ 2400 RPM
1.5 PROPELLER
Manufacturer: MT-Propeller Entwicklung GmbH, Federal Republic of Germany.
Type: MTV-9-B-C/C 198-25, 3-blade constant speed.
Alternative: MTV-14-B-C/C190-130, 4-blade constant speed
1.5.1 EXHAUST SYSTEM
Manufacturer: Gomolzig Flugzeug- und Maschinenbau GmbH, Federal Republic of Germany
Complete 6 in 1 System with integrated Silencer.
1.6 FUEL
Fuel type AVGAS 100/100 LL (for alternate fuel grades see later issues of Textron Lycoming
S.I. No 1070)
Minimum 100/130 octane. Maximum 115/145 octane.
Total fuel capacity: 189 L (49.9 US.gal)
- Wingtanks (2 x 60 L): 120 L (31.7 US.gal)
- Center tank: 60 L (15.9 US.gal)
- Acro tank: 9 L (2.3 US.gal)
Usable fuel capacity in the system: 187 L (49.4 US.gal)
Usable fuel capacity for acrobatic: 67 L (17.7 US.gal)
1.7 OIL
Maximum sump capacity: 15.13 L (16 US.qt)
Minimum sump capacity: 8.51 L ( 9 US.qt)
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)
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