Technical data

6 - 14 Page Date: 4. February 2011
Section 6
Weight and Balance and Equipment List
Pilot´s Operating Handbook
EXTRA 330LX
1 Governor MT-Propeller P-880-5 31509 1.10 -0.91 R
(max 2700 RPM)
1 Governor Woodward A-210988 01209 1.10 -0.91 A
(max 2700 RPM)
Powerplant (7X)
Engine
1 Engine Lycoming AEIO-580-B1A 31429 191.72 -0.72 R
4 Shock Mount Barry 94016-02 01817 1.70 -0.29 R
* Fuel. Oil. Sense Lines Parker/Statoflex PTFE Type 101 3.40 -0.15 R
in Eng. Comp.
Engine Fuel System
1 Fuel Injector Precision RSA 10 AD 1 3.90 -0.68 R
1 Mech. Fuel Pump Crane Lear Romec RG9080-J4A 0.57 -0.30 R
Ignition
1 Ignition Switch TCM 10-357200-1 00185 0.15 1.63 R
1 Magneto. LH Slick 6393 32860 2.30 -0.15 R
1 Magneto. RH Slick 6350 02337 2.00 -0.15 R
1 Slick Start; Magneto Unison SS1001 32598 0.27 -0.02 R
Start Booster
Engine Controls
1 RPM Vernier Control ACS Products Co. A-750-30-1200 00113 0.71 0.82 R
1 Mixture Vernier Control ACS Products Co. A-750-20-1080 00112 0.65 0.94 R
1 Throttle Control Teleflex CC330 10 33052 0.56 0.60 R
Engine Instruments
Conventional engine gauges
1 RPM Indicator digital Horizon P100-230- 33624 0.68 1.60 R
(max 2600 RPM) 635-00
1 RPM Indicator digital Horizon P100-230- 02489 0.68 1.60 A
(max 2700 RPM) 643-00
1 Oil Press / Oil Temp UMA D2-OP130U- 33428 0.09 1.62 R
Ind. (2 1/4") OT300U-01
1 Oil Temp. Sender UMA 1B3A 33428 0.08 -0.11 R
1 Oil Press Sensor UMA T1EU150G 33428 0.12 0.04 R
1 Manifold Pressure / United Instr. UI6331-H.217 03247 0.49 1.60 R
Fuel Flow Ind.
1 Fuel Qty. Ind. Wing VDO 301 030 001 G 200171 0.14 1.62 R
1 Fuel Qty. Ind. VDO 301 030 002 G 00390 0.14 1.62 R
Fuselage Tank
Optional add on to convent eng. Gauges
1 EGT/CHT Indicator UMA D2-ET1K7K- 32570 0.07 1.62 O
CT600J-01
QTY ITEM MANUFACT. MODEL NO PART OR P/N WEIGHT ARM R* INST
(kg) (m) A
O