Lycoming TEO-540-A1A Installation And Operation Manual page 103

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TEO-540-A1A Engine Installation and Operation Manual
Table A-1 contains engine specifications, Table A-2 identifies operating limits, and Table A-3 shows
accessory drives for the TEO-540-A1A Series Engine. This appendix includes the following charts:
• Cooling Air Requirements (Figure A-1)
• Propeller Governor Oil Transfer Leakage Rate (Figure A-2)
• Sonic Nozzle Airflow (Figure A-3)
• 2500 RPM Sea Level and Altitude Performance (Figure A-4)
• 2400 RPM Sea Level and Altitude Performance (Figure A-5)
• 2200 RPM Sea Level and Altitude Performance (Figure A-6)
• Fuel Flow versus Percent of Rated Power (Figure A-7)
Number of Cylinders
Cylinder Arrangement - Firing Order
Spark Plugs
Spark Plug Advance
Maximum Rated Continuous HP @ RPM - Altitude
Takeoff Rated
Performance Cruise (75% Rated)
Economy Cruise (60% Rated)
Fuel Injection
Fuel Injectors
Engine Back-up Fuel Filter
Fuel Pump, AN Type
Fuel Pump Ratio to Crankshaft and Rotation
Propeller Drive Ratio to Crankshaft and Rotation
Counterweight Order
Cylinder Bore
Cylinder Stroke
Piston Displacement
Compression Ratio
Dry Weight (lb)
Dimensions:
© 2018 Avco Corporation. All Rights Reserved
October 2018
APPENDIX A
Table A-1
TEO-540-A1A Engine Specifications
Height
Width
Length
6
1-4-5-2-3-6
12
20º BTC
350 HP @ 2500 rpm - 8000 ft. (2,438
350 HP @ 2500 rpm
262 HP @ 2400 rpm
210 HP @ 2200 rpm
Electronic
6 (one for each cylinder)
10 micron
Standard
1:1 - Clockwise
1:1 - Clockwise
One 5th order and one 6th order
pendulum-type counterweight
5.125 in.
4.375 in.
3
541.5 in.
7.3:1
588.6 lbs.
28.00 in.
46.52 in.
42.29 in.
Meters)
13.0 cm
11.1 cm
3
8,873 cm
267.0 kg
71.12 cm
118.16 cm
107.42 cm
Appendix A
Page 81

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