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TEO-540-A1A Engine Installation and Operation Manual
Fuel Pressure to Engine Drive Pump (relative to ambient
air pressure)
Fuel Rail Pressure (relative to manifold pressure)
Fuel Consumption
Maximum Throttle Body Air Inlet Temperature
(measured at the deck temperature sensor)
Maximum Turbine Inlet Temperature (TIT) (measured at
the exhaust bypass valve transition)
Maximum Manifold Pressure
Maximum Cylinder Head Temperature
Cylinder Head Temperature (for maximum service life) -
Above 85% power
Cylinder Head Temperature (for maximum service life) -
85% power and below, in level flight
Maximum Alternator Temperature - Stator Slot and
Stator End Turns
Maximum Alternator Temperature - Drive End Bearing
and Slip Ring End Bearing
Maximum Alternator Rectifier Temperature - Bridge
Critical Altitude (at standard day conditions)
ECU Operating Low Temperature
ECU Operating High Temperature
Short-Term ECU Operating Low Temperature
Short-Term ECU Operating High Temperature
Ground Survivable ECU Low Temperature
Ground Survivable ECU High Temperature
© 2018 Avco Corporation. All Rights Reserved
October 2018
Table A-2 (Cont.)
Table of Operating Limits for Engine
@ 75% Rated Power
65% Rated Power
60% Rated Power
Operational Limits for the EECS
Maximum 65 psig
Minimum -2 psig
Minimum 33 psid
21.50 gallons/hour
18.17 gallons/hour
15.83 gallons/hour
250°F
1750°F
42 in. hg.
500°F
475°F
435°F
356°F
325°F
305°F
8,000 ft.
-49°F
158°F
-49°F
230°F
-67°F
257°F
448 kPa
-14 kPa
228 kPa
121°C
954°C
142.2 kPa
260°C
246.1°C
224°C
180°C
163°C
152°C
2,438 Meters
-45°C
+70°C
-45°C
+110°C
-55°C
+125°C
Appendix A
Page 83
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