JetCat P550-PRO - Page 46

M
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GERMANY
Instruction
m
anual JetCat
-
PRO engines
,
1.7
-
V12.01V
Once these conditions are met, engine proceeds to Off.
Speed Control
Speed Control mode -- only active when the air speed sensor is connected. Regulates model
flight speed.
Table 2
Code Value Explanation
1 R/C Off AUX switched to Off position or throttle stick and throttle trim moved to the
minimum
position.
2 OverTemp Turbine running over temperature. Exceeded high temperature parameter and time
out.
3 IgnTimOut Turbine did not ignite within programmed time interval.
4 AccTimOut Turbine achieved ignition but did not accelerate within programmed time interval.
5 Acc.Slow Turbine achieved ignition, but acceleration was less than the programmed value,
during startup.
6
Over
-
RPM
Turbine exceeded the maximum RPM, by 5% and a delay of 0.5 seconds.
7 Low-RPM Turbine running under the minimum RPM, by 10% and a delay of 3 seconds.
Usually triggered by a flame out.
8 BattryLow Battery pack is dead. Cell voltage is < 1.0V.
9 Auto-Off Turbine shut down via the AutoOff sequence, using the AUX channel.
10 LowTemp EGT dropped below the minimum value. A dislodged EGT sensor can trigger this
shut down.
11 HiTempOff EGT exceeded the maximum range (~950 °C).
12 GlowPlug! Defective kero/glow plug.
13 WatchDog ECU processor was locked out usually from static discharge or voltage spike in
power supply.
14 FailSafe Turbine was shut down from a failsafe timeout condition.
15 ManualOff Turbine was shut off by using the GSU.
16 PowerFail The power failed to the ECU when the engine was running. This will occur if the
power was lost because of a defective battery, connection or if the switch is turned
off before the engine is shut-down.
Note: If this state is displayed the Info, Min/Max and Statistics menus retain
information from the previous run.
17 TempSensor Fail EGT sensor failed.
Note: This could happen only during startup.
18 FuelFail
19 Rpm2Fail Second rpm sensor defective, only for 2-shaft engines
20 2nd EngF Cross check enabled, and shut down was forced due to 2
nd
engine shut down
21 2nd Diff Cross check enabled, and shut down was forced due to thrust differential
22 2nd Comm Cross check enabled, communication error to 2
nd
engine.