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ENGINE PERFORMANCE AT MAXIMUM CRUISE POWER
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TM-1-1510-223-MTF Maintenance Test Flight Manual Army Model RC-12
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AVIONICS FLIGHT CHECKS-continued - TM-1-1510-223-MTF0133
TM 1-1510-223-MTF
6.
Power setting - Read torque for the recorded FAT from figure 6.
7.
Set torque on engine being tested to the torque from figure 6.
8.
Adjust opposite engine to maintain 160 KIAS.
9.
Allow conditions to stabilize for one minute, then record the
following for engine being tested.
*a. Pressure altitude.
*b. Propeller RPM.
*c. FAT.
*d. Torque.
*e. Fuel flow.
*f.
KIAS.
*g. TGT.
*h. N1.
10. Observed TGT should not exceed chart value.
11. Repeat steps 3 through 10 for the other engine if required.
G. AVIONICS FLIGHT CHECKS
PROCEDURE
TROUBLESHOOTING
REFERENCE
* 1. Autopilot - Check as follows:
Observe that all channels operate positively and
smoothly with no oscillation of any flight control.
a.
Trim aircraft for straight and level flight.
b.
AUTO PLT POWER switch - ON.
c.
TURN control - Place in center (detent)
position.
d.
AP ENGAGE switch - Press to engage.
4-7

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