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Page Title:
ENGINE PERFORMANCE AT MAXIMUM CONTINUOUS POWER |
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 TM 1-1510-223-MTF
*a. Pressure altitude.
*b. Propeller RPM.
*c. FAT.
*d. Torque.
*e. Fuel flow.
*f.
KIAS.
*g. TGT.
*h.
N1.
10. Indicated fuel flow must be within +21 and -25 lb/hr of chart value
for Jet-A fuel.
11. If observed TGT exceeds chart value, conduct the Engine
Performance at Maximum Cruise Power check.
12. Repeat steps 2 through 11 for opposite engine if required.
* E. ENGINE
PERFORMANCE
AT
MAXIMUM
CONTINUOUS
POWER
1.
Record the following:
*a. Engine serial number.
*b. Engine hours since new.
*c. Engine hours since overhaul.
2.
Altitude - Establish level flight at 16,000 feet pressure altitude.
3.
PROP levers - Set 1700 RPM.
4.
Adjust the opposite engine to maintain 160 KIAS.
5.
Ice vanes - Retracted.
* 6.
FAT - Determine and record.
7.
Power setting - Read torque for the recorded FAT from figure 5.
8.
Set torque on engine being tested to the torque from figure 5.
4-5
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