*a. Pressure altitude.
*b. Propeller RPM.
*e. Fuel flow.
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
Record the following:
*a. Engine serial number.
*b. Engine hours since new.
*c. Engine hours since overhaul.
Altitude - Establish level flight at 16,000 feet pressure altitude.
PROP levers - Set 1700 RPM.
Adjust the opposite engine to maintain 160 KIAS.
Ice vanes - Retracted.
FAT - Determine and record.
Power setting - Read torque for the recorded FAT from figure 5.
Set torque on engine being tested to the torque from figure 5.