Allow conditions to stabilize for one minute, then record the
following for each engine being tested.
*(a) Pressure altitude.
*(b) Propeller RPM.
*(e) Fuel flow.
Indicated fuel flow must be within +21 and -25 lb/hr of chart
value for Jet-A-fuel.
If observed TGT exceeds chart value, conduct the Engine
Performance at Maximum Cruise Power check.
Repeat steps 2 through 11 for opposite engine if required.
*ENGINE PERFORMANCE AT MAXIMUM CONTINUOS POWER
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.