+
Cards In This Set
| Front | Back |
|
Number of engines
|
2
|
|
Engine manufacturer
|
Pratt and whitney
|
|
Engine model
|
PT-6A-21
|
|
Number of drive shafts
|
21 compressor1 power turbine shaft
|
|
Engine shaft-horsepower rating
|
550 HP
|
|
Maximum take-off, maximum continous climb power
|
101.5% N1
|
|
Minimum airspeed for sustained icing flight: __________
|
140 KIAS
|
|
Airspeed Indicator red radial line means: __________.
|
VMCA
|
|
Minimum flight crew: __________.
|
One Pilot
|
|
Power lever(s) must not be moved into reverse except when __________.
|
Engine(s) are running
|
|
Operating respective engine with L FUEL PRES LO or R FUEL PRES LO annunciation is limited to __________ before __________
|
10 hours overhaul or replacement of engine-driven fuel pump
|
|
Transient N1 operating limit (%) is __________.
|
102.6%
|
|
Normal oil pressure range of 80-100 PSI is applicable for N1 speeds above __________.
|
72%
|
|
With oil pressure in flight between 40 and 80 PSI, fly at __________.
|
Reduced power setting
|
|
Normal oil pressure operating range for maximum reverse is __________.
|
80-100 PSI
|
