King Air 300 Limitations Flashcards
Generator Limitations
N1 62-70% —> 75% generator load
N1 70-100%—> 100% generator load
Starter Limits
30 Seconds on
5 min off
30 seconds on
5 min off
30 seconds on
30 min off
Total Usable Fuel
539 gallons/3611 lbs
Usable fuel main tanks
190 gallons/1273 lbs each
Usable Fuel Aux Tanks
79.5 gallons/533 lbs each
Max Fuel Imbalance
300 lbs
When is cross feed approved?
Only when one engine inop
Max Cabin Diff
6.6 PSI
Max Pneumatic Pressure
20 PSI
Propeller deice ammeter
26-32 amps
Max Ramp Weight
14,100 lbs
Max Takeoff Weight
14,000 lbs
Max Landing Weight
14,000 lbs
Max Zero Fuel Weight
11,500 lbs
Max Weight in Baggage
With fold up seats: 510 lbs
Without fold up seats: 550 lbs
Maneuver limits flaps up
3.1 positive G
1.24 negative G
Maneuver limits flaps down
2.0 positive G
0.0 negative G
What must be operational for every flight?
Rudder Boost & Autofeather
When must autofeather be armed?
Takeoff, climb, approach
Max operating altitude limit
Normal Operation
35,000 feet
Max operating pressure altitude limits (Avgas)
Either Standby Pump inop
Flight Prohibited
Max operating pressure altitude limits (Avgas)
Climbs without cross feed capability
20,000 feet
Max operating pressure altitude limits
Operation with Yaw Damp Inop
11,000 feet
Max OAT limit: sea level to FL250
ISA+37 C