Procedimientos Normales, Anormales y Sistemas
Battery bus
Triple fed bus
Dual fed bus
Four C-cell alkaline batteries
True
False
Motive flow pressure switch
Strart disengage button
Start switch moved to OFF at 50% N1
No loss of aircraft flight instruments or data
No adverse condition as the 350 has no inverters for AC avionics systems
A red warning annunciator and loss of appropiate AC bus equipment
A generator is offline
Respective generator bus has been isolated from center bus
Battery has been completely isolated
Battery
Triple fed
Dual fed
Either battery or dual fed
24.0
28.25 +- .25
28.75
75
88
100
24 VDC
Battery volts
0 volts
Battery, left & right generator buses
Center bus, left &right generator buses
Triple fed relay, left & right generator bus ties
True
False
True
False
True
False
The landing and taxi lights should be switched on for landing
At least one of the three landing and taxi lights switches are ON, and the nose gear uplock switch is engaged
At least one of the three landing and taxi lights are burned out.
True
False
Reverse-flow, free turbine.
Turboshaft
Free-flow, reverse-turbine, horizontally opposed
Option 4
97.8
60.5
90.0
During preflight inspection
Within 15-20 minutes after engine shutdown
Within 30 minutes after engine shutdown
Option 4
1,090°F for 5 seconds
820°C - 850°C for 20 seconds
1,000°C for 5 seconds
Auxiliary fuel transfer
Auto-ignition
Generator
Auxiliary fuel transfer and generator
156% transient torque for 20 seconds
ITT above 850°C. for 20 seconds transient and 1,000°C. for 5 seconds during start
60 PSI mínimum oil pressure at a máximum 62% torque
785°C máximum cruise climb ITT
104% máximum N1
All of the above
True
False
True
False
EXTENGUISHER PUSH switch lights
ENGINE FIRE switch lights
Both of the above
Under the copilot's seat
Under the pilot's seat
Behind the copilot's seat