King Air 350i
.jpg "King Air 350i")
Procedimientos Normales, Anormales y Sistemas
- 1.Electrical power for the Emergency Exit Signs are provided through
- A.
Battery bus
- B.
Triple fed bus
- C.
Dual fed bus
- D.
Four C-cell alkaline batteries
- 2.To open the emergency exit from the inside, pull down on the "Exit-Pull" handle
- A.
True
- B.
False
- 3.What normally terminates an engine start sequence?
- A.
Motive flow pressure switch
- B.
Strart disengage button
- C.
Start switch moved to OFF at 50% N1
- 4.Loss of one invertir causes which of the following conditions?
- A.
No loss of aircraft flight instruments or data
- B.
No adverse condition as the 350 has no inverters for AC avionics systems
- C.
A red warning annunciator and loss of appropiate AC bus equipment
- 5.What does illumination of a single GEN TIE OPEN annunciator indicate?
- A.
A generator is offline
- B.
Respective generator bus has been isolated from center bus
- C.
Battery has been completely isolated
- 6.The entry light circuit powers the cockpit emergency lights which is powered by the _______ bus
- A.
Battery
- B.
Triple fed
- C.
Dual fed
- D.
Either battery or dual fed
- 7.Normal generator voltaje is __________ VDC
- A.
24.0
- B.
28.25 +- .25
- C.
28.75
- 8.Generator load is limited to ____________ percent during ground operations below 70% N1
- A.
75
- B.
88
- C.
100
- 9.With th ebattery switch OFF and the battery bus switch EMER OFF, what should the battery bus voltaje read?
- A.
24 VDC
- B.
Battery volts
- C.
0 volts
- 10.What are the three sources from which the triple fed bus receives voltaje?
- A.
Battery, left & right generator buses
- B.
Center bus, left &right generator buses
- C.
Triple fed relay, left & right generator bus ties
- 11.The battery bus voltaje with the battery switch in the OFF position can still be read on the voltmeter with the voltmeter selector switch in the battery position.
- A.
True
- B.
False
- 12.The EXT POWER annunciator flashes with a GPU voltaje low or the GPU is electrically disconnected fron the aircraft.
- A.
True
- B.
False
- 13.Placing the BAT BUS switch in EMER OFF will open the battery relay, BAT tie and the RCCB.
- A.
True
- B.
False
- 14.The White LDG/TAXI advisory light indicates which of the following?
- A.
The landing and taxi lights should be switched on for landing
- B.
At least one of the three landing and taxi lights switches are ON, and the nose gear uplock switch is engaged
- C.
At least one of the three landing and taxi lights are burned out.
- 15.The cabin headliner lights will illuminate full-bright when oxygen pressure is supplied to the passenger masks.
- A.
True
- B.
False
- 16.The PT6 used in the King Air 350 is described as a ___________________ engine.
- A.
Reverse-flow, free turbine.
- B.
Turboshaft
- C.
Free-flow, reverse-turbine, horizontally opposed
- D.
Option 4
- 17.The conpressor bleed valve is closed above approximately _______________% N1
- A.
97.8
- B.
60.5
- C.
90.0
- 18.When should engine oil be checked for an accurate quantity Reading?
- A.
During preflight inspection
- B.
Within 15-20 minutes after engine shutdown
- C.
Within 30 minutes after engine shutdown
- D.
Option 4
- 19.What is the máximum ITT allowed during engine start with no inspection required?
- A.
1,090°F for 5 seconds
- B.
820°C - 850°C for 20 seconds
- C.
1,000°C for 5 seconds
- 20.If the start swich is left in the IGNITION and ENGINE START position, which of the following cannot be activated?
- A.
Auxiliary fuel transfer
- B.
Auto-ignition
- C.
Generator
- D.
Auxiliary fuel transfer and generator
- 21.Which of the following engine limitations are correct?
- A.
156% transient torque for 20 seconds
- B.
ITT above 850°C. for 20 seconds transient and 1,000°C. for 5 seconds during start
- C.
60 PSI mínimum oil pressure at a máximum 62% torque
- D.
785°C máximum cruise climb ITT
- E.
104% máximum N1
- F.
All of the above
- 22.Below 1,000 propeller RPM, torque is limited to 62%
- A.
True
- B.
False
- 23.Oil pressure between 60 and 90 PSI should be tolerated only for completion of the flight and torque limited to 62%
- A.
True
- B.
False
- 24.
![Placing the test switch in the DET position illuminates the - ProProfs]( "Placing the test switch in the DET position illuminates the")
Placing the test switch in the DET position illuminates the- A.
EXTENGUISHER PUSH switch lights
- B.
ENGINE FIRE switch lights
- C.
Both of the above
- 25.A portable fire extinguisher is in the cockpit
- A.
Under the copilot's seat
- B.
Under the pilot's seat
- C.
Behind the copilot's seat
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