NATOPS CB

Question 1

Thrust Produced by the F405-RR-401 engine

Answer 1

5,527lbs

Question 2

The BIT display will automatically display upon system power-up. T/F?

Answer 2

False

Question 3

The ___________ is the only portion of the aircraft protected from icing by ducted engine air.

Answer 3

The Fan Spinner

Question 4

The starter is inhibited from cranking the engine above _____%.

Answer 4

20%

Question 5

During engine start the GTS auto shuts down at approx ________% RPM.

Answer 5

45%

Question 6

GTS Duty Interval

Answer 6

3min x 3 then 30min

Question 7

Ingniters On Post GTS Start Button pressed

Weight on Wheels __________
Weight Off Wheels __________

Answer 7

WonW: Immediately
WoffW: 30”

Question 8

Ignition is inhibited when the throttle is advanced past the IDLE position. T/F?

Answer 8

False

Question 9

Yaw dampening function is active at all airspeeds

Answer 9

False

Question 10

The Generator automatically after an AirStart. T/F?

Answer 10

False

Question 11

External electrical power, when used during ground starting, is automatically cut off when the engine reaches 45 percent rpm.

Answer 11

True

Question 12

If both inverters FAIL, the standby attitude indicator becomes the primary attitude instrument. T/F?

Answer 12

False

Question 13

A hand pump is provided to charge the wheel brake accumulator prior to aircraft towing.
True or False

Answer 13

True

Question 14

The HYD FAIL warning light illuminates when HYD 1 and 2 systems drop below 600 psi.
True or False

Answer 14

False

Question 15

Protection circuits within the starting system automatically shut down the GTS if GTS idle speed is not achieved within 30 seconds after the GTS start button is pressed.
True or False

Answer 15

True

Question 16

17. After start, the closure of the bleed valve is indicated by an approximate 3 percent increase of N2 idle rpm and a 50 °C drop in EGT.
    True or False

Answer 16

True

Question 17

During an airstart using manual fuel control, after the GTS start button is released, the bleed valve remains open for 60 seconds.
True or False

Answer 17

True

Question 18

Manual fuel control, when selected, will provide for automatic fuel scheduling during an airstart.
True or False

Answer 18

False

Question 19

The FIRE warning light illuminates if the engine firewire reaches 300 °C.
True or False

Answer 19

True

Question 20

If flap/slat selection disagrees between the forward and aft cockpit, the flaps/slats will move to the most extended position.
True or False
Mechanically linked

Answer 20

False

Question 21

Following a generator failure the right MFD drops off line and the left MFD shows the ADI display. This is normal.
True or False

Answer 21

True

Question 22

Emergency hydraulic pressure prevents raising the landing gear handle with weight-on-wheels.
True or False

Answer 22

False

Question 23

If the SKID caution light illuminates in flight, the following procedure should be used:
a. Turn anti-skid off.
b. Use normal braking techniques.
True or False

Answer 23

False

Question 24

The launch bar will not extend if the nose wheel angle is greater than 30 degrees from center.
True or False

Answer 24

False

Question 25

If the fire warning lights extinguish due to a temperature decrease, an automatic reset may take 45 seconds. True or False

Answer 25

True

Question 26

To ensure there is enough pressure to reset the RAT shuttle valve, the engine rpm should be above 76 percent. True or False

Answer 26

False

Question 27

The HYD caution light illuminates when either HYD 1 or HYD 2 pressure drops below 1,660 ± 110 psi. True or False

Answer 27

True

Question 28

The nominal flap positions are approximately 50 degrees at full down and 25 degrees at 1/2. True or False

Answer 28

True

Question 29

A SP BRK advisory light illuminates when the speed brakes are not fully retracted. True or False

Answer 29

True

Question 30

IFF Mode C altitude reporting works off the forward cockpit altimeter. True or False

Answer 30

True

Question 31

During the VOR/ILS system BIT check, the VOR bearing pointer indicates 90 degrees; VOR/ILS system requires service. True or False

Answer 31

True

Question 32

After pressing the TEST button for 5 seconds during a TACAN BIT check, you observe the following: a. HSI TACAN bearing pointer indicates 180 ± 2.5 degrees. b. HSI TACAN range reads 0±1 nm. c. CDI bar centered. The TACAN system requires service. T/F?

Answer 32

False

Question 33

If cockpit pressure is lost, a warning is provided when the cockpit altitude exceeds 24,500 ±500 feet. True or False

Answer 33

True

Question 34

Pressing the ADR pushbutton initiates a 10-second parameter record. True or False

Answer 34

True

Question 35

On the ground (weight-on-wheels), inadvertently moving the landing gear handle from DN to UP will cause the landing gear to retract. True or False

Answer 35

False

Question 36

The FUEL caution light illuminates when the usable fuel remaining is less than approximately 350 pounds. True or False

Answer 36

True

Question 37

The speed brakes may not extend fully above 340 knots. True or False

Answer 37

True

Question 38

In the event of a HYD 1 system failure, power to the flaps is available from the wheel brake/emergency flap accumulator. True or False

Answer 38

True

Question 39

A valid BIT check for the VOR/ILS is as follows: a. The VOR bearing pointer indicates 315 ±3.0 degrees. b. The course deviation line moves to the left 2 dots maximum. c. The marker beacon lights illuminate. True or False

Answer 39

True

Question 40

The engine bleed valve is:

Answer 40

Open during engine starting to prevent N2 compressor stalling.

Question 41

Operation of the emergency jettison switch is inhibited by:

Answer 41

Weight-on-wheels.

Question 42

NWS is ______ controlled and ________ operated.

Answer 42

Electrically / hydraulically

Question 43

Select all that apply. In flight, the FIRE light illuminates but then goes out. What indications would verify that you do have an engine fire?

Answer 43

a. EGT indicates 710 °C and TP HOT caution light is on. b. EGT/RPM warning light is on and HYD 1 caution is on.

Question 44

The major components of the display system consist of.

Answer 44

FOUR MFDs, a DEU, TWO DEPs, and a HUD

Question 45

IFF MODE C coded transmissions contai

Answer 45

Altitude information from the main altimeter in the fwd cockpit.

Question 46

You are starting the engine and the rpm has stabilized. You advance the throttle through 65 percent and return it to IDLE. Checking your rpm and EGT, you find that they have not changed from their original position. What malfunction would give you these indications?

Answer 46

Bleed valve failure.

Question 47

Anti-Skid deactivates

Answer 47

Decelerating through 13-10 kts

Question 48

while in manual fuel control is that when in manual fuel control,

Answer 48

Throttle movements must be made judiciously.

Question 49

The OBOGS heat exchanger:

Answer 49

Reduces the temperature of engine bleed air.

Question 50

Select all that apply. Under what conditions may a safe ejection be initiated?

Answer 50

- Canopy closed and locked. - After MDC firing handle shatters canopy.

Question 51

Select all that apply. When the eject mode selector is set in the FWD-BOTH/AFT SELF position and the forward seat initiates ejection:

Answer 51

a. The aft seat fires first. b. Both cockpits fire.

Question 52

The Display Electronics Unit (DEU) acts as a ___________ computer.

Answer 52

display and mission

Question 53

During a high altitude ejection, which of the following occurs immediately after the drogue chute is deployed?

Answer 53

a. The seat is stabilized by the drogue during descent.

Question 54

The LP fuel pump is powered by the:

Answer 54

Engine-driven gearbox.

Question 55

While starting the engine, you receive no rise in EGT within 15 seconds after advancing the throttle, and the plane captain is pinching their nose and pointing at the tail pipe. What malfunction are you experiencing?

Answer 55

Wet start

Question 56

HEFOE

Answer 56

1. _HYDRAULIC SYSTEM_ 2. _ELECTRICAL SYSTEM 3. _FUEL SYSTEM______ 4. _OXYGEN SYSTEM_____ 5. _ENGINE______________

Question 57

The four basic steps of preparation for thunderstorm penetration are

Answer 57

HEAT AIRSPEED/ATTITUDE LIGHT TIGHT

Question 58

Max EGT Limits MRT ______ Trans _____ Contin ____

Answer 58

MRT: 610 Trans: 645 Cont: 550

Question 59

Max RPM Limits: MRT _____ Trans ____ Cont _____

Answer 59

MRT: 104 Trans: 106 Cont: 100