Numbers

Question 0

F-5F
Length:
Wingspan:
Height:

Answer 0

Length: 50’ 11”
Wingspan: 26’ 8”
Height: 13’ 2”

Question 1

F-5N

Length
Wingspan
Height

Answer 1

Length: 47’ 5’
Wingspan: 26’ 8”
Height: 13’ 4”

Question 2

Gross takeoff weight (No tank)

N
F

Answer 2

N: 15,400
F: 15,650

Question 3

Gross takeoff weight (With tank)

N
F

Answer 3

N: 16,790
F: 17,450

Question 4

Engine type and thrust (MIL / MAX)

Answer 4

J85-GE-21

MIL: 6500
MAX: 9300

Question 5

AUX doors open / close

Answer 5

Open: 235 KIAS +/-5
Close: 255 KIAS +/- 5

Question 6

What is the effect of the AUX doors failing in the open or closed condition?

Answer 6

Open: 10% increase in fuel consumption
Closed: 7% loss in thrust

Question 7

For ground starts only, the ignition duty cycle is: __ attempted starts, __ min off, an additional __ attempted starts, and __ min off.

Answer 7

For ground starts only, the ignition duty cycle is: 3 attempted starts, 3 min off, an additional 3 attempted starts, and 23 min off.

Question 8

Explain “Cruise Flat”

Answer 8

As the throttles advance towards MIL, nozzle position decreases towards 0% until approximately 85%. At this point, the nozzle remains fixed at 16-22% until the throttle is advanced to where the nozzles begin to close towards zero. Best cruise performance is here in cruise flat.

Question 9

On takeoff, AB light off should occur within __ seconds

Answer 9

5

Question 10

What is the serviceable engine oil quantity in each engine?

Answer 10

4 quarts

Question 11

In the airframe mounted gearbox, automatic shift occurs in the __ to __ % engine RPM range

Answer 11

68-72%

Question 12

The left engine should be at approximately __% for a crossbreed start.

Answer 12

95%

Question 13

The fuel low warning system operates on a __ second time delay and illuminates when the fuel level drops to ____ - ____ pounds.

Answer 13

3 second

350-400 lbs

Question 14

L or R fuel pressure light indicates:

Answer 14

Low fuel pressure of 66.5 psi or less

Question 15

The generators should come on the line at ___% RPM, and generator dropout should occur at __%.

Answer 15

48%

43%

Question 16

With the landing gear handle up, the red light and audible warning will activate at altitudes below ____’, at an airspeed less than ___ KIAS +/- __ KIAS with one or both throttles below __% RPM.

Answer 16

With the landing gear handle up, the red light and audible warning will activate at altitudes below 9500’, at an airspeed less than 210 KIAS +/- 10 KIAS with one or both throttles below 96% RPM.

Question 17

The drag chute can be released by

Answer 17

1) Rotating the T-handle 90 degrees clockwise and pulling it to the second detent or
2) Resetting the T-handle to the stowed position

Question 18

With fixed flaps, flaps are automatically positioned to half (12 deg / 8 deg) below __K’ and one quarter (0 deg / 8 deg) above __K’. Flaps automatically retract approaching ___ KIAS or ___ IMN. Warning tone goes off if flaps do not retract.

Answer 18

With fixed flaps, flaps are automatically positioned to half (12 deg / 8 deg) below 32K’ and one quarter (0 deg / 8 deg) above 32K’. Flaps automatically retract approaching 550 KIAS or .95 IMN. Warning tone goes off if flaps do not retract.

Question 19

With the LCOSS on, a G warning town will come on at ___ Gs. Tone will intensify as G increases.

Answer 19

+6.5

Question 20

What aircraft altitude corresponds to 10K’ cabin altitude?

Answer 20

25K’

Question 21

With the ENG ICE switch on, expect a __% loss of thrust at MIL and a __% loss of thrust at MAX. At MIL power, opening the anti ice valve may produce a ___ lb/hr decrease in fuel flow, and a __% increase in nozzle opening indication.

Answer 21

With the ENG ICE switch on, expect a 9% loss of thrust at MIL and a 6.5% loss of thrust at MAX. At MIL power, opening the anti ice valve may produce a 100 lb/hr decrease in fuel flow, and a 2% increase in nozzle opening indication.

Question 22

A short trip around the pattern takes ~___#

Answer 22

~200#

Question 23

Corner speed

Answer 23

360 KIAS

Question 24

Max sustained turn performance can be felt by light buffet at ___-___ units AOA

Answer 24

15-17

Question 25

Stall occurs at ___-___ units AOA

Answer 25

27-28

Question 26

Maneuvering and handling qualities are degraded at lower airspeeds; therefore, a min of ___ KIAS should be maintained except for inst approaches, max range descents, and tactical maneuvering.

Answer 26

300 KIAS

Question 27

Hydroplaning may occur above ____ KIAS

Answer 27

85

Question 28

Blank

Answer 28

Blank