Section 5-7

Question 1

Normal Thrust is Obtained at ___% or ___Degrees Whichever Occurs First

Answer 1

98% or 630 Degrees

Question 2

MIL Thrust is Obtained at ___% RPM

Answer 2

100%

Question 3

MAX Thrust is Obtained at ___% RPM With Afterburner Operating

Answer 3

100%

Question 4

Afterburner Augmentation of power is ___ to ___%

Answer 4

5 to 40%

Question 5

Flap Limits

Answer 5

• 1-45 - 300
• 46-60 - 240
• > 60 - 220

Question 6

Gear and Gear Doors Limiting Airspeed

Answer 6

240kts

Question 7

Do Not Extend Gear at Bank Angles Greater Than ___ Degrees OR More Than ___g’s

Answer 7

45 Degrees and 1.5 Gs

Question 8

Oxygen Pressure Operating Range

Answer 8

50-120 PSI

Question 9

Hydraulic Pressure Operating Range

Answer 9

1500 Minimum; 2850-3200 Normal; 3200 Maximum

Question 10

Abort Start if EGT Reaches ___ Degrees, Abort Jet if EGT Reaches ___ Degrees

Answer 10

845/925 Degrees

Question 11

Total EGT Fluctuations of ___ Degrees Permitted, Mean within the Green

Answer 11

15 Degrees

Question 12

Maximum Allowable Transient RPM

Answer 12

107%

Question 13

Rapid Throttle Movements, Nozzle Should Stabilize Within ___ Seconds

Answer 13

10 Seconds

Question 14

Nozzle Position May be Less Than ___ % When Operating in Less Than MAX AB

Answer 14

50%

Question 15

During Cold Weather Starts, Run Engines at ___ For ___ Minutes

Answer 15

MIL and 5 Minutes

Question 16

Oil Pressure Indication Change of ___PSI at Stabilized RPM, Reference Checklist

Answer 16

10 PSI

Question 17

Nose Wheel Steering Limitation

Answer 17

65kts

Question 18

Canopy Limitation

Answer 18

50kts

Question 19

Symmetrical Flight Load Factors for 3500/3000/2000/1000

Answer 19

• 2.3- +5.7
• 2.4- +5.9
• 2.6- +6.5
• 2.9- +7.2

Question 20

Unsymmetrical Flight Load Factors for 3500/3000/2000/1000

Answer 20

0 to +4.1
0 to +4.3
0 to +4.7
0 to +5.0

Question 21

Continuous Aileron Rolls Can Only Be Accomplished At ___g and ___ or Less Stick Deflection

Answer 21

1.0g and 3.4 or Less

Question 22

Maximum G’s

Answer 22

7.33 and -3.0 Gs

Question 23

To Prevent Flameout Due to Fuel Starvation Avoid MAX Thrust Dives With Less Than ___lbs

Answer 23

650lbs

Question 24

To Prevent Flameout Due to Fuel Starvation Avoid MAX Thrust in Zero or Neg G Flight Exceeding ____

Answer 24

10 Seconds at 10,000ft

30 Seconds at 30,000ft

Question 25

Oil Supply and Pressure Requirements Restrict Zero G Flight to ___ Seconds and Neg G Flight to ___ Seconds

Answer 25

10 Seconds | 60 Seconds

Question 26

After 0 or Neg G Flight, If Oil Pressure Does Not Recover Within ___ Seconds, Return to Normal Flight Conditions

Answer 26

10 Seconds

Question 27

Full Stop Landings Time Intervals if Gear is Retracted In Flight/if Gear is Left Extended

Answer 27

45 Minutes/15 Minutes

Question 28

Maximum Nosewheel Tire Speed

Answer 28

174kts

Question 29

Maximum Main Wheel Tire Speed

Answer 29

221 kts

Question 30

Sink Rates Should Not Exceed ___ for Normal and ___ for Crab When Less Than 1700lbs

Answer 30

590fpm and 395fpm

Question 31

Sink Rates Should Not Exceed ___ for Normal and ___ for Crab When Greater Than 1700lbs

Answer 31

340fpm and 200fpm

Question 32

WSSP Airspeed Limitations Normal/Severe Turbulence (SB)/Abrupt Control Movements

Answer 32

400 350 240kts

Question 33

WSSP G Limitations

Answer 33

0- +4 Symmetric | 0- +3 Unsymmetric

Question 34

Ejection from a Spin Must be Accomplished if Recovery is Not Completed by ___ft AGL

Answer 34

15,000ft

Question 35

G Overshoot May Occur If Pulsing the Stick Between ___ and ___ Mach

Answer 35

0.80 and 0.95 Mach

Question 36

The First ___ Inches of Stick Travel Provide ___ Aileron Deflection

Answer 36

4.5 Inches and 1/2 Aileron Deflection

Question 37

Minimum Stick Forces Occur Per G at ___ Mach

Answer 37

0.9 Mach

Question 38

EED Fuel Quantity Displays Near Thunderstorms Vary Up to ___lbs

Answer 38

200lbs

Question 39

Thunderstorm Penetration Airspeed

Answer 39

280kts

Question 40

Do not exceed max allowable A/S of

Answer 40

710 Kts

Question 41

Engine Damage May Occur if ___Inches of Ice Accumulates on Engine Inlet Duct Lips

Answer 41

0.25 Inches

Question 42

Engine Anti-Ice Requires ___ % RPM

Answer 42

80%

Question 43

At Temperatures Below ___ Degrees, Allow Engines to Run at Idle for ___Minutes

Answer 43

-30 for 2 Minutes

Question 44

During Cold Weather Ops, Cycle Flight Controls ___ to ___ Times 4 to 6 Times

Answer 44

4 to 6 Times

Question 45

At Temperatures Below ___ Degrees, Low Idle RPM May be Observed, Increast RPM for Generators to Cut In

Answer 45

- 16 F

Question 46

With Canopy Closed in Hot Weather, Cockpit Damage May Occur Above ___ Degrees

Answer 46

110 F