Reading...
Play button
Play button
Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
216 Cards in this Set
- Front
- Back
|
Wingspan
|
25 Feet 3 Inches
|
|
|
HUD Field of View/Instantaneous FOV From Combat Eye and Design Eye
|
24 Degrees/ 17 Degrees/ 15 Degrees
|
|
|
Gross Weight
|
12,800lbs
|
|
|
MIL/MAX Thrust
|
2,200/3,300
|
|
|
Length of Ignition
|
30 Seconds (Indefinite if Button is Held)
|
|
|
Avoid Throttle Bursts From IDLE to MIL in How Many Seconds
|
1 Second
|
|
|
EED Displays at Max Brightness
|
If Battery Has Less Than 22 Volts
|
|
|
T Button Held on EED Selects Calibration After How Many Seconds
|
15 Seconds
|
|
|
RPM Indicator Range
|
0-110%
|
|
|
EGT Indicator Range
|
0-1200 Degrees
|
|
|
NOZ Indicator Range
|
0-99%
|
|
|
Oil Indicator Range
|
0-80 PSI
|
|
|
MAX Fuel Flow at Sea Level on Standard Day
|
7300lbs/hr
|
|
|
MAX Fuel Flow at Sea Level on Standard Day at Mach 1
|
11,400lbs/hr
|
|
|
AC Generator Output
|
320-480 Cycles Per Second
|
|
|
Gearbox Shift Range
|
65-75%
|
|
|
Maneuvering Between __ and __ Increases Susceptibility to Stall/Flameout
|
28,000ft and 0.6 IMN
|
|
|
Grey Area on Flameout Susceptibility Restrict Throttle Movements To How Quick
|
1 Inch in 3 Seconds
|
|
|
EGT Droop Conditions and Indications
|
Low Altitude/500kts/3% Nozzle
|
|
|
Idle Decay Prevention
|
Maintain 80% When Less Than 200 KCAS and Above 20,000ft
|
|
|
Gravity Feed Provides Sufficient Fuel to MAX at What Altitude
|
25,000ft (6,000 Guaranteed/15,000 Occurences)
|
|
|
Fuel Low When EITHER System INDICATES
|
250 +- 25 For More Than 7.5 Seconds
|
|
|
Fuel Imbalance Indications Begin at ___lbs With White and Greater Than ___lbs with Red
|
60lbs and >200lbs
|
|
|
If One Fuel System Has Less Than ___ Boost Pump Output is Reduced ____
|
650lbs and 40%
|
|
|
Voltage of AC System
|
115/200
|
|
|
Transformer Rectifier Amperage
|
50amps
|
|
|
Voltage of Battery
|
24 Volts
|
|
|
Generator Cut-In Speed
|
43-48%
|
|
|
Oil System Contains ___qts of Oil, With Expansion of ___qts
|
4qts and 1qt
|
|
|
Oil May be Burnt Up to ___pints per Hour
|
1 Pint
|
|
|
Pressure of Hydraulic Systems
|
3,000 PSI Each
|
|
|
Hydraulic Lights Come on At ___ and Go Out at ___
|
1,500PSI and 1,800PSI
|
|
|
Landing Gear Extension/Retraction Time
|
6 Seconds
|
|
|
Landing Gear Warning System Activates When
|
210kts or Less, 10,000ft +-750ft, Both Throttles Below 96%
|
|
|
Landing Gear Warning Tones Don't Deactivate Until Accelerating Through
|
240kts
|
|
|
Landing Gear Alternate Release Handle Extension Length and Time
|
10 Inches; 15-35 Seconds
|
|
|
Nose Gear Extended __ Provides ___ Rudder Deflection (Both Answers)
|
Less Than 3/4; 6 Degrees and 3/4 or More; 30 Degrees
|
|
|
The Majority of Slab Compensation Occurs in the First ___ % of Flap Movement
|
35%
|
|
|
Pressurization Schedule
|
<8,000 = Ambient; 8,000-23,000 = 8,000 +-1,000; >23,000 = 5psi Above Ambient
|
|
|
Engine Anti Ice On/Off Schedule
|
Requires 80%, Turns on Below 65% Automatically
|
|
|
At Engine Speeds of __ Anti-Ice Increases EGT ___
|
94-98%; 15 Degrees
|
|
|
Loss Of Thrust at MIL and MAX Due to Anti-Ice
|
9% Loss in MIL; 6.5% Loss in MAX
|
|
|
All AOA Lights May Light, No Maintenance is Required Unless They Stay On For ___
|
2 Minutes
|
|
|
Birdstrikes at ___ Can Damage Windscreen and Hit the HUD
|
400kts
|
|
|
Avoid Opening the Canopy When Relative Wind Exceeds __
|
30 kts
|
|
|
Front Canopy Jettisons First Then __ Seconds Later the Rear Canopy With the D-Handle
|
1 Second
|
|
|
Aneroid Delays Parachute Opening Until Between
|
15,000ft and 11,500ft
|
|
|
Canopy is Jettisoned During Ejection Sequence After ____ Seconds
|
0.3 Seconds
|
|
|
Seat Can Be Adjusted __ Inches
|
5 Inches
|
|
|
Seat Kit is Automatically Released After a ____ Second Delay
|
4 Seconds
|
|
|
Oxygen Low Level Light Illuminates at ___, Blinking May Occur at ___ Due to Sloshing
|
1 Liter, 3 Liters
|
|
|
MDP Power Up Requires ___ Seconds
|
45 Seconds
|
|
|
MDP Warm Boot Requres ___ Seconds While a Cold Boot Requires ___ Seconds
|
10 Seconds/45 Seconds
|
|
|
Warm Boot Occurs If Power Loss is Between ___ and ___ Milliseconds
|
50 to 300
|
|
|
EED and HUD May Disagree on Fuel, When Greater Than ___ the EED is Correct
|
20lbs
|
|
|
ILS Commands are Optimized for GS Interception at ___ and ___ Ft Above Touchdown
|
6NM and 1800ft
|
|
|
Pitch Ladder on HUD Displayed at ___ the Pitch Angle
|
One - Half
|
|
|
RALT Readings Only Available Below ___
|
5,000
|
|
|
Section II
|
|
|
|
Main Gear Strut Extension
|
4 to 4 3/4 Inches (4 3/8 +- 3/8)
|
|
|
Nose Gear Strut Extension
|
5 3/4 to 6 1/8 Inches
|
|
|
Oxygen Hose Disconnection Tension
|
12 - 20lbs
|
|
|
When Battery is Less Than ___ Volts, EED Defaults to Max Day Mode Brightness
|
22 Volts
|
|
|
Ignition Should Occur Before ___ Fuel Flow
|
360lbs/hr
|
|
|
If Ignition Does Not Occur Wait How Long Before Attempting Second Start
|
2 Minutes with Air
|
|
|
EGT Should Rise Within __ Seconds of Fuel Flow, If Not Abort Start
|
12 Seconds
|
|
|
With Normal Movement, Hydraulic Pressure Should Not Drop Below ___ PSI
|
1500 PSI
|
|
|
If DTS Is Reporting NO CASSETTE, How Long Should You Wait Before Restarting Engines
|
30 Seconds
|
|
|
MDP Must be On For ___ Seconds Before Testing Lights
|
45 Seconds
|
|
|
Oxygen Quantity Light Illuminates at ___ Liters
|
1 Liter
|
|
|
Nosewheel Tires are Severly Damaged When Max Deflection Turns are Attempted in Excess of ___ kts
|
10kts
|
|
|
Main Nosewheel is Rated to ___kts But Has Been Tested Up to ___% of That
|
174 and 120%
|
|
|
Delay ___ Minutes for Large Aircraft and ___ Minutes for Heavy Aircraft
|
2 Minutes/4 Minutes
|
|
|
Wake Turbulence Time Limits May be Reduced if Crosswind Is More Than ___ kts
|
5kts
|
|
|
Abort Takeoff if AB Fails to Light After ___ Seconds
|
5 Seconds
|
|
|
Nosewheel Should Lift Off Runway at ___kts and The Aircraft Should Lift Off at ___kts
|
150kts and 165kts
|
|
|
Aerobraking Until Loss of Elevator Authority, Then Applying Brakes Increases Chart Landing Distance By ___ %
|
50%
|
|
|
Extreme Caution Must be Used When Apply Wheel Brakes Above ___kts
|
120kts
|
|
|
Use Caution When Braking at Speeds Above ___kts
|
100kts
|
|
|
Aerobraking Using Full Back Stick Will Cause a Hard Nosewheel Impact at ___kts
|
100kts
|
|
|
Rubber Deposits on Wet Runways Make Direction Control Difficult on Last ___ ft of Runway
|
2,000ft
|
|
|
Closed Pattern Requires ___lbs of Fuel
|
150lbs
|
|
|
Main Wheel Touchdown Should Occur at ___kts Below Final Approach Airspeed
|
25kts
|
|
|
Minimize Landing Roll by Decreasing Final Approach Airspeed ___kts
|
10kts
|
|
|
Charts Figure a Landing Attitude of ___ Degrees Nose High, Then Optimum Braking
|
12 Degrees
|
|
|
Land on Upwind Side of Runway if Crosswind Exceeds ___kts
|
15kts
|
|
|
Do Not Aerobrake if Crosswind Exceeds ___kts
|
15kts
|
|
|
Landing Distance Without Aerobraking May be Increased ___ %
|
50%
|
|
|
Chances for Optimum Braking are Greatly Increased Below ___kts
|
100kts
|
|
|
Pressure Equalization After Selecting Ram Dump May Take ___ Seconds
|
Several
|
|
|
Operate Engines Below ___% RPM For ___ Minutes Prior to Shutting Down
|
70%/ 1 Minute
|
|
|
Landing/Taxi Light Requires ___ Seconds to Retract Prior to Engine Shutdown
|
10 Seconds
|
|
|
Ram Dump Door May Require ___ Seconds to C lose Prior to Engine Shutdown
|
10 Seconds
|
|
|
Instrument Climb Minimum of ___fpm
|
1,000fpm
|
|
|
Power Settings Between ___ and ___ Will Provide Comfortable Climb Rates For Intermediate Level-Offs
|
90% and 95%
|
|
|
Maintain ___ Pitch Attitude For MAX Thrust Climb Once Reaching Desired Mach
|
20-25 Degrees
|
|
|
Holding Airspeeds
|
250 - 265kts
|
|
|
SE Holding at ___ ft or Above With More Than ___lbs of Fuel is Impossible
|
20,000ft and 1800lbs
|
|
|
Recommended RPM For Anti-Ice Operation
|
80% RPM
|
|
|
Circling Approach Minimum Airspeed and Configuration Prior to Final
|
180kts + Fuel and 60% Flaps
|
|
|
Straight-In Approach Minimum Airspeed
|
160kts + Fuel
|
|
|
Base Leg Minimum Airspeed
|
180kts + Fuel
|
|
|
Radar Pattern Requires ___lbs of Fuel
|
325lbs
|
|
|
Missed Approach Airspeeds
|
240-300kts
|
|
|
Bank Angles in Excess of ___ Degrees May Make Level Turns Impossible Under Some Heavyweight Conditions
|
45 Degrees
|
|
|
Adjust Final Approach and Touchdown Speeds by ___% the Gust Factor
|
50%
|
|
|
Crossfeed When Fuel Imbalance Exceeds ___lbs
|
200lbs
|
|
|
Main/Nosewheel Tire Pressure
|
250 PSI/ 75 PSI
|
|
|
Section III
|
|
|
|
Chopping for ___ Minutes May be Necessary to Open the Rear Canopy Manually
|
Several
|
|
|
Maximum Decceleration Can Be Obtained by Maximum Braking Below ___kts
|
130kts
|
|
|
Optimum Braking Should Not be Attempted Above ___kts
|
100kts
|
|
|
Use Aerodynamic Braking to the Maximum Extent Possible During Any Abort Over ___kts
|
100kts
|
|
|
Aerodynamic Braking Pitch Attitude
|
12 NH
|
|
|
Extreme Caution Must Be Excercised When Applying Brakes Above ___kts
|
120kts
|
|
|
SETOS Ensures ___fpm Climb Gradient
|
100fpm
|
|
|
Each Knot Above SETOS Provides ___fpm Up to SETOS +10
|
60fpm
|
|
|
When SE, Restrict Climb Until Airspeed Reaches ___kts and Flaps are Retracted
|
200
|
|
|
Do Not Retract Flaps During SE Takeoff Until Reaching ___kts
|
200
|
|
|
SE Takeoff is Impossible Above ___TOF and ___lbs
|
4.0 and 12,500lbs; 3.9 and 12,700lbs
|
|
|
With Left Engine Windmilling, Gear Retraction Between SETOS +10/Final Approach Speed and 190kts, Time?
|
1 Minute
|
|
|
Gear Down, Best Level Flight/Climb is ___kts With 60% and ___kts No Flap
|
200 and 220kts
|
|
|
With High Gross Weight and Gear Down, Do Not Retract Flaps Until ___kts
|
220kts
|
|
|
Tire Failure Effects Most Pronounced Below ___kts
|
100kts
|
|
|
If Engine is Shutdown in Flight, Wait ___ Seconds Before Attempting a Restart
|
10 Seconds
|
|
|
During SE Operations, Turn Both Boost Pumps On and Crossfeed On When Below ___lbs in Either Fuel System
|
250lbs
|
|
|
Zoom Maneuver Should Be ___ Degrees Nose High
|
20 Degrees
|
|
|
Minimum RPM For Restart During Flight (To Provide Fuel Flow Through PVC Valves)
|
12-14%
|
|
|
Heart of Airstart Envelope
|
18-20%
|
|
|
Leave Throttle at Idle for ___ Seconds Before Aborting a Start
|
30 Seconds
|
|
|
If Loss of Canopy May Occur or Has Occur, Slow Below ___kts
|
300kts
|
|
|
Minimum Drag Airspeed
|
225kts
|
|
|
Nozzle Stuck Open Range
|
20-100%
|
|
|
Controlled/Uncontrolled Ejection Minimums
|
2,000ft AGL and 15,000ft AGL
|
|
|
Medium/Severe/Excessive Wind Blast Forces During Ejection at What Airspeeds
|
<450/450-600/>600
|
|
|
Emergency Minimum Ejection Conditions
|
Ground Level and 50kts
|
|
|
Ejection Seat Weight Capabilities
|
140-211lbs
|
|
|
Seat Clears Aircraft in ___ Seconds
|
0.5 Seconds
|
|
|
Man-Seat Separation Occurs at ___ Seconds
|
1.22 Seconds
|
|
|
Parachute Opening is Delayed Until Between ___ft and ___ft
|
15,000ft and 11,500ft
|
|
|
Handgrips to Chute Deployment at 160kts (Without/With One Second Delay)
|
3.42 Seconds/4.12 Seconds
|
|
|
Bank Angles Up to ___ Degrees Are Safe For Level Flight At All Airspeeds Up to ___kts
|
60 Degrees and 500kts
|
|
|
SAS Can Fail With a Maximum of ___ Degrees Rudder Deflection
|
4 Degrees
|
|
|
Yaw Damper Switch May Only Be Reset ___ Times In Flight
|
1 Time
|
|
|
Fuel Low When EITHER System INDICATES
|
250lbs +-25 For More Than 7.5 Seconds
|
|
|
Battery Life
|
15 Minutes
|
|
|
Momentary Drops in Hydraulic Pressure Below ___ PSI May be an Indication of an Unpressurized System
|
1500 PSI
|
|
|
If Hydraulic Pressure in One System Reads 0, Transfer May Occur and Limit Flight Time to ___ Minutes
|
35 Minutes
|
|
|
Toucdowns Greater Than ___kts Should be Avoided
|
200kts
|
|
|
Execute Controlability Check Above ___ft AGL
|
15,000ft AGL
|
|
|
Maintain ___kts Above Minimum Controllable Airspeed
|
20kts
|
|
|
Touchdown ___kts Above Normal Approach Speed or MCA Whichever is Higher
|
10kts
|
|
|
Maintain ___kts Above Final Approach Speed When Flaps are Assymetric
|
20kts
|
|
|
Do Not Touchdown Below ___kts With Assymetric Flaps
|
165kts
|
|
|
Flap-Slab Malfunction, and Must Use Flaps, ___ to ___ Will Provide Adequate Nose Down Control
|
30-45%
|
|
|
With Flaps Down and Flap-Slab Malfunction, Pilot has ___ Seconds to React
|
3 Seconds
|
|
|
With Less Than Full Flaps, Landing Distance Will Increase by ___ft, Roll to Full If More Than ___ of RWY
|
500ft and 2/3
|
|
|
Maximum Airspeed During SE Approaches
|
300kts
|
|
|
Left Engine Windmilling, Gear Retraction Between Final Approach Speed and 190kts May Require ___ Minutes
|
1 Minute
|
|
|
Increase Final Approach and Touchdown Speeds by ___ the Gust Factor
|
One-Half
|
|
|
Increase Final Approach and Final Turn Airspeeds by ___kts if No-Flap
|
15kts
|
|
|
Land ___kts Above Normal Touchdown Airspeed When Landing With Gear Up
|
10kts
|
|
|
Aerobraking, Then Optimum Braking May ___ the Normal Landing Distance When Performing No-Flap Landing
|
Double
|
|
|
Landing Gear Alternate Extension Length and Time
|
10 Inches; 15-35 Seconds
|
|
|
PFR Lost for ___ Seconds and ___ Seconds Signifies a MDP Warm/Cold Reboot
|
10/60 Seconds
|
|
|
FULL GPS Includes a Drift Rate of Up To ___ NM/Hr
|
0.8 NM/Hr
|
|
|
HUD May Blank for ___ to ___ Seconds if Generator is Reset or Crossover Has Occurred
|
3 to 5 Seconds
|
|
|
Section V
|
|
|
|
Normal Thrust is Obtained at ___% or ___Degrees Whichever Occurs First
|
98% or 630 Degrees
|
|
|
MIL Thrust is Obtained at ___% RPM
|
100%
|
|
|
MAX Thrust is Obtained at ___% RPM With Afterburner Operating
|
100%
|
|
|
Afterburner Augmentation is ___ to ___%
|
5 to 40%
|
|
|
Flap Limits
|
1-45 - 300; 46-60 - 240; >60 - 220
|
|
|
Gear and Gear Doors Limiting Airspeed
|
240kts
|
|
|
Do Not Extend Gear at Bank Angles Greater Than ___ Degrees OR More Than ___g's
|
45 Degrees and 1.5 Gs
|
|
|
Oxygen Pressure Operating Range
|
50-120 PSI
|
|
|
Hydraulic Pressure Operating Range
|
1500 Minimum; 2850-3200 Normal; 3200 Maximum
|
|
|
Abort Start if EGT Reaches ___ Degrees, Abort Jet if EGT Reaches ___ Degrees
|
845/925 Degrees
|
|
|
Total EGT Fluctuations of ___ Degrees Permitted, Mean within the Green
|
15 Degrees
|
|
|
Maximum Allowable Transient RPM
|
107%
|
|
|
Rapid Throttle Movements, Nozzle Should Stabilize Within ___ Seconds
|
10 Seconds
|
|
|
Nozzle Position May be Less Than ___ % When Operating in Less Than MAX AB
|
50%
|
|
|
During Cold Weather Starts, Run Engines at ___ For ___ Minutes
|
MIL and 6 Minutes
|
|
|
Oil Pressure Indication Change of ___PSI at Stabilized RPM, Reference Checklist
|
10 PSI
|
|
|
Nose Wheel Steering Limitation
|
65kts
|
|
|
Canopy Limitation
|
50kts
|
|
|
Symmetrical Flight Load Factors for 3500/3000/2000/1000
|
Neg 2.3-5.7/-2.4-5.9/-2.6-6.5/-2.9-7.2
|
|
|
Unsymmetrical Flight Load Factors for 3500/3000/2000/1000
|
0 to 4.1/4.3/4.7/5.0
|
|
|
Continuous Aileron Rolls Can Only Be Accomplished At ___g and ___ or Less Stick Deflection
|
1.0g and 3.4 or Less
|
|
|
Maximum G's
|
7.33 and -3.0 Gs
|
|
|
To Prevent Flameout Due to Fuel Starvation Avoid MAX Thrust Dives With Less Than ___lbs
|
650lbs
|
|
|
To Prevent Flameout Due to Fuel Starvation Avoid MAX Thrust in Zero or Neg G Flight Exceeding ____
|
10 Seconds at 10,000ft and 30 Seconds at 30,000ft
|
|
|
Oil Supply and Pressure Requirements Restrict Zero G Flight to ___ Seconds and Neg G Flight to ___ Seconds
|
10 Seconds and 60 Seconds
|
|
|
After 0 or Neg G Flight, If Oil Pressure Does Not Recover Within ___ Seconds, Return to Normal Flight Conditions
|
10 Seconds
|
|
|
Full Stop Landings Time Intervals if Gear is Retracted In Flight/if Gear is Left Extended
|
45 Minutes/15 Minutes
|
|
|
Maximum Nosewheel Tire Speed
|
174kts
|
|
|
Maximum Main Wheel Tire Speed
|
204/195
|
|
|
Sink Rates Should Not Exceed ___ for Normal and ___ for Crab When Less Than 1700lbs
|
590fpm and 395fpm
|
|
|
Sink Rates Should Not Exceed ___ for Normal and ___ for Crab When Greater Than 1700lbs
|
340fpm and 200fpm
|
|
|
WSSP Airspeed Limitations Normal/Severe Turbulence (SB)/Abrupt Control Movements
|
400/350/240kts
|
|
|
WSSP G Limitations
|
0-4 Symmetric and 0-3 Unsymmetric
|
|
|
Section VI
|
|
|
|
Ejection from a Spin Must be Accomplished if Recovery is Not Completed by ___ft AGL
|
15,000ft
|
|
|
G Overshoot May Occur If Pulsing the Stick Between ___ and ___ Mach
|
0.80 and 0.95 Mach
|
|
|
The First ___ Inches of Stick Travel Provide ___ Aileron Deflection
|
4.5 Inches and 1/2 Aileron Deflection
|
|
|
The remaining ____ inches of stick travel provide full aileron deflection
|
1.5 Inches
|
|
|
Minimum Stick Forces Occur Per G at ___ Mach
|
0.9 Mach
|
|
|
Section VII
|
|
|
|
EED Fuel Quantity Displays Near Thunderstorms Vary Up to ___lbs
|
200lbs
|
|
|
Thunderstorm Penetration Airspeed
|
280kts
|
|
|
Engine Damage May Occur if ___Inches of Ice Accumulates on Engine Inlet Duct Lips
|
0.25 Inches
|
|
|
Engine Anti-Ice Requires ___ % RPM
|
80% RPM
|
|
|
At Temperatures Below ___ Degrees, Allow Engines to Run at Idle for ___Minuts
|
Negative 30 F/ 2 Minutes
|
|
|
During Cold Weather Ops, Cycle Flight Controls ___ to ___ Times
|
4 to 6 Times
|
|
|
At Temperatures Below ___ Degrees, Low Idle RPM May be Observed, Increast RPM for Generators to Cut In
|
Negative 16 F
|
|
|
With Canopy Closed in Hot Weather, Cockpit Damage May Occur Above ___ Degrees
|
110 F
|
