Section 1 Flashcards
HUD Field of View/Instantaneous FOV From Combat Eye and Design Eye
24 Degrees/ 17 Degrees/ 15 Degrees
Gross Weight
12,800 lbs
MIL/MAX Thrust
2,050/2900lbs after PMP mod 2200/3300lbs
Length of Ignition
30 sec
Avoid Throttle Bursts From IDLE to MIL in How Many Seconds
1 sec
EED Displays at Max Brightness
If Battery Has Less Than 22 Volts
T Button Held on EED Selects Calibration After How Many Seconds
15 sec
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
7300 lbs/hr
MAX Fuel Flow at Sea Level on Standard Day at Mach 1
11,400 lbs/hr
AC Generator Output
320-480 Cycles Per Second
Gearbox Shift Range
65-75%
Grey Area on Flameout Susceptibility Restrict Throttle Movements To How Quick
1 Inch in 3 Seconds
EGT Droop Conditions and Indications
At low altitude and high airspeed (500 KCAS), EGT droop can occur with engine at military power when accompanied by 3% or less nozzle indication.
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/ 7,000 has occurred)
Fuel Low When EITHER System INDICATES
less than 250 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
- The airspeed is 210 KCAS or less.
- The altitude is 10,000 feet or below.
- Both throttles are below 96% RPM.
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
- 3/4 or More; 30 Degrees
The Majority of Slab Compensation Occurs in the First ___ % of Flap Movement
35%
Pressurization Schedule
23,000 = Alt-6,000 / 2 +-2,000
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
