Term
| What is the EGT limit for engine start? |
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Definition
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Term
| What is the MAX allowable overshoot (temp and time) during engine start? |
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Definition
20°C for 10 seconds
pg. 4-2 |
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Term
| What is the MAX idle EGT? |
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Definition
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Term
| What is the normal idle RPM with the bleed valve closed? |
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Definition
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Term
| What is MAX continuous RPM and EGT? |
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Definition
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Term
| What are the MRT RPM and EGT? |
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Definition
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Term
| What is the MAX EGT for an airstart? |
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Definition
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Term
| What is the MAX allowable overshoot(temperature and time) during airstart? |
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Definition
50 °C for 10 seconds
pg. 4-2 |
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Term
| What are the MIN airspeed and MAX altitude limits for an unassisted airstart? |
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Definition
min airspeed: 250 KIAS
max altitude: 25,000 ft
pg 11-19 |
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Term
| What is the maximum airspeed for landing gear and/or flap/slats extension? |
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Definition
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Term
| Max gross weight for takeoff? |
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Definition
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Term
| Below what altitude (AGL) will a pilot eject if the aircraft is in uncontrollable flight? |
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Definition
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Term
| How is a failure of the undervoltage sensing unit confirmed? |
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Definition
If the generator will not reset and voltage indication is normal (27-29 volts) and GENERATOR light remains on, the likely cause is failure of the undervoltage sensing unit.
pg. 12-4 |
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Term
True or False?
The F405-RR-401 engine installed develops 5,527# of thrust at standard sea-level conditions. |
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Definition
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Term
True or False?
The OIL PRESS light on the CWP illuminates if the differential pressure increases above 10 psi. |
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Definition
False. OIL PRESS light illuminates when pressure differential decreases below 10psi.
pg 2-4 |
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Term
True or False?
Protection circuits within the starting system automatically shut down the GTS if the GTS idle speed is not achieved within 30 seconds. |
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Definition
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Term
True or False?
During engine start, the GTS will shut down automatically at approximately 45 percent engine rpm. |
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Definition
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Term
True or False?
The HUD is an electro-optical device located only in the front cockpit that projects flight and weapon delivery information in symbolic form into the pilots instantaneous field of view on a combining glass. |
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Definition
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Term
True or False?
During ground starting, engine ignition units are continuously energized for 30 seconds after the GTS start button is released. |
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Definition
False. During airstarting only. During ground starting, ignition ceases immediately when the GTS start button is releases.
pg 2-5 |
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Term
True or False?
During ground starting, allow an interval of 3 minutes between each GTS start, and 20 minutes after three consecutive GTS starts. |
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Definition
False. 30 minutes after three consecutive starts.
pg 2-6 |
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Term
True or False?
Engine light-off normally occurs within 10 seconds (15 seconds max) of selecting IDLE. |
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Definition
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Term
True or False?
After the bleed valve is closed, the engine should stabilize at 55+-1% RPM at sea level. (Increase 1% / 1,500' above sea level) |
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Definition
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Term
True or False?
Immediate airstarts may be attempted at any airspeed and altitude. |
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Definition
True. (Within 10 seconds of engine flameout or shutdown.)
pg 15-1 |
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Term
| After an airstart, when the engine has accelerated and stabalized, the GEN and HYD 2 should be reset. |
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Definition
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Term
True or False?
The BIT display will automatically display upon system power-up. |
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Definition
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