Shared Flashcard Set

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EVAL PREP
T-45C NATOPS QUESTIONS FROM NFM BANK
25
Aviation
Professional
04/18/2014

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Cards

Term
What is the EGT limit for engine start?
Definition
550°C pg.

4-2
Term
What is the MAX allowable overshoot (temp and time) during engine start?
Definition
20°C for 10 seconds

pg. 4-2
Term
What is the MAX idle EGT?
Definition
450°C

pg. 4-2
Term
What is the normal idle RPM with the bleed valve closed?
Definition
55+/-2 %

pg. 4-2
Term
What is MAX continuous RPM and EGT?
Definition
100% RPM 550°C

pg. 4-2
Term
What are the MRT RPM and EGT?
Definition
104% RPM 610°C

pg. 4-2
Term
What is the MAX EGT for an airstart?
Definition
600°C

pg. 4-2
Term
What is the MAX allowable overshoot(temperature and time) during airstart?
Definition
50 °C for 10 seconds

pg. 4-2
Term
What are the MIN airspeed and MAX altitude limits for an unassisted airstart?
Definition
min airspeed: 250 KIAS
max altitude: 25,000 ft

pg 11-19
Term
What is the maximum airspeed for landing gear and/or flap/slats extension?
Definition
200 KIAS

pg. 4-5
Term
Max gross weight for takeoff?
Definition
14,500 #

pg. 4-9
Term
Below what altitude (AGL) will a pilot eject if the aircraft is in uncontrollable flight?
Definition
10,000 FT AGL

pg 15-18
Term
How is a failure of the undervoltage sensing unit confirmed?
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
Term
True or False?
The F405-RR-401 engine installed develops 5,527# of thrust at standard sea-level conditions.
Definition
True

pg. 2-1
Term
True or False?
The OIL PRESS light on the CWP illuminates if the differential pressure increases above 10 psi.
Definition
False. OIL PRESS light illuminates when pressure differential decreases below 10psi.

pg 2-4
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.
Definition
True.

pg 2-6
Term
True or False?
During engine start, the GTS will shut down automatically at approximately 45 percent engine rpm.
Definition
True

pg 2-6
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.
Definition
True

pg 2-40
Term
True or False?
During ground starting, engine ignition units are continuously energized for 30 seconds after the GTS start button is released.
Definition
False. During airstarting only. During ground starting, ignition ceases immediately when the GTS start button is releases.

pg 2-5
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.
Definition
False. 30 minutes after three consecutive starts.

pg 2-6
Term
True or False?
Engine light-off normally occurs within 10 seconds (15 seconds max) of selecting IDLE.
Definition
True.

pg 2-7
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)
Definition
False. 55+-2%

pg 2-7
Term
True or False?
Immediate airstarts may be attempted at any airspeed and altitude.
Definition
True. (Within 10 seconds of engine flameout or shutdown.)

pg 15-1
Term
After an airstart, when the engine has accelerated and stabalized, the GEN and HYD 2 should be reset.
Definition
True.

15-4
Term
True or False?
The BIT display will automatically display upon system power-up.
Definition
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