T-1 Epq 5

Front 1

Aircraft basic zero fuel weight is _______

Back 1

11,000 lbs

Front 2

Center-of-gravity problems affecting longitudinal stability during flight should be considered prior to...

Back 2

personnel movement within the cabin area.

Front 3

What components are in the accessory gearbox?

Back 3

DC starter/gen, N2 speed sensors, oil pump, HMU, hydraulic pump, engine-drive fuel pump

Front 4

Capacity of each oil tank in each engine?

Back 4

2.03 gal

Front 5

Max oil consumption per engine?

Back 5

8.5 ounces per hour

Front 6

If the throttle linkage cable breaks and the engine flames out, or if necessary to control the aircraft due to an engine stuck at a high power setting, what do you do?

Back 6

Shutdown the engine using the Fuel/Hydraulic valve close switch, then do the Engine shutdown during flight checklist.

Front 7

What electric bus(s) are EFC's powered by?

Back 7

Their respective left or right LOAD BUS

Front 8

What does an EFC take into account?

Back 8

Throttle angle, ambient air temp, ambient air pressure, differential between ambient air temp and total air pressure.

Front 9

When must EFCs be on?

Back 9

Whenever engines are running unless there's a malfunction

Front 10

Operation of the engines with EFCs off may result in...

Back 10

fuel coking of the fuel nozzles.

Front 11

Max thrust lost due to EFC failure?

Back 11

40%

Front 12

If you have a failed turbine shaft, what will N1 and N2 show?

Back 12

windmilling N1, no N2

Front 13

T/F - If the engine will not start with the ignition switch in STBY, the manual mode should be used.

Back 13

FALSE.

Front 14

During start, what 2 things happen when engine speed is about 35-40%?

Back 14

Speed sensor of the start/gen sends a signal to the GCU

GCU removes starter's control power and the starter/generator begins to operate as a generator.

Front 15

T/F - If either EFC fails, engine sync will be inop.

Back 15

True

Front 16

For engine sync, which engine is the master and which is the slave?

Back 16

Left master, right slave.

Front 17

If the left engine fails while engine sync is on, there will be a maximum of ___% rpm spool down of the right engine.

Back 17

1.5

Front 18

Moving the throttle friction lever forward __________ friction.

Back 18

increases.

Front 19

How do you know if you have a HOT Start?

Back 19

ITT exceeds starting limits

Front 20

Each fire bottle is charged to _____ psi at ____ degrees F.

Back 20

600 , 70

Front 21

T/F - You can control the amount of HALON that is discharged by how long you hold the bottle armed push button.

Back 21

False

Front 22

In a forced landing, your minimum airspeed on final approach is...

Back 22

140 KIAS

Front 23

Ditch parallel to or near the crest of the swell unless there is a strong crosswind of ____ knots or more.

Back 23

20

Front 24

If hydraulic pressure is between 1550 and 1850, do what?

Back 24

land as soon as practical.

Front 25

What would cause one or both H PMP PRESS LO lights to illuminate momentarily when gear down is selected?

Back 25

Prolonged flight in cold temps, followed by rapid descent

Front 26

Without hydraulic pressure the following systems will be inop:

Back 26

Flaps, speed brakes, anti-skid, power brakes, normal landing gear extension...

You still have manual braking

Front 27

For zero hydraulic pressure, increase computed 30 degrees flap landing distance by ____%

Back 27

90

Front 28

T/F - if hydraulic pressure is not within normal operating range, bypass the Alternate Gear Down Verification checklist and accomplish the Emergency Gear Extension checklist.

Back 28

True

Front 29

When you emergency extend gear, it may be necessary to ______________________ to full extend the main gear into position.

Back 29

yaw the aircraft with rudder deflection.

Front 30

Approach speed of Vapp +___ KIAS is required for ice accumulations of approximately ____ inches.

Back 30

35, 1.5

Front 31

With dual RTU failure, all the frequencies will be displayed in yellow on the CDU except...

Back 31

Nav 1

Front 32

WG ICE TEMP LO comes on when...

Back 32

leading edge duct is below 140 F

Front 33

DEFOG AIR OV HT comes on when...

Back 33

>200F

Front 34

Holding the horizontal stabilizer backup switch momentarily to the spring-loaded manual position will energize the backup system for ____ seconds. Repeat every ___ minutes.

Back 34

30, 2

Front 35

ENG ICE TEMP LO comes on when...

Back 35

nacelle below 120F

Front 36

Per SOG, T/F - When filing to the VANCE 1A MOA, include the special use airspace delay time in the total ETE for that leg of flight.

Back 36

True

Front 37

Per SOG, Min speed for closed/break?

Back 37

160 KIAS

Front 38

Per SOG, Min runway length for all student-flown full stop landings is ________ feet.

Back 38

7000

Front 39

Per SOG, filling tanks to less than ______ lbs requires SUP approval.

Back 39

3000

Front 40

Per SOG, aircrew utilizing the ELEC HEAT should select ________ position on the AUX TEMP CONTROL panel prior to the trim system check.

Back 40

Blower 1

Front 41

Per SOG, touch and goes with less than _____ feet of runway require SUP approval.

Back 41

7000

Front 42

Per SOG, at temps above ____ C and/or pressure altitudes above _____ ft, touch and goes will not be performed.

Back 42

40C, 6000ft

Front 43

Per SOG, for take-off with icing at or below _____, 32 FTS/DO approval is required.

Back 43

2000ft AGL

Front 44

Wing anti-ice will not be activated until ...

Back 44

Deconfiguration altitude (400 or 1500 ft)

Front 45

T/F - When actual icing is anticipated below 1500 ft AGL, a deconfiguration altitude of 400ft must be used.

Back 45

True