Day 15 - All Previous Topics

Question 1

Normally the Landing Gear is __ actuated and __ operated

Answer 1

Electrically, hydraulically

Question 2

During emergency gear extension it takes approximately __ seconds for the gear to be down and locked

Answer 2

30

Question 3

The landing gear warning tone is initiated when

Answer 3

The landing gear are not down/locked and flaps are at the 0 or 10 degree position with one or both throttles retarded below 70% N2 OR the landing gear are not down/locked and flaps are extended beyond the 10 degree position

Question 4

Name the four modes of braking operation

Answer 4

Manual, power, anti-skid, and emergency

Question 5

T/F - The anti-skid system is fully functional during manual braking

Answer 5

FALSE

Question 6

T/F - Once the gear has been extended using the emergency method, do not recycle the landing gear handle

Answer 6

TRUE

Question 7

When does CABIN PRESSURE LO annunciator illuminate

Answer 7

Cabin altitude 9500 +/- 500 feet

Question 8

When does ENG ICE TEMP LO annunciator illuminate

Answer 8

Below 120 F

Question 9

When does AIR COND FAIL annunciator illuminate

Answer 9

400 F or 53 psi

Question 10

When does BL AIR DCT FAIL annunciator illuminate

Answer 10

350 F or 3.5 +/- 0.5 psi

Question 11

When does DEFOG AIR OV HT annunciator illuminate

Answer 11

200 F

Question 12

When does CABIN AIR OV HT annunciator illuminate

Answer 12

390 +/-15 F

Question 13

When does CABIN PRESSURE HI annunciator illuminate

Answer 13

11 +/- 1 psi

Question 14

What components are located on the accessory gearbox

Answer 14

DC starter generator, N2 speed sensors, oil pump, hydromechanical metering unit (HMU), hydraulic pump, engine driven fuel pump

Question 15

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

Answer 15

TRUE

Question 16

Define Takeoff Rated Thrust (TRT)

Answer 16

Maximum allowable thrust limited by 104% N1, 700C ITT, or 2900 lbs of thrust, whichever occurs first and limited to 5 minutes maximum

Question 17

Define Maximum Continuous Thrust (MCT)

Answer 17

Maximum allowable thrust that may be used without a time limitation and is limited by 104% N1, 680C ITT, or 2900 lbs of thrust, whichever occurs first

Question 18

Define Maximum Cruise Thrust (MCRT)

Answer 18

The highest thrust setting that is recommended for use in cruise

Question 19

Define Go-around %N1

Answer 19

The maximum allowable thrust for use during a go-around limited by 104%N1, 700C ITT, or 2900 lbs of thrust, whichever occurs first

Question 20

Define Critical Engine Failure Speed (Vcef)

Answer 20

The speed at which one engine can fail and the same distance is required to either continue to accelerate to lift-off speed, or to abort and decelerate to a full stop

Question 21

Define Critical Field Length (CFL)

Answer 21

The total length of runway required to accelerate on all engines to critical engine failure speed, experience an engine failure, then continue to lift-off or stop

Question 22

Define Minimum Control Speed Ground (Vmcg)

Answer 22

The minimum controllable speed (88 KIAS) during the take-off run, at which, when an engine is failed, it is possible maintain directional control using only primary aerodynamic controls without deviating more than 25 feet
 laterally with all 3 wheels on the runway

Question 23

What assumptions are considered for Vmcg

Answer 23

It assumes the remaining engine at TRT, the aircraft loaded at the most unfavorable weight and CG, aircraft trimmed for takeoff, and without exceeding 180 lbs of rudder control force with rudder boost operating

Question 24

Define Minimum Control Speed Air (Vmca)

Answer 24

The minimum controllable speed (89 KIAS) in the take-off configuration out of ground effect with one engine inoperative and the remaining engine at TRT

Question 25

Vmca is determined at __

Answer 25

The most critical combination of asymmetric thrust, light weight, and aft CG

Question 26

What assumptions are considered for Vmca

Answer 26

Aircraft trimmed for takeoff, 5 degrees angle of bank into the operating engine and no more than 180 lbs of rudder control force with the rudder boost operating

Question 27

Define Refusal Speed (Vr)

Answer 27

The maximum speed that can be attained, with normal acceleration, from which a stop may be completed within the available runway length

Question 28

Define S1

Answer 28

The go/no go speed

Question 29

State the S1 equation

Answer 29

Vmcg, Vcef < S1 < Vrot, Vr, Vb

Question 30

Define Climbout Speed (Vco)

Answer 30

The scheduled single-engine climbout speed which should be obtained prior to reaching the 50 foot obstacle height