Instruments

Question 1

T/F: The vision restriction device (hood) can be used in the front cockpit

Answer 1

False

Question 2

True/false: Students can perform landings from the rear cockpit

Answer 2

False

Question 3

Vertical S up pitch & power & airspeed

Answer 3

5 degrees nose high
55% power
150 knots

Question 4

Vertical S descent pitch, power &a airspeed

Answer 4

-1 degree pitch
15% power
150 knots

Question 5

45 degree bank instrument turn at 150 knots pitch & power

Answer 5

3 degrees nose high

45% power

Question 6

60 degree instrument banked turn at 150 knots pitch and power

Answer 6

4 degrees nose high

60% power

Question 7

Instrument wing over and aileron roll airspeed

Answer 7

220 knots

Question 8

Instrument aileron roll pitch

Answer 8

15-25% pitch

Question 9

Aileron roll and wing over (instrument) torque

Answer 9

80 - 100 % torque

Question 10

800 FPM Descent Penetration Airspeed, Pitch, Power

Answer 10

8 degrees nose low
5% power
200 knots

Question 11

1000 FPM penetration descent airspeed, pitch and power

Answer 11

10 degrees nose low, 25% power, speed brake

Question 12

200 knot en-route descent pitch power and airspeeds

Answer 12

5 degrees nose low/20% torque

7.5 degrees nose low/5% torque

Question 13

Final approach (level, configured) airspeed, Pitch, torque

Answer 13

110 knots, Flaps T/O, Gear down, 3 degrees nose high, 35% torque

Question 14

Precision final airspeed, Pitch, torque, resulting vsi

Answer 14

110 knots, flaps T/O, gear down, Line on line, 21% power, 600 fpm down on VSI

Question 15

Non-precision final airspeed, pitch, torque and resulting VSI

Answer 15

110 knots, flaps T/O, gear down, 1 degree nose low, 16% power, 1,000 FPM down on VSI

Question 16

Non-precision final (circling) airspeed, pitch, torque and resulting VSI

Answer 16

120 knots, flaps T/O, gear down, 1 degree nose low, 21% power, 1,000 FPM down on VSI

Question 17

Holding airspeed, pitch and power

Answer 17

150 knots, 2 degrees nose high, 35% (CLEAN)

Question 18

60 to 1 Rule:

Answer 18

1 degree of pitch = 100 ft of altitude change in 1 nautical mile

Question 19

Formula to calculate FPM descent using 60-1 rule and pitch

Answer 19

Speed (Nm/min) X Pitch X 100 = FPM

Nautical Miles/min = GS/60
The pitch x 100 comes from the gradient of descent and the 60 to 1 rule (1 degree pitch = 100 ft at 1NM)

Question 20

Instrument Slow Flight: airspeed, pitch

Answer 20

Airspeed: 110-120
3 degrees nose high
30 degrees angle of bank

Question 21

Wingover technique numbers: (bank and degrees nose high)

Answer 21

10 degrees nose high, 30 degrees of bank
20 degrees nose high, 60 degrees of bank
Passing through the horizon, 90 degrees of bank

Question 22

Course Intercept Inbound Steps

Answer 22

TIM
Dial in desired COURSE
CB + 30 (not to exceed 90)
Set Heading Bug on intercept heading

Question 23

Course Intercept Outbound procedure

Answer 23

TIM
Dial in desired RADIAL
TC + 45
Set heading bug to intercept heading

Question 24

Fix to Fix Navigation Procedure

Answer 24

• TIM
• Set RADIAL of the desired fix in the course window
• Turn in the shorter direction to a heading between the course arrow and the head of the bearing pointer (Favor the further fix)
• Update heading (fine-tune) using fix to fix map method (further fix is the outside of the EHSI “map”)
• Use heading bug to mark new heading

Question 25

Wind Drift Correction Equation for Fix to Fix method

Answer 25

Crosswind component/Speed (Nm/min) = Wind drift heading correction