8165C - My Aircraft and Systems

Question 1

Vy speed

Answer 1

76 knots

Question 2

Vx speed

Answer 2

64 knots

Question 3

Max Flaps down speed Vfe

Answer 3

100 knots

Question 4

Stall speed in landing configuration Vso

Answer 4

50 knots

Question 5

Stall flaps up Vs1

Answer 5

56 knots

Question 6

Never exceed speed

Answer 6

153 knots

Question 7

Maximum Structural Cruise Vno

Answer 7

121 knots

Question 8

Engine out glide max range

Answer 8

74 knots

Question 9

Service ceiling

Answer 9

12,700

Question 10

Absolute ceiling

Answer 10

14,960

Question 11

Make and HP of engine

Answer 11

Lycoming O-320-E3D 150hp

Question 12

Useable Fuel Capacity

Answer 12

48 gallons plus 2 unusable

Question 13

Octane rating and fuel color

Answer 13

100LL and blue

Question 14

Max Crosswind (demonstrated)

Answer 14

17 knots

Question 15

Max allowable baggage compartment weight

Answer 15

200 pounds

Question 16

Landing roll (flaps down)

Answer 16

595 feet

Question 17

Landing roll over 50 ft obstacle

Answer 17

1115 feet

Question 18

Gross weight

Answer 18

2325 pounds

Question 19

Standard Empty Weight

Answer 19

1331 pounds

Question 20

Maximum Useful Load

Answer 20

994 pounds

Question 21

Optimum Cruise Speed

Answer 21

116 knots

@75% power, leaned

Question 22

Optimum Cruise Range

Answer 22

720 miles

@55% power - 785 miles

Question 23

Optimum Cruise Range

Maximum Cruise Range

Answer 23

720 miles @75% power

@55% power - 785 miles

Question 24

Front tire size and pressure

Answer 24

5.00X5

30 psi

Question 25

Main tire size and pressure

Answer 25

6.00X6 | 24 psi

Question 26

Brake types

Answer 26

Cleveland single-disc hydraulic brake

Question 27

Nose gear is steerable through what range?

Answer 27

30 degrees on each side

Question 28

What are the types of struts

Answer 28

Struts are air-oil type

Question 29

Utility category max weight

Answer 29

1950 pounds

Question 30

Economy fuel flow

Answer 30

8.4 US gal / hr

Question 31

Best Power

Answer 31

92. US gal / hr

Question 32

Primary structure of aircraft is

Answer 32

aluminum allow construction

Question 33

Fuselage structure is

Answer 33

conventional semi-monocoque

Question 34

Wing type is

Answer 34

conventional semi-tapered incorporating laminar flow cantilever wings and tapered ailerons

Question 35

3 flap positions

Answer 35

10, 25 and 40 degree

Question 36

Horizontal Stabilator and vertical fin and rudder type

Answer 36

lightweight metal with fiberglass tips

Question 37

Describe engine

Answer 37

``` four-cylinder direct drive horizontally opposed 150 hp rated at 2700 RPM with starter 60 amps with 14 volt alternator dual magnetos vacuum pump fuel pump foam induction air filter ```

Question 38

engine is mounted with

Answer 38

steel tubing and dyna-focal mounts

Question 39

muffler(s) described

Answer 39

single muffler with heater shrouds for cabin, defroster for windshield and carburetor de-icing

Question 40

Brakes described

Answer 40

uses toe brakes on pedals hydraulic cylinders located above each pedal and adjacent to the hand breaklevel MIL-H-5606 petroleum base hydraulic brake fluid

Question 41

Brakes described

Answer 41

uses toe brakes on pedals hydraulic cylinders located above each pedal and adjacent to the hand brake lever MIL-H-5606 petroleum base hydraulic brake fluid