Systems Flashcards

1
Q

What type of engine does the Archer have?

A

A Lycoming O-360-A4M 180 hp 4-cylinder; horizontally-opposed, Air cooled, normally-aspirated, direct drive

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2
Q

What type of propeller does the Archer have?

A

A Sensenich 2 bladed, fixed-pitch, 76” diameter, metal alloy propeller

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3
Q

What is the Archer’s wingspan?

A

35’ 6”

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4
Q

What is the turning radius of the Archer?

A

30’

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5
Q

How far apart is the Archer’s landing gear?

A

10’ wide

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6
Q

How long is the Archer?

A

24’

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7
Q

How tall is the Archer?

A

7’ 3.5” to the top of the tail

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8
Q

What type of alternator is found on the Archer?

A

A 70 amp, 28 volt alternator

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9
Q

What type of struts does the Archer use for its landing gear, and what is their normal extension?

A

Oleo (Air-Oil) struts, with a normal extension of 3.25” for the nose gear, and 4.5” for the main gear

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10
Q

Describe the brake system on the Archer.

A

The brakes are hydraulic, with a disc and caliper on each of the main wheels. The brakes are operated by either the toe brakes on the rudder pedals, or by the parking brake lever below the instrument panel. The parking and toe brakes share a common fluid reservoir, but have separate cylinders.

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11
Q

What voltage is the battery in the Archer?

A

24 volt

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12
Q

What is the proper inflation for the tires on an Archer?

A

18 psi for the nose gear and 24 psi for the mains

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13
Q

How many static wicks are there on the Archer?

A

9 - 3 on each wing, 2 on the stabilator and 1 on the rudder

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14
Q

What type of flaps does the Archer have?

A

Slotted flaps, manually operated

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15
Q

What type of ailerons does the Archer have?

A

Differential ailerons

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16
Q

What is the maximum flight load limit for normal and utility maneuvers in the Archer?

A

3.8 G’s for normal maneuvers, 4.4 G’s for utility

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17
Q

Minimum Equipment; VFR Day:

A

91.205(b):

A - Altimeter

T - Tachometer(s)
O - Oil Temperature Gauge(s) (Air-cooled)
M - Manifold Pressure Gauge(s) (Constant-speed)
A - Airspeed Indicator
T - Temperature Gauge(s) (Liquid-cooled)
O - Oil Pressure Gauge(s)

F - Fuel Quantity Indicator(s)
L - Landing Gear Position Indicator (Retractable)
A - Anticollision Lights
M - Magnetic Direction Indicator
E - ELT
S - Safety Belts/Shoulder Harnesses
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18
Q

Minimum Equipment; VFR Night:

A

91.205(c):

VFR Day PLUS

F - Fuses (one spare set)
L - Landing Lights (if for hire)
A - Anticollision Lights
P - Position Lights
S - Source of Power
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19
Q

Minimum Equipment; IFR Day and Night:

A

91.205(d):

VFR Day PLUS (If IFR Night) VFR Night PLUS:

G - Generator/Alternator
R - Radio
A - Artificial Horizon
B - Ball (slip/skid indicator)

C - Clock
A - Adjustable Altimeter
R - Rate of Turn Indicator
D - Directional Gyro
D - DME (if above FL240)
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20
Q

What is the wingspan of the Seminole?

A

38’ 6.6”

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21
Q

What is the length of the Seminole?

A

27’ 7.2”

22
Q

What’s the height of the Seminole?

A

8’ 6” to the top of the tail

23
Q

What are the landing gear dimensions on a Seminole?

A

10’ 6.5” wide

24
Q

What is the turning radius of a Seminole?

A

33’

25
Q

What are the engines on a Seminole?

A

Left: Lycoming O-360
Right: Lycoming LO-360

4 cylinder, 180 horsepower, counter-rotating, horizontally-opposed, Air-cooled, normally aspirated, direct-drive

26
Q

What are the propellers on a Seminole?

A

Hartzell two-bladed, 72-74” diameter, constant speed, hydraulically-actuated, full-feathering, metal alloy propellers

27
Q

What is the fuel capacity for the Seminole?

A

110 gallons, 108 useable

28
Q

What is the fuel capacity for the Archer?

A

50 gallons, 48 useable

29
Q

What is the oil capacity for the Seminole?

A

1979-1980: 2-6 quarts, 4.5 minimum

2000+: 2-8 quarts, 6.5 minimum

30
Q

What is the oil capacity for the Archer?

A

2-8 quarts, 6 minimum

31
Q

What is the proper inflation for the tires on the Seminole?

A

50 psi for the nose gear, 55 psi for the mains

32
Q

What determines the critical engine?

A

P - P-Factor (yaw)
A - Accelerated slipstream (roll)
S - Spiral slipstream (yaw)
T - Torque (roll)

33
Q

How is Vmc determined?

A
S - Standard day at sea level
M - Max power
A - Aft CG
C - Critical engine windmilling
F - Flaps and gear up
U - Up to 5 degrees bank 
M - Most unfavorable weight
34
Q

Vso (Seminole)

A

55 (Stall speed in landing configuration)

35
Q

Vmc (Seminole)

A

56 (Minimum controllable airspeed with critical engine inop)

36
Q

Vs (Seminole)

A

57 (stall speed in clean configuration)

37
Q

Vr (Seminole)

A

75 (rotation speed)

38
Q

Vx (Seminole)

A

82 (best angle of climb speed)

39
Q

Vxse (Seminole)

A

82 (best single engine angle of climb speed)

40
Q

Vsse (Seminole)

A

82 (minimum speed for intentional engine failure)

41
Q

Vy (Seminole)

A

88 (best rate of climb speed)

42
Q

Vyse (Seminole)

A

88 (best single engine rate of climb speed)

43
Q

Vfe (Seminole)

A

111 (Maximum flaps extended speed)

44
Q

Vlo (up) (Seminole)

A

109 (Maximum gear retraction speed)

45
Q

Vlo (down) (Seminole)

A

140 (Maximum gear extension speed)

46
Q

Vle (Seminole)

A

140 (Maximum landing gear extended speed)

47
Q

Vno (Seminole)

A

169 (Maximum structural cruising speed)

48
Q

Vne (Seminole)

A

202 (never-exceed speed)

49
Q

Va (3800) (Seminole)

A

135 (maneuvering speed at 3800 pounds)

50
Q

Va (2700) (Seminole)

A

112 (maneuvering speed at 2700 pounds)