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PA28 > Ressenttial > Flashcards

Ressenttial Flashcards

1
Q

Maximum drift correction

A

30

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2
Q

DME arc exit formula

A

Radials of anticipation = 0.3 * GS / radius

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3
Q

Inbound -90º formula

A

DesCab30

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4
Q

S4 turn is

A

maintained

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5
Q

S3 turn is

A

Changed at top and bottom

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6
Q

S2 turn is

A

Changed at top

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7
Q

S1 turn is

A

Changed at the bottom

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8
Q

S0 turn is

A

Not performed (constant heading)

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9
Q

Vertical S starting configuration

A

3000ft
ROC/ROD 500FPM
100kt
3 descents of 400, 300 & 200ft

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10
Q

DME arc entry formula

A

NM of anticipation = GS / 200

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11
Q

Heat taken from the shroud of the dual muffler provides

A

Cabin heat
Windshield defrosting

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12
Q

Vapp Up
Vapp 10
Vapp 25
Vapp 40

A

100 kt
90 kt
80 kt
75 kt

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13
Q

Glide speed

A

79 kt

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14
Q

Vy

A

90 kt gear up
78 kt gear down

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15
Q

Enroute climb speed

A

104 kt

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16
Q

Rotation speed
lb - kt

A

2000 - 60
2200 - 63
2400 - 66
2600 - 69
2800 - 71

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17
Q

High cruise speed

A

110 kt

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18
Q

Medium cruise speed

A

100 kt

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19
Q

Low cruise speed

A

90 kt

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20
Q

Alternate air system…

A

Changes the engine air intake, from filtered to unfiltered heated air

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21
Q

1 kg to lb

A

2.2

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22
Q

1 USG to L

A

3.78

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23
Q

Maximum baggage

A

200 lb

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24
Q

Maximum weight

A

2750 lb

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25
Q

White arc

A

55 - 103 kt

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26
Q

Green arc

A

60 - 146 kt

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27
Q

Yellow arc

A

146 - 183 kt

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28
Q

Red line

A

183 kt

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29
Q

Vle

A

129 kt (landing gear extended)

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30
Q

Vlo

A

107 kt retraction
129 kt extension

31
Q

Vfe

A

103 kt (max flaps extended)

32
Q

Va

A

118 kt (max manoeuvring speed)

33
Q

Vno

34
Q

Vne

35
Q

Maximum crosswind

36
Q

Annunciator panel warnings

A

Alternator
Oil pressure
Vacuum

37
Q

Gyro instruments and type of gyro

A

Attitude (vacuum)
Directional (vacuum)
Turn indicator (electric)

38
Q

Fuel selector is checked every __ minutes, by previous engagement of the ____ ____

A

30
fuel pump

39
Q

Landing gear is actuated…

A

Hydraulically by an electrically-powered reversible pump

40
Q

Brake system components

A

Toe brakes
Hand brake
Shared reservoir

41
Q

Total usable fuel

42
Q

Total fuel in each tank

43
Q

Total fuel capacity

44
Q

There are _ drain valves, _ on each tank, and _ between the firewall and fuel pump where the fuel is filtered

45
Q

There are 3 drain valves, 1 on each _________, and 1 between the ________ and _________ where the fuel is ________

A

fuel tank
firewall - fuel pump - filtered

46
Q

Gear unsafe warning lights up if…

A

Gear up and manifold below 14inHg
Selector UP on the ground throttle retarded
More than flaps 10 with gear UP

47
Q

Gear actuation time

48
Q

Propeller type

A

Constant speed variable pitch propeller

49
Q

Alternator provides __A and __V
Battery capacity is __V

50
Q

Landing configuration order

A

Flaps 10
Gear DOWN
Flaps 25
Flaps 40

51
Q

Engine name & characteristics

A

Lycoming IO-360-C1C6 Four horizontally opposed, direct drive, injected 200Hp at 2700RPM

52
Q

Fuselage type

A

Semi-monocoque structure

53
Q

Airframe material

A

Basic aluminium alloy

54
Q

Middle wing chord length

55
Q

Wingtip chord length

56
Q

Landing gear horizontal separation

57
Q

Wingspan

58
Q

Fuselage length

59
Q

Maximum height

60
Q

Inbound +90º formula

A

RR (des)
Abeam = +1 min
90º def
90º def

61
Q

Outbound -90º formula

62
Q

Outbound +90º formula

A

RR (des)
Abeam = 45º def

63
Q

Go around callout

A

“Go around, speed check, flaps TO set & checked”

64
Q

Oil temperature green arc

A

75ºF to 245ºF

65
Q

Oil temperature red line

66
Q

Oil pressure green arc

A

60 to 90 PSI

67
Q

Oil pressure yellow arc

A

25 to 60 PSI idle
90 to 100 PSI startup & warm-up

68
Q

Oil pressure red lines

A

25 & 100 PSI

69
Q

Fuel flow limits

A

2 to 21.4 GPH

70
Q

Fuel pressure limits

A

0.05 to 12 PSI

71
Q

Oil levels (minimum & maximum)

A

6 to 8 Quarts

72
Q

There are _ fuel pumps of the types:

A

2
Engine-driven
Electrically driven

73
Q

Fuel quantity is announced ___________ from each tank

A

independently

PA28 (4 decks)

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