Essential Flashcards

(69 cards)

1
Q

Maximum drift correction

A

30

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2
Q

DME arc exit formula

A

Radials of anticipation = GS / (5*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

Altitude 3000ft
ROC & ROD 500FPM
Speed 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
White arc
55 - 103 kt
26
Green arc
60 - 146 kt
27
Yellow arc
146 - 183 kt
28
Red line
183 kt
29
Vle
129 kt (landing gear extended)
30
Vlo
107 kt retraction 129 kt extension
31
Vfe
103 kt (max flaps extended)
32
Va
118 kt (max manoeuvring speed)
33
Vno
146 kt
34
Vne
183 kt
35
Maximum crosswind
17 kt
36
Annunciator panel warnings
Alternator Oil pressure Vacuum
37
Gyro instruments and type of gyro
Attitude (vacuum) Directional (vacuum) Turn indicator (electric)
38
Fuel selector is checked every __ minutes, by previous engagement of the ____ ____
30 fuel pump
39
Landing gear is actuated...
Hydraulically by an electrically-powered reversible pump
40
Brake system components
Toe brakes Hand brake Shared reservoir
41
Total usable fuel
72 USG
42
Total fuel in each tank
38.5 USG
43
Total fuel capacity
77 USG
44
There are _ drain valves, _ on each tank, and _ between the firewall and fuel pump where the fuel is filtered
3 1 1
45
Gear unsafe warning lights up if...
Gear up and manifold below 14inHg Selector UP on the ground throttle retarded More than flaps 10 with gear UP
46
Gear actuation time
7 seconds
47
Propeller type
Constant speed variable pitch propeller
48
Alternator provides __A and __V & battery capacity is __V
60 12 14
49
Landing configuration order
Flaps 10 Gear DOWN Flaps 25 Flaps 40
50
Engine name & characteristics
Lycoming IO-360-C1C6 Four horizontally opposed, direct drive, injected 200Hp at 2700RPM
51
Fuselage type
Semi-monocoque structure
52
Airframe material
Basic aluminium alloy
53
Middle wing chord length
1.6 m
54
Wingtip chord length
1.07 m
55
Landing gear horizontal separation
3.04 m
56
Wingspan
10.67 m
57
Fuselage length
7.25 m
58
Maximum height
2.2 m
59
Inbound +90º formula
RR (des) Abeam = +1 min 90º def 90º def
60
Outbound -90º formula
ColDes45
61
Outbound +90º formula
RR (des) Abeam = 45º def
62
Go around callout
"Go around, speed check, flaps TO set & checked"
63
Oil temperature green arc
75ºF to 245ºF
64
Oil temperature red line
245ºF
65
Oil pressure green arc
60 to 90 PSI
66
Oil pressure yellow arc
25 to 60 PSI idle 90 to 100 PSI startup & warm-up
67
Oil pressure red lines
25 & 100 PSI
68
Fuel flow limits
2 to 21.4 GPH
69
Fuel pressure limits
0.05 to 12 PSI