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PPL > Cessna 152 > Flashcards

Cessna 152 Flashcards

1
Q

Engine

A

Avco Lycoming O-235-L2C Horizontally Opposed

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2
Q

Maximum engine power

A

110 BHP

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3
Q

Maximum engine speed

A

2550 RPM

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4
Q

Propeller

A

McCauley Accessory Division

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5
Q

Propeller Dimensions

A

69 inches max., 67.5 inches min., 12inches ground clearance

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6
Q

Wing area surface

A

160 ft2

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7
Q

Wing span

A

33 ft 4 in

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8
Q

Maximum height

A

8ft 6 in

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9
Q

Maximum width

A

24 ft 1 in

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10
Q

Service ceiling

A

14,700 ft

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11
Q

Rate of climb at sea level

A

715 FPM

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12
Q

Maximum weight

A

1670 LBS

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13
Q

Standard empty weight

A

1081 LBS

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14
Q

Maximum useful load payload and fuel

A

589 LBS

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15
Q

Maximum takeoff weight

A

1670 LBS

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16
Q

Maximum landing weight

A

1670 LBS

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17
Q

Baggage allowance, area 1 and area 2

A

120 LBS

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18
Q

Fuel capacity - standard tanks

A

26 gallons

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19
Q

Fuel Capacity - Usable

A

24.5 gallons

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20
Q

Fuel capacity - Unusable

A

1.5 gallons

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21
Q

Fuel capacity - long range tanks

A

39 gallons

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22
Q

Oil capacity:

A

6 quarts, 7 quarts (with filter)

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23
Q

Oil Grade - first 50 hours

A

MIL - L - 6082

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24
Q

Oil Grade - After 50 Hours

A

MIL - L - 22851

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25
Q

Take-off performance: ground roll

A

725 feet

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26
Q

Take off: total distance over 50ft obstacle

A

1340 feet

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27
Q

Landing performance: ground roll

A

475 feet

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28
Q

Landing: Total distance over 50ft obstacle

A

1200 ft

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29
Q

Stall speed (CAS) Flaps up, power off

A

48 knots

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30
Q

Stall speed (CAS) Flaps down, power off

A

43 knots

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31
Q

Vx

A

55 knots

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32
Q

Vy

A

67 knots

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33
Q

Maximum demonstrated crosswind

A

12 knots

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34
Q

Maneuvering speed

A

95 knots

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35
Q

Tire pressure nosewheel

A

30 PSI

36
Q

Tire pressure mainwheel

A

21 PSI

37
Q

Battery

A

24 volts, 14 ampere

38
Q

Alternator

A

28 volt, 60 ampere

39
Q

Approved fuel grade and color

A

100LL Blue;
100 (Former 100/130) Green

40
Q

Flight load factors, flaps up

A

+4.4g, -1.76g

41
Q

Flight load factor, flaps down

A

+3.5 g

42
Q

Wing loading

A

10.5 lbs/ft2
1670 lbs / 160ft2

43
Q

Power loading

A

15.2 lbs/hp
1670 lbs/110hp

44
Q

White arc

A

035-085 knots

45
Q

Green arc

A

040-111 knots

46
Q

Yellow arc

A

111-149 knots

47
Q

Red line

A

149 knots

48
Q

Maneuver - chandelles

A

95

49
Q

Maneuver - lazy eights

A

95

50
Q

Maneuver - steep turns

A

95

51
Q

Maneuver - spins

A

Use slow deceleration

52
Q

Maximum gross weight

A

1670 lbs

53
Q

Maximum useful weight

A

589 lbs

54
Q

Standard Empty Weight

A

1081 lbs

55
Q

Maximum baggage capacity

A

120 lbs

56
Q

Fuel Capacity - Standards Tanks

A

26 gallons

57
Q

Fuel Capacity - Optional Long range tanks

A

39 gallons

58
Q

Standard total usable fuel

A

24.5 gallons

59
Q

Maximum range, long range tanks - 10,000 ft

A

690 NM, 8.7HRS

60
Q

Maximum range, standard tanks - 10,000 ft

A

415 NM, 5.2 HRS

61
Q

Use of flaps 10

A

Shorten ground run by 10%

62
Q

Emergency Landing without engine power

A

60 KIAS (flaps down), 65 KIAS (flaps up)

63
Q

Ditching

A

Flaps 30, 300ft/m descent, 55 KIAS

64
Q

Oil pressure gauge should begin to show pressure in

A

30 seconds in summer time and twice as long in very cold weather

65
Q

Maxim speed at which you may use abrupt control travel

A

Va - 95 KIAS

66
Q

Cruise power

A

1900-2550 RPM

67
Q

Primary Flight Instrument for bank reference

A

Use heading indicator for primary check, turn coordinator for supporting check

68
Q

Static RPM power check

A

2280 - 2380 RPM

69
Q

Maximum Cruise speed, sea level

A
70
Q

If erroneous readings of the static source instruments (airspeed, altimeter, and rate of climb) are suspected, __________________, thereby applying static pressure to these instruments from the cabin

A

The alternate static source valve should be pulled on

71
Q

Normal take-off airspeed

A

65-75 KIAS

72
Q

Short fiel takeoff

A

54 KIAS, Flaps 10, speed at 50 ft

73
Q

Climb Flaps up, Normal airspeed

A

70 - 80 KIAS

74
Q

Landing, Normal Approach Flaps up

A

60 - 70 KIAS

75
Q

Landing, Normal Approach Flaps 30

A

55 - 65 KIAS

76
Q

Landing, Short field approach Flaps 30

A

54 KIAS

77
Q

Balked Landing, Maximum Power, Flaps 20

A

55 KIAS

78
Q

Spiral dive

A

Adjust elevator trim control to maintain a 70 kts glide

79
Q

Primary Flight Instrument for nose up and nose down reference

A

Altimeter for primary check, VSI for supporting check

80
Q

Level the nose should restore power within _____ to raise air temp - 1/4 - 1/2

A

20 seconds

81
Q

Change in engine oil

A

Every 6 months of every 100 hrs whichever comes first

82
Q

Cruise speed at sea level, 75%

A

100 KTAS

83
Q

Flight instrument for primary check for power

A

Use airspeed indicator for primary check, tachometer for support or confirm power settings

84
Q

Prior to starting on a cold morning, it is advisable to pull the propeller through several times by hand to

A

“break loose” or “limber” the oil, thus conserving battery energy

85
Q

If erroneous instrument readings are suspected due to water or ice in static pressure lines

A

The static pressure alternate source valve control knob located below the wing flap switch should be opened

86
Q

Engine Failure After Take off

A

Flaps up - 65 KIAS
Flaps down - 60 KIAS
Max Glide - 60 KIAS

PPL (15 decks)

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