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Drew's Test > 1972 C172M > Flashcards

1972 C172M Flashcards

1
Q

V1 for C172M

A

60-65

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2
Q

V2 for C172M

A

80

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3
Q

Vr for C172M

A

55

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4
Q

Vno for C172M

A

128

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5
Q

Vglide for C172M

A

80-65

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6
Q

Approach to land for C172M

A

55-65

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7
Q

Vx for C172M

A

64

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8
Q

Vy for C172M

A

78

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9
Q

Vso for C172M

A

41

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10
Q

Vs for C172M

A

47

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11
Q

Vfe for C172M

A

85

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12
Q

Va for C172M

A

80-97

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13
Q

Vne for C172M

A

160

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14
Q

Max Crosswind Component for C172M

A

15kts

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15
Q

Nosewheel turning limits for C172M

A

10 degrees

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16
Q

Wing Loading for C172M

A

13.2 lbs/sq.ft

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17
Q

Power Loading for C172M

A

15.3 lbs/hp.

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18
Q

Manuever Limits for C172M

A

60 Degrees Bank Angle

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19
Q

Manuevers Available for C172M

A

Chandelles (Entrance speed 105kts),
Lazy Eights (Entrance speed 105kts),
Steep Turns (Entrance speeds 95kts),
Spins (Entrance speed slow deceleration),
Stalls (Entrance speed slow deceleration)

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20
Q

Load Factor for C172M

A

(Flaps Up) +3.8G, -1.52G

(Flaps Down) +3.0G

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21
Q

Load Factor Utility Category for C172M

A

(Flaps Up) +4.4G, -1.76G

(Flaps Down) +3.0G

22
Q

Icing Conditions for C172M

A

Flying into icing conditions for C172M is prohibited

23
Q

Hydraulics for C172M

A

Cessnas use breaks independently controlled using toe breaks using differential pressure. When pressure is applied, it compresses hydraulic fluid in the master cylinder which pressurizes the lines and closes the brake clippers

24
Q

Cruise Speed for C172M

25
Q

Ceiling for C172M

26
Q

Range for C172M

27
Q

Wing Span of C172M

28
Q

Length of C172M

A

26’ 11”

29
Q

Height of C172M

A

8’ - 9’ 6”

30
Q

Type of Landing gear of C172M

A

Fixed Gear Landing

31
Q

Aircraft Type of C172M

A

High Wing Fixed Gear Single Piston Engine

32
Q

Propeller Type of C172M

A

Fixed Pitch Propeller: 2 blades,

Propeller Lengths 74”-75”

33
Q

Electrical System of C172M

A

14 Volt Alternator, 12 Volt Battery, 60 amp Alternator

34
Q

C172M Engine Type

A

Lycoming 0-320-E2D

35
Q

Lycoming 0-320-E2D Explained

A

Max 2700 RPM
150HP

Single Piston Engine, Horizontally Opposed, Normally-Aspirated, Direct-Drive, Air cooled, Carburetor Equipped, Four Cylinder engine, 320 cu. in displacement, Four stroke system

36
Q

Fuel of C172M

A

42 Gallon Capacity (38 Usable)

Fuel vent on left wing

Normal fuel 80/87 AVGAS. Alternate Fuels 100/130 AVGAS (Max lead 2 cc per gal), 100/130 Aviation Fuel (Max lead 4.6 cc per gal), and 100LL

Gravity fuel system, updraft carburetor

21.5 Per tank (19 Usable)

37
Q

Oil for C172M and Oil requirements of C172M

A
  • Usable Oil range 6-8 qts
  • Max Oil temp and pressure (118 Temp, 25-100 PSI)
  • Aviation Grade Straight Mineral Oil
  • Wet stump Oil System
38
Q

Maximum Baggage of C172M

A 
120 lbs (area 1), 
50 lbs (area 2)
39
Q

Maximum gross weight of C172M

40
Q

Maximum Allowable Weight of C172M

A

Front: 400lbs,
Rear: 400 lbs,
Luggage: 120 lbs

41
Q

Maximum Takeoff/Landing Weight of C172M

42
Q

Maximum Takeoff/Landing Weight Utility Category of C172M

43
Q

Maximum Useful Load of C172M

44
Q

Maximum Useful load of C172M with full fuel

45
Q

Max CG forward and Aft of C172M

A

35” Forward, 40.5” Aft

46
Q

Maximum Payload of C172M

47
Q

Empty Weight and Moment of C172M

A
  • 1392 lbs

- 54600 Moment

48
Q

Direct Drive Defined

A

Direct drive means that the propeller is bolted to, and turns at the same speed as, the crankshaft. No reduction gearing is used.

49
Q

Normally Aspirated Defined

A

internal combustion engine in which air intake depends solely on atmospheric pressure and does not have forced induction through a turbocharger or a supercharger.

50
Q

Wet Sump vs Dry Sump

A

Wet Sump, fuel sump is attached to engine

Dry Sump, Fuel sump is external of the engine

Drew's Test (10 decks)

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