CAAP EQC Flashcards

1
Q

engine manufacturer

A

avco lycoming

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2
Q

engine model

A

O-235-L2C

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3
Q

engine is equipped with a__________ and is __________

A

carburetor, normally aspirated

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4
Q

engine displacement

A

233.3 cubic inches

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5
Q

engine horsepower

A

110 hp

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6
Q

maximum rpm

A

2550 rpm

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7
Q

propeller manufacturer

A

mccauley/sensenich

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8
Q

blade and pitch of propeller

A

two-blade, fixed pitch

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9
Q

propeller model

A

1A103 / TCM6958

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10
Q

propeller diameter

A

at least 67.5 inches but no more than 69 inches

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11
Q

total fuel capacity - standard tanks

A

26 US gallons, 13 US gallons per tank

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12
Q

total usable fuel - standard tanks

A

24.5 US gallons

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13
Q

total fuel capacity long range tanks

A

39 US gallons, 19.5 US gallons per tank

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14
Q

total usable fuel - long range tanks

A

37.5 US gallons

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15
Q

approved avgas fuel grade

A

100LL Blue / 100 Green

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16
Q

oil system capacity

A

6 quarts

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17
Q

oil system capacity with oil filter

A

7 quarts

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18
Q

oil type

A

MIL-L-22851 ashless dispersant oil

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19
Q

MIL-L-22851 ashless dispersant oil mus be used after

A

first 50 hours or oil consumption has stabilized

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20
Q

main landing gear tire size and tire pressure

A

6.00 - 6 | 21 psi

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21
Q

nose landing gear tire size and tire pressure

A

5.00 - 5 | 30 psi

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22
Q

alternator voltage & amperes

A

28-volt, 60-amp

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23
Q

battery voltage & amperes

A

24-volt, 14-amp/hour

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24
Q

white arc airspeed

A

full flap operating speed / 35kn-85kn

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25
Q

green arc airspeed

A

normal operating speed / 40kn-111kn

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26
Q

yellow arc airspeed

A

caution range / 111kn-149kn

27
Q

red line airspeed

A

never exceed / 149kn

28
Q

never exceed speed

A

149 KIAS

29
Q

max structural cruising speed

A

111 KIAS

30
Q

maneuvering speed at maximum weight

A

104 KIAS

31
Q

max flap extend speed

A

85 KIAS

32
Q

max window open speed

A

143 KIAS

33
Q

wingspan

A

33 feet 4 inches

34
Q

length

A

24 feet 1 inch

35
Q

height

A

8 feet 6 inches

36
Q

wheel base length

A

58 inches

37
Q

propeller ground clearance

A

12 inches

38
Q

maximum turning radius

A

24 feet 8 inches

39
Q

total wing area

A

160 square feet

40
Q

maximum weight on both takeoff and landing

A

1670 lbs

41
Q

standard empty weight

A

1081 lbs

42
Q

maximum useful cargo weight

A

589 lbs

43
Q

maximum cargo/baggage weight

A

< 120 lbs

44
Q

max weight in baggage area 1

A

120 lbs

45
Q

max weight in baggage area 2

A

40 lbs

46
Q

Vx

A

55 knots

47
Q

Vy

A

67 knots

48
Q

maximum demonstrated crosswind velocity

A

12 knots

49
Q

wing loading

A

10.5 psf

50
Q

power loading

A

15.2 lbs / hp

51
Q

load factor limits

A

positive 4.4g || positive 3.5g (flaps down) || negative 1.76g

52
Q

Fuel Burn 2300RPM | 35C | 2000FT PA

A

5.1 GPH

53
Q

maximum glide speed

A

60 KIAS

54
Q

precautionary landing with engine power

A

55 KIAS

55
Q

landing without engine power - wing flaps up

A

65 KIAS

56
Q

landing without engine power - wing flaps down

A

60 KIAS

57
Q

tachometer normal operating range

A

1900 RPM - 2550 RPM

58
Q

tachometer maximum limit

A

2550 RPM

59
Q

oil temperature normal operating range

A

100F - 245F

60
Q

oil temperature maximum limit

A

245F

61
Q

oil pressure minimum limit

A

25 psi

62
Q

oil pressure normal operating range

A

60psi - 90 psi

63
Q

oil pressure maximum limit

A

100psi

64
Q

max entry speed for chandelles, lazy 8s, steep turns

A

95 knots