EQC (C - 152) Flashcards

1
Q

Engine manufacturer

A

Avco Lycoming

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2
Q

Propeller diameter and type

A

69 inches ; fixed pitch

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3
Q

Max. gross weight

A

1670 lbs / 759 kg

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4
Q

Max. baggage allowance

A

120 lbs / 24.6 kg

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5
Q

Standard empty weight (152 & 152 II)

A

152 = 1081 lbs

152 II = 1118 lbs

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6
Q

Fuel capacity (standard & extended)

A

standard = 26 gal

extended = 39 gal

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7
Q

Usable fuel (standard & extended)

A

standard = 24.5 gal

extended = 37.5 gal

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8
Q

Oil capacity

A

6 qts (sump)

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9
Q

Max. oil temperature

A

245 degrees F / 118 degrees C

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10
Q

Max. entry speed for chandelles, lazy eights, and steep turns

A

95 kts

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11
Q

White arc airspeed

A

35 - 85 kias

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12
Q

takeoff ground roll

A

725 ft

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13
Q

takeoff distance over 50 ft. obstacle

A

1340 ft

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14
Q

landing ground roll

A

475 ft

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15
Q

landing distance over 50 ft obstacle

A

1200 ft

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16
Q

Rate of climb @ sea level

A

715 fpm

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17
Q

alternator and battery voltage

A

alternator 28v

battery 24v

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18
Q

Engine failure during takeoff run procedures

A
  1. throttle IDLE
  2. brakes APPLY
  3. flaps RETRACT
  4. mixture IDLE CUT OFF
  5. Ignition OFF
  6. Master OFF
19
Q

Engine failure immediately after takeoff procedures

A
  1. airspeed 60 KIAS
  2. mixture IDLE CUT OFF
  3. fuel s/o valve OFF
  4. ignition OFF
  5. flaps AS REQUIRED
  6. master OFF
20
Q

Engine failure during flight procedures

A
  1. airspeed 60 KIAS
  2. carb heat ON
  3. primer IN & LOCKED
  4. fuel s/o valve ON
  5. Mixture RICH
  6. Ignition BOTH (or START if propeller is stopped)
21
Q

Emergency landing without engine power procedures

A
  1. airspeed 60 KIAS
  2. mixture IDLE CUT OFF
  3. fuel s/o valve OFF
  4. ignition OFF
  5. flaps AS REQUIRED
  6. master OFF
  7. doors UNLATCH PRIOR TOUCHDOWN
  8. touchdown SLIGHTLY TAIL LOW
  9. brakes APPLY HEAVILY
22
Q

Electrical fire in flight procedures

A
  1. master OFF
  2. all other switches (except ignition) OFF
  3. vents / cabin air / heat CLOSED
  4. fire extinguisher ACTIVATE

if fire out and electrical power is needed for flight:

  1. master ON
  2. circuit breakers CHECK (DO NOT RESET)
  3. radio / electrical switches - ON one at a time (except pitot heat)
  4. vents / cabin air / heat OPEN
23
Q

1 lb = __ kg

A
  1. 454 kg
24
Q

1 nm = __ km

A

1.852 km

25
Q

Max. useful load

A

589 lbs (152)

552 lbs (152 II)

26
Q

Tachometer normal operating range

A

1990 - 2550 rpm (green arc)

27
Q

normal oil temperature range

A

100 - 245 degrees F (green arc)

28
Q

normal oil pressure range

A

60 - 90 psi (green arc)

29
Q

minimum oil pressure

A

25 psi (red line)

30
Q

maximum oil pressure

A

100 psi (red line)

31
Q

Flight load factor @ flaps up

A

+4.4 g

-1.76 g

32
Q

Flight load factor @ flaps down

A

+3.5 g

33
Q

Maximum demonstrated crosswind velocity

A

12 kts

34
Q

Engine model number

A

O-235-L2C

35
Q

Maximum engine power

A

110 BHP

36
Q

Maximum engine speed

A

2550 rpm (red line)

37
Q

Propeller manufacturer

A

McCauley Accessory Division

38
Q

Center of gravity range

A

31 - 36.5 inches aft of datum (front face of firewall)

39
Q

Approved fuel grades

A
  • 100LL grade aviation fuel (blue)
  • 100 grade aviation fuel (green)
40
Q

Wing loading

A

10.5 lbs / sq. feet

41
Q

Power loading

A

15.2 lbs / HP

42
Q

Service ceiling

A

14,700 ft

43
Q

Maximum speed @ sea level

A

110 kts

44
Q

Maximum window open speed

A

143 KIAS