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RV-12 POH Flashcards

1
Q

Gross Weight

A

1320 lbs

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2
Q

Top Speed (@ gross weight)

A

117 KIAS

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3
Q

Cruise (@ gross weight, 5500 rpm)

KIAS

A

114 KIAS

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4
Q

Range (@ gross weight, 5500 rpm, 7500 ft, 30 min reserve)

A

425 nm

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5
Q

Rate of Climb (@ gross weigth, Vy 75 KCAS, sea level)

A

906 ft/min

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6
Q

Stall Flaps Down @ gross weight, Vso

A

41 KIAS

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7
Q

Stall @ gross weight, Vs

A

45 KIAS

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8
Q

Total Fuel Capacity

A

19.8 US gallons

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9
Q

Total Unusable Fuel (see warning on page 2-6)

A

Shallow climbs, level or descending flight: 0 US gallons
Vx Climb: 3 US gallons
Climbs: 4 US gallons

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10
Q

Approved Fuel Types

A

100LL Aviation Fuel
or
91 AKI Premium Unleaded Automotive

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11
Q

Maximum Engine Power

A

100 Hp @ 5800 (5 minutes maximum)

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12
Q

Prohibited Flights

A

WARNINGs

  • Night flight is prohibited (unless equipped with optional lighting)
  • Flight in IFR/IMC conditions prohibited
  • Flight into known icing conditions is prohibited
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13
Q

RV-12 designed for operation in the ____. ____ Category

A

Light Sport Category

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14
Q

Daytime flight conditions only approved provided that the aircraft is operating as specified under Part ___ of the FAR

A

Part 91

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15
Q

Stall Flaps Down at gross weight 1320 lbs Vso

A

41 KIAS

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16
Q

Stall at gross weight 1320 lbs Vs

KIAS

A

45 KIAS

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17
Q

Flap Operating Range Vso - Vfe

A

41-82 KIAS

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18
Q

Normal Operating Range (green arc)

KIAS

A

45-108 KIAS

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19
Q

Operating Maneuvering Vo 1320 lbs

KIAS

A

90 KIAS

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20
Q

Operating Maneuvering Vo 850 lbs

KIAS

A

72 KIAS

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21
Q

Maximum Structural Cruise Vno

KIAS

A

108 KIAS

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22
Q

Caution Range (yellow arc)

A

108-136 KIAS

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23
Q

Maximum Direct Crosswind Component

A

11 KTS

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24
Q

Maximum Wind Limitation

A

30 KTS

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25
Q

Never Exceed Vne (red line) below 16,000 ft

KIAS

A

136 KIAS

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26
Q

Never Exceed Vne (red line)

KIAS

A

136 KIAS

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27
Q

Service Ceiling

A

12,000 ft

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28
Q

Limit Load Factor

A

+4.0g / -2.0g

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29
Q

Prohibited Maneuvers

A

Aerobatics prohibited

Intentional spinning prohibited

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30
Q

Passenger weight limitation

Maximum pilot / passenger weight

A

Maximum pilot / passenger weight

300 lbs per seat, weight and balance permitting

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31
Q

Powerplant Limitation
Tachometer
Low End Caution Range (yellow arc)

A

1400 to 1800 RPM

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32
Q

Powerplant Limitation
Tachometer
Normal Range (green arc)

A

1800 to 5500 RPM

33
Q

Powerplant Limitation
Tachometer
High End Caution Range (yellow arc)

A

5500 to 5800 RPM

34
Q

Powerplant Limitation
Tachometer
Maximum (red line)

35
Q

Powerplant Limitation
Coolant/Cylinder Head Temperature
Normal in Cruise (green arc)

A

150 to 230 F

36
Q

Powerplant Limitation
Coolant/Cylinder Head Temperature
Caution Range (yellow arc)

A

230 to 248 F

37
Q

Powerplant Limitation
Coolant/Cylinder Head Temperature
Maximum (red line)

38
Q

Powerplant Limitation
Oil Temperature
Minimum

39
Q

Powerplant Limitation
Oil Temperature
Normal in Cruise

A

190 to 230 F

40
Q

Powerplant Limitation
Oil Temperature
Caution Range (yellow arc)

A

230 to 248 F

41
Q

Powerplant Limitation
Oil Temperature
Maximum (red line)

42
Q

Powerplant Limitation
Oil Pressure
Minimum at Cruise

43
Q

Powerplant Limitation
Oil Pressure
Maximum at Cruise

44
Q

Powerplant Limitation
Oil Pressure
Maximum - Cold (red line)

45
Q

Powerplant Limitation
Oil Pressure
Minimum at Idle (red line)

46
Q

Powerplant Limitation
Exhaust Gas Temperature
Maximum Cruise

47
Q

Powerplant Limitation
Exhaust Gas Temperature
Maximum Take-Off

48
Q

Unusable Fuel

A

Shallow climbs, level or descending flight: 0 US gallons
Vx Climb: 3 US gallons
Climbs: 4 US gallons

49
Q

Unusable Fuel Warning

A

When fuel is less than 4 gallons, extreme caution should be used during climbs to ensure that the tank outlet remains submerged. Prolonged high pitch angles (greater than 8 deg nose up), may result in fuel starvation and engine stoppage.

50
Q

Baggage capacity (max)

A

Maximum 50 lb on baggage bulkhead

51
Q

Engine is powered by a ______, _____ cylinder, ______ opposed, ______ cooled with ______ cooled cylinder heads, ______ carburators, rated at ______ HP/73.5 kW @ 5800 RPM

A

The RV-12 is powered by a Rotax 912 ULS four
cylinder, horizontaled opposed, air cooled with
liquid cooled cylinder heads, dual carburators, rated
at 100 HP/73.5 kW @ 5800RPM.

52
Q

Power to the dual spark plugs is provided by two independent _____ _____ units.

A

Two independent Electronic Ignition units

53
Q

Engine is furnished with a ______, _____ volt generator, and external _______- _______.

A

The engine is furnished with a starter, a 14 volt

generator and external rectifier-regulator.

54
Q

The full span ailerons and flaps are combined into

one unit called ______.

A

Flaperons

The full span ailerons and flaps are combined into
one unit called flaperons. An internal machanical
mixer allows the ailerons, via torque rods, to
“droop” performinmg the function of flaps.

55
Q

The stabilator and rudder are connected to the controls by _____ _____.

A

The stabilator and rudder are connected to the

controls by pull-pull cables.

56
Q

The trim tab is driven by a _____ motor.

57
Q

Rated horsepower:

A

100 Hp @ 5500 RPM (continuous)

58
Q

Wing span

A

26 ft 9 in

59
Q

Length

A

20 ft 7 in

60
Q

Height

61
Q

Empty weight

A

740 lbs (average)

62
Q

Gross weight

63
Q 
Performance (1050 lbs)
Top speed (KIAS)
64
Q

Performance (1050 lbs)
Cruise (KIAS)
5500 rpm, 7500 ft

65
Q

Performance (1050 lbs)
Cruise (KIAS)
5000 rpm, 7500 ft

66
Q

Performance (1050 lbs)
Stall - flaps up
KIAS

67
Q

Performance (1050 lbs)
Ground Performance
Take-off distance (ft)

68
Q

Performance (1050 lbs)
Ground Performance
Landing distance (ft)

69
Q

Performance (1050 lbs)
Climb/Ceiling
Rate of climb (ft/min)

A

1135 ft/min

70
Q

Performance (1050 lbs)
Climb/Ceiling
Ceiling (estimated) (ft)

71
Q 
Performance (1320 lbs)
Top speed (KIAS)
72
Q

Performance (1320 lbs)
Cruise (KIAS)
5500 rpm, 7500 ft

73
Q

Performance (1320 lbs)
Cruise (KIAS)
5000 rpm, 7500 ft

74
Q

Performance (1320 lbs)

Stall - flaps up (KIAS)

75
Q

Performance (1320 lbs)
Ground Performance
Take-off distance (ft)

76
Q

Performance (1320 lbs)
Ground Performance
Landing Distance (ft)

77
Q

Performance (1320 lbs)
Climb/Ceiling
Rate of Climb (ft)

A

900 ft/min

78
Q

Performance (1320 lbs)
Range
5500 rpm, 7500 ft

79
Q

Performance (1320 lbs)
Range
5000 rpm, 7500 ft

PPL Material (2 decks)

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