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RV-12 POH Flashcards

(79 cards)

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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
Never Exceed Vne (red line) below 16,000 ft | KIAS
136 KIAS
26
Never Exceed Vne (red line) | KIAS
136 KIAS
27
Service Ceiling
12,000 ft
28
Limit Load Factor
+4.0g / -2.0g
29
Prohibited Maneuvers
Aerobatics prohibited | Intentional spinning prohibited
30
Passenger weight limitation | Maximum pilot / passenger weight
Maximum pilot / passenger weight | 300 lbs per seat, weight and balance permitting
31
Powerplant Limitation Tachometer Low End Caution Range (yellow arc)
1400 to 1800 RPM
32
Powerplant Limitation Tachometer Normal Range (green arc)
1800 to 5500 RPM
33
Powerplant Limitation Tachometer High End Caution Range (yellow arc)
5500 to 5800 RPM
34
Powerplant Limitation Tachometer Maximum (red line)
5800 RPM
35
Powerplant Limitation Coolant/Cylinder Head Temperature Normal in Cruise (green arc)
150 to 230 F
36
Powerplant Limitation Coolant/Cylinder Head Temperature Caution Range (yellow arc)
230 to 248 F
37
Powerplant Limitation Coolant/Cylinder Head Temperature Maximum (red line)
248 F
38
Powerplant Limitation Oil Temperature Minimum
120 F
39
Powerplant Limitation Oil Temperature Normal in Cruise
190 to 230 F
40
Powerplant Limitation Oil Temperature Caution Range (yellow arc)
230 to 248 F
41
Powerplant Limitation Oil Temperature Maximum (red line)
248 F
42
Powerplant Limitation Oil Pressure Minimum at Cruise
29 psi
43
Powerplant Limitation Oil Pressure Maximum at Cruise
73 psi
44
Powerplant Limitation Oil Pressure Maximum - Cold (red line)
100 psi
45
Powerplant Limitation Oil Pressure Minimum at Idle (red line)
12 psi
46
Powerplant Limitation Exhaust Gas Temperature Maximum Cruise
1560 F
47
Powerplant Limitation Exhaust Gas Temperature Maximum Take-Off
1616 F
48
Unusable Fuel
Shallow climbs, level or descending flight: 0 US gallons Vx Climb: 3 US gallons Climbs: 4 US gallons
49
Unusable Fuel Warning
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
Baggage capacity (max)
Maximum 50 lb on baggage bulkhead
51
Engine is powered by a ______, _____ cylinder, ______ opposed, ______ cooled with ______ cooled cylinder heads, ______ carburators, rated at ______ HP/73.5 kW @ 5800 RPM
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
Power to the dual spark plugs is provided by two independent _____ _____ units.
Two independent Electronic Ignition units
53
Engine is furnished with a ______, _____ volt generator, and external _______- _______.
The engine is furnished with a starter, a 14 volt | generator and external rectifier-regulator.
54
The full span ailerons and flaps are combined into | one unit called ______.
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
The stabilator and rudder are connected to the controls by _____ _____.
The stabilator and rudder are connected to the | controls by pull-pull cables.
56
The trim tab is driven by a _____ motor.
DC
57
Rated horsepower:
100 Hp @ 5500 RPM (continuous)
58
Wing span
26 ft 9 in
59
Length
20 ft 7 in
60
Height
8 ft 4 in
61
Empty weight
740 lbs (average)
62
Gross weight
1320 lbs
63
``` Performance (1050 lbs) Top speed (KIAS) ```
119 KIAS
64
Performance (1050 lbs) Cruise (KIAS) 5500 rpm, 7500 ft
117 KIAS
65
Performance (1050 lbs) Cruise (KIAS) 5000 rpm, 7500 ft
105 KIAS
66
Performance (1050 lbs) Stall - flaps up KIAS
41 KIAS
67
Performance (1050 lbs) Ground Performance Take-off distance (ft)
600 ft
68
Performance (1050 lbs) Ground Performance Landing distance (ft)
475 ft
69
Performance (1050 lbs) Climb/Ceiling Rate of climb (ft/min)
1135 ft/min
70
Performance (1050 lbs) Climb/Ceiling Ceiling (estimated) (ft)
15,000 ft
71
``` Performance (1320 lbs) Top speed (KIAS) ```
117 KIAS
72
Performance (1320 lbs) Cruise (KIAS) 5500 rpm, 7500 ft
114 KIAS
73
Performance (1320 lbs) Cruise (KIAS) 5000 rpm, 7500 ft
101 KIAS
74
Performance (1320 lbs) | Stall - flaps up (KIAS)
45 KIAS
75
Performance (1320 lbs) Ground Performance Take-off distance (ft)
700 ft
76
Performance (1320 lbs) Ground Performance Landing Distance (ft)
525 ft
77
Performance (1320 lbs) Climb/Ceiling Rate of Climb (ft)
900 ft/min
78
Performance (1320 lbs) Range 5500 rpm, 7500 ft
482 nm
79
Performance (1320 lbs) Range 5000 rpm, 7500 ft
534 nm

PPL Material (2 decks)

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