PA-44-180 Seminole General & Limitations Flashcards

1
Q

Engines

A

2 Lycoming 0-360-A1H6, 4 cylinder, direct drive, horizontally opposed, air cooled rated to 180 hp at 2700 rpm on a standard day at sea level

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2
Q

Prop

A

2 Hartzell, max of 74”, min 72”, Constant speed, hydraulically actuated, full feathering

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3
Q

Fuel

A

110 total capacity, 108 usable (54 useable each tank), 100 Green or 100LL Blue only

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4
Q

Oil

A

8 qts per engine, do not operate less than 6 qts.

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5
Q

Max Weights

A

Max ramp: 3816
Max T.O.: 3800
Max Landing: 3800
Max weight in baggage comp: 200

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6
Q

Vne

A

202

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7
Q

Vno

A

169

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8
Q

Va

A

3800 lbs: 135

2700 lbs: 112

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9
Q

Vle

A

Landing gear extended: 140

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10
Q

Vlo

A

Landing gear extension: 140

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11
Q

Vlo

A

Landing gear retraction: 109

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12
Q

Vfe

A

111

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13
Q

Vyse, OEI best rate of climb

A

88

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14
Q

Vmca

A

Air min control speed, lowest speed at which airplane is controllable with OEI and no flaps (stalled condition): 56

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15
Q

Red radial line

A

Vne: 202

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16
Q

Yellow arc

A

Caution range: 169-202

17
Q

Green arc

A

Normal operating range: 57-169

18
Q

White arc

A

Flaps down: 55-111

19
Q

Blue radial line

A

Vyse, OEI best rate of climb: 88

20
Q

Inner red radial line

A

Vmca: 56

21
Q

Vr

A
75
Shortfield:
 3800: 70
  3400: 66
  3000: 62
  2600: 57
22
Q

Vlof

A

N/A

23
Q

Vxse

A

Best angle of climb OEI: 82

24
Q

Vsse

A

Safe, intentional OEI speed: 82

25
Q

Vx

A

82

26
Q

Vy

A

88

27
Q

Max CHT

A

500 F

28
Q

Max oil temp

A

245 F

29
Q

Oil pressure

A

Min 25psi

Mac 115psi

30
Q

Fuel pressure

A

Min (red line) 0.5psi
Normal (green arc) 0.5-8psi
Max (red line) 8psi

31
Q

Flight Load factors

A

Max positive load factor
Flaps up: 3.8g
Flaps down: 2.0g

Max negative load factor
N/A: no inverted maneuvers approved

32
Q

Vacuum Pump

A

4.8 - 5.2 inches of mercury