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PA28-161 Cadet > Aircraft Data > Flashcards

Aircraft Data Flashcards

1
Q

Wingspan

A

10.67m

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2
Q

Length of Fuselage

A

7.25m

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3
Q

Wheel gauge

A

3.05m

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4
Q

Engine

A

Lycoming 0-320-D3G, 160PS, 2700rpm/min, horizontally opposed, 4 cylinders, air cooled, direct drive

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5
Q

Propeller

A

Sensenich 72’-74’ fixed pitch

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6
Q

Fuel

A

50USG (190l), 48 USG (182l) usable, AVGAS 100 (green) or 100LL (blue)

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7
Q

Oil

A

8 quarts (7.8l)

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8
Q

Mass limits

A

Ramp mass 2447lbs = 1058kg, Starting mass 2440lbs = 1055kg, landing mass 2440lbs = 1055kg, baggage compartment 50lbs = 23kg

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9
Q

VNE

A

160kt IAS

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10
Q

VNO

A

126kt IAS

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11
Q

VFE

A

103kt IAS

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12
Q

VA

A

1055kg - 111kt, 694kg - 88kt

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13
Q

Yellow arc

A

126 - 160kt

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14
Q

Green arc

A

50 - 126kt

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15
Q

White arc

A

44 - 103kt

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16
Q

Oil pressure

A

25 - 100psi

17
Q

Positive load

A

3.8g

18
Q

V best glide

A

73kt (1055kg)

19
Q

Vy

A

79kt IAS, Power full, Pitch +9°

20
Q

Vx

A

63kt IAS

21
Q

Vapp 40

A

63kt IAS, Power 1600, Pitch 0°

22
Q

Vapp 25

A

70kt IAS, Power 1600, Pitch 0°

23
Q

VR

A

55kt IAS, initial Rotate +9°

24
Q

V cruise climb

A

87kt IAS, Power full, Pitch +7°

25
Q

V cruise

A

~110kt IAS, 2500 RPM, Pitch +2°

26
Q

Vp clean

A

90kt IAS, 2300 RPM, Pitch +2°

27
Q

Vp 10 level

A

85kt IAS, 2200 RPM, Pitch +2°

28
Q

Vp 10 descent

A

85kt IAS, 1600 RPM, Pitch -1°

29
Q

Vp 25 decent

A

75kt IAS, 1600 RPM, Pitch - 1°

30
Q

Max crosswind

A

17kt

31
Q

Max Tailwind

A

5kt

32
Q

V min Flaps 10

A

58kt IAS

33
Q

V min Flaps Up

A

Vx = 63kt IAS

34
Q

Vp clean descent (0 Flaps Approach)

A

90kt, 1600 RPM, Pitch - 1

35
Q

Vapp clean (0 Flaps Approach)

A

75kt, 1600 RPM, Pitch +2

PA28-161 Cadet (1 decks)

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