PA32-260 Flashcards

1
Q

Gross weight

A

3400

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2
Q

TO distance over 50 ft obstacle, 10 degrees of flaps @ sea level

A

1900

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3
Q

Best rate of climb Vy

A

105

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4
Q

Best angle of climb Vx

A

95

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5
Q

Max speed @ sea level

A

164

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6
Q

Cruise speed @ 65% power

A

145

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7
Q

Cruise speed @ 75% power

A

152

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8
Q

Stalling speed Vso

A

63

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9
Q

Stalling speed Vs

A

71

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10
Q

Landing distance over 50 ft obstacle

A

1000

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11
Q

Type of engine

A

Lycoming O-540-E4B5 260, Hp

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12
Q

Oil capacity

A

12 quarts

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13
Q

Fuel capacity main tanks

A

50 (25 each side)

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14
Q

Fuel capacity tip tanks

A

34 gallons (17 each side)

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15
Q

Fuel grade

A

100 aviation grade

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16
Q

Max forward baggage weight

A

100 Lbs

17
Q

Max aft baggage weight

A

100 Lbs

18
Q

Nose tire PSI

A

28-30

19
Q

Main tire PSI

A

35-40

20
Q

Aircraft description

A

6 place single engine low wing all metal

21
Q

Landing gear description

A

Main gear have brake drums

22
Q

Nose gear description

A

Steerable with rudder pedal. Can be turned 24 degrees to each side

23
Q

Struts description

A

Oleo struts air-oil type. Normal extensions = nose 3 1/4 inches, main 4 1/2 inches

24
Q

Flaps description

A

Manually operated 10, 25, 40 degrees

25
Q

Fuel selector description

A

5 positions: Off, left tip, left main, right main, right tip

26
Q

Number and location of fuel sumps

A

5: under each tank, plus the engine. That switch is located on the inside floor in front of seat 4

27
Q

Number of fuel pumps

A

2: engine pump, electric pump for back up cases

28
Q

Electrical system description

A

14 volt electrical system with a 12 volt battery for starting and alternator backup. 60 amp alternator

29
Q

Pitot Static instruments

A

Airspeed, altimeter, VSI

30
Q

Vacuum system

A

Heading, attitude, turn coordinator

31
Q

Heating system

A

Heater muff attached to the exhaust system

32
Q

How many seat configurations can be used

A

5