PA32-260 Flashcards
Gross weight
3400
TO distance over 50 ft obstacle, 10 degrees of flaps @ sea level
1900
Best rate of climb Vy
105
Best angle of climb Vx
95
Max speed @ sea level
164
Cruise speed @ 65% power
145
Cruise speed @ 75% power
152
Stalling speed Vso
63
Stalling speed Vs
71
Landing distance over 50 ft obstacle
1000
Type of engine
Lycoming O-540-E4B5 260, Hp
Oil capacity
12 quarts
Fuel capacity main tanks
50 (25 each side)
Fuel capacity tip tanks
34 gallons (17 each side)
Fuel grade
100 aviation grade
Max forward baggage weight
100 Lbs
Max aft baggage weight
100 Lbs
Nose tire PSI
28-30
Main tire PSI
35-40
Aircraft description
6 place single engine low wing all metal
Landing gear description
Main gear have brake drums
Nose gear description
Steerable with rudder pedal. Can be turned 24 degrees to each side
Struts description
Oleo struts air-oil type. Normal extensions = nose 3 1/4 inches, main 4 1/2 inches
Flaps description
Manually operated 10, 25, 40 degrees
Fuel selector description
5 positions: Off, left tip, left main, right main, right tip
Number and location of fuel sumps
5: under each tank, plus the engine. That switch is located on the inside floor in front of seat 4
Number of fuel pumps
2: engine pump, electric pump for back up cases
Electrical system description
14 volt electrical system with a 12 volt battery for starting and alternator backup. 60 amp alternator
Pitot Static instruments
Airspeed, altimeter, VSI
Vacuum system
Heading, attitude, turn coordinator
Heating system
Heater muff attached to the exhaust system
How many seat configurations can be used
5
