Section 1 General Flashcards
Engines
Teledyne Continental Motors
IO-520-M
285 rated HP @ 2700 RPM
Length
31’ 11.5”
Height
10’ 8”
Wheelbase
9’ 2”
Wingspan
36’ 11”
Main Wheel Track
11’ 9.5”
Horizontal Tail
17’
Tip tanks
10’
Propeller Ground Clearance
10.3 inches
Total Wing Area
179 Sq Ft
Min Turning Radius
48’ 8.5”
Props
3 blade McCauley Diameter 6’ 4.5” Constant Speed, full feathering Nonreversible hydraulically actuated Low Pitch 13.9 deg +- 0.2 Feather 81.7 deg +- 0.3
Fuel Capacity
100 Gal Mains
63 Gal Auxs
166 Gallons Total
163 Gallons Usable
Oil
Sump 12 qts Drain n fill: 13 qts Min qty 9 qts Fill to 10 qts flight to 3 hours Dip stick indicated 1 quart lower than actual quantity
Max T/O Weight
5500 lbs
Max Landing Weight
5400 lbs
Max Zero Fuel Weight
4900 lbs
Baggage Weights
Wing Lockers 120 lbs each
Nose Bay 350 lbs
Station 96 (3rd row seats) 200 lbs
Station 124/126 (behind 3rd row) 160 lbs
Baggage Volume
Nose 21 cubic feet
Wings each 9.25 Cubic feet
Aft 26.1 cubic feet
Wing Locker Dimensions
50” x 25.5” x 12.5”
Door 27” x 25.5”
Nose Baggage Dimensions
59” x 19”
Door 32.25”
Standard Empty Weight
3337 lbs
Max Useful Load
2163
Va
Maneuvering Speed: the maximum speed at which application of full available aerodynamic control will not overstress the plane.
Vfe
Max Flap Extend Speed
Vle
Max Landing Gear Extend Speed
Vlo
Max landing gear operating speed
Vmca
Air Min Control Speed: the minimum flight speed at which the airplane is controllable with a bank not more than 5 degrees when one engine suddenly becomes inoperative and the remaining engine is operating at T/O power
Vne
Never exceed speed
Vno
Max Structural Cruise Speed: The speed that should not be exceeded except in smooth air and then only with caution.
Vx
Best Angle of Climb
Vy
Best Rate of Climb
