Tuesday, January 1, 2008

1968 Piper Cherokee 235C (N9474W)



piper
Engine make/model:Lycoming O-540-B4B5
Horsepower@altitude: 235@SL
Horsepower for takeoff:235
TBO hrs.:
2000
Fuel type:100/100LL
Propeller type/diameter:
Hartzell CS
Landing gear type:
Tri/Fixed
Max ramp weight (lbs.):2900
Gross weight (lbs.): 2900
Landing weight (lbs.):2900
Empty weight, std. (lbs.): 1467
Useful load, std. (lbs.): 1433
Payload, full std. fuel (lbs.):
929
Usable fuel, std. (gals.): 84
Oil capacity (qts.):12
Wingspan: 32 ft.
Overall length: 23 ft. 9 in.
Height: 7 ft. 1 in.
Wing area (sq. ft.):171.6
Wing loading (lbs./sq. ft.):
17
Power loading (lbs./hp.):
12.4
Wheel size (in.):
6.00 x 6
Seating capacity: 4
Cabin doors:
1
Cabin width (in.): 44
Cabin height (in.): 47
Baggage capacity (lbs.):200
 
PERFORMANCE
Cruise speed (kts.):  
75% power @ 8,000 ft.: 136
65% power @ 8,000 ft.: 130
55% power @ 8,000 ft.:
122
  
Max range (w/ reserve) (nm):  
75% power:
813*
65% power:
879*
55% power:
949*
  
Fuel consumption (gph):
 
75% power: 12.3*
65% power:10.7*
55% power:
9.0*
  
Estimated endurance (65%) (hrs): 6.5*
Stall speed (flaps up) (knots):57
Stall speed (flaps down) (knots):52
Best rate of climb (SL fpm): 825
Best rate of climb, 8000 ft. (fpm):
500*
Service ceiling (ft.): 14,500
Takeoff ground roll (ft.): 800
Takeoff over 50-ft. obstacle (ft.):1360
Landing ground roll (ft.): 680
Landing over 50-ft. obstacle (ft.):
1300
 
* calculated





Labels: Specs

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