PL KR

Specification

Specification Model 912 Model 912S
Weight 703 703
Wing Span 31.5 ft 31.5 ft
Wing Area 142 ft 2 142 ft 2
Chord 54 inches 54 inches
Aspect ratio 7.01 7.01
Length 18.6 ft 18.6 ft
Height (At Wing) 6.23 ft 6.23 ft
Cockipt Height 54 inches 54 inches
Width 47.25 inches 47.25 inches
Headroom 33.5 inches 33.5 inches
Legroom 43.3 inches 43.3 inches
Seats 2 2
Baggage Compartment 2 x 25 L (max 81 lbs) 2 x 25 L (max 81 lbs)
Fuel Capacity 24.8 Gallons 24.8 Gallons
Doors 2 2
Dual rudder foot controls std std
Central aileron and elev. std std
Central Flap controls std std
Dual throttle controls std std
4 point seat harness std std
Power Plant Model 912 Model 912S
Engine 912 UL 912 ULS
Output 80 HP 100 HP
Propeller 2/3 Blade 2/3 Blade
Reduction ratio 2.43 : 1 2.43 : 1
Fuel Consumption (80%) 4.5 Gal / hr 5 Gal / hr
Performance at Sea Level at MAUW Model 912 Model 912S
Take Of Roll 328 ft 262 ft
Rate of Climb 1000 ft/min 1200 ft/min
Service Ceiling 12,000 ft asl 14,000 ft asl
Max crosswind component 32 mph 32 mph
Cruise Speed (65 %) 95 mph 105 mph
Maximum level Speed 105 mph 110 mph
VNE 125 mph 125 mph
Glide Ratio ~10:1 ~10:1
Power Off Stall, No Flaps 40 mph 40 mph
Power Off Stall, Flaps 35 mph 35 mph
Landing Ground Roll 328 ft 328 ft
Gross Weight 1041lb 1041lb
Useful Load 617 617
Load Factors +4 -2 +4 -2
Roll Rate ~3 sec 45/45 ~3 sec 45/45
Endurance (width reserve) ~7.5 hrs ~7.0 hrs
Range (with reserve) ~670 miles ~700 miles