5
Hoffmann
1
H 36 DIMONA
General
TECHNICAL DATA
Wing Span
-----------
16,0 Meters ( 52 ft.)
Length
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6,85 Meters ( 22 ft.)
Wing Area
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15,20 m
2
( 164 sq. ft.)
Wing Ratio
-----------
16,8
Maximum Gross Weight
--
770 kg (1698 lbs.)
Maximum Wing Loading
--
50,7 daN/m
2
( 10,38 lbs/sq. ft.)
Airfoil
--------------------
Wortman FX 63-137
Engine
--------------------
Limbach L 2000 EB 1.C (59 kw/80 hp. rated at 3,400 Rpm)
Propeller
-------------------
Hoffmann Ho—V 62 R/L 160 T or. L 160 BT
1.3
Description:
The Hoffmann H 36 DIMONA is a two seat motor glider constructed from glass fiber. Design features
are unbraced wing, T-type stabilizer, fixed landing gear with steerable tail wheel. All three wheels are
covered with fairings. Seating arrangement is side—by—side. Air brakes are provided in the wings
upper surface. The aircraft is certified in accordance with JAR 22 in the UTILITY CATEGORY.
1.4
Engine:
Limbach L 2ooo EB 1.C,Four cylinders, opposed, air-cooled, direct drive. The engine produces 59
KW/80 Hp at 3.400 RPM.
1.5
Propeller:
Hoffmann Ho—V 62 R/L 160 T or , L 160 BT, two blade with a diameter of 160 cm ( 63 inches). The
propeller has three pitch positions controlled by the pilot.
1.6
Fuel:
The approved fuels are Aviation Grade 100 LL or Automotive fuel ‘Super’. The capacity of the fuel
tank is 83 liters 22 gal. ) . The total usable fuel is 83 liters ( 22 gal)
1—4
