Seating arrangement is sidebyside air brakes are

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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
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6 Hoffmann 1 H 36 DIMONA General 1.7 Approved Lubricants: Automotive lubricants with SAE ratings compatible with the seasonal temperatures. Refer to Section 8, Servicing for lubrication usage chart. CAUTION Under no circumstances should Aviation Grade oil be used! 1.8 Maximum Certified Weights : The maximum allowable take off weight is 770kg (1698 lbs.) Maximum weight for non-lifting parts is 560 kg (12361bs.) 1.9 Symbols, Abbreviations and Terminology: Liters Ltr. Ki1ogramms Kg Indicated airspeed IAS Indicated airspeed in Knots KIAS Maneuvering Speed Va Max. speed in rough air Vb Stalling Speed Vso (Airbrakes retracted) Max. speed not to be exceeded Vne (calm air) Max. speed with flaps extended Vfe Stalling speed Vsl (Airbrakes extended) Max. speed with airbrakes extended Vle 1-5
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7 Hoffmann 2 H 36 DIMONA Limitations Table of Contents Section 2 LIMITATIONS Paragraph: Page 2.1 Category of Airworthiness ------------------------------------ 8 2.2 Permitted Operations --------------------------------------------- 8 2.3 Minimum Equipment --------------------------------------------- 8 2.4 Engine Limitations ------------------------------------------------------ 9 2.5 Oil Pressure ------------------------------------------------------ 9 2.6 Oil Temperature ------------------------------------------------------ 9 2.7 Cylinder Head Temperature -------------------------------------------- 9 2.8 Voltmeter -------------------------------------------------------------- 9 2.9 Airspeed Limitations and Load Factor Limits ----------------- 10 - 11 2.10 Airspeed Indicator Markings ------------------------------------ 12 2.11 Crew Requirements ----------------------------------------------------- 12 2.12 Weights --------------------------------------------------------------- 12 2.13 Center of Gravity Limitations ------------------------------------ 13 2.14 Placards and Markings --------------------------------------------- 14 - 17
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2—1
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8 Hoffmann 2 H 36 DIMONA Limitations 2. Operating Limitations 2.1 Category of Airworthiness Utility (U) according to JAR 22 Certifications basis: JAR 22 (Joint Airworthiness Requirements for gliders and motorgliders) effective 15.3.82 2.2 Permitted Operations: The H 36 DIMONA is certified for VFR flights . (Day) Flights into known icing conditions are prohibited. Approved aerobatic maneuvers are: All aerobatic maneuvers inclusive spin and flights in clouds are forbidden. 2.3 Minimum Equipment: 1 Airspeed indicator 1 Altimeter 1 RPM counter with hour-meter 1 Oil pressure indicator 1 Oil temperature indicator 1 Voltmeter 1 Fuel quantity indicator 1 Magnetic compass 1 Cylinder-head temperature indicator 2 Seat Belts Loading Placard Data Plate Flight Manual (Approved) 2—2
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9 Hoffmann 2 H 36 DIMONA Limitations 2.4 Engine Limitations Engine Type: Limbach L 2000 EB 1C RPM Limitations (Indicator Markings) Maximum take off RPM (maximum 5 minutes) 59 KW (So hp.) 3,400 RPM Maximum ambient atmospheric temperature + 38 0 C (+100 F) Maximum RPM (METO) 53 KW (72 hp.) 3,000 RPM Red Line 3,400 RPM Caution Range - Yellow Arc 3,000 – 3,400 RPM Operating RPM - Green Arc 700 – 3,000 RPM CAUTION Avoid RPM during cruise below 2300 min –1!
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