M20R 3810 Rev A page.. - Delta Aviation LLC

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SECTION I GENERAL MOONEY M20R - OVATION 2 GX BLANK 1--2 ORIGINAL ISSUE - 12-11-07
MOONEY M20R - OVATION 2 GX SECTION I GENERAL ENGINE DESCRIPTIVE DATA Number of Engines .............................................................. 1 Engine Manufacturer .............................. Teledyne Continental Motors (TCM) Model ............................................................... IO--550--G(6) Recommended TBO .................................................... 2000 Hours Type .......................................... Reciprocating, air cooled, fuel injected Number of Cylinders ......................................... 6, Horizontally opposed Displacement ................................................. 550 Cu. In. (9014 cc) Bore ............................................................ 5.25 In. (13.3 cm) Stroke .......................................................... 4.25 In. (10.8 cm) Compression Ratio ......................................................... 8.5 : 1 Fuel System Type ................................................................ Fuel Injection Make ....................................................................... TCM Fuel -- Aviation Gasoline ......................................... 100 octane --100LL Accessories Magnetos ...................................................... Bendix -- S6RN--25 Ignition Harness ................................................... Shielded/Braided Spark Plugs ........................................ AC 273 (or equivalent) (18 m/m) Oil Cooler .......................................................... TCM Full Flow Alternator ................................................... 28 Volt DC, 100 AMPS Starter ................................................................. 24 volt DC Ratings: Maximum Take Off Sea Level BHP/RPM .................................... 280/2500 PROPELLER Hartzell: Number ........................................................................ 1 Manufacturer ............................................................. Hartzell Model Number ......................................... PHC--J3YF--1RF/F7693DF--2 The (B) denotes a booted prop (for TKS) .............. PHC--J3YF--1RF/F7693DF(B)--2 Number of Blades ............................................................... 3 Diameter (MAX.) .................................................. 76 in. (193.0 cm) (MIN.) ........................................................... 75 in. (190.5 cm) Type .............................................................. Constant Speed Governor (McCauley) ............................. Hydraulically controlled by engine oil Blade Angles @ 30.0 in. Sta.: Low .................................................. 16.5 degrees +/-- 0.2 degrees High .................................................. 38.0 degrees +/-- 1.0 degrees FUEL Minimum Fuel Grade (Color) ...................... 100 LL (Blue) or 100 Octane (Green) Total Fuel Capacity -- Standard .............................. 95 U.S. Gal. (359.6 liters) Usable Fuel .............................................. 89 U.S. Gal. (336.9 liters) Unusable Fuel: ............................................... 6 U.S. Gal. (22.7 liters) ORIGINAL ISSUE - 12-11-07 Revision A -- 08-03-2010 1--5
Page 1 and 2: PILOT’S OPERATING HANDBOOK AND FA
Page 3 and 4: MOONEY M20R - OVATION 2 GX INTRODUC
Page 9: MOONEY M20R - OVATION 2 GX SECTION
Page 13 and 14: MOONEY M20R - OVATION 2 GX SECTION

M20R 3810 Rev A page.. - Delta Aviation LLC

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