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M20R 3810 Rev A page.. - Delta Aviation LLC

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MOONEY<br />

<strong>M20R</strong> - OVATION 2 GX<br />

SECTION I<br />

GENERAL<br />

ENGINE<br />

DESCRIPTIVE DATA<br />

Number of Engines .............................................................. 1<br />

Engine Manufacturer .............................. Teledyne Continental Motors (TCM)<br />

Model ............................................................... IO--550--G(6)<br />

Recommended TBO .................................................... 2000 Hours<br />

Type .......................................... Reciprocating, air cooled, fuel injected<br />

Number of Cylinders ......................................... 6, Horizontally opposed<br />

Displacement ................................................. 550 Cu. In. (9014 cc)<br />

Bore ............................................................ 5.25 In. (13.3 cm)<br />

Stroke .......................................................... 4.25 In. (10.8 cm)<br />

Compression Ratio ......................................................... 8.5 : 1<br />

Fuel System<br />

Type ................................................................ Fuel Injection<br />

Make ....................................................................... TCM<br />

Fuel -- <strong>Aviation</strong> Gasoline ......................................... 100 octane --100LL<br />

Accessories<br />

Magnetos ...................................................... Bendix -- S6RN--25<br />

Ignition Harness ................................................... Shielded/Braided<br />

Spark Plugs ........................................ AC 273 (or equivalent) (18 m/m)<br />

Oil Cooler .......................................................... TCM Full Flow<br />

Alternator ................................................... 28 Volt DC, 100 AMPS<br />

Starter ................................................................. 24 volt DC<br />

Ratings:<br />

Maximum Take Off Sea Level BHP/RPM .................................... 280/2500<br />

PROPELLER<br />

Hartzell:<br />

Number ........................................................................ 1<br />

Manufacturer ............................................................. Hartzell<br />

Model Number ......................................... PHC--J3YF--1RF/F7693DF--2<br />

The (B) denotes a booted prop (for TKS) .............. PHC--J3YF--1RF/F7693DF(B)--2<br />

Number of Blades ............................................................... 3<br />

Diameter (MAX.) .................................................. 76 in. (193.0 cm)<br />

(MIN.) ........................................................... 75 in. (190.5 cm)<br />

Type .............................................................. Constant Speed<br />

Governor (McCauley) ............................. Hydraulically controlled by engine oil<br />

Blade Angles @ 30.0 in. Sta.:<br />

Low .................................................. 16.5 degrees +/-- 0.2 degrees<br />

High .................................................. 38.0 degrees +/-- 1.0 degrees<br />

FUEL<br />

Minimum Fuel Grade (Color) ...................... 100 LL (Blue) or 100 Octane (Green)<br />

Total Fuel Capacity -- Standard .............................. 95 U.S. Gal. (359.6 liters)<br />

Usable Fuel .............................................. 89 U.S. Gal. (336.9 liters)<br />

Unusable Fuel: ............................................... 6 U.S. Gal. (22.7 liters)<br />

ORIGINAL ISSUE - 12-11-07<br />

<strong>Rev</strong>ision A -- 08-03-2010<br />

1--5

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