TCDS E-216

Page No. 1 2 Rev. No. 3 3 Reformatted 10/94 DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION E-216 Revision 3 RANGER 6-440-C2 (Military L-440-1) 6-440-C3 6-440-C4 6-440-C5 (Military L-440-2,3,5,7) June 21, 1960 AIRCRAFT ENGINE SPECIFICATION Engines of models described herein conforming with this specification and approved data on file with the Civil Aeronautics Administration are rated as airworthy for use in certificated aircraft in accordance with pertinent aircraft specifications and the manufacturer's installations, operation, repair and overhaul instructions. Manufacturer Ranger Aircraft Engines, Division of Fairchild Engine & Airplane Corp. Farmingdale, L.I., New York Model 6-440- C2 C3 C4 C5 6LIA - - - - - - Rating Max. continuous, hp, rpm, at sea level pressure altitude 175-2450-S.L. 180-2450-S.L. 190-2450-S.L. 200-2450-S.L. Take-off hp, rpm, at full throttle 175-2450 180-2450 190-2450 200-2450 Fuel (Minimum octane aviation gasoline) 65 73 80 87 Bore and stroke, inches 4.125 x 5.50 - - - - - - Displacement, cubic inches 440 - - - - - - Compression ratio 6.0:1 6.2:1 6.8:1 7.5:1 Weight (dry), lbs. 372 - - - - - - Propeller shaft, SAE No. 20 - - - - - - Carburetion Stromberg NAR-4B carburetor, setting No. 8036 - - - - Stromberg NAR-4B carburetor, setting No. 8038, or Marvel MA4-5 carburetor, setting No. C-1417 Ignition, dual Edison-Splitdorf Type RM, SB6RD-1 or -2 magnetos with impulse coupling (retard 45°), or Bendix Type SB6R-8, -10 or SB6RN-8, -10, magnetos - - - - - - Spark Plugs C26, C-27, BG 417, 417S - - - - - - Ignition timing, °BTC 22 25 - - - - NOTES 1,2,3,4,5 1,2,3,4,5 1,2,3,4,5 1,2,3,4,5 "- -" indicates "same as preceding model". "" indicates "does not apply". Certification basis Type Certificate No. 216 Production basis Production Certificate No. 6 E-216 2 NOTE 1. Maximum permissible cylinder head, barrel, and oil inlet temperature, 500°F, 300°F, and 200°F. respectively. NOTE 2. Eligible with aluminum parts replacing all magnesium parts except crankshaft oil plugs with a weight increase of 14 lbs. NOTE 3. The indicated military models are identical to the pertinent commercial model and are characterized as follows: Military Commercial Characteristics L-440-1 6-440-C2 Stromberg Carburetor - unshielded ignition L-440-2 6-440-C5 Stromberg Carburetor - shielded ignition L-440-3 6-440-C5 Marvel Carburetor - unshielded ignition L-440-5 6-440-C5 Stromberg Carburetor - shielded ignition L-440-7 6-440-C5 Marvel Carburetor - shielded ignition These military models are eligible for installation in certificate aircraft; however, a new nameplate should be incorporated which bears the commercial model designation and/or Type Certificate No. 216. The manufacturer will furnish the new nameplate in exchange for the old one. NOTE 4. The following accessories are eligible at the indicated weight increases: Accessory Model Weight Starters (Hand) Eclipse Type 393, Model 4 12 (Electric) Eclipse Type 396 or 397, Model Y-150 18 Generators Ranger (Electric Specialties Co.) NA-1 18 Champion Aviation Products W-128 9 Eclipse Type 309 22 Regulators Delco Remy No. 116254 5 Eclipse Type 320, Model 1 or 2 4 Fuel Pumps Romeo RB-4360 2 Pesco 227-D or DA 2 Hydraulic Pump Pesco IP-203-RA or IP-204-LC 4 Vacuum Pumps Pesco 3P-207-D 5 Eclipse Type B2A, Model 548-3A 4 Romeo Type B2A, Model R-D-2112 4 Wood Propeller Hub Warner Part No. 8599 11 NOTE 5. The following accessory drive provisions are available: Direction of Maximum Torque Maximum Overhang Rotation Facing Drive Inch - Pounds Moment Drive Engine Pad Ratio Continuous Static Inch - Pounds Starter Clockwise 1:1  7600 85.0 Generator Clockwise 1.5:1 268 2400 145.0 Fuel Pump Clockwise 0.5:1 270 1840 2.0 Hydraulic Pump Clockwise 1.5:1 400  12.0 Vacuum Pump Clockwise 1.5:1 123 517 15.0 Tachometer Clockwise 0.5:1    ....END....