Continental Motors O-200-D, Инструкция по установке и эксплуатации

Страница: 46 / 112

2-24 O-200-D & X Series Engine Installation and Operation Manual
3 January 2017
Engine Description
Oil
CAUTION: Oil must be aviation oil conforming to SAE J1899 or
SAE J1966 specifications
Oil Pressure - Normal Operation @ 75° to 240°F (24° to116°C) 30 to 60 psig
Maximum Allowable Oil Pressure
6
(cold oil)
100 psig
Minimum Oil Pressure @ Idle (600 RPM)
6
10 psig at or below 200°F
Maximum Allowable Oil Temperature
7
240°F 116°C
Minimum Take-off Oil Temperature
7 75°F 24°C
Cruise Flight Oil Temperature 170° to 220° F 77° to 104° C
Oil Sump Capacity 5.0 quarts 4.73L
Usable Oil - 16° Nose Up 4.5 quarts 4.25L
Usable Oil - 10° Nose Down 4.0 quarts 3.78L
Oil Grade, Specification See Section 3-1 of M-0, Standard Practice
Maintenance Manual
Brake Specific Oil Consumption
Maximum BSOC = 0.006 lb. /HP/HR
Engine Physical Specifications
Weight , dry (basic engine), lb. (kg) +/- 2.5%
Basic engine, minus: starter, alternator, magnetos, spark plugs,
ignition harness, baffles, filters, air box, oil sump, engine mount
isolators, and exhaust 158.2 (71.75)
Overall Dimensions, inches (mm)
Height
Width
Length
26.25
31.56
26.22
(666.75)
(801.62)
(665.98)
Center of Gravity , inches (mm)
Forward of rear accessory case
Below crankshaft centerline
Beside crankshaft centerline toward 1-3 side
14.55
0.96
0.06
(369.60)
( 24.40)
( 1.50)
1. Performance is based on sea level, standard day, zero water vapor pressure conditions at the carburetor inlet, with no engine accessory
load. Standard day conditions are 29.92 in. Hg and 59°F. Horsepower will vary approximately 1% for each 10°F (5.6° C) change in inlet air
temperature. Correction must also be made for the effect of exhaust back pressure and accessory drive losses. Contact Continental Motors
engineering for correction factors for specific applications.
2. 675 rpm if propeller inertia is greater than 9 in.-lbs.-sec
2
or 900rpm if propeller inertia is between 3.8 and 9 in-lbs.-sec
2
3. This engine is certified for operation with 100/100LL aviation fuel. If the minimum fuel grade is not available, use the next higher available
grade. Never use a lower grade fuel. Refer to Section 7-2.2 in M-0, Standard Practice Maintenance Manual.
4. Engine Operation with this fuel is limited to 9840 ft (2999 m) at maximum continuous power and speed and 19680 ft (5998 m) at maximum
continuous power and speed.
5. Measured using spark plug ring thermocouples
6. Measured at rear of crankcase, 1, 3 side.
7. Measured at oil filter adapter or oil cooler adapter with thermocouple
Table 2-3. O-200-D Specifications