
33
To preclude overcooling of the engine in cold weather or at prolonged gliding, close shutters of the
cowling and oil cooler or periodically warm up the engine by giving throttle.
When gliding before landing shift the speed governor control lever to the LOW PITCH poaition so that in
case of necessity (faulty landing planning, etc. ) it would be possible to select take-off rating.
When gliding at idle rating, oil pressure should not drop below 1 kgf/cm , Short-time
(up to 0.5 s) engine inlet oil pressure drop to 0.5 to 1 kgf/cm at near-zero and
negative accelerations as well as to a pressure of 1.8 kgf/cm for up to 5 s is allowed in flight. The total
time of engine operation under such conditions shall not exceed 5 min during service life.
To preclude overheating, taxi at low ratings with shutters of the cowling and oil cooler fully open.
2.2.5. In-Flight engine Operation at Low Ambient Temperatures
Engine ratings at take-off, climbing, level flight and descent in winter are similar to those of summer time;
however, when operating the engine in winter, it is necessary to take into account the following notes:
(1) Take-off and climbing may be performed with air heater disengaged when the carburetor inlet air
temperature is from 10 to 45 °C. If icing is possible, fully engage carburetor inlet air heating.
(2) To preclude freezing of oil in the airscrew cylinder during level flight periodically (in 20 to 30 min)
change over the airscrew from low pitch to high one and back and then reset the original speed of rotation.
(3) When gliding from high altitude in cold weather, engage the carburetor inlet air heating and close the
cowling shutters to preclude overcooliiif; of the cylinders and periodically warm up the engine so that the cylinder
head temperature does not drop below 120 °C.
Содержание M-14P
Страница 6: ...19 Engine M 14P Front View Figure 1...
Страница 7: ...20 Engine M 14P Rear View Figure 2...
Страница 27: ...40 Arrangement of Airborne Tools in Case Figure 1...
Страница 39: ......
Страница 44: ...57 Engine M 14P Test Run Chart Figure 201...
Страница 67: ...80...
Страница 163: ...176 Crankshaft Thrust Ball Bearing Front Cover Figure 1 Intermediate Crankcase Figure 2...
Страница 166: ...179 Intermediate Grankcase Front Portion Figure 3 Intermediate Crankcase Rear Portion Figure 4...
Страница 173: ...186 Front view Cylinder Figure 1 Rear view...
Страница 174: ...187 1 Inlet Valve 2 Outer Spring 3 Inner Spring 4 Split Retainer 5 Valve Plate Inlet Valve Figure 2...
Страница 178: ...191 Intake Pipe of Cylinders Nos 4 5 and 6 Figure 4 Piston Piston Rings and Piston Pin with Plugs Figure 5...
Страница 180: ...193 Timing Mechanism Schematic Diagram Figure 6 Cam Plate Figure 7...
Страница 189: ...Blower Longitudinal Section View Figure 1...
Страница 191: ...Rear view Mixture Collector Figure 2 Diffuser Figure 3...
Страница 194: ...1 Plate 2 Spring 3 Plate 4 Gear 5 Accessory Drive Shaft Blower Coupling Figure 4...
Страница 204: ...Oil Sump Figure 4...
Страница 216: ...Engine M 14P Gear Train Figure 1...
Страница 247: ...Carburetor AK 14P Operation Diagram Figure 1...
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Страница 267: ...OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CH ECKED BY Carburetor AK 14P Right Side View Figure 201...
Страница 273: ...Carburetor Altitude Control Needle Position Versus Barometric Pressure Barometric Graph Figure 203...
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Страница 288: ...T t en 0 CO 0 T K D fi h0 Ol f 01 3 0 F4...
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Страница 309: ...SPARK PLUG SD 49SMM MAINTENANCE PRACTICES 1 LIST OF TASK CARDS Title Task Card Uo Removal 201 Installation 202...
Страница 344: ...Generator Electrical Connection Diagram Commutator Side View Figure 3 1 Main Pole 2 Interpole...
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