
161
(8) Perform external preservation of the filter non-painted surface with gun grease heated to a
temperature of 105 to 110 °C. Apply grease with a brush.
(9) Wipe the engine outer surfaces with a clean cloth (or rags) moistened in gasoline Nefras-S 50/170 or
BR-1, BR-2 and the rubberized fabric hoses with a clean dry cloth.
(10) Carefully inspect the engine externally, dress corrosion with sandpaper No. 170 or 230 and coat
with preservation oil K-17.
(11) Coat the non-painted outer parts of the engine and accessories with oil K-17.
Close the exhaust pipe (or manifold) holes with polyethylene film, install shipping covers on breather
holes.
(12) On expiration of the preservation term the engine may be preserved again for a
storage period of from 20 to 90 days. Depreserve the engine before represervation.
For represervation, remove the airscrew from the engine, wash the airscrew shaft end and the airscrew
hub assembly with gasoline Nefras-S 50/170 or BR-1, BR-2;
remove corrosion, carefully wipe, coat with gun grease and reinstall the airscrew.
(13) To depreserve the engine, proceed as follows:
(a) Wipe the engine exterior dry with a cloth moistened in gasoline Nefras-S 50/170 or BK-1, HR-2 and
blow with compressed air.
(b) Drive out spark plugs from all the cylinders and plugs of the intake pipes of cylinders Nos 4 through 6
and drain grease from the lower cylinders, turning the airscrew shaft for 8 to 10 turns; remove oil from cylinders
Nos 1, 2, 3» 7, 8 and 9 using a syringe.
At an ambient temperature below 10 °C, drain oil after heating the engine.
(c) Depreserve the compressor (Ref. 080.00.00, Task Card No. 202). Carry out this operation
simultaneously with operations under Item 2.4(13)(b).
(d) Depreserve the carburetor (Ref. 073.10.03, Task Card No. 202).
(14) Repeat preservation of the engine for a period of 90 days only once. On expiration of the second
preservation term, fully depreserve the engine and test run it for 30 min at all ratings after which preserve the
engine again for the required storage period.
NOTE: If oil sprayer 77MR-1, preservation tanks 77BK-1, engine oil flushing unit 77PD-1 are
available at the User's, it is recommended to preserve the engine with the aid of this equipment in
accordance with the Instructions.
3.PRESERVATION OF ENGINE FOR STORAGE PERIOD OF UP TO ONE
YEAR
Subject to preservation for a storage period of up to one year are the engines removed from the airplane
and directed to prolonged storage or for repair.
(1) Prior to removing the engine from the airplane, carry out operations indicated in Items 2.3(1) through
2.3(4) for preserving the engine for a storage period of up to 30 days,
(2) Drain oil from the engine and oil tank (Ref. Task Card No. 244).
(3) Remove the engine from the airplane and arrange it on the support (Ref. Task Card No. 403).
C4) Remove the generator from the engine and install a blanking cover in its place (Ref. 024.30.01, Task
Card No. 201).
(5) Fill preservation oil K-17 heated to a temperature of 40 °G into the engine crank-case through the
rear breather hole till oil appears in the front breather hole. Install auxiliary covers on the flanges of the front and
rear breather holes.
(6) Fill oil MS-20 heated to a temperature of 60 to 80 °C into the fuel pump through the fuel supply
connection and turn the airscrew shaft till it appears in the outlet connection.
(7) Using a syringe, fill 60 g of oil K-17 heated to a temperature of 40 °C in the compressed air distributor
through the air supply connection, turning the airscrew shaft through 3 to 4 turns.
(8) Preserve the compressor as follows:
(a) Remove the spring lock, mesh, filter and the second mesh.
(b) Charge oil K-17 heated to a temperature of 40 °C through the suction valve turning the airscrew till oil
appears in the delivery valve connection.
(9) Remove excessive grease from the fuel pump and compressor interior, to which end turn the
airscrew shaft for 3 to 4 turns. Install the mesh, filter, the second mesh and the spring lock after accomplishing
operations under Item 3(12).
(10) Perform internal preservation of the carburetor as instructed under Item 2.3(9).
(11) Remove the valve case covers, apply preservation oil K-17 heated to a temperature of 40 °C to the
valve springs, cylinder exhaust ports, mushroom heads and stems of the valves.
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...
Страница 249: ......
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...
Страница 274: ......
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Страница 288: ...T t en 0 CO 0 T K D fi h0 Ol f 01 3 0 F4...
Страница 293: ......
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...
Страница 355: ......
Страница 358: ......