163
(21) Preserve the engine spares (except for gaskets and rubber parts) and airborne tools with oil K-17 at
a room temperature. Wrap the preserved spares in paraffined paper, prepare the box for packaging, insert
spares into it and secure the box cover.
(22) Package the airborne tools into the case using the following procedure:
(a) Carefully inspect the case, clean it of soil by blowing with dry clean compressed air or wipe with clean
dry cloths.
(b) Place the airborne tools into the case. The tools should be securely fixed in the clamps.
NOTE: Never touch the tools with ungloved hands.
(c) Dry the case with airborne tools with dry compressed air passed through the oil/moisture separator
heated to a temperature of 60 °G and dried to a dew point of not above minus 20 °C.
(d) Insert the first bag with silica-gel dehydrator, grade KSMG and ShSMG (500 g) with up to 2 %
moisture in the case.
(e) Place the airborne tool list in the case, close and seal the latter. The locks should be positively fixed.
(f) Wrap the case with two layers of paraffined paper and fix with twine. Wrap the handles with paper
and tie with twine additionally.
(g) Secure the second bag with ailica-gel dehydrator (500 g) and the silica-gel indicator cartridge to the
case by Mac-Key threads folded six or with twine,
(h) Make a cover of polyethylene film.
(i) Place the case in the cover and fuse its edges. Evacuate air from the cover through the valve so that
the cover presses to the case and ensure tightness of the valve.
Accurately position the case in the packaging box and close the box cover,
(j) Store and check condition of the silica-gel indicator as instructed in Section 8.
(23) Enter the preservation date, operation description, preservation term, name of person in charge of
preservation and place of preservation in the engine Log Book and accessory Certificate.
(24) Install and secure the individual SPTA set box and airborne tool case on the bottom of the
packaging box.
(25) Insert the engine Log Book, accessory Certificates and engine Packaging List in a special box.
(26) Close the engine with the packaging container cover, secure the cover to the bottom by four dowel
pins and seal it (the packaging container should be cleaned of dust and soil beforehand). Erase inscriptions
which do not pertain to the given engine and apply new ones.
(27) Send the engine to the addresses.
4. REMOVAL OF CORROSION FROM ENGINE PARTS
Preserve the engine for prolonged storage only after removing corrosion from parts.
(1) Remove corrosion from steel parts with sandpaper No. 170 or 230 moistened in oil MS-20 and polish
with paste GOI.
After polishing the surface, wipe it with a clean cloth moistened in gasoline, then with dry cloth and coat
with preservation grease, selected depending on the preservation term (Ref. Table 901).
(2) Remove corrosion from aluminium parts by a scraper, then dress the area with
powdered pumice or sandpaper not coarser than No. 230; wipe the parts with a cloth moistened in
gasoline, then with a dry cloth and paint the matching color or coat with preservation grease.
(3) Corrosion spreads quickly on magnesium alloy parts; therefore, immediately dress the affected areas
with a scraper, then with sandpaper not coarser than No. 230, wash with gasoline and wipe dry.
Oxidize the dressed magnesium alloy parts.
It is recommended to oxidize the parts at a room temperature in the solution of the -following formula:
Selenic acid ...................................... 20 g
Sodium bichromate ................................. 10 g
Water ............................................. 1000 ml
Exposure - 1 to 2 min.
If the parts cannot be removed from the engine, they may be oxidized by lightly rubbing with cotton wool
moistened in the solution. After oxidizing the magnesium alloy parts, dry them blowing with clean dry air and
paint the matching color or coat with preservation grease.
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...
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Страница 358: ......