Vedeneyev M-14P Maintenance Manual

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TITLE

TABLE OF CONTENTS

INTRODUCTION

ENGINE M-14P

DESCRIPTION AND OPERATION

Description

Operation

Appendices:

TROUBLE SHOOTING

MAINTENANCE PRACTICES

List of Task Cards

Operation Procedure

REMOVAL/INSTALLATION

List of Task Cards

Operation Procedure

STORAGE INSTRUCTIONS

ENGINE FRONT

DESCRIPTION AND OPERATION

General

Construction

CRANK MECHANISM ASSEMBLY

DESCRIPTION AND OPERATION

General

Construction

CYLINDER ASSEMBLY

DESCRIPTION AND OPERATION

General

Construction

TROUBLE SHOOTING

SUPERCHARGING

DESCRIPTION AND OPERATION

General

Construction

LUBRICATION

DESCRIPTION AND OPERATION

General

Description

Lubrication System Units

TROUBLE SHOOTING

MAINTENANCE PRACTICES

List of Task Cards

Operation Procedure

ACCESSORY DRIVES

DESCRIPTION AND OPERATION

General

Description

TROUBLE SHOOTING

FUEL SYSTEM

DESCRIPTION AND OPERATION

General

Fuel and Lubricants

Table of Contents

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Do you have a question about the M-14P and is the answer not in the manual?

Questions and answers

Jeff hathorn

June 17, 2025

Yak52TW with 300 TT: oil pressure gage flickering up & down taxiing in after landing.oil quantity 11 on stick after shutdown( started with 12).

1 comments:

Mr. Anderson

August 20, 2025

The flickering of the oil pressure gauge on a Vedeneyev M-14P engine in a Yak52TW after landing could be due to a faulty pressure gauge or a loose connection in the oil pressure system. The oil quantity reading of 11 on the stick after shutdown indicates adequate oil, so low oil level is not the cause. Other possible causes include air in the oil lines, partially clogged oil passages, or a malfunctioning pressure relief valve.

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Summary of Contents for Vedeneyev M-14P

Page 1 TITLE TABLE OF CONTENTS INTRODUCTION ENGINE M-14P DESCRIPTION AND OPERATION Description Operation Appendices: Fuel and Lubricants TROUBLE SHOOTING MAINTENANCE PRACTICES List of Task Cards Operation Procedure REMOVAL/INSTALLATION List of Task Cards Operation Procedure STORAGE INSTRUCTIONS ENGINE FRONT DESCRIPTION AND OPERATION...
Page 2 Description FUEL PUMP 702ML DESCRIPTION AND OPERATION General Description Operation TROUBLE SHOOTING MAINTENANCE PRACTICES List of Task Cards Operation Procedure FILTER 8D2.966.064 DESCRIPTION AND OPERATION General Description Operation MAINTENANCE PRACTICES List of Task Cards Operation Procedure CARBURETOR AK-14P DESCRIPTION AND OPERATION General Description TROUBLE SHOOTING...
Page 3 STARTING SYSTEM DESCRIPTION AND OPERATION General Airborne Air Compressor AK-50A TROUBLE SHOOTING MAINTENANCE PRACTICES List of Task Cards Operation Procedure SPINNING SYSTEM DESCRIPTION AND OPERATION General Construction TROUBLE SHOOTING MAINTENANCE PRACTICES List of Task Cards Operation Procedure ELECTRICAL POWER SYSTEM DC ELECTRICAL POWER SYSTEM GENERATOR GSR-3000M, SERIES 4 DESCRIPTION AND OPERATION...
Page 4 INTRODUCTION The M-14P engine Maintenance Manual is a one-book publication comprising description and operating instructions, including data on the construction, purpose, arrangement and. operating principle of engine systems (Ref. 073.00.00, 074.00.00, 080.00.00), as well as all the information necessary for proper operation, storage and maintenance of the engine.
Page 5 The M-14P airplane engine (Ref., Figs 1 and 2) is a piston, fourstroke, air-cooled gasoline, nine-cylinder carburetor, single-row radial engine. The M-14P engine is not of a high-altitude type, but to improve performance it is provided with one-speed centrifugal blower.
Page 6 Engine M-14P. Front View Figure 1...
Page 7 Engine M-14P. Rear View Figure 2...
Page 8: Specifications
1.2. SPECIFICATIONS 1.2.1. Engine Designation................M-14P Cooling system ................Air-type Engine starting system .............. Air-type Engine continuous operation time: At take-off rating ......……..…………....Up to 5 min At maximum permissible speed, of rotation ......Up to 1 min At other ratings ................ Not limited Iverted engine operation: Ratings ...........
Page 9 1.2.2. Gearbox Type ..................six-sateliite, planetary, single-stage Transmission ratio ..............0. 658 1.2.3. Airscrew Designation ................V530TA-D35 Type ..................Variable-pitch, push-type 1.2.4. Blower Type ..................Centrifugal, single-stage, single-speed, mechanical drive Drive transmission ratio ............8.16 1.2.5. Carburetor Designation ................AK-14P Type ..........
Page 10 Number per engine ..............1 Working fluid ................Gasoline B91/115 GOST 1012-72 g Working pressure ..............0.2 to 0.5 kgf/cm Maximum throughput ..............5 1/min Filtering fineness ..............36 to 40//m 1.2.8. Oil Pump Designation ....…............W-14A Type ..........
Page 11 NOTE: Foreign fuel and oil grades allowed for use with engine and their physical and chemical properties are given in Appendix 1. 1.2.9. Magneto Designation ................M-9F Type ..................Pour-spark, shielded Number per engine ..............2 Drive transmission ratio ......
Page 12 Advance angle for LH and BH magneto (before TDC at end of compression stroke) ......(23±1)° 1.2.12. Air Compressor Designation ................AK-50A Type ..................Piston-type Number per engine ..............1 Drive transmission ratio ............0.9 Drive direction of rotation ......
Page 13 Operating ratings of the M-14P engine are given in the Table, the throttle characteristic is shown in Fig. 3, external and altitude characteristics, in Figs 4 and 5, while the timing diagram is represented in Fig. 6. Reduced power near...
Page 14 1 - power curve 2 - specific fuel consumption curve 3 - per-hour fuel consumption curve Throttle Characteristics Figure 3...
Page 15 power line specific fuel consumption line per-hour fuel consumption line External Characteristics Figure 4...
Page 16 take-off rating (n = 2900 r/min) nominal rating I (n = 2400 r/min) nominal rating II (n = 2050 r/min) cruise rating I (n = 1860 r/min) cruise rating II (n = 1730 r/min) Design Altitude-Performance Characteristics Figure 5...
Page 17 Timing Diagram Figure 6 CAUTION: WHEN OPERATING THE ENGINE, IT IS PROHIBITED TO DO THE FOLLOWING: (1) USE FUEL, OIL, GREASE GRADES AND COMPRESSED GASES WHICH ARE NOT SPECIFIED IN THIS MANUAL. (2) USE OTHER TOOLS THAN INDICATED IN APPENDIX 2. TO PERFORM MAINTENANCE OF THE CARBURETOR, LAGNETO AND SPEED GOVERNOR USE THE TOOLS INCLUDED IN THE INDIVIDUAL SPTA SETS FOR THESE UNITS.
Page 18 2.2. IN-PLIGHT OPERATION OF ENGINE 2.2.1. Taxiing After starting, warming up and test running the engine and. in the course of taxiing, watch engine instruments to avoid, overheating or overcooling of the engine. When air temperature at carburetor inlet is below zero, perform taxiing with heater engaged so that the carburetor inlet air temperature is not less than 10 °C.
Page 19 Figure 7. 1. Nut 34. Tappet Push Rod 68. Rubber Sealing Ring 2. Sealing Ring 35. Starting Valve 69. Starting Pipe 3. Exhaust Pipe Connection 36. Tappet Push Rod Casing 70. Attachment Nut 4. Satellite 37. Lock 71. Intake Pipe 5.
Page 20 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.
Page 21: Fuel And Lubricants
Appendix 1 FUEL AND LUBRICANTS 1. FUEL Engine M-14P should be operated on gasoline B91/115. Physical and chemical properties of gasoline B91/115: Octane rating ................Not less than 91 Gasoline rating (rich mixture) ..........Not less than 115 Lead tetraethyl content .........
Page 22 70 and its substitutes at preservation and depreservation of the engine is PROHIBITED. 2.LUBRICANTS The M-14P engines use oil MS-20. Specifications of oil MS-20 GOST 21743-76. Kinematic viscosity at 100 °C ..........Not less than 20 cSt Ratio of 50 °C viscosity to 100 °C viscosity ......Not more than 7.85 Conradson carbon value ........
Page 23 Table 2 Characteristics Parameter DEngRD-2472 grade B/0 Mil-L-6082B grade 1100 (USA) (England) 1950 1955 Kinematic viscosity at 98.9 °C Not less than 18.80 cSt Not less than 18.9 cSt Dyne and Devine viscosity index at 37.8 °C Up to 95 Up to 95 Acidity Up to 0.1 mg KOH per 1 g of oil...
Page 24 Appendix 2 Place in case Designation Description Purpose (Fig. 1) 14-024-020 Case (empty) For placing airborne tools 10-32-12 Wrench for intake pipe For removing and installing intake pipe connection nut 700880-8 Flat wrench 24x27 For oil pump reducing valve cap, for attaching rod covers 14-32-21 Flat wrench 36x41...
Page 25 Place in case Designation Description Purpose (Fig. 1) 14-232-03 Two-head box wrench For securing generator, carburetor, speed 14x17 governor and engine frame bolts 700880-2 Flat wrench 7x9 For attachment nuts of compressed air distributor, filter with chip detector and air pipe clamps 14-324-10 Universal wrench handle...
Page 26 Place in case Designation Description Purpose (Fig. 1) UB-24-16 Socket wrench 14 For securing magneto, carburetor and generator Feeler gauge For checking clearance between valve L = 100 mm, set 2, ccuracy stem and rocker roller class 2 GOST 882-75 Flat-nosed, pliers For locking and coffering bolts, nuts, 7814-0091x9...
Page 27 Arrangement of Airborne Tools in Case Figure 1...
Page 28 ENGINE M-14P - TROUBLE SHOOTING Troubles -that may be encountered, during starting and. operation of the M-14P engine at different ratings, their causes and remedies are presented in the Table in the order of probability of their appearance. Troubles and remedies of engine assemblies and systems are given in the respective sections of this Maintenance Manual.
Page 29 Trouble Possible cause Correction (11) Oiled or burnt magneto Burnish and wash points with alcohol breaker points 2. Engine starts but stalls (1) Fuel shut-off valve is Open fuel shut-off valve after several firings closed Drive out fuel chamber plug and check (2) No fuel in carburetor or if carburetor is filled with fuel.
Page 30 Trouble Possible cause Correction 4. Engine misses or (1) Damaged, wires Replace defective wires shakes (2) Poor contact with spark Check attachment of elbows to apark plug center electrode Plugs (3) Fouled or damaged spark Check spark plugs under pressure, plugs replace defective plugs.
Page 31 Trouble Possible cause Correction 5. Engine shuts (1) Idle rating is maladjusted Adjust carburetor throttle by its stop down when selecting idle screw to size D indicated in carburetor Certificate to accuracy of ±1. 5 mm (2) Incorrect mixture at Adjust mixture by idle needle idling (3) ouction system leaks...
Page 32 Trouble Possible cause Correction (2) Clogged oil cooler Clean honeycombs of soil honeycombs (3) Congealed, oil in oil Heat oil cooler cooler (4) Poor scavenging of oil Check cleanliness of filter in oil sump, from engine (leaks, clogging, air rear cover, attachment of oil pump to rear cover lock in pump) (5) Gases blow-by into Remove cylinders, replace piston rings...
Page 33 Trouble Possible cause Correction (18) Blow-by of gases in Remove cylinders, replace piston rings crankcase sentatives. 10. Engine is smoky (1) Piston is burnt through Check compression, find defective or scored, cylinder oval piston, remove cylinder. If piston is scored and cylinder is oval, replace piston and cylinder, if piston is burnt through, remove engine for overhaul...
Page 34 Trouble Possible cause Correction (8) Incorrect spark advance Adjust spark advance (Ref. 074.10.01, Task Card No. 202) (9) Carburetor is mal- Check carburetor adjustment, smooth adjusted. or needle sticks movement of needle (10) Exhaust valves are Replace valves burnt through (11) Incorrect clearances Adjust clearances (Ref.
Page 35 ENGINE M-14P - MAINTENANCE PRACTICED 1. LIST OF TASK CARDS Task Card No. Engine Starting CAUTION: COLLECTION OF OIL AMD GASOLINE CAN BE ENCOUNTERED IN ENGINE LOWER CYLINDERS, THEIR INTAKE PIPES AMD EXHAUST MANIFOLD. TO PRECLUDE HYDRAULIC SHOCK, PRIOR TO STARTING WHILE IGNITION IS SWITCHED OFF, TURN AIRSCREW MANUALLY IN ITS NORMAL DIRECTION FOR 3 TO 4 TURNS.
Page 36 Heating and winterization of the engine, dilution of oil with gasoline facilitate starting, decreases wear of parts, particularly of cylinders and pistons. Perform engine maintenance under low ambient temperatures according to the following Task Cards: Title Task Card No. Winterization of Powerplant Dilution of Oil with Gasoline Maintenance of Engine Operating on Diluted Oil Preparation of Engine for Starting...
Page 37 Title Task Card No. Check of Reliable Attachment and Locking of Oil Line Joints, Drain Cocks and Plugs and Visual Inspection of Oil ay-stem for Leakage Check of Filter with Chip Detector Circuit for Continuity Check of Fuel Line Joints, Drain Cocks and Plugs for reliable Attachment and Locking Check of Fuel Line for Leakage under Pressure of 0.2 to 0.5 kgf/cm2 Check of Fuel Line and Membrane Mechanism Fuel Valve for Leakage under Pressure of 0.12 to 0.15 kgf/cm...
Page 38 Title Task Card No. Change of Oil Teat Run of Engine after Scheduled Maintenance Operations Check of Valve Mechanism Parts for Condition Check of Clearance between Rocker Rollers and Valve Stem Ends Check of Cylinder Compression Inspection and Washing of Engine Rear Cover Mash Filter Inspection and Washing of Filter with Chip Detector Inspection and Washing of Speed Governor Oil Supply Filter Washing of Inlet Oil Filter...
Page 40 TASK CARD No. 201 TO M-14P MS M.S. ITEM PROCEDURE: Engine Starting OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED 1. Shift the speed governor lever to the LOW PITCH position. NOTE: At a carburetor inlet air temperature of below 10 °C, open the air heating shutter at the carburetor inlet.
Page 41 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 7. Give command "Clear off" and on receiving "Cleared" reply, open the onboard bottle valve and push the START () button. CAUTION: DO HOT DEPRESS THE "START" () BUTTON FOR MORE THAN 30 s CONTINUOUSLY, INTERVALS BETWEEN DEPRESSIONS SHALL BE AT LEAST 3 min AND AFTER 10 DEPRESSIONS AT LEAST 10 min.
Page 42 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS (5) Turn the airscrew manually for 3 to 4 turns in its normal direction to drain accumulated oil or mixture of gasoline and oil from the intake pipes, exhaust manifold and cylinders. (6) Reinstall the spark plugs and drain plugs. (7) Lock the plugs and repeat starting as instructed in Items 1 through 7.
Page 43 T A S K C A R D No. 202 TO M-14P MS MS ITEM PROCEDURE Engine Warm-up and Test Run CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Warm up the engine at a speed of 41 to 44 % (1200 to 1300 r/min) in 0.5 to 1 min after In case of unsteady run- starting till engine inlet oil temperature starts rising (the engine test run chart is given in Pig.
Page 44 Engine M-14P Test Run Chart Figure 201...
Page 45 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 6. Check engine instrument readings for correspondence to the Specification. If speed drops for more CAUTION: than 3 %, proceed as follows: TO AVOID OVERHEATING BECAUSE OF INSUFFICIENT BLOWING, DO NOT (1) Check attachment of spark OPERATE THE ENGINE FOR A LONG TIME AT NOMINAL RATING II ON GROUND.
Page 46 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 8. Check operation of the generator at engine rotational speed of 57 to 58 % (1680 to If voltage drops below 27 to 27.5 1700 r/min). V, proceed as instructed in T.R. When pushing the voltmeter button, voltage should be 27 to 27.5 V with power generator Certificate or replace consumers switched on.
Page 47 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED (2) Set engine rotational speed of 70 % (2050 r/min) using the carburetor throttle control For cause of speed lever. variation, refer to Section (3) Increase the airscrew pitch to a speed of 64 % (1860 r/min) by the speed governor "Trouble Shooting", Item 11 control lever.
Page 48 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS (4) Note engine instrument readings and make sure they are in line with the Specification. In case of troubles, refer T.R. The engine rotational speed, the blower outlet pressure and oil pressure should to Section "Trouble Shooting", correspond to the Specification.
Page 49 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED Take-Off Rotational Speed of Engine M-14P with Alracrew V530TA-D35 on Airplanes (on Groun) Versus Ambient Temperature at Atmospheric Pressure P = 720 to 770 mm Hg Figure 202 TEST EQUIPMENT TOOLS AND FIXTURES...
Page 50 TO M-14P M.S. TASK CARD No. 203 M.S. ITEM procedure: Engine Shutdown OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED 1. Prior to shutdown, cool the engine as follows: (1) Fully open the cowling and oil cooler shutters. (2) Decrease engine speed to 28 to 34 % (800 to 1000 r/min) (the airscrew is in the LOW PITCH and run the engine at this rating till cylinder head temperature drops to 140 to 150 °C.
Page 51 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED CAUTION: 1. TO AVOID SCORING OF PISTONS AND CYLINDER SURFACE AT SUB-CAUSE OF RAPID FLOW DOWN OF OIL FROM CYLINDER WALLS AT HIGH HEAD TEMPERATURES, NEVER SHUT DOWN THE ENGINE DIRECTLY FROM CRUISE AND HIGHER RATINGS. 2.
Page 52 TO M-14P M.S. TASK CARD No. 204 procedure: Winterization of Powerplant m.s. item CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Install covers on the R-2, series 04, speed governor, oil cooler and. oil tank. NOTES: 1. Arrange the covers so that it is possible to fill oil into the tank and warm the engine with hot air from ground heaters without removing the covers.
Page 53 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS NOTES: 1. If oil trapping is detected, replace the pipes where pockets are formed. 2. Check drainage of oil from the oil cooler. MATERIALS TEST EQUIPMENT TOOLS AND FIXTURES Needle Threads, coarse,flax No. 105x6 Tape,calico, cotton 16x0.22, grade 1 Enamel, brown PP-223 Glass, water sodium...
Page 54 TO M-14P MS TASK CARD No. 205 MS ITEM PROCEDURE Dilution of Oil with Gasoline CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS At an ambient temperature below+ 5 °C, dilute oil with gasoline as follows: If oil pressure drops (1) Heat the engine with a ground heater to a cylinder head temperature of 30 °C.
Page 55 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS NOTE: Perform dilution at the end of the flying day or in case of engine dead periods when engine oil may cool down below+ 5 °C. (7) Shut down the engine (Ref. Task Card No. 203). TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS...
Page 56 TASK CARD No. 206 TO M-14P M.S. M.S. ITEM PROCEDURE: Maintenance of Engine Operating on Diluted Oil CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Warm up the engine for 5 to 6 min at a speed of 41 to 44 % (1200 to 1300 r/min).
Page 57 TO M-14P M.S. TASK CARD No. 207 M.S. ITEM PROCEDURE: Preparation of Engine for Starting OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Warm up the engine, airscrew cylinder and oil system with hot air from a ground heater so that the cylinder head temperature is at least 30 °C as read off the indicator if the ambient...
Page 58 T A S K C A R D No. 208 TO M-14P MS MS ITEM procedure Engine Starting CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Start as indicated in Task Card No. 201 the engine preheated according to Item 1, Task Card No.
Page 59 TO M-14P MS TASK CARD No. 209 M.S ITEM PROCEDURE: Engine Warm-up and Test Run OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Warm-up and test run the engine as instructed in Task Card No. 202. NOTE: To ensure appropriate mixing and preclude icing of carburetor venture, the carburetor inlet air temperature should not be less than 10 °C.
Page 60 TASK CARD No. 210 TO M-14P M.S. M.S. ITEM procedure: Engine Shutdown CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Dilute oil with gasoline (Ref. Task Card No. 205). 2. Shut down the engine (Ref. Task Card No. 203).
Page 61 TO M-14P M.S. TASK CARD No. 211 M.S. ITEM PROCEDURE: Obtaining Pilot's Complaints on Engine Troubles in Plight 072.00.00a OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Listen to pilot's complaints on engine troubles encountered in flight. 2. Enter the information in the airplane preparation Register.
Page 62 R-2, series 04, speed governor, boss for the R-2, series 04i governor attachment and boss for the centrifuge (on engines M-14P, series 2) where torque wrench cannot be used, tighten the nuts with the wrench.
Page 63 TO M-14P M.S. T A S K C A R D No. 213 M S ITEM Procedure: Inspection and Check of Reliability of Engine Mounting 072.00.00d, 072.20.00a CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Inspect the engine crankcase-to-frame attachment bosses.
Page 64 TO M-14P M.S. TASK CARD No. 214 M.S. ITEM PROCEDURE: Cleaning of Engine 072.00.00e CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Clean the engine of dust, dirt, runs of oil and fuel. T.R. Soiling of the engine is not If soiling is detected, allowed.
Page 65 TO M-14P MS TASKCARD No. 215 MS ITEM PROCEDURE: Drainage of Oil for Inspecting It for Metal Particles 072.00.00f OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Drain 0.5 lit of oil from the engine oil sump as follows: If metal particles are (1) Unlock and.
Page 66 CHECKE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS D BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Wrench 7x9 700880-2 Gasoline Nefras-S 50/170 or BR-1, BR- Wrench 9x11 700002 Funnel, fine-mesh...
Page 68 TO M-14P M.S. TASK CARD No. 216 M.S. ITEM PROCEDURE: Engine Test Run before Shutdown to Determine Troubles 072.00.00g OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Taxi the airplane to the parking ground. Determine and eliminate 2. Listen to engine operation before shutdown. Make sure the engine does not miss, there cause of missing and pops are no pops in suction and exhaust systems.
Page 69 TO M-14P MS TASK CARD No. 217 MS ITEM PROCEDURE: Dilution of Oil with Gasoline 072.00.00h CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS Dilute oil with gasoline if ambient temperature drops below 5 °C (Ref. Task Card No. 205). TEST EQUIPMENT...
Page 70 TO M-14P MS TASK CARD No. 218 MS ITEM procedure: Engine Covering after Inspection and Elimination of Troubles 072.00.001 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Eliminate defects detected in flight and in the course of inspection. 2. Cover the engine as follows: (1) Put folded cover on the engine and spread it. (2) Fasten the cover straps.
Page 71 TASK CARD No. 219 TO M-14P MS MS ITEM procedure: External Inspection of Speed Governor 072.10.00a CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Inspect the speed governor externally to make sure it is free from defects, plays in the (1) Replace damaged roller, damaged locking.
Page 72 TO M-14P M.S. T A S K C A R D No. 220 M.S. ITEM procedure; Check of Reliable Attachment and Operability of Speed Governor Control System 072.10.00b OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Inspect the speed governor location. T.R. Oil leakage is not allowed.
Page 73 TASK CARD No. 221 TO M-14P MS MS ITEM procedure: Inspection of Cylinders, Exhaust Manifold, Its Pipes at Joints with Cylinders 072.30.00a CORRECTIVE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS 1. Inspect the cylinders. (1) Replace cylinder with 2. Inspect the exhaust manifold and its pipes at joints with the engine cylinders.
Page 74 TASK CARD No. 222 TO M-14P MS MS ITEM PROCEDURE: Check of Cylinder Intake Pipes for Condition 072.30.00b OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Check condition and attachment of the cylinder intake pipes. Tighten loose attachment T.R. Loosening of cylinder intake pipe attachment nuts is not allowed.
Page 75 TO M 14P MS TASK CARD No. 223 MS ITEM procedure Check of Deflectors for Condition and Reliable Attachment 072.30.00c CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Check the engine deflectors for condition and reliable attachment. T.R. The deflectors Tighten deflector attach- should be fully tightened.
Page 76 TO M-14P M.S. TASK CARD No. 224 M.S ITEM PROCEDURE: Check of Covers and Cables of Valve Mechanism Case Cables for Condition 072.30.00d OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Check the valve mechanism caae covers for condition.
Page 77 TASK CARD No. 225 TO M-14P M.S. M.S ITEM procedure: Check of Reliable Attachment and Locking of Oil Line Joints, Drain Cocks and Plugs and Visual 072.50.00a. Inspection of Oil System for Leakage 072.50.00b CORRECTIVE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS 1.
Page 78 TASK CARD No. 226 TO M-14P MS MS ITEM procedure: Check of Filter with Chip Detector Circuit for Continuity 072.50.00c CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Remove the rubber cap from the filter terminal. Detect fault in external 2.
Page 79 TASK CARD No. 227 TO M-14P MS MS ITEM PROCEDURE Check of Fuel Line Joints, Drain Cocks and Plugs for Reliable Attachment and Locking 073.00.00a CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Check condition and locking of the fuel lines, hoses, connections and plugs.
Page 80 TASK CARD No. 228 TO M-14P M.S. M.S. ITEM 073.00.00b, PROCEDURE: Check of Fuel Line for Leakage under Pressure of 0.2 to 0.5 kgf/cm 073.00.00d OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Eliminate leakage of fuel 1. Build up a pressure of 0.2 to 0.5 kgf/cm with a priming pump.
Page 81 TASK CARD No. 229 TO M-14P MS MS ITEM PROCEDURE. Check of Fuel Line and Membrane Mechanism Fuel Valve for Leakage under Pressure of 073.00.00b, 0.12 to 0.15 kgf/cm 073.00.00c OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Open the fuel shut-off valve. 2. Fill the fuel line with fuel by building up pressure of 0.12...
Page 82 TASK CARD No. 230 TO M-14P MS M S ITEM PROCEDURE: Visual Check of Fuel System for Leakage of Gasoline 073.00.00d OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Check the pipeline and unit joints of the fuel system visually for leakage.
Page 83 TASK CARD No. 231 TO M-14P MS MS ITEM procedure: Check of Fuel System and Carburetor for Leakage under Fuel Pressure of 0.4 to 0.5 kgf/cm2 073.00.00e, 073.00.03a CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Start and test tvs. the engine (Ref. Task Card. No. 201). 2. Shut down the engine (Ref.
Page 84 TO M-14P M.S. TASK CARD No. 232 M S ITEM procedure: Check of Fuel lines for Proper Attachment 073.00.00f OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Check reliable attachment of fuel lines excluding their contact with other parts of the Bend away and reattach engine.
Page 85 TO M-14P MS TASK CARD No. 233 M S ITEM PROCEDURE: Check of Fuel Pump Attachment 073.00.01a CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Inspect the fuel pump attachment place, make sure its attachment and locking are in good Tighten attachment nuts repair.
Page 86 TO M-14P M.S. TASK CARD No. 234 M.S. ITEM PROCEDURE: Check of Pine Fuel Filter Joints for Leakage 073.00.02a OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Make sure there is no leakage through the joints of the fine fuel filter.
Page 87 TO M-14P MS TASK CARD No. 236 M S ITEM PROCEDURE: Check of Attachment of Magneto to Engine and Wires to Magneto and Spark Plugs 074.10.01a OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Check attachment of the magneto to the engine, wires to the magneto and spark plugs.
Page 88 TO M-14P MS TASK CARD No. 237 M S ITEM PROCEDURE: Check of Ignition Cable Braids for Condition 074.20.01a CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Make sure the ignition cable shielding is not chafed or damaged. T.R. Chafing of and Replace damaged damage to cable shielding are not allowed.
Page 89 TO M-14P M.S. TASK CARD No. 238 M.S. ITEM PROCEDURE: Check of Routing of Ignition Harness 074.20.01b OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Check routing of ignition harness paying special attention to the contacts with the other Turn and secure the har- parts and gaps between the harness and cylinder cooling fins.
Page 90 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 17. Pit the cover attachment cables and lower the wing nuts with the stops downwards If the cables sag, lift the using a special wrench. wing nut upwards to the stop, T.R. The valve case cover cables should be properly tightened. unscrew it to obtain required 18.
Page 91 TO M-14P M.S. TASK CARD No. 239 M.S. ITEM procedure: Sampling Inspection of Spark Plug Tightening Using Wrench 074.20.02a CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Perform sampling inspection of spark plug tightening using a wrench according to the...
Page 92 TO M-14P MS TASK CARD No. 240 MS ITEM procedure: Check of Air Line Joints, Drain Cocks and Plugs for Reliable Attachment and Locking 080.00.00a CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Check reliable attachment and locking of the air line joints, drain cocks and plugs.
Page 93 TO M-14P M.S. TASK CARD No. 241 M.S. ITEM PROCEDURE: Check of Reliable Attachment of Compressed Air Distributor, Pipes and Connections for 080.10.00a Supply and Discharge of Compressed Air CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Check reliable attachment of the compressed air distributor, pipes and connections for Secure the compressed supply and discharge of compressed air.
Page 94 TO M-14P M.S. TASK CARD No. 242 MS ITEM procedure: Check of Compressor for Good Repair and Reliable Attachment 080.00.00b OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Check the compressor for good. repair. (1) Wash compressor o T.R. The bottle air- pressure should be at least 50.kgf/cm .
Page 95 TO M-14P MS TASK CARD No. 243 M S ITEM procedure Check of Starting Valves for Reliable Attachment 080.10.00b CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Check attachment of the starting valves and. make sure the valves and pipes are free Secure starting valves from traces of overheating.
Page 96 TO M-14P M.S. TASK CARD No. 244 M.S. ITEM PROCEDURE: Change of Oil 072.00.00j OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Unlock and open the cock for draining oil from the oil sump, having fitted a rubber hose Eliminate oil leakage to it.
Page 97 TO M-14P M.S. TASK CARD NO. 245 M.S. ITEM PROCEDURE: Test Run of Engine after Scheduled Maintenance Operations 072.00.00k OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. After accomplishment of scheduled maintenance, start and warm up the engine (Ref.
Page 98 TO M-14P MS TASK CARD No. 246 M S ITEM PROCEDURE: Check of Valve Mechanism Parts for Condition 072.30.00e OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Move the cable tensioning wing nuts upwards. 2. Remove the cables and valve case Replace broken springs covers.
Page 99 TO M-14P M.S. TASK CARD No. 247 M.S ITEM procedure: Check of Clearance between Rocker Rollers 072.30.00f and Valve Stem Ends OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Lift the cable tensioning wing nuts upwards. 2. Remove the cables and. valve case Adjust clearance as in- covers.
Page 100 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 10. Install wrench 10-32-07 in the adjustment screw slot and while turning it clockwise or counterclockwise, set clearance indicated in Item 8. 11. Tighten the locking nut with wrench 14-24-660 supporting the adjustment screw with wrench 10-32-07.
Page 101 TO M-14P M.S. TASK CARD No. 248 M.S. ITEM procedure: Check of Cylinder Compression 072.30.00g OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Remove all the front spark plugs (Ref. 074.20.02, Task Card No. 201). If compression is less 2.
Page 102 TO M-14P M.S. TASK CARD No. 249 M.S. ITEM procedure: Inspection and Washing of Engine Rear Cover Mesh Filter 072.50.00d CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Unlock the mesh filter on the engine rear cover. 2. Undo the filter.
Page 103 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Pliers, flat-nosed 150 Wrench, socket 36 Gasoline Nefras-S 50/170 or BR-1, 14-24-620 BR-2 Air, compressed Wire, locking KO-0.8...
Page 104 TO M-14P M.S. TASK CARD No. 250 M.S. ITEM PROCEDURE: Inspection and Washing of Filter with Chip Detector 072.50.00e OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS HECKED 1. Drain oil from the engine and oil sump (Ref. Task Card No. 215). 2. Unlock and undo Detect and eliminate the the filter wire attachment nut.
Page 105 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 11. Pill fresh oil into the engine (Ref. Task Card No, 215). 12. Start and test run the engine Eliminate oil leakage (Ref. Task Card No. 201). 13 Check the filter with chip detector joints for leakage. T.R.
Page 106 TO M-14P MS TASK CARD No. 251 MS ITEM procedure Inspection and Washing of Speed Governor C 072.50.00f CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Unlock and undo the speed governor oil supply filter. Detect and eliminate the 2.
Page 107 TO M-14P M.S. TASK CARD No. 252 M.S. ITEM PROCEDURE: Washing of Inlet Oil Pilfer 072.50.00g OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Unlock and undo the filter. Detect and eliminate the 2. Inspect the filter to make sure it is free from metallic particles.
Page 108 TASK CARD No. 253 TO M-14P MS MS ITEM procedure; Check of Filter with Chip Detector Internal Circuit for Continuity 072.50.00h CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Remove the filter with chip detector from the engine: (1) Open the oil sump drain cock Replace defective filter and drain oil.
Page 109 TASK CARD No. 254 TO M-14P M.S. M.S. ITEM PROCEDURE: Washing of Engine Oil Lines with Clean Unleaded Gasoline 072.50.001 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS HECKED 1. Drain oil from the engine and oil tank (Ref. Task Card No. 244).
Page 110 TO M-14P MS TASK CARD No. 255 MS ITEM procedure: Drainage of Oil from Generator Drive 072.70.00a OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Unlock and. drive the plug out of the generator drive body. 2. Drain oil from the drive.
Page 111 TO M-14P M.S. TASK CARD No. 256 M.S. ITEM PROCEDURE: Drainage of Oil from Magneto Drives 072.70.00b OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Unlock and drive out the plugs on the rear cover near the magneto drives, Tighten and re lock the Drain oil.
Page 112 TO M-14P M.S. TASK CARD No. 257 M.S. ITEM PROCEDURE: Replacement of Filtering Element in Fuel Pine Filter 8D5.886.027 073.00.03c OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY CAUTION: WHEN PERFORMING SCHEDULED MAINTENANCE. PRECLUDE CONTAMINATION OF THE FILTER INTERIOR. IT IS STRICTLY PROHIBITED TO DISASSEMBLE THE FILTER UNLESS FOR REPLACING THE FILTERING ELEMENT.
Page 113 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 10. Wash the filtering element soiled in operation and check it for leakage according to the effective instructions. 11. Check the filtering element for leakage at an air pressure of 120 mm of water column. 12.
Page 114 TO M-14P M.S. TASK CARD No. 258 M.S ITEM PROCEDURE: Inspection and Washing of Carburetor Fuel Filter 073.00.03d CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Close the fuel shut-off valve. 2. Unlock and undo the carburetor fuel filter. 3. Wash the filter in clean gaaoline.
Page 115 TO M-14P M.S. TASK CARD No. 259 M.S. ITEM procedure.: Accomplishment of Carburetor Scheduled Maintenance according to Carburetor Maintenance Manual 073.00.03e CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Close the fuel shut-off valve in the pilot's cabin, 2. Unlock and undo the fuel filter. 3.
Page 116 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 15. Reinstall the suction jet. 16. Install and lock the suction jet plug. Clean and wash 17. Measure the initial position of the altitude control needle and adjust it if necessary breathing holes with clean (Ref.
Page 117 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Pliers, flat-nosed 150 Wrench 14x17 14- Gasoline Nefras-S 50/170 or BR-1, 232-03 Wrench 19x22 700880-7 Screwdriver BR-2 Syringe UB-24-05 Wrench 11x14 14-24-861 Brush, hair Wire, locking KO-0.8 Template Wrench 7x9 700880-2...
Page 118 TO M-14P M.S. TASK CARD No. 260 M S ITEM procedure: Accomplishment of Magneto Scheduled Maintenance according to Magneto Maintenance 074.10.01b Manual CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Drive out three magneto shield attachment screws. 2. Drive out four magneto pipe Tighten loosened screws attachment screws.
Page 119 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY (6) Inspect metal surfaces of parts and assemblies located in the breaker mechanism Ref. Item (13) space. If runs of oil or oil films are detected, remove them with a clean cloth moistened in clean Replace damaged parts rectified alcohol and squeezed dry.
Page 120 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Tighten the screw fully with a screwdriver. Replace screws with Bend one of the lock washer tabs so that it tightly contacts the screw face. stripped thread with new ones (c) Install the upper cover on the magneto, secure its attachment screws to the body. from individual SPTA set If transformer attachment screw thread is stripped, replace the screw.
Page 121 TASK CARD No. 261 TO M-14P M.S. M.S. ITEM procedure: Accomplishment of Spark Plug Scheduled Maintenance according to Spark Plug Maintenance Manual 074.20.02b CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. On expiration of spark plug life till first regapping, remove the spark plugs from the engine Replace spark plugs with cracked (Ref.
Page 122 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 8. Check the gap between the central and side electrode with a 0.4-nnn feeler gauge and regap the spark plug if necessary. Carry out regapping only on special fixture RIP-1 of tester "Iskra". Wo other regapping methods are allowed. CAUTION: WHEN REGAPPING, NEVER INSERT THE GAUGE INTO THE GAP AND PRESS THE CENTRAL ELECTRODE, OTHERWISE DAMAGE TO THE CENTRAL ELECTRODE OR CERAMIC INSULATOR NOSE MAY RESULT.
Page 123 TO M-14P M.S. TASK CARD No. 262 M.S. ITEM procedure: Check of Compressor Attachment 080.00.00c CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Check compressor attachment. T.R. The compressor should be Tighten compressor attach- reliably attached. ment nuts 2. Drain condensate from the air system filter sump (blow the pipe in cold weather).
Page 124 TO M-14P M.S. TASK CARD No. 263 M.S. ITEM procedure: Replacement of Compressor Filtering Element 080.00.00d CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Remove the spring lock and hold-down mesh. 2. Remove the filtering element and the other mesh of the compressor. 3. Wash all the removed parts in clean unleaded gasoline. 4. Dry the parts with dry compressed air.
Page 125 TO M-14P M.S TASK CARD No. 264 M.S. ITEM procedure: Check of Compressor Inlet Valve for Easy Travel 080.00.00e CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Carry out operations under Task Card No. 263, Items 1 through 4. 2. Push the compressor inlet valve with hand.
Page 126 TO M-14P MS TASK CARD No. 265 M.S. ITEM 080.00.00f procedure: Washing of Compressor Delivery Valve CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Remove the compressor delivery valve. 2. Disassemble the valve and clean the valve parts of coking products. Wash with gasoline and blow with dry compressed air.
Page 127 ENGINE M-14P - REMOVAL/INSTALLATION 1. LIST OF TASK CARDS Title Task Card No. Unpackaging of New Engine Depreservation of Engine under Field Conditions Removal of Engine from Airplane Installation of Engine on Airplane...
Page 128 TO M-14P MS T A S K C A R D No. 401 MS ITEM PROCEDURE: Unpackaging of New Engine OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Prepare the working place, handling equipment, tools. If packaging defects are 2.
Page 129 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 9. Inspect the engine. NOTE: When detecting engine defects, damaged packaging or missing parts, accessories and tools of the engine set, draw the external inspection statement. Send a copy of the statement to the Supplier.
Page 130 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ECKED ACTIONS Engine Slinging Diagram Figure 401 TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Cable Gasoline Nefras-S 50/170 or BR-1, Crane or hoist at least 500 kg in capacity BR-2 Hammer 700016 Pliers, flat-nosed 150 Brush, hair Wrench 19x22 700880-7...
Page 131 TO M-14P M.S. TASK CARD No. 402 M.S. ITEM PROCEDURE: Depreserration of Engine under Field Conditions OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Place a tray for draining grease under the support with the engine. 2. Perform external depreservation of the engine and its accessories by removing grease from their surfaces with a hair brush moistened in gasoline Nefras-S 50/170 or BR-1, BR-2.
Page 132 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 6. Perform internal depreservation of the magneto (Ref. 074.10.01, Task Card No. 201). 7 Drive out dehydrators and adapters to them from the spark plug holes. 8. Drive out all plugs from the cylinder exhaust ports. 9.
Page 133 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 16. Blow the filter with chip detector with compressed air. 17. Reinstall the filter with chip detector (Ref. Task Card No. 250). 18. Reinstall the spark plugs (Ref. 074.20.02, Task Card No. 202).
Page 134 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 29. Connect the fuel line and fuel pressure measuring pipe to the carburetor. 30. Connect the fuel line to the fuel pump. 31. Tighten and lock all the fuel pump joints. NOTE: Other accessories mounted on the engine are not subject to internal depreservation.
Page 135 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 35. Install and lock the filter with chip detector and the rear cover oil filter. 36. Fill fresh oil, NOTE: Do not re-use or recycle the drained oil. 37. Check presence of locking on the nuts of connections, pipelines, drain cocks and plugs, TEST EQUIPMENT TOOLS AND FIXTURES...
Page 136 TO M-14P M.S. TASK CARD No. 403 M.S. ITEM procedure: Removal of Engine from Airplane CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Warm up the engine at a speed of 35 to 41 % on gasoline B-70 till the oil inlet temperature is 50 °C (Ref.
Page 137 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 11. Unlock and undo the oil system pipelines. 12. Disconnect wires from the generator, thermocouple of the cylinder rear spark plug, wires of the tachometer generator. 13. Unlock and disconnect the carburetor throttle control rod. 14.
Page 138 1. Shock-Absorbing Stack Washer 2. Hut 3. Washer 4. Engine Frame Ring 5. Stud Engine Frame Installation Diagram Figure...
Page 139 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Crane Oil MS-20 Grease K-17 Hoist Gasoline Hefras-S 50/170 or Tray for oil draining BR-1, BR-2 Shackle, engine mounting Syringe UB-24-05 Wrench 14x17 14-232-03 Pliers, flat-nosed 150 Screwdriver 700345 A150x0.5 Wrench 27x30 7811-0041 Wrench 24x27 700880-8 Wrench 17x19 UB-24-07 Hammer 700016 Wrench...
Page 140 TO M-14P MS TASK CARD No. 404 MS ITEM procedure Installation of Engine on Airplane 072.00.00 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Unpackage the engine (Ref. Task Card No. 401). 2. Depreserve the engine (Ref. Task Card Ho. 402).
Page 141 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 6. Install the engine on the airplane: (1) Install the airplane braces on the engine frame ring. (2) Bring the engine with braces to the airplane. (3) Insert four brace-to-airplane attachment bolts having made sure they are intact, (4) Install the washers.
Page 142 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 10. Connect the pipes to the oil and fuel pressure transmitters. 11. Lock the pipes. 12. Connect and lock the control rods of the carburetor, speed governor, cowling shutters. 13. Connect primary circuits of both magnetos with the selector switch. Connect the high- tension wire from starting coil KP-4716 to jack S (starting) of the LH magneto distributor.
Page 143 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 23. Remove plugs from the exhaust porta of all the cylinders. Detect and eliminate cause of leakage 24. Install the exhaust manifold having coated thread of its nuts with grease ST (NK-50). Replace damaged filter Detect 25.
Page 144 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 35. Install and lock the filter with chip detector and the rear cover oil filter. 36. Fill fresh oil, NOTE: Do not re-use or recycle the drained oil. 37. Check presence of locking on the nuts of connections, pipelines, drain cocks and plugs, TEST EQUIPMENT TOOLS AND FIXTURES...
Page 145 AN-W-576 GOST 10877-76 Engine M-14P is delivered in a wooden container comprising a bottom and a detachable cover. The overall dimensions of the packaging container are 1350x1250x1360 mm.The engine is attached to the container bottom by braces and shipping brackets installed on the engine frame. All fasteners are painted red and should be removed when installing the engine on the airplane.
Page 146 (2) Run the engine for 10 to 15 min at a speed of 35 to 41 % (1000 to 1200 r/min) on gasoline B-70 with 10 % oil MS-20 and on oil used to operate it. (3) Stop the engine and cool it down to the cylinder head temperature of 30 to 40 °C. (4) Drive out the front spark plugs.
Page 147 drain oil from the carburetor through the open holes. (1) Reinstall the plugs, connect fuel pipes to connections (6) and (7) and lock the plugs and nipples with wire. (10) Wipe the engine outer surfaces with a clean cloth (or rags) moistened in gasoline Hefras-S 50/170 or BR-1, BR-2 and the rubberized fabric hoses with a clean dry cloth.
Page 148 (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.
Page 149 (12) Using a syringe, fill 150 to 200 g of oil K-17 heated to a temperature of 40 °C into each cylinder through the spark plug holes with the piston being at the BDC turning the airscrew shaft for 3 to 4 turns, then refill the oil into the cylinders without turning the airscrew shaft.
Page 150 (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.
Page 151 5. LOADING OF DEHYDRATOR CARTRIDGE WITH SILICA-GEL INDICATOR (1) To load the dehydrator cartridge with silica-gel indicator, use the following procedure: (a) Insert a disk of filtering paper inside the dehydrator cartridge onto its perforated bottom. (b) Wrap the perforated 'bottom of the dehydrator cartridge in polyethylene film and secure with a rubber ring.
Page 152 The storeroom for the engine, accessories and spares should be absolutely isolated against various gases (smoke, chemical plant flue gases, sulfur oxide, ammonia, chlorine , etc.). It is prohibited to store chemicals, acids, alkalis, storage batteries and hygroscopic materials (cotton, paper, rags, etc.) in one room with the engines and spares.
Page 153 Make sure, without touching by hands or damaging the grease coat, that there is no corrosion under the grease coat. If no corrosion traces are detected, wrap the parts in paper again and place in the boxes. When inspecting, do not remove the parts from paper, only unwrap them and inspect, carefully turning on paper.
Page 154 (29) of the gearbox, the satellites roll around it and move the airscrew shaft in the direction of crankshaft rotation. The M-14P engine gearbox transmission ratio is 0.658. The gearbox housing carries the airscrew speed governor. The speed governor drive is located on the bracket of the crankshaft thrust bearing front cover.
Page 155 Gearbox housing (10) (Ref. Pig. 2) is adapted to accommodate the gearbox parts and is cast of magnesium alloy ML-5. It is a truncated cone attached to the engine intermediate crankcase with its rear flange by means of studs driven into the intermediate crankcase front part. The gearbox housing takes up load created by the airscrew and transmits it to the crankcase attachment units and engine frame.
Page 156 Gearbox Power Train Figure 1 2.2. AIRSCREW SHAFT Airscrew shaft (1) (Ref. Fig. 2) is made of heat-treated high-grade alloyed steel. The hollow shaft has at its front end a round flange with end face splines and six holes for airscrew attachment bolts. The shaft is installed with its rear cylindrical shank in the bushing of the crankshaft front end bearing the rear support for the airscrew shaft.
Page 157 The oil seal bushing is free fit in the bushing of the crankcase front end. To align oil supply holes, the bushing is fixed through its round hole with set screw (27) driven into the threaded hole of the gearbox housing and safetied with a plate lock.
Page 158 1. Airscrew Shaft 2. Bushing 3. Sealing Collar 4. Oil Baffle 5. Hut 6. Cover 7. Bushing 8. Ball Bearing 9. Thrust Ring 10. Housing 11. Oil Sealing Ring Bushing 12. Sun Gear Hub 13. Bolt 14. Screw 15. Satellite 16.
Page 159 Oil baffle (4) is made of steel. It is intended, to restrict flow of oil to oil sealing collar (3) of the airscrew shaft. The rubber oil sealing collar with metal insert is intended for sealing the airscrew shaft. Oil flows from the radial ball bearing cover space and through the hole in the crankcase front end to the crankcase space.
Page 160 Holes for decreasing cage weight are drilled in the bridges between the ports. The hub has rectangular splines for fitting the satellite cage onto the airscrew shaft. Milled flats are made at the spline ends on the solid wall side and the wall is provided with six oil passages to supply oil to the needle roller bearings of the satellites. To secure locking strips of the satellite pivots, the solid side wall has twelve threaded holes.
Page 161 1. Gearbox Housing 2. Speed Governor Shank 3. Crankshaft Front Thrust Ball Bearing Cover 4. Ball Bearing 5. Bushing 6. Intermediate Timing Shaft 7» Adjustment Washer 8. Speed Governor Drive Bevel Gear 9. Lock 10. Woodruff Key 11. Nut 12. Speed Governor Driven Gear 13.
Page 162 Arranged on timing intermediate shaft (6) by Woodruff key (10) is drive level gear (8) of the speed governor drive, made of cemented steel. The drive gear meshes with driven gear (12) of the speed governor drive. The driven gear is made of cemented steel and transforms into a hollow shank, with internal splines. The shank rotates in vertical bushing (13).
Page 163 Crankshaft Thrust Ball Bearing Front Cover Figure 1 Intermediate Crankcase Figure 2...
Page 164 Three holes provided in the conical wall of the front cover are intended to breath internal spaces of the crankcase and a hole for draining oil from the gearbox housing to the intermediate crankcase. 2.2. INTERMEDIATE CRANKSHAFT The engine intermediate crankcase is adapted to accommodate the parts of the crank mechanism, timing mechanism and to mount the cylinders.
Page 165 The roller bearing is precluded against longitudinal displacement by the crankcase holder internal collar at the front and by a spring ring lodged in the crankcase holder recess at the rear. In addition to the central hole, the vertical wall has four more holes: three holes for breathing and one hole for fixing the cam plate when timing the engine.
Page 166 Intermediate Grankcase Front Portion Figure 3 Intermediate Crankcase Rear Portion Figure 4...
Page 167 Crankshaft Figure 5 Cotter Pin Cotter Pin Cotter Pin King Drive Gear Rear Main Roller Bearing Spacer Crankshaft Rear Section Ring Web Bushing Front Main Roller Bolt Bearing Thrust Strip Bushing Cotter Pin Plug Rear Counterweight Pin Rear Counterweight Bushing Crankshaft Front Section Rear Counterweight...
Page 168 The slot inner surface is copper plated to preclude cold hardening. 2.4. CONMECTING ROD ASSEMBLY Connecting rod assembly (Ref. Fig. 6) of the M-14P engine comprises one master connecting rod (1) and eight articulated connecting rods (5) which are hinged to the master rod by steel pins (7).
Page 169 Provided on both end faces of the pin is a straight cutout forming a projection to which the projection of strip (3) adjoins. The strip prevents the pin against longitudinal displacement. The pin attachment strips are identical and are installed on outer sides of the master connecting rod side plates.
Page 170 CRANKSHAFT ASSEMBLY - TROUBLE SHOOTING For mostly often encountered troubles and their remedies refer to the Table given below. Trouble Possible cause Correction Impeded rotation or (1) Oil accumulated in lower Drive out one lower spark plug from crankshaft cylinders at prolonged engine dead each of cylinders Nos 4, 5, 6 and drain plugs period or because of incomplete from intake pipes of these cylinders and plugs...
Page 171 CYLINDER ASSEMBLY - DESCRIPTION AND OPERATION 1. GENERAL The engine cylinder assembly comprises cylinders with valve mechanisms, pistons, timing mechanism parts, intake pipes and deflectors. The engine cylinder with its bottom forms a chamber where fuel-air mixture is combusted and thermal energy is converted into mechanical work.
Page 172 the stem is concaved; the mushroom-type head diameter is larger and the stem diameter is smaller than those of the exhaust valve. The inlet valve stem friction surface and tip are hardened with high-frequency currents while the mushroom-type head and a part of the stem (except the land) are subjected to anti- corrosive chemical nickel plating and heat treatment.
Page 173 Front view Cylinder Figure 1 Rear view...
Page 174 1. Inlet Valve 2. Outer Spring 3. Inner Spring 4. Split Retainer 5. Valve Plate Inlet Valve Figure 2...
Page 175 1. Exhaust Valve 2. Sealing Ring 3. Bushing 4. Inner Spring 5. Guide Bushing 6. Satellite Facing 7. Metallic Sodium 8. Washer 9. Spacing Washer Sealing and Scraping Device of Exhaust Valve Figure 3...
Page 176 The upper ends of both springs thrust against plate (5) which in its turn rest on split taper copper-plated retainer (4) entering the groove in the valve stem. The inlet valve retainer surface is copper plated, that of the exhaust valve is brass plated. The exhaust valve is made of steel 4Ch14N14V2M and its mushroom-type head is convened towards the combustion chamber.
Page 177: Timing Mechanism
2.4. TIMING MECHANISM The timing mechanism ensures periodic admission of fuel-air mixture into the engine cylinders and exhaust of combustion products to the atmosphere.
Page 178 Intake Pipe of Cylinders Nos 4, 5 and. 6 Figure 4 Piston, Piston Rings and Piston Pin with Plugs Figure 5...
Page 179 The timing mechaniam comprises a cam plate, a cam plate drive, tappet guide bushings, tappets with rollers, push rods in casings, valve rockers with adjustment screws and rollers, inlet valves and exhaust valves with springs, plates and retainers. The valve mechanism is described in Section 2.1. The schematic diagram of the timing mechanism is given in Pig.
Page 180 Timing Mechanism Schematic Diagram Figure 6 Cam Plate Figure 7...
Page 181 Drive Timing Gear Spacer Cam Plate Intermediate Timing Shaft Rear Ball Bearing Intermediate Timing Gear Ball Bearing Bushing Front Ball Bearing Adjustment Washer Speed Governor Drive Gear Plate Lock...
Page 182 The set of a tappet (Ref. Pig. 9) includes guide bushing (3), tappet (4), tappet end piece (2), spring (1), roller (5), roller bushing (6), roller pivot (7). Tappet (4) is a steel cylindrical rod having a slot, in its lower part with holes for the pivot carrying a floating bronze bushing and the roller.
Page 183 1. Spring 2. Tappet End Piece 3. Tappet Guide Bushing 4. Tappet 5. Roller 6. Roller Bushing 7. Roller Pivot Set of Tappet Figure 9 1. Push Rod 2. Rubberized Fabric Hose 3. Clamp 4. Push Rod Casing 5. Union Nut 6.
Page 184 1.Rocker 2.Roller 3.Roller Pivot 4.Needle Roller Bearing Bushing 5.Ring 6.Adjustment Screw 7.Lock Nut 8.Needle Roller 9.Needle Roller Bearing Washer 10.Rocker Axle 11.Rocker Axle Nut 12.Washer 13.Washer Valve Rockers Figure 11...
Page 185 Needle rollers are mounted on axle (10) by bushing (4), ring (5) and nitrated washers (9). To seal axle (10) of the rocker, aluminium washers (13) are installed on both sides of the valve case in special recesses and steel washers (12) are placed under the axle head and nut (11). Rocker needle rollers of the valve mechanisms of cylinders TSoa 1, 2, 3, 8 and'9 are lubricated under pressure.
Page 186 1. Inter-Cylinder Deflector Upper Deflector 2. Rubber Stop Clamp 3. Lock Spring 4. Rubber Stop Cylinder Deflectors Figure 12 Engine Cooling Diagram Figure 13...
Page 187 CYLINDER ASSEMBLY - TROUBLE SHOOTING For mostly often encountered troubles and their remedies refer to the Table given below. Trouble Possible cause Correction Loss of (1) Incomplete closing of Check clearances between rocker rol- compression valves ler and valve stem, adjust them (Ref. (2) Leaky spark plugs or 072.00.00, Task Card No.
Page 188 To increase engine power to the desired level near the ground and maintain nominal power up to the design altitude, the M-14P engine is equipped with a centrifugal blower with positive one-speed drive. Apart from increasing power, the blower promotes mixing of fuel with air and more uniform distribution of the mixture among the engine cylinders, which is particular important when starting the engine.
Page 189 Blower. Longitudinal Section View Figure 1...
Page 190 The front part of the steel bushing has drilled holes communicating with the atmosphere through the annular recess, passage in the vertical wall and a steel pipe. A boss with passage to supply mixture from the carburetor to the blower impeller is located in the lower part of the mixture collector.
Page 191 Rear view Mixture Collector Figure 2 Diffuser Figure 3...
Page 192 2.3. IMPELLER Impeller (5) (Ref. Pig. 1) is the most stressed part of the blower. At take-off rating of the engine its rotational speed reaches as high as 23,700 r/min. To decrease inertia forces and dynamic loads on the impeller drive shaft bearings, the impeller is stati-cally balanced before installing in the engine by removing metal from the surface between the blades.
Page 193 The accessory drive shaft is a hollow cemented steel part. The rear part of the shaft has involute splines whereby it is connected with the internal splines of the drive bevel gear of the rear cover drive. Two copper-plated bands in the rear part of the shaft are intended for aligning the shaft relative to the drive bevel gear of the rear cover drive (the rear band) and for sealing the oil gallery (the front band).
Page 194 1. Plate 2. Spring 3. Plate 4. Gear 5. Accessory Drive Shaft Blower Coupling Figure 4...
Page 195 Gear (4) is made of alloyed steel and has five internal projections. When the coupling is assembled, the gear internal projections are in the slots of the drive shaft disk which excludes axial displacement of gear (4) relative to the shaft. Two plates (1) and (3) and one spring (2) are installed in each space between the projections of the gear and shaft disk.
Page 196 Oil seal bushings (8) and (35) are made of steel and have four grooves each to receive rings contacting with their outer surfaces bushings (20) and (36), pressed in mixture collector (1) and diffuser (24). The oil sealing rings are made of bronze. Each bushing receives four rings. A wide annular groove with radial holes emerging to the annular spaces defined by the bushings and the shaft is made at the middle of the oil seal bushing surface.
Page 197 1.Oil Tank 2.Oil Line 3.Oil Cooler 4.Oil Temperature and Pressure Gauge 5.Oil Filter 6.Oil Pump 7.Oil Pump Delivery Section 8.Dilution Cock 9.Oil Sump 10.Pilfer with Chip Detector 11.Speed Governor Oil Pump Breathing Connection Pipeline Engine Lubrication and Breathing Diagram Figure 1...
Page 198 2. DESCRIPTION Oil from the tank is fed to the oil pump via an oil line through the oil inlet connection, mesh filter in the rear cover and inner space of the driven shaft to the oil pump delivery section (Ref. Fig. 1). Oil under pressure from the delivery section of the oil pump is fed to the space of the oil pump drive shaft, then through the hollow vertical shaft, radial holes in its walls to the annular racess of the vertical boss of the crankcase rear cover to lubricate the bushings of the upper and lower supports of the vertical shaft.
Page 199 The oil is fed to the speed governor and airscrew as follows. Oil from the airscrew shaft apace is supplied through the longitudinal receaa on the airscrew shaft plug surface and radial hole in the airscrew shaft and spacer to the rear annular space formed by the oil transfer bushing.
Page 200 3. LUBRICATION SYSTEM UNITS 3.1. OIL PUMP MN-14A The oil pump is intended to deliver oil from the tank to the engine oil gallery and to scavenge oil from the oil sump to the tank. Specifications Direction of rotation ................Left Drive transmission ratio ...............
Page 201 1.Fuel Pump Attachment Stud 10.Scavenging Section Gear 2.Lower Cover 11.Key 3.Rubber Seal with Metal Insert 12.Scavenging Section Gear 4.Delivery Section Housing 13.Rear Cover Vertical Shaft 5.Drive Shaft 14.Upper Cover 15.Delivery Section Gear 6.Delivery Section Gear 7.Rear Cover Attachment Stud 16.Driven Shaft 8.Rear Cover 17.Driven Gear 9.Scavenging Section Housing...
Page 202 Lower cover (2) (Ref. Pig. 2) has a locating collar and is attached by six studs (18) to the delivery section housing. The cover has a flange with four studs (1) to mount the fuel pump and a seat for rubber seal with metal insert (3) which precludes leakage of oil from the oil pump and fuel pump.
Page 203 The filter with chip detector is intended to timely warn of troubles linked with failure of parts and to clean oil fed from the engine to the oil pump. The filter with chip detector comprises a filtering section and a detector section. The filtering section comprises filter (10) (Ref.
Page 204 Oil Sump Figure 4...
Page 205 1. End Piece 2. Contact Stem 3. Insulation Bushing 4. Nut 5. Washer 6. Bushing 7. Body 8. Ring 9. Plate Stack 10. Filter 11. Oil Drain Cock...
Page 206 LUBRICATION - TROUBLE SHOOTING For mostly often encountered troubles and their remedies, refer to the Table given below. Trouble Possible cause Correction 1.Low oil (1) Air lock in line for supply of Eliminate air lock, heat oil line and oil, pressure oil to oil pump, thickened oil (in winter), clean oil tank vent pipe...
Page 207 LUBRICATION - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Task Card: Title Task Card No. Removal Depreservation of New Oil Pump Installation Adjustment of Oil Pressure...
Page 208: Operation Procedure
2. OPERATION PROCEDURE TO M-14P MS TASK CARD No. 201 MS ITEM : Removal PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Unlock and open the oil sump drain cock and drain oil from the engine. 2. Disconnect Dress nicks and dents the fuel and oil system pipelines.
Page 209 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Tray for draining oil Hose Pliers, flat-noaed Cloths 150 V/rench 11x14 14-24-861 Wrench 9x11 700002 Wrench 24x27 700880-8 Wrench 27x30 7811-0041...
Page 210 TO M-14P MS TASK CARD No. 202 MS ITEM : Depreservation of New Oil pump PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Release the oil pump from packaging and remove all blanking covers from it. 2. To remove preservation grease, immerse the oil pump into a bath with clean oil MS-20 heated to a temperature of 75 to 85 °G and while rotating the drive splined shaft leftwards by...
Page 211 TO M-14P MS TASK CARD No. 203 MS ITEM procedure Installation CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Carefully inspect the support surface of the flange, aligning surface of the housing and Carefully remove nicks and dents splined shaft.
Page 212 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 9. Start the engine (Ref. 072.00.00, Task Card No. 201) and adjust oil pressure (Ref. Task Card No. 204). NOTE: The oil pump is installed by the Supplier. TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Pliers, flat-nosed 150 Wrench 11x14 14- Sealant "50"...
Page 213 TO M-14P MS T A S K C A R D No. 204 MS ITEM Adjustment of Oil Pressure PROCEDURE CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Check oil pressure with the engine running at a crankshaft speed, of 64 % Shut down engine (Ref.
Page 214 CHECKE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS D BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Pliers, flat-nosed 150 Wire, locking KO-0.8 Screwdriver 700346 A200x1 Wrench 27x30 7811-0041 Wrench 24x27 700880-8...
Page 215 ACCESSORY DRIVES - DESCRIPTION AND OPERATION 1. GENERAL The present section describes engine accessory drives located in the rear cover. The engine accessory drives and gear trains are shown in the kinematic diagram (Ref. Fig. 1). The data on transmission ratios and directions of rotation of the drives are given in the Table . Transmission Drive Designation of gear...
Page 217 3. DESCRIPTION 2.1. CRANKCASE REAR COVER The crankcase rear cover (Ref. Fig. 2) cast of aluminium alloy is attached to the mixture collector and simultaneously secures the blower diffuser by its flange. The lower part of the rear cover has a boss with wella to accommodate the oil pump and filter. The boas has two flanges with two studs each for connecting oil inlet and outlet branch pipes.
Page 218: Drive Gear
Grankcase Rear Cover Figure 2 2.2. DRIVE GEAR Drive gear (16) (Ref. Pig. 3) of the rear cover drives is made of nickel-chrome steel. Its front has a cylindrical shank for sealing the oil gallery and the internal splines for coupling with the drive shaft of the accessory drive.
Page 219 2.3. REAR COVER VERTICAL SEARING Vertical gearing transmits torque from the drive bevel gear of the rear cover drives to the drives of the compressor, compressed air distributor, oil and fuel pumps, tachometer generator. The vertical gearing comprises vertical shaft (18) and bevel gear (17). Vertical shaft (18) of the rear cover is a hollow nickel-chrome steel part.
Page 220 Oil to lubricate bearings of driven shaft (20) (Ref. Pig. 3) is fed under pressure through passages drilled in the drive housing and in the rear cover. Plug (29) is intended for periodic drainage of oil seeping into the space between the generator drive and generator flange during inverted flight.
Page 221 1. Compressed Air Distributor 13. Crankcaae Rear Cover Bevel Gear 14. Generator Drive Housing 2. Tachometer Generator Drive 15. Bushing Housing 16. Rear Cover Drive Gear 3. Tachometer Generator Cover 17. Bevel.Gear 1B. Vertical 4. Tachometer Generator Drive Shaft Shaft 19.
Page 222 2.7. COMPRESSOR DRIVE The compressor drive comprises housing (8) (Ref. Fig. 3) and torque-limiting pin coupling. Housing (8) is made of aluminium alloy and has a round flange with six holes to receive the attachment studs, one hole to supply oil to the compressor, two holes to drain oil from the compressor space and three milled flats to remove the housing from the engine.
Page 223 ACCESSORY DRIVES - TROUBLE SHOOTING For mostly often encountered troubles and their remedies,refer to the Table given below. Trouble Possible cause Correction Oil leaks through Oil accumulated in magneto Unlock drain plugs, drain accumulated vents or along magneto drive oil (Ref. 072.00.00, Task Card No. 256) attachment flange...
Page 224 FUEL SYSTEM - DESCRIPTION AND OPERATION 1. GENERAL The engine fuel system comprises a fuel pump, a fine fuel filter, a carburetor and interconnecting pipelines. During operation of the engine the fuel pump supplies fuel from the fuel tanks through the filters to the carburetor from which the fuel-air mixture is fed to the engine blower.
Page 225 FUEL PUMP 702ML - DESCRIPTION AND OPERATION 1. GENERAL The 702ML fuel pump (referred to hereinafter as "pump" is intended, to supply fuel from the airplane fuel tanks through the filters to the engine carburetor. The pump features a reducing chamber detachable housing accommodating two valves;a reducing valve and a priming valve.
Page 226 2.2. CONSTRUCTION The 702ML pump (Ref. Pig. 1) comprises a rotary vane-type pumping unit, reducing valve unit with priming valve and sealing parts. The pumping unit comprises housing (33), rotor (20), four vanea (37), sleeve (19), floating pin (36), bearings (21) and (18). Pumping unit vanes (37) are lodged in slots of rotor'(20) and rest with one side on floating pin (36) and with the other on the inner surface of sleeve (19).
Page 227 1.Reducing Valve Nut 16. Retaining Ring 31.Plug 2.Reducing Valve Nut Lock 17. Seal 32.Plug 3.Diaphragm Washer 18. Upper Bearing 33.Pump Housing 4.Spring Washer 19. Sleeve 34.Pin 5.Washer 20. Rotor 35.Nameplate 6.Reducing Valve 21. Lower Bearing 36.Floating Pin 7.Reducing Chamber Housing 22.
Page 228 The reducing valve assembly comprises valve (6) with diaphragm (25) and spring (27) secured on it by nut (1). Nut (1) is safetied with lock (2). One end of spring (27) thrusts against the valve stem seat and the other end,against the end of adjustment screw (28).
Page 229 The rotor with four vanes and floating pin (36) form a rotary mechanism which divides the chamber of sleeve (19) into two spaces - suction space A (Ref. Fig. 2) and delivery space B. As the rotor rotates, the volume of the suction and delivery spaces is continuously varying. The volume behind the vanes increases ensuring suction of g&soline from the tanks, while in front of the vanes it decreases and gasoline under pressure is supplied to the carburetor.
Page 230 FUEL PUMP 702ML - TROUBLE SHOOTING For mostly often encountered troubles and their remedies, refer to the Table given below. Trouble Possible cause Correction 1. Soon after starting Leaky joints in suction sys- Check suction line joints for engine, fuel pressure gradually tem (air suction) leakage and eliminate suction of air drops to zero and engine stalls...
Page 231 FUEL PUMP 702ML - MAINTENANCE PRACTICES 1. LIST OF TASK CARD Title Task Carda No. Removal Depreservation of New Fuel Pump Iristallation Adjustment and Test...
Page 232: Operation Procedure
2.OPERATION PROCEDURE TO M-14P MS. TASK CARD No. 201 PAGE(S) 203 M.S. ITEM procedure: Removal CORRECTIVE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS 1. Disconnect the fuel system pipelines. 2. tJndo four fuel pump attachment nuts and Dress nicks carefully if remove the pump from the engine.
Page 233 TO M-14P MS TASK CARD No. 202 page(s) 205, 206 ' MS ITEM procedure: Depreservation of New Fuel Pump CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Release the pump from packaging. 2. Wash off grease from the outer surface with clean gasoline, wipe with a cloth and blow with dry compressed air.
Page 234 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Syringe UB-24-05 Wrench 11x14 7811- Gasoline Hefras-S 50/170 or BR-1, 0041 Bath, depreservation BR-2 Mr, compressed Cloths Oil MS-20...
Page 235 TO M-14P MS. TASK CARD No. 203 PAGE(S) 207 M.S. ITEM procedure: Installation OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Install a sealing gasket between the pump flange and its mounting plane. 2. Arrange the fuel pump so that the shank freely enters its seat. 3. Place washers and uniformly tighten four pump attachment nuts.
Page 236 TO M-14P M.S. TASK CARD No. 204 page(s) 209, 210 M.S. ITEM procedure-. Adjustment and Test CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Start the engine and adjust fuel pressure, if required, using the following procedure: 1. Unlock and undo for four turns the cap of the fuel pump adjustment screw, holding the adjustment screw against turning with a screwdriver inserted into the screw slot (Ref.
Page 237 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS Adjusting Fuel Pressure by Fuel Pump Reducing Valve Figure 201 TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Wrench 27x30 7811-0041 Wrench 24x27 Wire, locking KO-0.8 700880-8 Screwdriver 700346 A200x1 Pliers, flat- nosed 150...
Page 238: Specifications
FILTER 8D2.966.064 - DESCRIPTION AND OPERATION 1. GENERAL Filter 8D2.966.064 is intended to clean fuel of mechanical impurities in the airplane fuel system. The filter operates on the principle of retaining mechanical particles contained in the fuel flow by means of a mesh partition.
Page 239 Flange 1. Filter Housing 10. Sealing Ring 2. Cover 11. Filtering Element Body 3. Filtering Element 12. Bottom 4. Sealing Ring 13. Frame 5. Valve 14. Holder 6. Spring 15. Shipping Plug 7. Disk 8. Sealing Ring Fuel Filter 8D2.966.064 Figure 1...
Page 240 Maximum throughput ................. 5 1/min Clean filter hydraulic resistance at maximum throughput and ambient temperature and fuel temperature of (25±10) °C ..............Up to 0.03 kgf/cm Filtering element pressure difference of by-pass valve opening ..................(0.1±0.02) kgf/cm Operating pressure .........
Page 241 FILTER 8D2.966.064 - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Title Task Card No. Removal Depreservation of New Filter Installation...
Page 242 TASK CARD No. 201 TO M-14P M.S. PAGE(S) 203 M.S ITEM : Removal PROCEDURE CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Make sure there is no fuel pressure in the fuel system. 2. Drain fuel from the system. 3. Unlock the filter-to-airplane attachment.
Page 243 TO M-14P M.S. T A S K C A R D No. 202 PAQE(S) 205 M.S. ITEM : Depreservation of New Filter PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Remove the filter from the shipping container, make sure locking is intact and Supplier's seals are not missing;...
Page 244 TO M-14P MS TASK CARD No. 203 PAGE (S) 207 M S ITEM Installation PROCEDURE CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY 1. Install the filter on the airplane vertically with the cover down and tighten the nuts. Eliminate leakage and...
Page 245 1. GENERAL The AK-14P carburetor is intended to be mounted on a four-stroke radial nine-cy-linder air-cooled engine, type M-14P. The carburetor is of a floatleas, single-barrel type. To ensure engine pickup, the carburetor features mechanical and air acceleration pumps; an altitude control is provided to adjust mixture quality in climbing.
Page 246 2.2.1. Carburetor Body The carburetor body is a magnesium alloy casting with a system of fuel and air passages (Ref, Fig. 2). Located at the left side of the body (on the emblem side) is a pressure regulator fuel chamber; the link mechanism chamber, idle needle space and fuel valve apace are at the right side.
Page 247 Carburetor AK-14P Operation Diagram Figure 1...
Page 248 Carburetor AK-14.P Figure 2...
Page 250 Driven with pitch diameter interference into the bushing threaded holes of the upper flange are attachment studs. The lower flange has two threaded holes for the air manifold attachment screws. Other features of the body are outlined when describing the base units and parts of the carburetor. 2.2.2.
Page 251 1.Diaphragm Assembly 11.Fuel Valve 2.Washer 12. Adjustment Shim 3.Cover Attachment Screw 13.Lower Drain Plug 4.Diaphragm Trunnion 14.Washer 5.Elongated Cover Attachment 15.Fuel Valve Cover Screws Attachment Screw 6.Copper Sealing Ring 16.Spring 7.Lever Spring 17.Fuel Valve Cover 8.Lever Support 18.Gasket 19.Fuel Jet 9.Lever Pivot 10.Lever Diaphragm Assembly and Fuel Valve Figure 3...
Page 252 Connec-tion (7) (Ref. Fig. 5) is screwed, into the threaded hole of the loss on the outside of the fuel valve cover. 'Support (8) (Ref. Fig. 3) of the fuel valve lever is inserted into a special seat in the carburetor body and is so fitted to it that the support plane is aligned with the body flange or is depressed from it for up to 0.2 mm.
Page 253 Carrier 15. Link Lever Pin Adjustment Washer 16. Link Lever Clearance Take-Up Spring 17. Bushing Bushing 18. Link Chamber Cover 19. Washer Holes, Dia. 2 mm 20. Gasket Bushing 21. Sealing Ring Setting Pin 22. Thrust Lever Metering Needle Lever 23.
Page 254 A -A Screw Washer Slide Link Lever Tapered Cotter Pin Screw Fuel Pressure Measuring Connection Fuel Valve Cover Idle Needle 10. Coupling 11. Cap 12. Gasket Link Mechanism and Idle Needle Figure 5...
Page 255 Setting pin (8) is inserted into the hole and. safetied against dropping out with lock (22) (Ref. Pig. 2) which is secured to the metering needle lever by two screws. The same screws are used to rigidly secure metering needle (12) lever to link shaft (20). The upper part of the lever of metering needle (12) is a rectangular slot whose walls have one through hole each.
Page 256 The thrust lever is precluded, against turning "by flats provided on throttle shaft (14). Thrust lever (22) and carrier (1) have holes of equal diameter uniformly spaced around the periphery; the carrier is provided with eight holes, and the thrust lever, nine holes. When mounting thrust washer (24) on the throttle shaft, the setting pin enters the aligned holes of carrier (1) and thrust lever integrating them into one assembly.
Page 257 The nozzle interior serves as guide for metering needle (12). The metering needle haa a shaped portion intended to meter fuel. At the end of the needle the shaped portion transforms into a flat shank whereby the needle is turned to adjust fuel consumption. Twelve longitudinal splines are milled on the outer cylindrical surface of the needle other end, Drilled at the shaped portion base are four inclined holes to supply metered fuel to the inner space of the needle.
Page 258 is brazed to the other end of the frame. The filter assembly is sealed in the housing with a rubber sealing ring. Venturi (14) is inserted into the carburetor barrel from the lower flange side. The nozzle with sleeve are accommodated in the venturi slot.
Page 259 screws; steel washers are placed under "the screw heads. The joint between the cover and the body is sealed with a paronite gasket. A through threaded hole made at the center of cover (4) receives connection (34). The joint between the connection and the cover is sealed with a rubber sealing ring. Adjustment shaft (33) is inserted in connection (34) through the internal through hole.
Page 260 passed through the hole at the holder end and in the attachment bolts of the mechanical acceleration pump cover. The wire is sealed with the Supplier's seal. 2.2.7. Idle Needle A threaded hole in a special boss above the link chamber receives idle adjustment needle coupling sealed at the end with a lead gasket.
Page 261 1. Sealing Ring Retaining Ring 15. Lock Nut 22. Suction Jet 2. Plug Thrust Ring 16. Bushing 23. Inlet Air Jet 3. Sealing Ring 10. Spring 17. Plug 24. Plug 4. Screw 11. Cover 18. Plug 25. Sealing Ring 5. Needle 12.
Page 262 In climbing, aneroid, capsule (12) moves needle (5) in the bushing to shut off shaped ports. The needle is returned back by spring (6). The threaded shank of aneroid capsule (12) is screwed into cover (14) and is safetied with lock nut (15); the cover is screwed into the body and is sealed with rubber ring (13).
Page 263 The cover is attached to the adapter by four nuts with spring washers. The cover-to-body joint is sealed by the diaphragm. The carburetor adapter is secured on the body upper flange studs by four nuts safetied with plate locks. The adapter-to-carburetor joint is sealed with a paronite gasket.
Page 264 CARBURETOR AK-14P -TROUBLE SHOOTING For mostly often encountered troubles and their remedies, refer to the Table given below. Trouble Possible cause Correction 1. Exhaust to (1 ) Excessive opening of throttle Close throttle carburetor at idle rating at starting (especially in cold weather) Enrich mixture by idle adjustment 2.
Page 265 CARBURETOR AK-14P - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Title Task Card No. Removal Depreservation of New Carburetor Installation Idle Adjustment Adjustment at Main Ratings Adjustment of Altitude Control Adjustment of Acceleration Pump...
Page 266: Operation Procedure
2.OPERATION PROCEDURE TO M-14P MS. TASK CARD No. 201 MS ITEM : Removal PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1.Disconnect the fuel line from fuel inlet connection (6) (Ref. Fig, 201). 2.Disconnect the throttle control rod. 3.Disconnect the fuel pressure measuring pipe from connection 4.Unlock and.
Page 267 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY Carburetor AK-14P (Right Side View) Figure 201...
Page 268 TO M-14P MS T A S K C A R D No. 202 preservation of Hew Carburetor MS ITEM PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1, Unpack the new carburetor. 2, Remove preserving grease from the external surfaces with a brush moistened in clean gasoline.
Page 269 1. Altitude Control Needle Adjustment Screw 2. Suction Jet Plug 3. Plug for Measuring Initial Position of Altitude Control Needle 4. Breathing Plug 5. Lower Drain Plug 6. Plug for Measuring Air Pressure in Regulator Air Space 7. Throttle Control Lever 8.
Page 270 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BV 27. Disconnect the hand pump line from connection (6) (Ref. Fig. 201). 28. Install the shipping cap on the connection, 29. Wipe the carburetor externally with a clean cloth. TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Bath, depreservation Wrench 11x14 14-24- Gasoline Mefras-S 50/170 or BR-1,...
Page 271 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 13. Keep on flushing till- clean gasoline emerges from the hole for plug (3) (Ref. Fig. 202) of the altitude control. 14. Reinstall altitude control plug (3). 15. Keep on flushing till clean gasoline emerges from the nozzle.
Page 272 TO M-14P MS T A S K C A R D No. 203 MS ITEM : Installation PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CKED BY 1. Measure the initial position of the altitude control needle (Ref. Fig. 202). Dress nicka 2.
Page 273 Carburetor Altitude Control Needle Position Versus Barometric Pressure (Barometric Graph)Figure 203...
Page 275 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Template 60660-3863 Pliers, flat-nosed 150 Sealant "50" i/rencl-i 19x22 700880-7 drench 11x14 14-24-861 iVire, locking KO-0.8 Grease TsIATIM- Wrench 7x9 700880-2 Screwdriver 530-280-1 Pump, priming UB-24--05 './rench 17x19 UB-24-07...
Page 276 TO M-14P MS T A S K C A R D No. 204 M S ITEM : Idle Adjustment PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS HECKED 1. Start and warm up the engine (Ref. 072.00.00. Task Card Mo, 201), 2.
Page 277 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Throttle Idle Stop Screw 2. Carburetor Throttle Control Lever Determining size D Figure 204 TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Pliers, flat-nosed 150 Screwdriver 700345 A150x0.5 Wire, locking KO-0.8...
Page 278 TASK CARD No. 205 TO M-14P MS MS ITEM Adjustment at Main Ratings PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Check engine operation at all ratings on the initial adjustment starting from the take-off rating (Ref. 072.00.00, Task Card No. 202), NOTE: If engine operates poorly at separate ratings, adjust the carburetor.
Page 279 TO M-14P M.S T A S K C A R D No. 206 MS ITEM : Adjustment of Altitude Control PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CKED BY 1. Measure the altitude control needle position, using the following procedure. (1) Unlock and drive out plug (3) (Ref.
Page 280 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Template 60680-3863 Wrench 11x14 14-24- Wire, locking KO-0.8 861 Wrench, flat 7x9 700880-2 Pliers, flat-nosed...
Page 281 TO M-14P M S T A S K C A R D No. 207 M S ITEM procedure: Adjustment of Acceleration Pump CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1.Unlock and drive out plug (10) (Ref. Fig. 202). 2. Drive out the acceleration pump fuel jet.
Page 284 1. GENERAL The ignition system ensures well-timed igniting of the working mixture in the cylinders, The M-14P engine ignition system includes two M-9F magnetos, SD-49SMM spark plugs, shielded ignition harness (magneto selector switch and high-tension starting coil KP-4716). 2. DESCRIPTION...
Page 285 High-tenaion starting coil KP-4716 is connected, to the starting electrode of the LH magneto. The ignition circuit diagram is shown in Fig. 1. Magneior on Ignition Diagram Figure 1...
Page 286 MAGNETO M-9F - DESCRIPTION AND OPERATION 1. GENERAL The M-9F magneto (Ref, Fig. 1) is intended, to generate high-tension current and, distribute it among the spark plugs of piston engines for igniting the working mixture. The M-9F magneto is of a rotor construction (permanent magnet is rotating, the transformer is stationary). The M-9F magneto has fixed spark, i.e.
Page 287 MAGNETO M-9F - TROUBLE SHOOTING For mostly often encountered troubles and their remedies, refer to the Table given below. Trouble Possible cause Correction 1. Magneto does (1) Heavy carbon deposit or Burnish breaker (18) points not produce sparks oxidation on points (4) (Ref. Fig. 1) of Tighten screws (11) securing 2.
Page 288 - <-t- ' ^~ - K) <D fi ^- h0 Ol - 01...
Page 289 MAGNETO M-9F - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Title Task Cards No. Depreservation of New Magneto Installation Adjustment of Breaker Point Gap Replacement of Magneto Distributor and. Ignition Harness Cables Removal...
Page 290: Operation Procedure
2.OPERATION PROCEDURE TO M-14P M S TASK CARD No. 201 MS ITEM : Depreservation of New Magneto PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY If oil gets on points (4), wipe them with clean chamois or calico cloth moistened in alcohol...
Page 291 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED 7. Pill two droplets of turbine oil T22 on the end of wick (2) protruding from the oil fitting cup Dress corroded areas, wipe to lubricate cam (24) using a medical pipet. them and lubricate CAUTION: FILL THE OIL PITTING WHEN DEPRESERVING THE MAGNETO AFTER Replace corroded parts PROLONGED STORAGE (AT LEAST TWO YEARS) OR WHEN STORING ON...
Page 292 TO M-14P MS TASK CARD No. 202 M S ITEM '. Installation PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Inspect the magneto and make sure the arrow on front cover (31) (Ref. Fig, 1) of the magneto shows LH rotation and. the gaps of points (4) of breaker (18) are properly adjusted.
Page 294 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY opening the breaker points which corresponds -to supply of spark to cylinder No. 4 in operation. 7. Carefully remove the magneto from the engine, insert the adjustment screw, tighten and lock the nuts of the coupling bolt and adjustment screw of the coupling, precluding turning of the latter* 8.
Page 295 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 14. Secure high-tension lead of starting coil KF-4YKS to term-nal P of the LH or .SH magneto distributor. 15. Check proper setting of the distriou-tor and. its shield and close both magne bos. LIake sure that: The high-tension lead gets into its aeat in the distributor.
Page 296 TO M-14P MS T A S K C A R D No. 203 M S ITEM '. Adjustment of Breaker Point Gap PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1. Drive out four screws (26) (Ref. Fig, 1) which secure the magneto pipe. 2, Drive out Adjust gap under Item 7.
Page 297 TO M-14P MS TASK CARD No. 204 MS ITEM :Replacement of Magneto Distributor and Ignition Harness Cables PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1, Carry out operations under Items 1 through 4 (Ref. Task Card No. 203), 2, Loosen screws (27) (Ref.
Page 298 NOTE: Figures indicate numbers of cylinders to which distributor cables are to be connected. Cables from LH magneto run to front spark plugs, from RH one, to rear spark plugs. Magneto Distributor Figure 201...
Page 299 CORRECTIVE OPERATIONS AND TECHNICAL REQUIREMENTS ACTIONS ECKED BY (the front, spark plugs operate). In position "2" or "RH" - the RH magneto is on and the LH one is off (the rear spark plugs operate). In position “1+2” or "LH+RH" - both magnetos are cut in. 8.
Page 300 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Screwdriver 70346 A200x1 Wrench 7x9 700880-2 Solder Paraffine Wrench 36x41 14-32-11 Screwdriver 700345 A150x0.5...
Page 301 TO M-14P MS TASK CARD No. 205 MS ITEM : Removal PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED 1. Disconnect the magneto selector switch wire using the following procedure: (1) Move away lock (14) (Ref. Fig. 1) and undo shaped nut (13) from connection (12) of upper cover (17).
Page 302 MAGNETO M-9F - STORAGE INSTRUCTIONS When receiving the magneto, check intactness of the container. The magneto delivered, in winter and, not intended for placement in storage should be unpackaged in 2 to 3 h. after being kept indoors. In summer the magneto may be unpackaged immediately after bringing them indoors.
Page 303 MAGNETO M-9F - SHIPMENT The packaged magnetos may be shipped, by any transport and. over any distances. In shipment protect the containers with the packaged magnetos against dust, snow, water and liquids. CAUTION: NEVER DROP OR TURN OVER THE CONTAINERS WITH THE PACKAGED MAGNETOS IK SHIBIENT.
Page 304 SPARK DISTRIBUTION - DESCRIPTION AND OPERATION 1. GENERAL High-tension current from the magneto is transmitted, to the spark plugs via high-tension cables enclosed, in metal shield. - shielded ignition harness.
Page 305 IGNITION HARNESS - DESCRIPTION AND OPERATION The shielded, ignition harness (Ref. Fig. 1) serves to eliminate interference of electromagnetic waves generated by high-tension cables into operation of radio equipment. The high-tension cables between the magneto and the ring are enclosed in a flexible shield hose being a common shield for all the cables.
Page 306 SPARK PLUG SD-49SMM - DESCRIPTION AND OPERATION 1. GENERAL The spark plug together with the magneto and high-tension cables is intended to Ignite fuel-air mixture in the engine cylinder. 2. DESCRIPTION 2.1. CONSTRUCTION The spark plug (Ref. Fig. 1) is a non-detachable, shielded ceramic insulator device. The working part of the spark plug has central electrode (l) and side electrode (2).
Page 307 1. Central Electrode Heat Transfer Bushing 2. Side Electrode Nipple 3. Damping Resistor 10. Shaped Ring 4. Contact Head 11. Heat-Resistant Cement 5. Spark Plug Shell A, Spark Gap 6. Ceramic Tube B. Thread M1 43:1. 25 7. Copper-Asbeatos Sealing C.
Page 308 SPARK PLUG SD-49SMM - TROUBLE SHOOTING The spark plug la not subject to repair and ensures the specified service life of the engine if operated properly. The main parameter determining operability of the spark plug in service is absence of missing. Possible causes of missing are given in the Table "below.
Page 309 SPARK PLUG SD-49SMM - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Title Task Card Uo. Removal Installation...
Page 310: Operation Procedure
2.OPERATION PROCEDURE TASK CARD No. 201 PAGEIS) 203 TO M-14P MS M.S ITEM •. Rem oval PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Check spark plugs un- 1. Disconnect ignition cable elbows from the spark plug shields. screwed with torque above 9 kgf- 2.
Page 311 T A S K C A R D No- 202 TO M-14P MS PAGE(S) 205, 206 MS ITEM : Installation PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKE ACTIONS D BY 1. Inspect the spark plug* Replace damaged ring HOTS: The spark plugs delivered in -the Supplier's packaging are installed on the engine without pre-testing on the instrument, CAUTION: 1.
Page 312 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY Replace defective 6. Check the elbow and contact system for condition. contact spring and insulation T.R. The contact spring end should be bent inward and the insulation bushing should be free bushing from damage.
Page 313 STARTING SYSTEM - DESCRIPTION AND OPERATION 1. GENERAL The M-14P engine is equipped with a compressed air starting system (Ref. Fig. 1) comprising an air compressor, compressed air distributor, starting valves, pipelines, compressed air bottle and a fuel priming system.
Page 314 Compressor AK-50A 12. Pressure Gauge Sump 13. Oil Dilution Cock Adapter 14. Fuel Shut-Off Valve Safety Valve 15. Fuel Filter Check Valve 16. Fuel Pump Filter 17. Fine Fuel Filter Solenoid Valve 18. Compressed Air Two-Pointer Pressure Distributor Gauge 19. Nozzle System Charging Valve 20.
Page 315 2.2. DESCRIPTION 2.2.1. Specifications First stage cylinder diameter 46 mm Second stage cylinder diameter 40 mm Piston stroke 20 mm 3 Operating pressure Up to 50 kgf/cm Drive direction of rotation Arbitrary Compressor speed of rotation: Maximum at continuous operation during 1 min Up to 2655 r/min Maximum at continuous operation during 10 min .....
Page 316: Operation
Connecting rod. (22) has a needle bearing at the big end. connected, to eccentric (2). The connecting rod. small end. ia connected to piston (15) by pin (5). Two-atep piston (15) made of aluminium alloy has five sealing rings on each step. The piston head has a by-pass valve serving to by-pass air from the first-stage cylinder to the second-stage one.
Page 317 When the pis-ton moves upward, the volume of space A decreases and air fed to it is p compressed to 5 to 6 kgf/cm , the volume of space B increases and rarefaction is created in it. The pressure difference in spaces A and B opens by-pass valve (2) and air compressed, in space A is fed, via the passages in the piston to space B of the second-stage cylinder.
Page 318: Starting System - Trouble Shooting
STARTING SYSTEM - TROUBLE SHOOTING For mostly often encountered troubles and their remedies, refer to the Table given below. Trouble Possible cause Correction 1. Compressor does (1) Leaky joints of air system Ensure tightness by tightening not ensure normal pressure nuts of air system joints and replacing pipelines in airplane bottle...
Page 319 Trouble Possible cause Correction (6) Ovartorque coupling pins are Install new coupling from the sheared, off individual SPTA set, having checked free rotation of the compressor by the shaft ahank using wrench UB-24-07...
Page 320 STARTING SYSTEM - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Title Task Card No. Removal Depreservation of New Compressor Installation...
Page 321 TO M-14P MS TASK CARD No. 201 M S ITEM : Removal PROCEDURE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Disconnect the compressed air outlet pipe. 2. Undo six nuts for attachment of the compressor to the engine crankcase rear cover, remove the washers.
Page 322 TO M-14P MS TASK CARD No. 202 M S ITEM Depreservation of Kew Compressor PROCEDURE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1.move the new compressor from its packaging. 2. Remove the blanking cover from the delivery valve. 3. Remove the spring lock, mesh, filtering element and the aecond mean.
Page 323 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Screwdriver 700345 A150x0.5 Gasoline Nefraa-S 50/170 or BR-1, BR-2 Air, compressed Brush, hair Glotha...
Page 324 TO M-14P MS TASK CARD No. 203 M S ITEM ' Installation PROCEDURE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Carefully wipe and, inspect the flange and. shank of the new compressor. T.R. Soiling If soil is detected, wash and.
Page 325 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 8. Run the engine to teat operation of the compressor and tightness of the No. 202). If leakage ia detected, system (Ref. 072,00.00, Task Card check and tighten the T.R. Leakage of .toints is not allowed. compressor connection nut TEST EQUIPMENT TOOLS AND FIXTURES...
Page 326 SPINNING SYSTEM - DESCRIPTION AND OPERATION 1. GENERAL To perform the engine spinning at starting, use is made of the compressed air distributor, starting valves and fuel priming system. The compressed air distributor automatically distributes compressed air among the cylinders at power stroke thus rotating the crankshaft.
Page 327 17. Thrust Bearing Plug 18. Gasket Gasket 19. Gasket Bushing 20.Check Valve Connection Ball 21. Sealing Ring Valve Seat 22. Check Valve Spring Slide Valve 23. Ball Housing Cover 24. Valve Spring Thrust Bushing 25. Inlet Connection Stud 26. Sealing Ring Compression Spring 27.
Page 328 Air is fed through the port located, away from the slide valve center and through the oval holes in the distributor cover to the lower cylinders Nos 4» 5, 6 and 7 for scavenging them during exhaust stroke, The check valve comprises connection (20), ball (23), spring (22) and bushing (24). It is intended to preclude oil from the distributor to the compressed air supply pipeline during operation of the engine, Installed in thrust bearing (17) is a ball valve including ball (4) and seat (5) to pass oil during operation of the engine to the shank of the slide valve to lubricate the latter.
Page 329 1. Nut 5. Housing 2. Spring 6. Valve 3. Gasket 7. Swivel Elbow Body 4. Gasket 8. Cap Starting Valve Figure 2 1. Body 3. Atomizer Nozzle .Figure 3...
Page 330 The nozzle includes steel body (1) (Ref. Fig. 3) and atomizer (2). The body has a hexagon for the wrench and thread on both ends for screwing into the mixture collector and connecting the pipe with gasoline supply connection. Pressed and flared in the nozzle body ia the atomizer having four inclined holes to ensure fine pulverization of gasoline in the mixture collector with a short jet.
Page 331 SPINNING SYSTEM - TROUBLE SHOOTING For mostly often encountered troubles and. their remedies, refer to the Table given, below. Trouble Possible cause Correction When starting the (1) Low air pressure in bottle Fill bottle to pressure of 50 engine with compressed air, (2) Air pressure loss because' of kgf/cm Check starting system for...
Page 332 SPINNING SYSTEM - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Title Task Card No. Removal Depreservation of New Compressed Air Distributor Installation of Compressed Air Distributor Housing Adjustment of Compressed Air Distributor Installation of Cover of Compressed Air Distributor Housing...
Page 333 TO M-14P MS TASK CARD No. 201 ) 203, 204 PAGE M.S ITEM : Removal PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED 1. Undo nine caps. 2. Remove nine pipes for supply of air to the cylinders and aluminium sealing washers.
Page 334 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Pliers, flat-nosed 150 Wrench 7x9 700880-2 Wrench 17x19 UB-24-07 Screwdriver 700345 A150x0.5 Hammer 700016...
Page 335 TO M-14P MS T A S K C A R D No. 202 PAGE IS) 205 MS ITEM : De preservation of New Compressed Air Distributor PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKED ACTIONS 1. Remove packaging covers and withdraw the distributor from packaging. 2. Remove the distributor housing cover supporting the pad.
Page 336 TO M-14P MS TASK CARD No. 203 PAGE<S) 207 MS ITEM ' Installation of Compressed Air .Distributor Housing PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED Dress nicks 1. Inspect the distributor housing flange and the locating seat on the rear cover and make sure they are free from nicks.
Page 337 TO M-14P MS T A S K C A R D No. 204 pAGEfsi 209, 210 MS ITEM : Adjustment of Compressed Air Distributor PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED 1. Secure the arrow under the airscrew shaft thrust bearing cover attachment nut and bring it to the scale applied to the flange of the airscrew shaft.
Page 338 T A S K C A R D No. 205 TO M-14P MS 211, 212 PAGEISI MS ITEM : Installation of Cover of Compressed Air Distributor Housing PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED 1. Coat the paronite and rubber gaskets with sealant "50" and install them on the distributor housing, 2, Install the housing cover on.
Page 339 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKED ACTIONS TEST EQUIPMENT TOOLS ANO FIXTURES MATERIALS Pliers, flat-nosed 150 Wrench 19x22 Sealant "50" Wire. locking KO-0.8 700880-7 Wrench, spark plug 22 15-32-173 Wrench 7x9 700880-2...
Page 340 GENERATOR GSR-3000M, SERIES 4 - DESCRIPTION AND OPERATION 1. GENERAL The G3R-3000M, aeries 4 generator (Ref. Fig. 1) is intended, to feed the airplane electrical system with DC power. The generator is a shunt-wound four-pole DC machine with four interpoles. The generator is designed for LH rotation (counterclockwise) if viewed from its drive side.
Page 341: Specifications
End shield (12) ia secured to the frame by bolts (20), The inner surface of the end shield carries four brush holders (6). Each brush holder receives two brushes (7) which are pressed to the commutator by helical springs (8) and levers.
Page 342: Operation
Mount vibration corresponds to that of the operating engine which carries the generator 3. OPERATION As regards its operating principle, the GSR-3000M, series 4 generator does not differ from conventional DC machines, The generator electric connection diagram is shown in fig. 3. When the armature rotates in the magnetic field created by the main poles with field windings, electromotive force is induced in the armature winding.
Page 343 1.Interpole Winding 12. End Shield 2.Interpole 13. Pole 3.Pipe 14. Frame 4.Nut 15. Armature 5.Nut 16. Field Winding 6.Brush Holder 17. Bearing 7.Brush 18. Hollow Shaft 8.Spring 19. Flexible Shaft 9.Bearing 20. Bolt 10.Terminal Panel 21. Protective Band 11.Commutator...
Page 344 1. Main Pole 2. Interpole Generator Electrical Connection Diagram (Commutator Side View) Figure 3...
Page 345 GENERATOR GSR-3000M, SERIES 4 - TROUBLE SHOOTING For mostly often encountered troubles and their remedies, refer to the Table given below. Trouble Possible cause Correction 1, Generator (1) Unserviceable brushes: Replace brushes Replace produces no voltage (a) Brushes swell and can hardly brushes 2, Generator does be removed from seats, brushes seize in...
Page 346 Trouble Possible cause Correction 3. Heavy sparking (2) Breakdown in armature Replace generator under brushes causing winding. Check generator in operation and Seat and grind brushes burning of commutator bars inspect commutator after work* If heavy Replace brushes brush sparking is observed during Wipe commutator with clean cloth operation of generator and burning of slightly moistened in gasoline.
Page 347 Trouble Possible cause Correction (6) Excessive runout of commu- Replace generator tator Commutator is grooved by Eliminate trouble in gearbox oil brushes slinger. Replace generator (7) Traces of oil on commutator. Check gearbox oil slinger...
Page 348 GENERATOR GSR-3000M, SERIES 4 - MAINTENANCE PRACTICES 1. LIST OF TASK Title Task Card No. Servicing Removal/Installation Inspection/Check...
Page 349 TO M-14P MS T A S K C A R D No. 201 MS ITEM Servicing PROCEDURE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. GENERAL The following conditions shall be ensured for normal operation of the generator: Cooling and loading according to Specifications,' Item 2.2.
Page 350 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED Inspect working surfaces of the brushes; make sure they are free from chipping. Measure the brush length. The bruahea shorter than 17 nun and having chipping should, be replaced. Check rotation of the armature with bruahea lifted. The armature should rotate freely, CLEANING COMMUTATOR (1) Arrange the generator on the support.
Page 351 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 7/hen dressing, rotate the generator armature and. press a strip of glass paper fitted, over a pointed wooden stick to the commutator surface. Move th-e glass paper with the stick to and fro throughout the commutator length;after cleaning the commutator, carefully blow its interior with clean compressed, air at a pressure of 1 to 2 kgf/cm 4.
Page 352 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS (3) Fit the brushes after seating. The brushes are fitted with the generator run idle in the motor mode at a voltage of up to 15 V. The brushes are considered to be fitted properly if their working surfaces are bright (mirror-like) for at least 85 % of the areas.
Page 353 TO M-14P MS T A S K C A R D No. 202 MS ITEM : Removal/Installation PROCEDURE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. INSTALLATION (1) Depreserve the generator by wiping its preserved, surfaces with a clean cloth moistened in.
Page 354 CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS (8) Connect the cooling air hose to the generator pipe. Check reliable attachment of the pipe to the end shield. CAUTION: INSTALL THE HOSE ON THE AIRPLANE SO THAT THE GENERATOR IS PROTECTED AGAINST DIRECT INGRESS OF DUST, SNOW, WATER, ETC. (9) Start the engine and check operation of the generator.
Page 356 TO M-14P M.S. TASK CARD No. 203 M.S. ITEM : Inspection/Check PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED CAUTION: PERFORM OPERATIONS OTHERWISE SPECIFIED WITHOUT REMOVING THE GENERATOR FROM THE ENGINE. (1) Check attachment of the generator, make sure the generator-to-engine attachment nuts are reliably tightened.
Page 357 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS CHECKED TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Screwdriver 700346 A200x1 Pliers, flat-nosed 150 Wire, locking KO-0.8 Cloths Brush, hair Paper, Wrench 14x17 14-232-03 Wrench 17x19 UB-24-07 glass,grain size up to 8 Wrench, socket 14 UB-24-16 Caliper, vernier...
Page 359 CONSTANT SPEED GOVERNOR R-2, SERIES 04- DESCRIPTION AND OPERATION 1. GENERAL The R-2, aeries 04 airscrew constant speed governor (Ref. Fig* 1) is a unit intended to automatically control the hydraulic airscrew, The R-2, series 04 governor is designed for operation on the M-14F engine with airscrew V530TA-D35 and ensures acconiplishntent of the following functions: Automatic maintenance of the preset airscrew speed of rotation by varying its pitch.
Page 360 Governor drive shaft rotational speed. ensuring stable operation of engine ..........1400 to 3085 r/min (engine speed in this case is 1340 to 2950 r/min5 Operating principle ................Centrifugal-hydraulic Operation pattern ................One-way, positive Working fluid ..................Oil MS-20 COST 21743-76 from engine ......................
Page 361 Governor Body 14. Reducing Valve Oil Pump Body 15. Cup Weight Pivot 16. Ball Bearing Bracket 17. Adjustment Washer Retaining Ring 18. Drive Shaft Gear Transmission Body 19. Weight Drive Shaft 20. Control Shaft Slide Valve 21. Slide Valve Spring Driven Gear Axle 22.
Page 362 The lower shoulder controls supply of oil to the airscrew cylinder, the upper shoulder serves as a seal to preclude ingress of high-pressure oil to the centrifugal governor chamber. Installed on the upper shoulder of the elide valve ia ball bearj-ng (16) whose inner race is pressed to the shoulder by nut (11).
Page 363 The hex end. of the shaft protruding from the body receives a roller or remote control lever, The governor body is connected with the oil pump body by four studs driven into the governor body bosses. The joint of the bodies is sealed by a paronite gasket. 2.2.2.
Page 364: Power Plant
2.2.3. Transmission Body Transmisaion body (6) is the lower cover of the oil pump and. -the flange for mounting the governor on the engine gearbox case. Oil is fed from the engine to the governor and from the governor to the airscrew via internal routes for which purpose the transmission body flange has three holes (1), (2), (4) (Ref.
Page 365 1.Hole to Supply Oil from Engine to Governor 2.Hole to Supply Oil from Governor to Airscrew 3.Coupling Screw 4.Hole for Returning Oil from Governor to Engine Crankcase 5.Coupling Screw Governor Locating Flange Figure 4...
Page 366 1.Passage between Governor and Airscrew 2.Weight 3.Spring 4.Toothed Rack 5.Control Shaft 6.Slide Valve 7.Oil Pump 8.Passage to Supply Oil from Engine to Governor 9.Reducing Valve 10.Slide Valve Shoulder 11.Drive Shaft Governor Operation Diagram for Equilibrium Speed of Rotation. (Steady-State Conditions) Figure 5...
Page 367 Thus, shoulder (10) of slide valve (6) seals off passage (1) connecting the governor with the airscrew. The oil contained in the airscrew space is confined within the latter. Acted upon by the centrifugal force moments of the counterweights installed on the blade sleeves, the blades tend to turn "towards higher pitch, but the oil retained in the airscrew cylinder precludes them from turning so that the pitch remains constant.
Page 368 Passage between Governor and. Airscrew Weight Spring Toothed Rack Control Shaft Slide Valve Oil Pump Passage to Supply Oil from Engine to Governor Reducing Valve Slide Valve Shoulder Drive Shaft Governor Operation Diagram for Increasing Engine Speed Figure 7...
Page 369 As speed of rotation restores to the preset one, overadjustment can also take place, i.e. the slide valve may overshoot the equilibrium position one or two times. 3.2. FORCED CHANGE OF PRESET SPEED OF ROTATION OF AIRSCREW AND ENGINE 3.2.1. Change of Engine Speed of Rotation The airscrews are adapted for changing the engine speed of rotation upon the pilot's will both in flight and on the ground without touching the throttle quadrant.
Page 370 CONSTANT SPEED GOVERNOR R-2, SERIES 04 - MAINTENANCE PRACTICES 1. LIST OF TASK CARDS Title Task Card No. Removal Depreservation of Hew Governor Installation Adjustment of Governor on Engine...
Page 371 2. OPERATION PROCEDURE TASK CARD No. 201 TO M-14P MS M S ITEM '. Removal PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS ECKED BY 1, Unlock and undo the attachment nut of the governor control roller and remove the roller.
Page 372 TO M-14P MS TASK CARD No. 202 MS ITEM : Depreservation of New Governor PROCEDURE CHECKED OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE ACTIONS 1. Unpackage the new governor. 2. Make sure governor seals and locks are not missing. 3. Undo four nuts, remove shipping covers and support from the governor.
Page 373 TO M-14P MS TASK CARD No. 203 MS ITEM : Installat ion PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKED ACTIONS 1, Inspect the mating planes of the governor and engine, drive coupling splines and Dreas nicks governor shank. Replace governor in T.R.
Page 374 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKED ACTIONS TEST EQUIPMENT TOOLS AND FIXTURES MATERIALS Wrench 11x14 14-24-861 Pliers, flat-nosed Sealant "50" 150 Screwdriver 700345 A150x0.5 tVrenoh 9x11 700002...
Page 375 TO M-14P MS TASK CARD No. 204 MS ITEM -. Adjustment of Governor on Engine PROCEDURE OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKED ACTIONS 1. Set the governor control lever in the pilot's cabin to the extreme position corresponding Eliminate playa and to the airscrew maximum pitch.
Page 376 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKED ACTIONS NOTE: The adjustment is regarded to be completed, if with throttle fully open and the governor control lever aet to the low pitch stop, the engine gains a speed of 99 % (2900 r/min) and when the lever is shifted to the high pitch from nominal rating II 70 % (2050 r/min), the speed of rotation drops drastically to 53 %.
Page 377 OPERATIONS AND TECHNICAL REQUIREMENTS CORRECTIVE CHECKED ACTIONS 5. If oil leaks through the control shaft, remove retaining ring (2) (Ref. Fig. 3) and tighten up bearing (7). If trouble persists, replace sealing ring (6) (part PN1-1513) with the ring taken from the SPTA set.
Page 378 CONSTANT SPEED GOVERNOR R-2, SERIES 04 - STORAGE INSTRUCTIONS 1. STORAGE The governor which is not meant for immediate installation on the engine should be stored preserved in closed racks in a clean, dry, heated room at an air temperature of 10 to 30 °0 and relative humidity of 45 to 70 %. CAUTION: IT IS PROHIBITED TO STORE ACIDS, ALKALIS.
Page 379 Use preservation oil K-17 for preservation. Preservation may be also performed with gun grease PVK. When preserving with oil K-17, immerse the non-painted parts and assemblies into a bath with oil for 1 to 2 min. Repeat immersion several times. Keep the coated, parts and assemblies over the bath to let the oil drain down.
Page 380 Material Standard, Specifications Gasoline Nefras-S 50/170 COST 8505-80 or BR-1, BR-2 GOST 443-76 Grease gun PVK GOST 19537-74 Oil, preservation K-17 GOST 10877-76 Paper, paraffined GOST 9569-79 Twine GOST 17308-71 Film, polyethylene 5S or 30, 150, grade 1 GOST 10354-82 Dehydrator silica-gel, grade KSM or ShSM GOST 3956-76 Cartridges,dehydrator (indicators)
Page 381 CONSTANT SPEED GOVERNOR R-2, SERIES 04 - SHIPMENT 1. GENERAL The governor may be shipped by any transport. Shipment may be carried, out at atmospheric pressure decreased to 0,2 kgf/cm and temperature of down to minus 60 °C,...