SERVICE VALVE REPLACEMENT.
The valves on the York compressor are sealed with a gasket placed in the valve port boss. Lubricate the
gasket with refrigerant oil of the type used in the compressor, place the valves with the tube fitting facing aft
and secure with .312 bolts, torque to 15-23 inch-pounds.
—NOTE—
Whenever the air conditioning refrigerant lines or system is
opened for any reason, the lines and fittings should be capped
and sealed immediately to prevent dirt and other contaminants
from entering the system. (It is not advisable to put a plug into
the hoses or fittings.)
TEST GAUGE AND MANIFOLD SET.
The proper testing and diagnosis of the air conditioning system require that a manifold gauge set be
attached into the system. This set consists of two gauges mounted to a manifold. One gauge is a high pressure
gauge used in the discharge side of the system. The other is a low pressure gauge used in the suction side of
the system. The manifold is a device having fittings for both gauges and connection hoses with provisions for
controlling the flow of refrigerant through the manifold. (See Figures 21-6 and 21-7.)
The center port of the manifold set is used for charging or evacuation procedures, or any other service that
may be necessary.
Both the high and low side of the manifold have hand shut-off valves. When the hand valve is turned all
the way in, in a clockwise direction, the manifold is closed. The pressures on the side of the system will,
however, be recorded on the gauge above the hose.
Cracking the hand valve, in the counterclockwise direction, opens the system to the middle service port of
the manifold set. This is desirable only when it is necessary to let refrigerant out or into the system. (Refer to
Figures 21-6 and 21-7.)
CHECKING THE SYSTEM FOR LEAKS.
There are several methods of doing this operation, depending on the type of equipment which is available.
Two methods of performing this check will be covered in the following paragraphs.
—NOTE—
Evacuate system prior to leak check.
21-50-07
Page 21-18
December 1, 1978
1F17
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Summary of Contents for Arrow IV
Page 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...
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Page 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Page 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Page 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Page 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Page 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Page 66: ...CHAPTER PARKING AND MOORING 1C18...
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Page 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Page 77: ...CHAPTER SERVICING 1D5...
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Page 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Page 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Page 168: ...THIS PAGE INTENTIONALLY LEFT BLANK 1G24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...
Page 169: ...CHAPTER AUTO FLIGHT 1H1...
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Page 176: ...CHAPTER COMMUNICATIONS 1H8...
Page 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Page 233: ...CHAPTER FLIGHT CONTROLS 1J17...
Page 297: ...CHAPTER FUEL 2A18...
Page 320: ...CHAPTER HYDRAULIC POWER 2B17...
Page 355: ...CHAPTER LANDING GEAR 2D4...
Page 418: ...CHAPTER LIGHTS 2F19...
Page 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Page 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Page 464: ...CHAPTER VACUUM SYSTEM 2H17...
Page 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Page 477: ...CHAPTER STRUCTURES 2I6...
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Page 496: ...CHAPTER DOORS 2J1...
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Page 505: ...CHAPTER STABILIZERS 2J10...
Page 514: ...CHAPTER WINDOWS 2J19...
Page 519: ...CHAPTER WINGS 2J24...
Page 550: ...CHAPTER PROPELLER 3A18...
Page 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Page 568: ...CHAPTER POWER PLANT 3B12...
Page 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Page 611: ...CHAPTER IGNITION 3D7...
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Page 655: ...CHAPTER ENGINE INDICATING 3F16...
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Page 664: ...CHAPTER EXHAUST 3G1...
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Page 669: ...CHAPTER OIL SYSTEM 3G6...
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Page 673: ...CHAPTER STARTING 3G10...
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Page 688: ...CHAPTER TURBINES 3H1...
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Page 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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