1. With the system evacuated as outlined in Evacuating the System, connect the refrigerant charging hose
to the manifold (refer to Figure 21-11) and purge the charging hose of air.
2. Place the refrigerant container on a scale to observe the amount of refrigerant entering the system.
Open the high pressure valve and add as much refrigerant as possible.
3. Close the high pressure valve, start the engine and operate it at 900 to 1000 RPM.
4. Operate the air conditioner and set controls to maximum cooling.
5. Open the low pressure valve and complete charging the system.
6. Close the low pressure valve after two pounds of refrigerant has been added to the system.
7. With the system still operating, observe the sight glass in the top of the receiver-dehydrator by
removing the plastic plug.
8. The sight glass should be clear of any bubbles or foam. If bubbles or foam are seen passing through
the sight glass, it is an indication of a low refrigerant charge in the system and more refrigerant is required.
This check should be made with OAT of 70°F or higher and with the air conditioner operating.
9. If more refrigerant must be added to the system, open the low pressure valve and increase engine
speed to 2000 RPM and observe the sight glass. After the sight glass has cleared, close the low pressure valve
and observe the pressure gauges. At 1000 RPM the gauge pressure should be 15 to 20 psi on the low side and
150 to 200 on the high side.
—NOTE—
Suspect leaks or an inaccurate scale if two pounds of refrigerant
does not fill the system.
10. Shut off the air conditioning system and airplane engine. Then, remove the charging lines from the
Schrader valves with care due to the refrigerant remaining in the hose.
—NOTE—
A shop cloth should be used to divert escaping refrigerant when
disconnecting the charging hose from the Schrader valve. Recap
the valve.
ADDITION OF PARTIAL CHARGE TO SYSTEM.
It is possible to top off this system with refrigerant by the following method:
1. Remove the access panel at the rear of the cabin.
2. Connect a charging hose to a refrigerant cylinder and also to the Schrader valve fitting on the suction
line. (Refer to Figure 21-11.)
3. Purge the charging hose by allowing a small amount of refrigerant gas to escape at the Schrader valve
fitting.
4. Start the engine and operate at 1000 RPM and turn the air conditioner on maximum cool.
5. Remove the plastic plug from the sight glass in the top of the receiver-dehydrator.
6. With a low refrigerant charge in the system, bubbles will be seen passing through the sight glass when
the system is operating.
7. Open the valve on the refrigerant cylinder.
8. Allow refrigerant to flow into the system until the bubbles disappear from the sight glass.
21-50-15
Page 21-26
December 1, 1978
1G1
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 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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