COOLING (cont.)
M. Charging The System (cont.)
(1) Charging stand method (cont.)
— NOTE —
If bubbling occurs in sight glass, reopen cylinder base valve
momentarily to equalize drum and cylinder pressure.
(e) Connect the heating element plug to a 110 volt outlet.
(6) Turn cylinder sight glass to match pressure reading on cylinder pressure gauge, this scale
should be used during entire charging operation.
(7) Close valve 1 (low pressure control), fully open valve 4 (refrigerant control) and allow all the
liquid refrigerant contained in the charging cylinder to enter high side of aircraft system.
(8) When the full charge of refrigerant has entered the system, close valve 4 (refrigerant control)
and valve 2 (high pressure control).
(9) After completion of charging, close all valves on the charging stand. Disconnect the high and
low pressure charging lines from the aircraft system. (A small amount of refrigerant remain-
ing in the lines will escape.) Replace lines on holder of charging stand to keep air and dirt out
of lines. Open the valve at the top of cylinder to relieve any remaining pressure, then close
the valve.
(10) Reinstall protective caps of Schrader valves and any access panels previously removed.
(2) Using the airplane compressor to charge system
This method is least desirable due to requirement of operating airplane’s engine to run compressor.
— CAUTION —
Ensure area around airplane is clean and a qualified person is
at the controls of the airplane.
(a) With system evacuated, connect refrigerant charging hose to manifold and purge the charging
hose of air. (Refer to Figure 9)
(b) Place refrigerant container on a scale to observe amount of refrigerant entering system. Open
high pressure valve and add as much refrigerant as possible.
(c) Close high pressure valve. Start engine and operate it at 900 to 1000 rpm.
(d) Operate air conditioner and set controls to maximum cooling.
(e) Open low pressure valve and complete charging system.
(f) Close low pressure valve after two pounds of refrigerant has been added to the system.
(g) While system is operating, observe the sight glass in top of receiver-dehydrator by removing
plastic plug.
(h) Sight glass should be clear of any bubbles or foam. If bubbles or foam are seen passing
through sight glass, it is an indication of a low refrigerant charge in the system and more
refrigerant is required. Make check with OAT of 70 F or higher and with air conditioner
operating.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
21-50-00
Page 21-28
Reissued: July 1, 1993
1I11
Summary of Contents for PA-32R-301T SARATOGA S
Page 26: ...CHAPTER 4 AIRWORTHINESS LIMITATIONS 1C1 ...
Page 29: ...CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS 1C4 ...
Page 53: ...CHAPTER 6 DIMENSIONS AND AREAS 1D6 ...
Page 64: ...CHAPTER 7 LIFTING AND SHORING 1D21 ...
Page 68: ...CHAPTER 8 LEVELING AND WEIGHING 1E1 ...
Page 72: ...CHAPTER 9 TOWING AND TAXIING 1E5 ...
Page 76: ...CHAPTER 10 PARKING AND MOORING 1E9 ...
Page 80: ...CHAPTER 11 REQUIRED PLACARDS 1E13 ...
Page 92: ...CHAPTER 12 SERVICING 1F1 ...
Page 126: ...CHAPTER 20 STANDARD PRACTICES AIRFRAME 1G17 ...
Page 127: ...THIS PAGE INTENTIONALLY LEFT BLANK ...
Page 139: ...CHAPTER 21 ENVIRONMENTAL SYSTEMS 1H5 ...
Page 188: ...CHAPTER 22 AUTOFLIGHT 1J7 ...
Page 193: ...CHAPTER 23 COMMUNICATIONS 1J12 ...
Page 203: ...CHAPTER 24 ELECTRICAL POWER 1J22 ...
Page 263: ...CHAPTER 25 EQUIPMENT FURNISHINGS 2A13 ...
Page 269: ...CHAPTER 27 FLIGHT CONTROLS 2A20 ...
Page 332: ...CHAPTER 28 FUEL 2D11 ...
Page 363: ...CHAPTER 29 HYDRAULIC POWER 2E18 ...
Page 404: ...CHAPTER 30 ICE AND RAIN PROTECTION 2G16 ...
Page 470: ...CHAPTER 32 LANDING GEAR 3A13 ...
Page 550: ...CHAPTER 33 LIGHTS 3D24 ...
Page 562: ...CHAPTER 34 NAVIGATION AND PITOT STATIC 3E12 ...
Page 582: ...CHAPTER 35 OXYGEN 3F8 ...
Page 604: ...CHAPTER 37 VACUUM 3G6 ...
Page 616: ...CHAPTER 39 3G18 ELECTRIC ELECTRONIC PANELS MULTIPURPOSE PARTS ...
Page 620: ...CHAPTER 51 STRUCTURES 3G22 ...
Page 636: ...CHAPTER 52 DOORS 3H14 ...
Page 650: ...CHAPTER 55 STABILIZERS 3I4 ...
Page 662: ...CHAPTER 56 WINDOWS 3I16 ...
Page 670: ...CHAPTER 57 WINGS 3I24 ...
Page 688: ...CHAPTER 61 PROPELLER 3J18 ...
Page 704: ...CHAPTER 70 STANDARD PRACTICES ENGINES 3K10 ...
Page 708: ...CHAPTER 71 POWER PLANT 3K14 ...
Page 737: ...CHAPTER 73 ENGINE FUEL SYSTEM 4A13 ...
Page 749: ...CHAPTER 74 IGNITION 4B1 ...
Page 783: ...CHAPTER 77 ENGINE INDICATING 4C11 ...
Page 793: ...CHAPTER 78 EXHAUST 4C21 ...
Page 801: ...CHAPTER 79 OIL 4D5 ...
Page 805: ...CHAPTER 80 STARTING 4D9 ...
Page 819: ...CHAPTER 81 TURBINES 4D23 ...
Page 833: ...CHAPTER 91 CHARTS WIRING DIAGRAMS 4E13 ...