COOLING (cont.)
B. Air Conditioning (cont.)
(1) Description and Operation. (Refer to Figure 2)
This installation consists of a compressor with its special brackets and associated hardware, an
evaporator, a condenser, a receiver-dehydrator, circulating fan, thermal expansion valve, and relat-
ed plumbing.
The evaporator filters, dehumidifies and cools the air. The evaporator is mounted in a fabricated
housing along with the receiver-dehydrator, circulating fan, thermal expansion valve and related
plumbing. This housing is located at the rear of the cabin, aft of the baggage area. The compressor
is a two cylinder, piston type compressor which is supported by special brackets at the front of the
engine. A V-belt connected to the engine ring gear drives the compressor through a magnetic
clutch. The condenser is installed on a hinge mounted door that is located on the bottom portion
of the fuselage tail section. The condenser door is hinge mounted to allow extension into the
airstream during system operation. The condenser door is electrically activated to provide the
following positions, (system on - fully extended; system off - fully retracted).
The system is protected by a Ranco type pressure switch which automatically controls the
condenser maximum head pressure by temporarily de-clutching the compressor in the event
the pressure becomes excessively high. The controls are located on the aircraft instrument panel
adjacent to the heater and defroster levers, and consist of an Air Conditioning control, a fan
control to govern the cold air velocity, and a temperature control.
The system is such that there is no increase in drag to the aircraft during its take-off flight
conditions. During maximum power demands the compressor is de-clutched and the condenser
door is automatically retracted.
The air conditioning system in this aircraft is a recirculating, independent unit. It filters,
dehumidifies and cools the air as it cycles through the evaporator. The unit is operated from
controls mounted on the right side of the instrument panel. The air conditioning master switch
has two positions, ON-OFF. When the AIR COND position is selected the compressor clutch
engages, the condenser scoop opens and the circulating fan is turned on. The temperature is
controlled by a thermostat operated by the temperature control selector. A two position fan switch
(LOW-HIGH) operates the blower. The fan may be operated to circulate air without using the air
conditioning unit.
The air conditioning system uses Refrigerant 12. The refrigerant enters the compressor as a vapor.
The compressor pressurizes the heat-laden vapor until its pressure and heat reach a point much
hotter than the outside air. The compressor then pumps the vapor to the condenser where it cools
and changes to a liquid. The liquid then passes to the receiver-dehydrator. Its function is to filter,
remove any moisture and insure a steady flow of liquid refrigerant into the evaporator through the
expansion valve. The expansion valve is a temperature controlled metering valve which regulates
the flow of the liquid refrigerant to the evaporator. The evaporator absorbs the heat from the air
passing over the coils. From the evaporator the refrigerant vapor returns to the compressor where
the cycle is repeated.
— NOTE —
The air conditioning system should be operated at least once a
month to prevent sticking valves and keep the system
lubricated.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
21-50-00
Page 21-10
Reissued: July 1, 1993
1H17
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 ...