Piper SARATOGA PA-32-301 Maintenance Manual page 147

1774
PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
8. Make and check electrical connections. (Refer to Figure 21-17.)
9. Check operation of blower and refrigerant systems.
10. Install rear bulkhead panels. Be certain to seal. (See WARNING.)
- WARNING -
Whenever it is necessary to remove and replace the rear cabin panel,
it should be replaced and sealed in the original manner to prevent
exhaust from entering the cabin. After removing and replacing the
rear panel, conduct a carbon monoxide test on the ground and in
flight with and without the air conditioner operating. Presence of
C02 shall not exceed one part in 20,000.
WRAP TAPE AROUNDTHERMO
STAT CAPILLARY LEAVING SER-
VICE PORT ACCESSIBLE
1. SIGHT GLASS
2 SERVICE VALVE (SCHRADER) (HI)
3 CAPILLARY COIL
4. HOUSING ASSY
5. SERVICE VALVE (SCHRADER) (LOW)
6 RECEIVER DEHYDRATOR CLAMP
7. RECEIVER DEHYDRATOR
8 PRESSURE RELIEF SWITCH (RANCO)
9EXPANSION VALVE
10 OUTLET HOSE
Figure 21-16. Components Installation
21-58-24
Page 21-41
Revised: August 11. 1983
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