5. Start the vacuum pump and open the low side manifold hand valve. Observe the compound, low pressure
gauge needle, it should show a slight vacuum.
6. Continue to operate the vacuum pump until 26 to 28 inches of vacuum is attained on the low pressure
gauge, then extend the operation for another 25 minutes.
7. If the system cannot maintain 26 to 28 inches of vacuum, close both manifold hand valves and observe
the compound gauge.
8. Should the compound gauge show a loss of vacuum, there is a leak in the system which must be repaired
before continuing with evacuation.
9. If no leaks are evident, reopen both manifold hand valves and continue the evacuation for another 30
minutes.
10. Close both manifold hand valves, stop vacuum pump and disconnect center manifold hose from the
vacuum pump.
11. Proceed to charge the system.
— Note —
The system should be charged as soon as it has been evacuated.
CHARGING THE SYSTEM.
Once the system has been completely evacuated, it must be charged utilizing a charging stand (preferred
method) or utilizing the airplane's compressor.
CHARGING STAND METHOD.
— Note —
The following instructions apply to Kent Moore, J23500 charging stand Refer to
Figure 21-29.
1. With the system discharged and evacuated, proceed to hook-up the charging stand.
2. Fill the charging cylinder by operating the valve at the base of the charging cylinder and filling the sight
glass with two pounds of liquid refrigerant.
3. As refrigerant stops filling the sight glass, open the valve at the top of the gauge neck assembly
intermittently to relieve head pressure and allow refrigerant to continue filling the sight glass to the
required amount.
4. When refrigerant reaches the required level in the sight glass, close the valve at the base of the cylinder
and the valve at the bottom of the refrigerant tank. Be sure the top valve is fully closed.
— Note —
If bubbling occurs in sight glass, reopen the cylinder base valve momentarily to
equalize drum and cylinder pressure.
5. 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.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 5 2 - 0 8
Page 21-64
Revised: May 15, 1989
1H7
PIPER AIRCRAFT
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...