2. Method 2:
A.
Remove the access panel at the rear of the cabin to gain access to the service valves.
B.
Remove the protective cap on the high pressure Schrader valve fitting and connect a charging hose
with a shut-off valve arrangement to the fitting. The charging hose must have a Schrader fitting or
adapter to fit the valve.
C.
Connect the other end of the charging hose to a small cylinder of refrigerant and purge the hose by
allowing a slight amount of refrigerant gas to escape from the Schrader valve fitting.
D.
The cylinder of refrigerant should be placed upright in a container of warm (125° F max.) water on
a small scale.
E.
Allow approximately 1/2 pound of refrigerant to enter the system by opening the valve on the
charging hose and observing the weight change on the scale.
F.
Using an electronic leak detector, check all joints and repair any leaks.
G.
After completion of repair of any leaks, proceed to check the system in accordance with one of the
methods outlined for any other leaks.
H.
If no further repair is required on the system, it is now ready to evacuate.
DISCHARGING THE SYSTEM. (Required only if the system contains refrigerant.)
— Note —
Applies to Kent Moore J23500 or similar charging station. Refer to Figure 21-29.
1. Close all valves on charging station.
2. Connect red high pressure charging line to high pressure Schrader valve at the evaporator fitting.
3. Open valve 8 (high pressure control) on charging station one turn.
4. Hold end of blue low pressure charging line in a shop rag and slowly open valve 2 (low pressure control)
on charging station allowing refrigerant to exhaust from system into shop rag.
— CAUTION —
REFRIGERANT CAN CAUSE FREEZING OF SKIN. BE PA RT I C U L A R LY
CAREFUL NOT TO ALLOW CONTACT WITH EYES
— CAUTION —
DO NOT ALLOW REFRIGERANT TO ESCAPE TOO RAPIDLY, AS
EXCESSIVE OIL MAY BE CARRIED OUT OF SYSTEM. WHEN HISSING
S TOPS, SYSTEM IS EMPTY AND VA LVE SHOULD BE CLOSED IF NO
FURTHER WORK IS PLANNED.
EVACUATING THE SYSTEM.
— Note —
If the system has been operated in a discharged condition or anytime the system has
been open to atmospheric pressure, the receiver-dehydrator must be replaced and the
system evacuated to remove any trapped air and moisture which has entered it.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 5 2 - 0 7
Page 21-62
Revised: May 15, 1989
1H5
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...