5. Evacuate and charge the system.
— WARNING —
IF THE AIR CONDITIONER IS TO BE OPERATED ON THE GROUND FOR
S E RVICING, THE TEST AREA SHOULD BE CLEAN AND FREE OF ANY
LOOSE OBJECTS LYING ON THE RAMP. ONLY THE SERVICE VA LV E S
L O C ATED ON THE EVA P O R ATOR ASSEMBLY SHOULD BE USED FOR
TESTING.
COMPRESSOR OIL LEVEL CHECK.
— Note —
Compressor oil level should be checked any time the system is discharged
1. Run the compressor for 10 minutes with engine at 1900 RPM.
— WARNING —
IF THE AIR CONDITIONER IS TO BE OPERATED DURING GROUND
S E RVICING, THE TEST AREA SHOULD BE CLEAN AND FREE OF ANY
LOOSE OBJECTS LYING ON THE RAMP. ONLY THE SERVICE VA LV E
L O C ATED ON THE EVA P O R ATOR ASSEMBLY SHOULD BE USED FOR
TESTING.
2. Discharge the system being careful not to lose any oil.
3. Remove the oil fill plug.
4. Position the rotor to top dead center (Refer to Figure 21-31 by rotating the clutch front plate until the
casting mark is visible in the center of the hole.
5. Rotate the clutch front plate clockwise by approximately 110°. (Refer to Figure 21-32.)
6. Insert dipstick No. 32447 purchased from Sankyo.
7. Remove the dipstick and count the number of increments of oil. The acceptable oil level in increments is
7 to 10. This represents between 2.6 and 4.4 fluid ounces.
8. When oil is added Piper refrigerant oil PMS-L2000 or equivalent 500 viscosity refrigerant oil must be
used.
9. When installing the oil filter plug, make sure the sealing O-ring is not twisted and that no dirt nor
particles are on the O-ring or seat. Torque the plug to 6-9 foot-pounds. Do not overtighten the plug to
stop a leak; remove the plug and install a new O-ring.
10. Evacuate and charge the system.
— CAUTION —
THE OIL PLUG SHOULD NOT BE REMOVED WITH PRESSURE IN THE
SYSTEM.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 5 3 - 0 4
Page 21-70
Revised: May 15, 1989
1H13
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...