3. Remove valve and gear case from reservoir as follows:
A.
Remove eight screws from flange of body and separate the two assemblies.
B.
Pump gears and valves should be removed for cleaning purposes only. To remove cap securing
Gears, remove attaching bolts. The two valve springs should be positively identified with their
cavities; otherwise, it will be necessary to readjust each valve for proper operating pressure.
CLEANING, INSPECTION AND REPAIR OF PRESTOLITE HYDRAULIC PUMP
— CAUTION —
R E PAIR FACILITIES MUST BE CLEAN TO PREVENT
CONTAMINATION OF PUMP COMPONENTS. PROPER
AND CAREFUL HANDLING SHOULD BE EXERCISED
TO PREVENT DAMAGING PUMP COMPONENTS.
1. Discard all O-rings.
2. Remove caps or plugs and clean all components with a dry type cleaning solvent and dry thoroughly.
3. Inspect pump components for scratches, scores, chips, cracks and wear.
4. Inspect motor for worn brushes (minimum of .218 of an inch brush remains between the braided and
commutator end), excess commutator wear and excess bearing wear.
5. Repairs are limited to O-ring and brush replacement as follows:
A.
One brush holder has the winding wire attached. Locate this wire and remove by using a solder-
ing gun.
B.
The head assembly can now be removed and worked on for ease of brush replacement if required.
C.
Remove brush wire and brush from bimetal heat protector.
D.
Solder new brush wires to head assembly and bimetal heat protector, and wire from winding to
one brush holder.
E.
Install brush springs and brushes into brush holders and secure in place (temporary) with a piece
of string looped around the brush and holder and tied in a knot.
— NOTE —
Ensure that the braided wire is in the holder slot for proper brush
movement.
F.
Install the head assembly with new brushes to the frame and commutator in accordance with
instructions given in Step I of the next paragraph.
ASSEMBLY OF PRESTOLITE HYDRAULIC PUMP (Refer to Figure 29-3.)
1. To assemble pump motor and install on reservoir:
A.
Position motor frame on reservoir. Note aligning marks on frame and reservoir.
B.
Place thrust washers, of the same amount removed, on the drive end of the armature.
C.
Lubricate the entire length of the armature shaft, on the drive end, with light grease to protect 0-
ring seal from damage. Insert end of shaft in reservoir.
D.
Saturate felt oiling pad around commutator end bearing with SAE 20 oil. Allow excess oil to
drain off before assembling motor.
E.
Insert thrust ball in bearing of motor head. To hold ball in position, place a small amount of
grease inside the bearing.
F.
Place head assembly on frame and allow brushes to extend over commutator. Remove the string
securing the brushes in the holders. Push head assembly on frame and insure proper indexing of
head and frame assemblies. Secure in place with thru bolts.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
29-11-04
Page 29-14
Revised: June 20, 1995
2C9
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...