OILDYNE HYDRAULIC PUMPS.
REMOVAL OF OILDYNE HYDRAULIC PUMP (Refer to Figure 29-5, Sheet 1 of 2)
The Oildyne hydraulic pump with reservoir incorporated is located in the aft section of the fuselage
between stations 156 and 191. Access to the pump is through the access panel in the baggage compartment.
1. Remove the ABS nose gear cover.
2. Remove anti-splash cover (Piper P/N 96374-0) by removing the four attaching screws,
3 . Disconnect the three knife connectors that attach the black, blue, and green forward and reverse
h a rness wires.
4. Disconnect and plug the UP and DOWN pressure hydraulic lines from pump mount. Cap the lines .
5. Remove the three each mounting bolts and washers securing pump mount to deck
6. Lift assembly from airplane.
FIELD SERVICE OF OILDYNE HYDRAULIC PUMP
Field service of Oildyne hydraulic pump is limited to motor replacement and removal, cleaning, and
inspecting the hydraulic fluid reservoir. Should pump malfunction, either replace pump, or return pump to
Piper Aircraft, via the local Piper distributor, for servicing or repairs.
DISASSEMBLY OF OILDYNE HYDRAULIC PUMP FROM BRACKET (Refer to Figure 29-5, Sheet 1
of 2)
1. Remove safety wire securing two bolts that attach bracket to pump.
2. Remove the two bolts and washers.
3. Separate pump assembly from bracket.
D I S A S S E M B LY OF MOTOR ASSEMBLY FROM OILDYNE PUMP-ADAPTER ASSEMBLY (Refer to
Figure 29-5, Sheet 2 of 2)
1. Remove two each mounting bolts on flange of motor assembly and separate the motor assembly from
the pump.
2. Remove coupling and O-ring and discard.
— NOTE —
New O-ring and coupling are included in replacement motor
assembly.
D I S A S S E M B LY OF RESERVOIR ASSEMBLY FROM OILDYNE PUMP-ADAPTER ASSEMBLY
(Refer to Figure 29-5, Sheet 2 of 2)
— CAUTION —
DO NOT DISASSEMBLE PUMP ASSEMBLY FROM
ADAPTER ASSEMBLY. DAMAGE TO VA LVES AND
P R E SSURE SETTINGS, WHICH ARE NON-ADJUSTABLE,
WILL OCCUR.
1. Remove screw and O-ring securing the reservoir to the adapter assembly.
2. Remove reservoir and reservoir seal.
3. When replacing reservoir, remove the cushion pad. It will have to be bonded to the new reservoir base
using Scotch Grip 2210 or Contact Adhesive B-10161 rubber cement.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
29-11-25
Page 29-18
Added: June 20, 1995
2C13
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...