REMOVAL OF VACUUM PUMP.
1. Remove the top portion of the engine cowling. (Refer to Chapter 71.)
2. Loosen the hose clamp and remove the hose from the pump fitting.
3. Remove the four retaining nuts, lock washers and plain washers used to secure the pump to the engine;
then remove the pump.
REPLACING PUMP FITTINGS.
1. Before installing any fittings on the pump, check for any external damage. A pump that has been
damaged or dropped should not be installed.
2. When a vise is used to hold the pump while installing fittings, suitable caution must be exercised to
avoid pump damage. The square mounting flange must be held between soft wood blocks and only at right
angles to the vise jaws. Use only enough vise pressure to hold the pump firmly.
—CAUTION—
DO NOT apply vise pressure to the outside diameter or overall
length of the pump.
3. The ports of the AIRBORNE pump have been treated with a dry film lubricant and the AIRBORNE
fittings are cadmium plated thus eliminating any need for thread lubricants. If thread lubricant is required, use
a powdered moly-sulfide or graphite in dry form or in an evaporating vehicle; or employ a silicone spray.
Apply sparingly to external threads of fittings only.
—CAUTION—
DO NOT use pipe tape, thread dope, hydrocarbon oil or grease,
as these can contaminate the pump and cause malfunction.
4. With the pump properly secured in the vise, insert fittings in ports and hand tighten firmly.
5. Using a wrench, tighten each fitting from one-half to two additional turns.
INSTALLATION OF VACUUM PUMP.
1. Place the pump gasket in its proper place and align the spline on the pump drive with the spline on the
engine drive assembly.
—CAUTION—
The only pump mounting gasket authorized and approved for use
on the Airborne vacuum pump is the Airborne gasket B3-1-2,
Piper part number 751 859. Use of any other gasket may result in
oil seepage or leakage at the mounting surface.
37-10-05
Page 37-05
December 1, 1978
2H23
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Summary of Contents for Arrow IV
Page 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...
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Page 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Page 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Page 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Page 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Page 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Page 66: ...CHAPTER PARKING AND MOORING 1C18...
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Page 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Page 77: ...CHAPTER SERVICING 1D5...
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Page 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Page 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Page 169: ...CHAPTER AUTO FLIGHT 1H1...
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Page 176: ...CHAPTER COMMUNICATIONS 1H8...
Page 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Page 233: ...CHAPTER FLIGHT CONTROLS 1J17...
Page 297: ...CHAPTER FUEL 2A18...
Page 320: ...CHAPTER HYDRAULIC POWER 2B17...
Page 355: ...CHAPTER LANDING GEAR 2D4...
Page 418: ...CHAPTER LIGHTS 2F19...
Page 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Page 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Page 464: ...CHAPTER VACUUM SYSTEM 2H17...
Page 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Page 477: ...CHAPTER STRUCTURES 2I6...
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Page 496: ...CHAPTER DOORS 2J1...
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Page 505: ...CHAPTER STABILIZERS 2J10...
Page 514: ...CHAPTER WINDOWS 2J19...
Page 519: ...CHAPTER WINGS 2J24...
Page 550: ...CHAPTER PROPELLER 3A18...
Page 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Page 568: ...CHAPTER POWER PLANT 3B12...
Page 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Page 611: ...CHAPTER IGNITION 3D7...
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Page 655: ...CHAPTER ENGINE INDICATING 3F16...
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Page 664: ...CHAPTER EXHAUST 3G1...
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Page 669: ...CHAPTER OIL SYSTEM 3G6...
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Page 673: ...CHAPTER STARTING 3G10...
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Page 688: ...CHAPTER TURBINES 3H1...
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Page 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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