3. Bleed the brakes per Bleeding Brakes.
BLEEDING BRAKES.
BRAKE BLEEDING PROCEDURE. (Gravity)
1. On both main landing gear wheel brake assemblies, attach a clear plastic hose to the brake bleeders
and extend into container partially filled with hydraulic fluid, MIL-H-5606. The ends of this hose should be
submerged in the fluid. Open both bleeders approximately one and one-half to two turns.
2. Fill the brake reservoir on the firewall with hydraulic fluid, MIL-H-5606.
3. Disconnect the toe brake cylinders from the pedal connection by removing clevis pin, washer and
cotter pin.
4. Invert toe brake cylinder to aid in releasing trapped air in the top of the cylinder.
5. Check toe brake pedals in the cockpit to insure pedals are pulled full aft.
6. Pull the hand brake handle, pumping the master cylinder very slowly approximately 25 times until
fluid is observed passing through the clear plastic hoses at the wheel cylinder.
—NOTE—
Fluid level in the reservoir must be maintained to prevent air
from entering in the line.
7. Tighten both wheel bleeders.
8. Pull hand brake until a firm handle is maintained.
BRAKE BLEEDING PROCEDURE. (Pressure)
1. Place a small clear plastic hose on the vent tube of the brake reservoir and place a second small clear
plastic hose on the bleeder fitting on one main landing gear. Place the open ends of these tubes in a suitable
container to collect the fluid overflow. Open the bleeder fitting one or two turns.
2. On the other main gear, slide the hose of the pressure unit over the bleeder fitting then open the fitting
one or two turns and pressure fill the brake system with MIL-H-5606 fluid.
3. With fluid continually flowing through the brake system, SLOWLY and together actuate the hand
brake and the toe brake pedal of the side being bled, several times, to purge the cylinders of air. On dual brake
installations, both right and left pedals must be actuated.
—NOTE—
By watching the fluid pass through the plastic hose at the fluid
reservoir and the bleeder fitting on the gear being bled, it can be
determined whether any air is left in the system. If air bubbles are
evident, filling of the system shall be continued until all the air is
out of the system and a steady flow of fluid is obtained. Should
the brake handle remain spongy, it may be necessary to
disconnect the bottom of the toe brake cylinders (next to the
pedal) and rotating the cylinder horizontally or even above
horizontal and by use of the hand brake alone, purge the air from
the system.
32-40-25
Page 32-54
December 1, 1978
2F13
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 168: ...THIS PAGE INTENTIONALLY LEFT BLANK 1G24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...
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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