INSTALLATION OF HYDRAULIC PUMP.
1. Install the rubber shock mounts through the mounting holes of the pump. Insert a bushing through the
holes of each shock mount.
2. Position the pump on its mounting flange. Install mounting bolt with washer and tighten. (Refer to
3. Connect the hydraulic lines to the pump.
4. Connect the pump electrical leads. Green wire to outboard relay, blue wire to inboard relay and black
wire to ground on battery shelf.
5. Check fluid level in pump. Fill per instructions given in Chapter 12.
6. With the airplane on jacks, operate the pump to purge the hydraulic system of air, and check for leaks.
After operation, recheck fluid level.
GEAR BACK-UP EXTENDER ACTUATOR ASSEMBLY.
REMOVAL OF GEAR BACK-UP EXTENDER ACTUATOR ASSEMBLY. (Refer to Figure 29-8.)
The back-up extender actuator is located under the rear seat. To reach the actuator, remove the rear seats.
1. Disconnect the actuator electrical leads at the quick disconnect terminals.
2. Disconnect the pressure and static hoses from the elbows of the diaphragm housing by releasing
clamps and sliding the hoses from their elbows. The hoses should be tagged for ease of reassembly.
3. Place a shop cloth under the actuator hydraulic valve to absorb fluid, and then disconnect the hydraulic
lines from the elbows of the hydraulic valve. Cover the lines to prevent contamination.
4. Remove the machine screws that secure the actuator base to the mounting brackets. There are two
mounting screws at the inboard side of the base and one at the outboard side of the diaphragm housing.
Remove the actuator from the mounting brackets.
INSTALLATION OF GEAR BACK-UP EXTENDER ACTUATOR ASSEMBLY. (Refer to Figure 29-8.)
1. Position the gear back-up extender actuator against its mounting brackets and install attaching machine
screws. Do not tighten screws.
—NOTE—
With the base attached and before installing the attaching screw
through the ring of the diaphragm housing, insure that the
attaching holes in the housing and mounting bracket align
without using force. Should they misalign, it may be necessary to
reform the main fuselage mounting bracket.
To reform the main fuselage mounting bracket, an Aligning Tool
may be used. (Refer to Figure 29-7.) This tool may be fabricated
from dimensions given in Chapter 91. When proper alignment
has been accomplished, tighten the machine screws.
29-10-10
Page 29-22
Revised: November 6, 1979
2C16
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Содержание Arrow IV
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Страница 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Страница 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Страница 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Страница 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Страница 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Страница 66: ...CHAPTER PARKING AND MOORING 1C18...
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Страница 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Страница 77: ...CHAPTER SERVICING 1D5...
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Страница 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Страница 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Страница 169: ...CHAPTER AUTO FLIGHT 1H1...
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Страница 176: ...CHAPTER COMMUNICATIONS 1H8...
Страница 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Страница 233: ...CHAPTER FLIGHT CONTROLS 1J17...
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Страница 297: ...CHAPTER FUEL 2A18...
Страница 320: ...CHAPTER HYDRAULIC POWER 2B17...
Страница 355: ...CHAPTER LANDING GEAR 2D4...
Страница 418: ...CHAPTER LIGHTS 2F19...
Страница 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Страница 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Страница 464: ...CHAPTER VACUUM SYSTEM 2H17...
Страница 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Страница 477: ...CHAPTER STRUCTURES 2I6...
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Страница 496: ...CHAPTER DOORS 2J1...
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Страница 505: ...CHAPTER STABILIZERS 2J10...
Страница 514: ...CHAPTER WINDOWS 2J19...
Страница 519: ...CHAPTER WINGS 2J24...
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Страница 550: ...CHAPTER PROPELLER 3A18...
Страница 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Страница 568: ...CHAPTER POWER PLANT 3B12...
Страница 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Страница 611: ...CHAPTER IGNITION 3D7...
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Страница 655: ...CHAPTER ENGINE INDICATING 3F16...
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Страница 664: ...CHAPTER EXHAUST 3G1...
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Страница 669: ...CHAPTER OIL SYSTEM 3G6...
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Страница 673: ...CHAPTER STARTING 3G10...
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Страница 688: ...CHAPTER TURBINES 3H1...
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Страница 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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Страница 739: ...CHAPTER 95 SPECIAL PURPOSE EQUIPMENT 3K1...
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