6. Remove stabilator control push rod from the fin by disconnecting attachment hardware at the balance
weight arm and at bellcrank.
7. Remove the two bolts at the leading edge of the fin.
8. Remove the eight bolts which secure the fin spar to the aft bulkhead. Remove the fin.
9. Install the fin in reverse of removal instructions. Check all bolts for safety. Refer to installation and
rigging of stabilator trim cable, and rudder cable for adjustment of cables.
RUDDER.
REMOVAL AND INSTALLATION OF RUDDER. (Refer to Figure 55-4.)
1. Remove the fairing.
2. Disconnect the rudder cables at the turnbuckles within the fuselage tail section and disconnect the
cable from the rudder sector.
3. While supporting the rudder, remove the hinge bolts and remove the rudder from the fin.
4. Install the rudder in reverse of removal instructions; check cable tension if disturbed.
BALANCING RUDDER. (Refer to Figure 55-5.)
To balance the rudder, the assembly must be complete including the rudder lower fairing assembly and all
attaching screws and the position light wiring. Place the complete assembly horizontally on knife edge
supports in a draft free area in a manner that allows unrestricted movement. Place the tool on the rudder with
the beam perpendicular to the hinge center line. Calibrate the tool as described in previous paragraph. Read the
scale when the bubble level has been centered by adjustment of the movable weight and determine the static
balance limit. If the static balance is not within the limits given, proceed as follows:
1. Nose Heavy: This condition is highly improbable; recheck calculations and measurements.
2. Nose Light: In this case, the mass balance weight is too light or the rudder is too heavy because of
painting; it will be necessary to strip the paint and repaint. If the rudder is too heavy as a result of repairs, the
repair must be removed and the damaged parts replaced.
55-40-02
Page 55-05
Revised: February 23, 1979
2J16
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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