E. Should tension be incorrect, loosen the turnbuckle of the lower cable in the aft section of the
fuselage and adjust the turnbuckle of the upper cable to obtain correct tension. Cable tension
should be obtained with the control wheel at the one-half + 1/4 inch dimension from the stop and
the stabilator contacting its stop.
F. Check safety of all turnbuckles and bolts.
G. With the tension of the upper cable correct and the control wheel still forward, adjust the
turnbuckle of the lower cable to obtain correct tension.
H. Check the full travel of the control wheel with relation to the full travel of the stabilator to
determine that the stabilator contacts its stops before the control wheel contacts its stops. With the
control wheel in the fore and aft positions, the travel distance from the point where the stabilator
contacts its stops and the control wheel contacts its stops should be approximately equal. Readjust
turnbuckles if incorrect.
I.
Reinstall access panels.
4. Remove the airplane from jacks.
STABILATOR TRIM CONTROLS.
REMOVAL OF STABILATOR TRIM ASSEMBLY. (Forward) (Refer to Figure 27-18.)
1. To remove the trim control wheel assembly and/or the trim control cables, first remove the panel to the
aft section of the airplane.
2. If the aft trim cable is not to be removed, block the cables at the pulleys in the upper aft section of the
fuselage to prevent them from unwrapping from the trim drum. (Refer to Figure 27-17.)
3. Loosen the cables if the trim control wheel is to be removed or disconnect if the cables are also to be
removed. Do this at the trim cable turnbuckles in the aft section of the fuselage.
4. The control wheel with drum may be removed by the following procedure:
A. Remove the control wheel cover by removing the cover attaching screws.
B. The wheel assembly may be removed from its mounting brackets by removing nut, washer and
bolt that secures the wheel between the brackets. Draw the wheel from the brackets. Use caution
not to damage trim indicator wire.
C. Unwrap the left cable from the drum.
D. The wheel and drum are joined by a push fit, separate these two items with their center bushing
and unwrap the right cable.
E. Tie the cables forward to prevent them from slipping back into the floor tunnel.
5. The trim control cables may be removed by the following procedure:
A. Remove the rear seat bottom or floor panel, whichever applies, and the front seats, if desired.
B. Unfasten the carpet from the aft portion of the floor tunnel and lay it forward.
C. Remove the tunnel cover located between the trim control wheel and the spar cover by removing
attaching screws.
D. Remove the cable pulleys located in the tunnel by removing the cotter pin, washer and clevis pin.
E. Remove the cable rub blocks located on the aft side of the main spar by removing the block
attaching screws.
F. Remove the cable guard pin at the pulley cluster located just aft of the wing flap torque tube at
station 127.25.
27-35-01
Page 27-32
Revised: February 23, 1979
1L3
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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