STABILATOR CONTROL SYSTEM (cont.)
(1) To check and set the correct degree of stabilator travel (cont.):
(d) If stabilator travel is not correct in either the up or down position:
1 Remove tail cone by removing the attachment screws.
2 With use of rigging tool and bubble protractor, turn stops located at each stabilator hinge
in or out to obtain correct degree of travel. (Refer to Figure 21.)
3 Check that locknuts of stop screws are secure.
4 Install the tail cone.
(2) To check and set stabilator control cable tension:
(a) Check that stabilator travel is correct.
(b) Remove access panel to aft section of fuselage and tail cone.
(c) Position and secure tee bar (control column) 1/2 inch ± 1/4 inch off forward tee bar stop .
(d) Check each stabilator control cable for correct tension as given in Figure 20.
(e) If tension is not correct, loosen turnbuckle of
lower
cable in aft section of fuselage and adjust
turnbuckle of
upper
cable to obtain correct tension. Cable tension should be obtained with
control wheel one-quarter inch dimension from stop and stabilator contacting its stop.
(f) With the tension of upper cable correct and control wheel still forward, adjust the turnbuckle
of
lower
cable to obtain correct tension.
(g) Check safety of all turnbuckles and bolts.
(h) Check the full travel of the control wheel with relation to the full travel of the stabilator.
Determine that stabilator contacts its stop before control wheel contacts its stops. Move con-
trol wheel to full fore and aft positions. Travel distance from point where stabilator contacts
its stops, and control wheel contacts its stops, should be approximately equal. Adjust turn-
buckles if incorrect.
I.
Install access panels and tail cone.
Stabilator Travel Adjustments
Figure 21
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
27-30-00
Page 27-37
Reissued: July 1, 1993
2C11
1
1. STABILATOR TRAVE L ADJUSTM ENT
Summary of Contents for PA-32R-301T SARATOGA S
Page 26: ...CHAPTER 4 AIRWORTHINESS LIMITATIONS 1C1 ...
Page 29: ...CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS 1C4 ...
Page 53: ...CHAPTER 6 DIMENSIONS AND AREAS 1D6 ...
Page 64: ...CHAPTER 7 LIFTING AND SHORING 1D21 ...
Page 68: ...CHAPTER 8 LEVELING AND WEIGHING 1E1 ...
Page 72: ...CHAPTER 9 TOWING AND TAXIING 1E5 ...
Page 76: ...CHAPTER 10 PARKING AND MOORING 1E9 ...
Page 80: ...CHAPTER 11 REQUIRED PLACARDS 1E13 ...
Page 92: ...CHAPTER 12 SERVICING 1F1 ...
Page 126: ...CHAPTER 20 STANDARD PRACTICES AIRFRAME 1G17 ...
Page 127: ...THIS PAGE INTENTIONALLY LEFT BLANK ...
Page 139: ...CHAPTER 21 ENVIRONMENTAL SYSTEMS 1H5 ...
Page 188: ...CHAPTER 22 AUTOFLIGHT 1J7 ...
Page 193: ...CHAPTER 23 COMMUNICATIONS 1J12 ...
Page 203: ...CHAPTER 24 ELECTRICAL POWER 1J22 ...
Page 263: ...CHAPTER 25 EQUIPMENT FURNISHINGS 2A13 ...
Page 269: ...CHAPTER 27 FLIGHT CONTROLS 2A20 ...
Page 332: ...CHAPTER 28 FUEL 2D11 ...
Page 363: ...CHAPTER 29 HYDRAULIC POWER 2E18 ...
Page 404: ...CHAPTER 30 ICE AND RAIN PROTECTION 2G16 ...
Page 470: ...CHAPTER 32 LANDING GEAR 3A13 ...
Page 550: ...CHAPTER 33 LIGHTS 3D24 ...
Page 562: ...CHAPTER 34 NAVIGATION AND PITOT STATIC 3E12 ...
Page 582: ...CHAPTER 35 OXYGEN 3F8 ...
Page 604: ...CHAPTER 37 VACUUM 3G6 ...
Page 616: ...CHAPTER 39 3G18 ELECTRIC ELECTRONIC PANELS MULTIPURPOSE PARTS ...
Page 620: ...CHAPTER 51 STRUCTURES 3G22 ...
Page 636: ...CHAPTER 52 DOORS 3H14 ...
Page 650: ...CHAPTER 55 STABILIZERS 3I4 ...
Page 662: ...CHAPTER 56 WINDOWS 3I16 ...
Page 670: ...CHAPTER 57 WINGS 3I24 ...
Page 688: ...CHAPTER 61 PROPELLER 3J18 ...
Page 704: ...CHAPTER 70 STANDARD PRACTICES ENGINES 3K10 ...
Page 708: ...CHAPTER 71 POWER PLANT 3K14 ...
Page 737: ...CHAPTER 73 ENGINE FUEL SYSTEM 4A13 ...
Page 749: ...CHAPTER 74 IGNITION 4B1 ...
Page 783: ...CHAPTER 77 ENGINE INDICATING 4C11 ...
Page 793: ...CHAPTER 78 EXHAUST 4C21 ...
Page 801: ...CHAPTER 79 OIL 4D5 ...
Page 805: ...CHAPTER 80 STARTING 4D9 ...
Page 819: ...CHAPTER 81 TURBINES 4D23 ...
Page 833: ...CHAPTER 91 CHARTS WIRING DIAGRAMS 4E13 ...