FLAPS (cont.)
(c) To install flap torque tube assembly (cont.):
8 Connect cable ends to torque tube pulley assembly and secure with cotter pins.
9 Connect electrical connections to limit switches mounted to torque tube switch plate.
10 Connect left and right flap control tubes (rods) either:
a At flaps by installing nuts, washers and bolts at torque tube cranks (arms) or by;
b. Installing bolts and washers to inner side of each crank. Install bolt through a hole in
the fuselage side skin located over torque tube .
11 Install access plate located between underside of aft section of each wing and fuselage by
installing attaching screws.
1 2 Install floor panel located aft of main spar and secure with screws
1 3 Install center seats and seat belt attachments.
14 Retract flaps.
(3) Rigging and Ajustment of Electrically Operated Wing Flaps:
(a) To Rig Control Cable:
1 Loosen lever cable clamp nut so that cable can move freely through cable clamp. Secure
lever in the full down position. (Refer to Figure 30).
2 Position the swash plate assembly on torque tube and secure inplace. (Refer to Figure 30.)
3 Loosen cable housing clamps at pulley support channel. Adjust cable tension so that a
5 ± 0.5 pound pull midway between cable housing clamps and swash plate assembly will
deflect the cable 0.38 inch from relaxed position. Tighten cable housing clamp. (Refer to
4 Tighten lever cable lamp nut so that cable is compressed to 1/2 its full diameter. (Refer to
Flap Selector and Cable Assembly
Figure 30
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
27-50-00
Page 27-55
Reissued: July 1, 1993
2D5
SELECTOR
ASSEMBLY
LEVER CABLE
CLAMP NUT
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 ...