Piper PA-34-200T Seneca II, Service Manual

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PIPER SENECA II SERVICE MANUAL
01/01/09 V - SURFACE CONTROLS
1F23
The wing flap system consists of an operating handle, a cable routed from the handle to a torque
tube and push-pull rods. Through the push-pull rods and torque tube, the flaps are interconnecting
and can be positioned in three locations of 10, 25 and 40 degrees.
5-2a. FLIGHT CONTROL SURFACE TRAVEL
See Table V-I for specifications, see appropriate section for rigging instructions.
5-2b. FLIGHT CONTROL CABLE TENSION
CAUTION: CABLE TENSIONS GIVEN IN TABLE V-I APPLY ONLY TO AIRPLANES WITHOUT
AUTOPILOT BRIDLE CABLE INSTALLATIONS. IF AN AUTOPILOT USING BRIDLE
CABLES HAS BEEN INSTALLED, CONSULT THE APPROPRIATE AUTOPILOT
VENDOR PUBLICATION FOR CORRECT CABLE TENSIONS WITH AUTOPILOT
BRIDLE CABLES ATTACHED.
a. See Table V-I for specifications; see appropriate section for rigging instructions.
b. When a new cable is installed, cable tension must be rechecked after flight test.
TABLE V-II. CABLE TENSION VS. AMBIENT TEMPERATURE
(PIR-PPS50009-2)
120
110
100
90
80
70
60
50
40
30
20
-10 -8 -6 -4 -2 0 2 4 6 8 10
Add
Rigging Load Correction, Pounds
Subtract
T
emperature
, Degrees F
ahrenheit (°F)