Technical data

13773-001
22-10
Page 2 31 July 2001
C. Altitude Transducer (See Figure 22-101)
(1) Removal - Altitude Transducer
(a) Ensure BAT 1, BAT 2, and AVIONICS master switches are in off position.
(b) Pull AUTOPILOT circuit breaker.
(c) Remove MFD. (Refer to 34-40)
(d) Disconnect cable from altitude transducer.
(e) Disconnect static line from altitude transducer.
(f) Remove screws and washers securing altitude transducer to console rib.
(g) Remove altitude transducer from airplane.
(2) Installation - Altitude Transducer
(a) Align altitude transducer over console rib mounting holes and secure with washers and
screws.
(b) Connect static line to attitude transducer.
(c) Connect cable to altitude transducer.
(d) Perform Pitot System Leakage Test. (Refer to 34-10)
(e) Perform Static System Leakage Test. (Refer to 34-10)
(f) Install MFD. (Refer to 34-40)
(g) Reset AUTOPILOT circuit breaker.
D. Autopilot Disconnect Switch
The autopilot disconnect switch is integral to the 4-way trim switch on the control yoke. For mainte-
nance practices pertinent to the control yoke, see Flight Controls. (Refer to 27-10)