Airplane Flight Manual

control and overpower electric trim to stop trim action. Operate each half of the trim switch separately trim should not operate unless both switch knob segments together. - - - are moved Trim when With Trim Operating Depress trim interrupt switch. motion should stop while interrupt switch is depressed released trim should operate normally. FAA/DAS APPROVED P/N: 891138 DATE: 1-5-95 Page 5 of 8 Autotrim S-TEC CORPORATION MINERAL WELLS, TEXAS 76067 FAA/DAS APPROVED PILOT'S OPERATING HANDBOOK AND/OR AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR CESSNA MODELS 210N AND T210N AND THESE MODELS WHEN MODIFIED PER STC SA756NW (ROBERTSON STOL) a. b. C. P - After Engage HDG and VS modes of the autopilot. Grasp control and apply forward pressure (NOSE DOWN) approximately three (3) seconds trim should run NOSE UP. Apply aft approximately three (3) seconds trim should run NOSE DOWN. pressure control wheel (NOSE switch UP) to UP or DN in the Autopilot commanded after should direction. trim operates will disconnect autopilot only when pitch is Move manual trim disconnect and (Trim Switch engaged.) e. Reengage autopilot £ auto HDG may be and VS Modes - and depress Autopilot should disconnect. Check all controls for freedom Trim Interrupt/AP Disconnect Switch Retrim aircraft for take-off of motion and to determine that the autopilot and trim have disconnected. If either the manual the above check procedure, electric or autotrim fails any portion of attempt to use the trim system until the fault is corrected. move the Trim Master Switch "OFF" and do not Trim Master Switch "OFF" the autopilot trim indicators and audio system will return to operation. With the failure in flight the system will automatically revert to the indicator If the electric trim system suffers a power If this using the indicators until the fault Occurs turn the Trim Master Switch can be lights and audio horn. "OFF" and trim manually, located and corrected. FAA/DAS APPROVED P/N: 891138 DATE: 1-5-95 Page 6 of 8 S-TEC CORPORATION MINERAL WELLS, TEXAS 76067 PILOT'S OPERATING HANDBOOK AND/OR FAA/DAS APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR CESSNA MODELS 210N AND T210N AND THESE MODELS WHEN MODIFIED PER STC SA756NW (ROBERTSON STOL) GLIDE SLOPE FLIGHT PROCEDURE 10° Approach the GS intercept point (usually the OM) with the flaps set to approach deflection of aircraft stabilized intercept, (See Limitations Section) in altitude hold mode. At the descent speed. lower the landing gear and adjust power for the desired and with the small, smooth increments to maintain desired airspeed. For best tracking results make power adjustments in glide slope approach point or landing or for the go-around maneuver (See Limitations Section). the decision height, disconnect the autopilot for At the missed missed approach is required, the autopilot may be reengaged after the aircraft has been reconfigured for climb. and established in a stabilized OPTIONAL EQUIPMENT ALTITUDE SELECTOR/VERTICAL SPEED SELECTOR P/N 0114 (OPTIONAL) refer to For and If a The altitude selector option operates in conjunction with an altitude encoder and transponder. procedures pre-flight normal the operating Selector and Altitude Vertical Speed Selector", P/N 8702, dated 2-91. "Pilot's Operating Handbook for Altitude This option does not affect the limitations or emergency procedures section of this supplement. ALTITUDE SELECTOR/ALERTER/VERTICAL SPEED SELECTOR P/N 0140 (OPTIONAL) The altitude selector/alerter option is a digital device providing a digital liquid crystal display of the selected altitudė, the vertical speed and other functions. The altitude selector function operates in conjunction with an altitude encoder and transponder. For pre-flight and Operating This normal operating procedures refer to the "Pilot's Handbook for Altitude Selector/Alerter", P/N 8716, dated 10-93. option does not affect the limitations or emergency procedures section of this supplement. FAA/DAS APPROVED P/N: 891138 Page 7 of 8 DATE: 1-5-95 NOTE: SECTION V S-TEC CORPORATION MINERAL WELLS, TEXAS 76067 FAA/DAS APPROVED PILOT'S OPERATING HANDBOOK AND/OR AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR CESSNA MODELS 210N AND T210N AND THESE MODELS WHEN MODIFIED PER STC SA756NW (ROBERTSON STOL) When using either of the above referenced Altitude Selectors with the System 55 Autopilot, the pilot should always program the desired altitude and vertical speed into the altitude selector before simultaneously pressing ALT and VS modes on the System 55 Autopilot programmer. This action will isolate the VS selector knob on the autopilot and the aircraft will respond only to the respective altitude selector commands until capturing the desired altitude. OPERATIONAL DATA The text of this Section not affected by the installation of this equipment. SECTION VI REQUIRED OPERATING EQUIPMENT The text of this Section not affected by installation of this equipment. SECTION VII WEIGHT AND BALANCE The tex this fect by IEC VALO birot nbbTEWEN I equipmen FAA/DAS APPROVED P/N: 891138 DATE: 1-5-95 Page 8 of 8