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S–TEC * Asterisk indicates pages changed, added, or deleted by List of Effective Pages current revision. Retain this record in front of handbook. Upon receipt of a Record of Revisions revision, insert changes and complete table below. Revision Number Revision Date Insertion Date/Initials Mar 14, 00 Dec 13, 00...
S–TEC Table of Contents Sec. Overview......................1–1 Document Organization..............1–3 Purpose....................1–3 General Control Theory..............1–3 Block Diagram..................1–4 Pre-Flight Procedures...................2–1 Pre-Flight Test..................2–3 In-Flight Procedures..................3–1 Normal Operating Procedures............3–3 3.1.1 Heading (HDG) Mode............3–3 3.1.2 Global Positioning System Steering (GPSS) Mode..3–3 Approach Procedures...............3–4 3.2.1 Standard Approach.............3–4 3.2.2 GPS Overlay of VOR / DME-A Approach......3–4 3.2.3 GPS-T Approach..............3–4...
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S–TEC List of Figures Fig. 1–1 HDG / GPSS Selector Switch...............1–5 1–2 ST-901 GPSS Converter Block Diagram...........1–5 2–1 HDG / GPSS Selector Switch (Pre-Flight)..........2–4 3–1 GPS Overlay of VOR / DME-A Approach............3–5 3–2 GPS-T Approach.....................3–6 3–3 GPS Approach with Holding Pattern............3–7 3–4...
Section 5 Glossary 1.2 Purpose This Pilot's Operating Handbook (POH) provides Pre-Flight and In-Flight operating procedures for the S-TEC ST-901 Global Positioning System Steering (GPSS) Converter. Note: This POH must be carried in the A/C and made available to the pilot at all times.
S–TEC It has the following modes of operation: HDG Mode - Used to turn onto a Selected Heading and Hold it GPSS Mode - Used to Laterally Steer along a Course defined by Waypoints, that have been programmed into the GPS Navigator Pressing the HDG / GPSS Selector Switch will alternately engage the HDG mode and GPSS mode.
S–TEC 2.1 Pre-Flight Test Prior to takeoff and with engine running, perform the actions shown in Table 2-1. For each action, verify the corresponding response where applicable. Table 2-1. Pre-Flight Test (continued on page 2-4) ACTION RESPONSE 1. Set Battery Master Switch to ON ------ position.
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S–TEC Table 2-1. Pre-Flight Test (continued from page 2-3) ACTION RESPONSE 10. Press HDG / GPSS Selector GPSS lamp is illuminated and HDG Switch. lamp is extinguished on HDG / GPSS Selector Switch, as an indication that GPSS Converter’s GPSS mode is engaged.
S–TEC 3.1 Normal Operating Procedures 3.1.1 Heading (HDG) Mode Set the Heading Bug to the desired heading on the compass card (HSI or DG). Engage the GPSS Converter's HDG mode. Engage the autopilot's HDG mode. The autopilot will turn the aircraft onto the selected heading and hold it. The turn rate will be limited to 90% of a standard rate turn, although for some higher performance (turboprop) aircraft this is 75%.
S–TEC 3.2 Approach Procedures 3.2.1 Standard Approach Set the Heading Bug under the Lubber Line. Engage the GPSS Converter's HDG mode. Engage the autopilot's HDG mode. Program the GPS Navigator with the desired approach. Engage the GPSS Converter's GPSS mode. The autopilot will begin tracking to the Initial Approach Fix (IAF).
S–TEC 1. a. Set the Heading Bug under the Lubber Line. b. Engage the GPSS Converter's HDG mode. c. Engage the autopilot's HDG mode. d. Program the GPS Navigator with the desired approach. e. Engage the GPSS Converter's GPSS mode. f.
S–TEC 1. a. Set the Heading Bug under the Lubber Line. b. Engage the GPSS Converter's HDG mode. c. Engage the autopilot's HDG mode. d. Program the GPS Navigator with the desired approach. e. Engage the GPSS Converter's GPSS mode. f.
S–TEC 1. a. Set the Heading Bug under the Lubber Line. b. Engage the GPSS Converter's HDG mode. c. Engage the autopilot's HDG mode. d. Program the GPS Navigator with the desired approach. e. Engage the GPSS Converter's GPSS mode. f.
S–TEC 1. a. Set the Heading Bug under the Lubber Line. b. Engage the GPSS Converter's HDG mode. c. Engage the autopilot's HDG mode. d. Program the GPS Navigator with the desired approach. e. Engage the GPSS Converter's GPSS mode. f.
S–TEC 3.3 Emergency Procedures In the event of a GPSS Converter malfunction, proceed as follows: 1. Disconnect the autopilot. 2. Regain control of the aircraft. 3. Do Not attempt to use the GPSS Converter's HDG mode or GPSS mode. 4. Do Not attempt to use the autopilot's HDG mode. Note: It may be possible to use other autopilot roll modes (i.e., NAV, APR, REV, STB, LO TRK, HI TRK).
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S–TEC Term Meaning Alternating Current Aircraft Aircraft Flight Manual AFMS Aircraft Flight Manual Supplement Approach Direct Current Directional Gyro Distance Measuring Equipment Federal Aviation Administration Final Approach Fix Global Positioning System GPSS Global Positioning System Steering Heading HI TRK High Track Horizontal Situation Indicator Initial Approach Fix Instrument Flight Rules...