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Pilot's Operating Handbook
ENT
SEL ALR
DH
VS BARO
ALT

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Summary of Contents for S-TEC ST 360 ALT

  • Page 1 Pilot’s Operating Handbook SEL ALR VS BARO...
  • Page 2 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 Oct 26, 00 Jan 15, 08...
  • Page 3 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 4: Table Of Contents

    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 Selector / Alerter Operation..............3–3 3.1.1 Data Entry................3–3 3.1.2 Barometric (BARO) Calibration........3–3 3.1.3 Altitude (ALT) Select............3–4 3.1.4 Vertical Speed (VS) Select..........3–5 3.1.5 Decision Height (DH) Select..........3–7 3.1.6...
  • Page 5 S–TEC List of Figures Fig. 1–1 ST-360 ALT / VS Selector / Alerter Block Diagram........1–5 2–1 Selector / Alerter Display, All Segments and Annunciations Appear..2–4 2–2 Selector / Alerter Display, Enter Barometric Correction......2–4 3–1 Selector / Alerter Display, Loss of Encoded Altitude........3–8 List of Tables Table 2–1...
  • Page 6: Overview

    S–TEC SECTION 1 OVERVIEW 2nd Ed. Jan 15, 08...
  • Page 7 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 8: Document Organization

    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-360 Altitude (ALT) / Vertical Speed (VS) Selector / Alerter. Note: This POH must be carried in the A/C and made available to the pilot at all times.
  • Page 9: Block Diagram

    S–TEC The Encoding Altimeter / Blind Encoder sends the encoded altitude to the Selector / Alerter. The encoded altitude must be converted to the true altitude, through barometric calibration. The selected altitude and selected vertical speed must be programmed into the Selector / Alerter.
  • Page 10: St-360 Alt / Vs Selector / Alerter Block Diagram

    S–TEC Fig. 1-1. ST-360 ALT / VS Selector / Alerter Block Diagram 2nd Ed. Jan 15, 08...
  • Page 11 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 12: Pre-Flight Procedures

    S–TEC SECTION 2 PRE-FLIGHT PROCEDURES 2nd Ed. Jan 15, 08...
  • Page 13 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 14: Pre-Flight Test

    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.
  • Page 15: Selector / Alerter Display, All Segments And Annunciations Appear

    S–TEC Fig. 2-1. Selector / Alerter Display, All Segments and Annunciations Appear Fig. 2-2. Selector / Alerter Display, Enter Barometric Correction 2nd Ed. Jan 15, 08...
  • Page 16 S–TEC Table 2-1. Pre-Flight Test (continued from page 2-3) ACTION RESPONSE 8. Set Altimeter to posted airport ------ elevation. 9. Rotate Selector / Alerter Modifier ------ Knob as required, until barometric pressure (inches of mercury) on display matches that shown Kollsman scale of Altimeter.
  • Page 17 S–TEC Table 2-1. Pre-Flight Test (continued from page 2-5) ACTION RESPONSE 16. Press Autopilot mode annunciation appears selector switch to engage heading Autopilot display. mode. Note: This may not apply to the System Sixty PSS. 17. Press/Hold Autopilot VS mode ALT and VS annunciations appear on selector switch, and then press ALT Autopilot display.
  • Page 18: In-Flight Procedures

    S–TEC SECTION 3 IN-FLIGHT PROCEDURES 2nd Ed. Jan 15, 08...
  • Page 19 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 20: Selector / Alerter Operation

    S–TEC 3.1 Selector / Alerter Operation 3.1.1 Data Entry Press the DTA switch, such that ENT is annunciated. Any of the following quantities can now be entered into the Selector / Alerter: Barometric Calibration (reference section 3.1.2) Selected Altitude (reference section 3.1.3) Selected Vertical Speed (reference section 3.1.4) Selected Decision Height (reference section 3.1.5) Whenever ENT is annunciated, the Selector / Alerter is decoupled from the...
  • Page 21: Altitude (Alt) Select

    S–TEC Once the barometric pressure setting has been entered, press the DTA switch to make it operational, such that the ENT annunciation is extinguished and the BARO annunciation stops flashing. To change the barometric setting at times other than immediately following power-up, press the DTA switch such that ENT is annunciated.
  • Page 22: Vertical Speed (Vs) Select

    S–TEC 3.1.4 Vertical Speed (VS) Select Press the VS switch. The VS annunciation will appear, along with the selected vertical speed. The latter appears as a number in units of FPM x 100, prefixed by either a "+" to indicate a climb, or a "-" to indicate a descent (i.e., for example, +5 indicates 500 FPM climbing).
  • Page 23 S–TEC Suppose that the aircraft is at an initial altitude of 10,000 FT, with a selected vertical speed of 1600 FPM climbing and a selected altitude of 11,100 FT. The scheduled reduction in vertical speed will be as follows: Altitude (FT) Vertical Speed (FPM) 10,000 1600...
  • Page 24: Decision Height (Dh) Select

    S–TEC 3.1.5 Decision Height (DH) Select This selection activates both an audible alert and a visual alert, first when entering and then when departing a 100 FT window about the actual decision height. The actual decision height does not have to be at the center of this window.
  • Page 25: Loss Of Encoded Altitude

    S–TEC 3.1.7 Loss of Encoded Altitude Should the encoded altitude at the input of the Selector / Alerter ever be lost (i.e., interrupted), then a two-tone audible alert will sound 3 times, while the displayed altitude is replaced by flashing dashes as shown in Fig. 3-1. Thereafter, these dashes stop flashing but remain.
  • Page 26: Autopilot Operation

    S–TEC 3.2 Autopilot Operation Program the Selector / Alerter for the selected vertical speed and selected altitude. On the autopilot, press/hold the VS mode selector switch and then press the ALT mode selector switch, to engage the vertical speed mode and arm the altitude hold mode.
  • Page 27 S–TEC Page Intentionally Blank 3-10 2nd Ed. Jan 15, 08...
  • Page 28: Operating Parameters

    S–TEC SECTION 4 OPERATING PARAMETERS 2nd Ed. Jan 15, 08...
  • Page 29 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 30: Ranges

    S–TEC 4.1 Ranges Altitude (ALT) Select Range 0.0 to 35.9 Thousand FT Altitude Alerter (ALR) Function Range 0.0 to 35.9 Thousand FT Barometric (BARO) Calibration Range 27.9 to 32.0 inHg 945 to 1083 m b Decision Height (DH) Select Range 0.0 to 35.9 Thousand FT Vertical Speed (VS) Select Range Selector / Alerter PN 01279-PX: 1600 FPM Climbing or Descending...
  • Page 31 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 32: Glossary

    S–TEC SECTION 5 GLOSSARY 2nd Ed. Jan 15, 08...
  • Page 33 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 34 S–TEC Term Meaning Aircraft Aircraft Flight Manual AFMS Aircraft Flight Manual Supplement Alerter Altitude Barometric BARO Barometric Counter-Clockwise Clockwise Directional Gyro Decision Height Down Data Enter Federal Aviation Administration Flight Level Feet–per–Minute Feet Heading Horizontal Situation Indicator Instrument Flight Rules Increment inHg Inches of Mercury...
  • Page 35 S–TEC Page Intentionally Blank 2nd Ed. Jan 15, 08...
  • Page 36 Information contained in this document is subject to change without notice. © 2008 S-TEC. All rights reserved. Printed in the United States of America. S-TEC and the S-TEC logo are registered trademarks of S-TEC. Notice: Contact S-TEC Customer Support at 800-872-7832 for a Service Repair Order (SRO) number prior to the return of any component for any reason.

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