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Flight Control Products & Systems Full-function Two-Axis Flight Control System The System Fifty Five X is a high-performance, 2-axis (roll & pitch) autopilot in an avionics stack-mounted case, containing the mode selector/programmer, annunciator, roll & pitch computers, and servo amplifiers. HDG (heading) mode – heading pre-select and hold*. When HDG & NAV are activated simulta- neously, enables Dual Mode Intercept – autopilot operates in heading mode to automatically intercept and track selected course or localizer; at which point HDG extinguishes. NAV (coupled navigation) mode – automatic intercept and tracking of enroute NAV signals (VOR/GPS), or LOC (REV for backcourse). 3-level gain selection for NAV mode is automatic. When APR is lit (simulta- neous with NAV), indicates high gain localizer mode for high sensitivity coupled approach. Flashing NAV or REV annunciates course deviation by a needle deflection of 50% or more. Selecting APR increases gain sensitivity for VOR or GPS approaches. Pitch modes include: VS, indicating vertical speed control has been selected; ALT, indicating altitude hold is engaged, capturing existing alti- tude when activated; and GS, indicating glide slope coupling is armed and/or active. In altitude hold mode, altitude can be adjusted (trimmed) in 20' increments using VS knob. TRIM & arrows annunciate motion of auto trim or manual electric trim, if equipped; if not equipped, annunciates out-of-pitch-trim condition. Mode selector buttons for HDG (heading hold and head- ing pre-select*), NAV (tracking VOR enroute), APR higher gain for GPS enroute, and LOC, VOR & GPS approaches), REV (LOC backcourse), ALT (altitude) hold, and VS (vertical speed) command. Control Wheel Steering (CWS) – allows you to hand-fly the aircraft and then let the autopilot take- over to hold the existing turn rate and vertical speed; can be over- ridden and hand flown, then re-engaged. Digital vertical speed in 100' increments. GPSSby S-TEC (GPS Steering) integrates A/P with GPS Navigator function, which outputs roll steering commands. GPSS does not follow a CDI needle movement; it acts on direct left/right steering com- mands from the Navigator for extremely accurate, hands-off GPS navigation. See separate GPSS data sheet for details. S-TEC’s flagship autopilot system, the System Fifty Five X replaces the System 55, and incorporates these performance enhancements: New Display – LCD display now black-on-silver for greater contrast and significantly improved readability. GPSSby S-TEC (GPS Roll Steering) – flies the composite roll steering com- mands output by the newer GPS Navigators, for enroute navigation and limited approach/transition procedures such as DME arcs. GPS manu- facturers are currently expanding their databases and software to include full procedure approaches, transitions to approaches, procedure turns, holding patterns and more. Lift Compensation in Turns – holds altitude more precisely in A/P com- manded turns, with little or no loss of altitude. Heading Intercepts – newly commanded headings, even in large changes, result in minimal or no S-turning to accomplish intercept. Course Intercepts – enhanced by improved reaction to varying closure rates during leg changes. ILS Coupling Performance – as a result of the above enhancements, coupled performance on ILS Approaches is dramatically better. Flight Director Performance – improved so the pilot is able to hand fly the airplane more precisely in response to commands from the system. Please see the reverse side for a system schematic, and detailed features, functions and options.

Flight Control Products & Systems Full-function Two-Axis ...vonesh.com/pdf_files/sys55X.pdfseparate GPSS data sheet for details. S-TEC’s flagship autopilot system, the System Fifty

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Page 1: Flight Control Products & Systems Full-function Two-Axis ...vonesh.com/pdf_files/sys55X.pdfseparate GPSS data sheet for details. S-TEC’s flagship autopilot system, the System Fifty

Flight Control Products & Systems

Full-function Two-Axis Flight Control SystemThe System Fifty Five X is a high-performance, 2-axis (roll & pitch) autopilot in an avionics stack-mountedcase, containing the mode selector/programmer, annunciator, roll & pitch computers, and servo amplifiers.

HDG (heading) mode – headingpre-select and hold*. When HDG

& NAV are activated simulta-neously, enables Dual Mode

Intercept – autopilot operates inheading mode to automatically

intercept and track selectedcourse or localizer; at which

point HDG extinguishes.

NAV (coupled navigation) mode – automaticintercept and tracking of enroute NAVsignals (VOR/GPS), or LOC (REV forbackcourse). 3-level gain selection for NAVmode is automatic. When APR is lit (simulta-neous with NAV), indicates high gain localizermode for high sensitivity coupled approach.Flashing NAV or REV annunciates coursedeviation by a needle deflection of 50% ormore. Selecting APR increases gain sensitivityfor VOR or GPS approaches.

Pitch modes include: VS, indicating verticalspeed control has been selected; ALT, indicatingaltitude hold is engaged, capturing existing alti-tude when activated; and GS, indicating glideslope coupling is armed and/or active. In altitudehold mode, altitude can be adjusted (trimmed) in20' increments using VS knob.

TRIM & arrows annunciate motion of auto trim ormanual electric trim, if equipped; if not equipped,

annunciates out-of-pitch-trim condition.

Mode selector buttons forHDG (heading hold and head-ing pre-select*), NAV (tracking

VOR enroute), APR highergain for GPS enroute, and

LOC, VOR & GPSapproaches), REV (LOC

backcourse), ALT (altitude)hold, and VS (vertical

speed) command.

Control Wheel Steering (CWS) –allows you to hand-fly the aircraftand then let the autopilot take-over to hold the existing turn rateand vertical speed; can be over-ridden and hand flown, thenre-engaged.

Digital vertical speedin 100' increments.

GPSSby S-TEC (GPS Steering) integrates

A/P with GPS Navigator function, whichoutputs roll steering commands. GPSSdoes not follow a CDI needle movement;it acts on direct left/right steering com-mands from the Navigator for extremelyaccurate, hands-off GPS navigation. Seeseparate GPSS data sheet for details.

S-TEC’s flagship autopilot system, the System Fifty Five X replaces theSystem 55, and incorporates these performance enhancements:

• New Display – LCD display now black-on-silver for greater contrast andsignificantly improved readability.

• GPSSby S-TEC (GPS Roll Steering) – flies the composite roll steering com-mands output by the newer GPS Navigators, for enroute navigation andlimited approach/transition procedures such as DME arcs. GPS manu-facturers are currently expanding their databases and software to includefull procedure approaches, transitions to approaches, procedure turns,holding patterns and more.

• Lift Compensation in Turns – holds altitude more precisely in A/P com-

manded turns, with little or no loss of altitude.

• Heading Intercepts – newly commanded headings, even in large changes,result in minimal or no S-turning to accomplish intercept.

• Course Intercepts – enhanced by improved reaction to varying closurerates during leg changes.

• ILS Coupling Performance – as a result of the above enhancements,coupled performance on ILS Approaches is dramatically better.

• Flight Director Performance – improved so the pilot is able to hand flythe airplane more precisely in response to commands from the system.

Please see the reverse side for a system schematic, and detailed features,functions and options.

Page 2: Flight Control Products & Systems Full-function Two-Axis ...vonesh.com/pdf_files/sys55X.pdfseparate GPSS data sheet for details. S-TEC’s flagship autopilot system, the System Fifty

© Copyright 2001 S-TEC Corporation All rights reserved.

Meggitt Avionics / S-TECOne S-TEC WayMunicipal AirportMineral Wells, TX 76067-9236

Tel: 940.325.9406 or Toll-free 800.872.7832Fax: 940.325.3904

www.S-TEC.com P/N 86212

Features/Functions

• Case-contained, radio stack mount• GPSS by S-TEC (GPS Roll Steering)• Heading Preselect & Hold• Altitude Hold with Altitude Trim• Course Intercept Capability

NAV ModeDual Mode – HDG/NAV & HDG/APR

• VOR/LOC/GS/REV/GPS Coupling with 3 Gain Levels• Selectable Coupling Gain• VOR/LOC/GS/REV/GPS Course Deviation and NAV

Flag Warning• Digital Vertical Speed Command

• Pitch Trim Annunciation• Control Wheel Steering

Options

• Directional Gyro with Heading Bug, Vacuum Driven• ST-180 HSI Slaved Compass System• ST-361 Single Cue Flight Director• ST-360 Altitude Selector/Alerter System• Remote Annunciator• Automatic or Manual Electric Trim (where STC’d)• Yaw Damper (where STC’d)

* Operational if optional heading system (e.g., DG or HSI with headingbug) is installed and active.