Safegate Group safedock User Manual
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Safegate Group safedock User Manual

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SAFEDOCK®
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Summary of Contents for Safegate Group safedock

  • Page 1 SAFEDOCK® Manual...
  • Page 2 Note: This page is blank for convenient double-sided printing.
  • Page 3 Operator Panel Softkey Setup Reference CHAPTER 3. OPERATION Reference Appendix A. Operation Procedures Reference Appendix B. Safedock Features Reference CHAPTER 4. MAINTENANCE Reference Appendix A. Stand Configuration Utility Reference Appendix B. Safedock Log Viewer Reference CHAPTER 5. DRAWINGS Reference Page 1 of 1...
  • Page 4 Digital countdown (including closing rate bar) configurable from max 30m or 98ft. Note: For type 3 is dig countdown available from max 20m. Safedock Maintenance Tool - SMT Yes or No More Options Battery backup (UPS) Yes or No Camera Yes or No Safedock Log Viewer –...
  • Page 5 Subsidiary Company Product/System Warranty Safegate Group guarantees that the performance of the Safegate Group product/system, when sold by Safegate Group or its licensed representatives, meets the requirements of and is in compliance with standards:  ICAO Annex 14 - Aerodromes Volume I - Aerodrome Design and Operations - 4th Edition July 2004 [5.3.24 Visual Docking guidance System].
  • Page 6 © Copyright 2012 by Safegate Group. All rights reserved. This item and the information contained herein are the property of Safegate Group. No part of this document may be reproduced, transmitted, transcribed, stored in a retrieval system, or translated into any language or computer language in any form or by any means otherwise, without the expressed written permission of Safegate Group, Djurhagegatan 19, SE-213 76 Malmö, Sweden.
  • Page 7 A description of procedures used for system operation and itemized docking. For example, an Operation Procedures Appendix (with instructions to pilots) gives an explanation of signs and signals in a Safedock system. A Features Appendix provides information about the optional operational features in the system.
  • Page 8 Version: 2.7 SAFETY INFORMATION Safedock system is an Advanced Visual Docking Guidance System, an aircraft parking aid for airport and aircraft safety and efficiency. The design is according to strict airport industry standards for the safety of, and use by authorised airport personnel.
  • Page 9 Symbol Safety Advisory Laser Safety Information Safedock system is a Class 1 laser product, which means that it is safe under foreseeable conditions of operation, including the use of optical instruments for intra beam viewing. The Laser Scanning Unit compartment of the Pilot Display unit contains a Laser Range Finder, which is a Class 1M laser product.
  • Page 10 Maintenance PC A PC used to run the Safedock Maintenance Tool. It can be a portable PC connected locally to a Safedock system, or a stationary PC connected to the units via LAN or through Superior System.
  • Page 11 Marshal or handling agent. Stand configuration file A complete configuration for a Safedock system can be stored on disk in a stand configuration file. This file can be used to review and/or to document the stand configuration. The file can also be used to restore the configuration for a in case of a hardware breakdown.
  • Page 12 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: INTRODUCTION Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 10 of 10...

  • Page 13: Table Of Contents

    2.1.3 Reliability Calculation................15 2.1.4 Technical Availability ................16 TECHNICAL DATA ..................... 17 PERFORMANCE .................... 17 SAFEDOCK UNITS DIMENSIONS AND WEIGHTS ........17 3.2.1 Safedock Main Unit .................. 17 3.2.2 Operator Panel ..................17 SUB UNIT CHARACTERISTICS ..............18 3.3.1 Power Unit ....................
  • Page 14 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 1 SYSTEM DESCRIPTION Version: 2.7 3.4.9 Acoustic Sound and Noise ..............20 3.4.10 Pollution Limits ..................20 3.4.11 Installation Over-voltage Limits ............. 20 ELECTROMAGNETIC COMPATIBILITY ............20 3.5.1 General ...................... 20 3.5.2...

  • Page 15: Equipment And System Description

    EQUIPMENT AND SYSTEM DESCRIPTION BRIEF SYSTEM ARCHITECTURE The figure 1.1 is an overview of the Safedock system and the following section is a brief description of the system and its sub units. 1. The Safedock main unit consists of a real time Pilot Display Unit, a Control Unit and a Laser Scanning Unit.
  • Page 16 Power Intensity control Supply Motor Climate control Control Serial ports Parallel ports I/O, Alarm 110-240V AC Single Phase Mother Board 50/60 Hz Central Unit RS 485 Laser Range Finder Laser Scanner FIGURE 1.1 SAFEDOCK SYSTEM OVERVIEW Page 4 of 20...

  • Page 17: Safedock System Sub-Units

    LED-boards. 1.3.2 Control Unit The Control Unit, located with, or inside the Safedock unit, comprises a motherboard with a microprocessor unit, and two stepper motor drive boards. It continuously monitors and controls the operation of the docking guidance system.

  • Page 18: Laser Scanning Unit

    Horizontal scanning mirror and stepper motor Laser Horizontal stepper motor and mirror Vertical mirror and stepper motor FIGURE 1.2 - SAFEDOCK T1 LASER SCANNING UNIT Vertical stepper motor and mirror Laser Horizontal stepper motor and mirror FIGURE 1.3 - SAFEDOCK T2/3 LASER SCANNING UNIT...
  • Page 19 Chapter: 1 SYSTEM DESCRIPTION Version: 2.7 The Laser Scanning Unit is housed in the lower part of the Safedock unit for model T2 & T3, and for T1 in the upper part. It is based on 3D-technology and consists of a Laser Range Finder, comprising both a transmitting and a receiving lens.

  • Page 20: Power Unit

    Optionally the Pilot Display Unit also has a heater to prevent moisture on the window during cold weather. 1.3.7 Operator Panel The Operator Panel is used to control the Safedock system from a location close to the Aircraft Loading Bridge. The Operator Panel, controlled Test...

  • Page 21: Operation

    Superior System. From the Superior System all connected systems can be individually controlled and monitored. b) In the Safedock system a number of aircraft types are configured by a set of parameters such as the nose profile etc. At start of docking an aircraft type is assigned by the operator.

  • Page 22: Safety With The Docking Procedure

    If the safety margin is too small, the display will show STOP ID FAIL, and the docking procedure will be automatically interrupted. The Safedock measures the position of the aircraft in relation to aircraft stand centre- line and the defined stop position for the particular aircraft type. During the tracking process the relative position of the aircraft is displayed on the Pilot Display unit, clearly visible from the whole cockpit area.
  • Page 23 4. Obstruction in the apron area for example PBB out of position or positioned for an incorrect aircraft type.  Safedock monitors the stand area for the selected aircraft type and displays information if there is an obstruction, for example Gate Blocked or STOP ID FAIL.
  • Page 24 1.4.2.5 Docking Other Aircraft Types (than the type selected) If another aircraft type than the selected type is accepted by the Safedock system into "Selected A/C" the stand, it is stopped with the nose at the same position where PLB red hatchet line "Other A/C"...
  • Page 25 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 1 SYSTEM DESCRIPTION Version: 2.7 1.4.2.6 Practical Aspects If another aircraft type than the type selected is accepted into the stand (discrimination criteria is not met), there is a risk to the normal parking position and stop position accuracy.

  • Page 26: Interfaces To Other Systems

    Chapter: 1 SYSTEM DESCRIPTION Version: 2.7 INTERFACES TO OTHER SYSTEMS The diagram below describes the general Safedock interfaces to external systems. These might be: a) Superior System (GOS/ SafeControl – Apron Management System) and related systems, such as FIDS/GMS and Central Maintenance Systems...

  • Page 27: System Availability/Line Replaceable Units

    Date: 6 February 2015 Chapter: 1 SYSTEM DESCRIPTION Version: 2.7 SYSTEM AVAILABILITY/LINE REPLACEABLE UNITS The table below contains all Line Replaceable Units (LRU) used in the Safedock system. For more information, see Chapter 5 DRAWINGS. 2.1.1.1 Availability and Reliability General Definitions...

  • Page 28: Technical Availability

    1.5/MTBF_Safedock = 1/MTBF_Cu + 1/MTBF_Cpu + 2/MTBF_Mcb + 2/MTBF_Led + 0.1/MTBF_Laser + 2/MTBF_Motor + 1/MTBF_Power + 0.25/MTBF_OPanel Using this formula, considering operating temperature and duty cycle, the calculated MTBF figure for the Safedock system would be 24 800 hours. 2.1.4 Technical Availability Suppose that continuous operation is 24 hours a day, and Mean Down Time (MDT) is 6 hours.

  • Page 29: Technical Data

    Note: This depends on configuration, LEDs. LED configuration (typical module totals) 42 (T1), 18, 24 (T2), 9, 15 (T3) Maximum separation - two centre lines 30° (T1), 18° (T2/3) SAFEDOCK UNITS DIMENSIONS AND WEIGHTS 3.2.1 Safedock Main Unit T1 Main Unit...

  • Page 30: Sub Unit Characteristics

    Safedock (power supply/control) glands: diameter is 9-13 mm. Safedock (OP communication) nut: diameter is 9-13 mm. Safedock communication (option such as GOS): diameter is 4-8 mm. Operator Panel (Safedock communication) nut: diameter is 8-13 mm. Operator Panel (option such as PBB) extra holes: diameter is 20.5 mm.

  • Page 31: Environmental Limits

    It is recommended that units are kept in the shipping box and in a dry covered storage area until installed for operation. 3.4.5 Wind Load The Safedock system is designed to resist damage in wind speed up to 44 m/s (no active operation). 3.4.6 Snow Load...

  • Page 32: Brightness

    3.4.9 Acoustic Sound and Noise The Safedock system is tested to meet a sound level not exceeding 45 dBA, relative a sound reference pressure of 2x10 Note: This information may be subject to change for T1 with a Supercooler option.
  • Page 33 Height Calculation ................... 12 3.1.3 Offset Calculation ..................13 3.1.4 Mounting of Support Fixture ..............13 3.1.5 Installation of the Safedock Unit ............15 3.1.6 Installation of the Operator Panel ............16 3.1.7 Calibration Check (Auto Calibration) ............. 16 ELECTRICAL INSTALLATION ................... 18 GENERAL .......................
  • Page 34 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 2 INSTALLATION Version: 2.7 CONFIGURATION PHASES ................23 PREPARATION ....................23 5.3.1 Prepare the Stand for Aircraft Stop-positions ........23 5.3.2 Prepare the Maintenance Computer ............25 5.3.3 Connect the Maintenance Computer to Operator Panel ...... 25 COMMUNICATION ..................

  • Page 35: Scope

    Manual Date: 6 February 2015 Chapter: 2 INSTALLATION Version: 2.7 SCOPE Installation of the Safedock System is performed in three phases and often by three different personnel categories: 1. Mechanical installation 2. Electrical installation 3. System configuration Note: This document is focused on the mechanical and electrical installations with system configuration, for example software set-up procedures briefly described with references to other sections or chapters in the manual.

  • Page 36: Installation Considerations

    Position. Mounting height FIGURE 2.1 MOUNTING HEIGHT Note: A Safedock unit overlooking a PBB or walkway may have operational constraints, which requires an adjusted mounting height and/or re-positioning of aircraft stop-positions to create an obstacle free scanning area. STOP-POSITION The longest recommended stop-position is 65.0 metres (T1) or 50 metres (T2/3).

  • Page 37: Centrelines

    CENTRELINES The Safedock system can handle up to three centrelines, convergent or parallel. For an accurate guidance the centrelines must be placed within the laser’s aircraft scanning range of the system. The limits for centreline position are defined according to the image below.

  • Page 38: Aircraft Safety Check

    1. Distances to the countdown area, to stop-position(s) and the Safedock unit. 2. A frontal view of the approaching aircraft from the Safedock unit which is unobstructed (laser scanning view). 3. The distance from the Safedock unit from which the incoming aircraft will appear while entering the stand area.

  • Page 39: Free Space On The Apron

    This is the maximum angle for a sector where foreign objects are allowed. VIEWING RANGE The Safedock unit must have an unobstructed view of the aircraft nose throughout the docking procedure. For additional features (such as ID-verification) to work properly, the viewing range must be extended so that it covers the particular needs of the feature.

  • Page 40: System Without Id-Verification

    The minimum clipping angle to each side of the centreline can be defined by finding a line from the Safedock unit to a point half the aircraft width from the centreline at the stop-position (nose) for the aircraft.
  • Page 41 The minimum viewing range that allows engine measurement is defined by finding the aircraft that needs the widest view according to:  = ArcTan( engineToCentre / (aircraftNosePos + 15 + engineToNose)) Example: A B777-200 with stop-position (nose) 30m from the Safedock unit aircraftNosePos = 30.0m engineToCenter = 9.7m engineToNose = 20.3m...

  • Page 42: Mechanical Installation

    When installed, the Safedock unit is usually mounted from 4 to 8 metres (12 to 24 feet, related to bottom edge of the unit) above ground. The actual mounting height...
  • Page 43 Date: 6 February 2015 Chapter: 2 INSTALLATION Version: 2.7 The figure below shows the Safedock unit rear view examples and the mounting hardware for a typical support fixture for mounting the unit. Note: For more information, for example Safedock types with other/more specific configuration options, see Chapter 5 DRAWINGS.

  • Page 44: Height Calculation

    If no acceptable mounting height at the desired position can be used, an alternative location for the Safedock may be necessary, for example a free standing pole. Note: It is important to always check with the Project Manager for the location, height and alignment requirements, for each Safedock installation.

  • Page 45: Offset Calculation

    OFFSET CALCULATION 3.1.4 Mounting of Support Fixture A support fixture is required for the Safedock unit to be attached to with clamps, for example a steel pipe Ø139.7 mm or 5 ½” in diameter. Clamps are supplied for these dimensions.
  • Page 46 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 2 INSTALLATION Version: 2.7 3.1.4.1 Maximum Allowable Deflection in Mounting The table below is a guideline to deflection when mounting on a support fixture. Deflection Guideline FIGURE 2.13 DEFLECTION GUIDELINE Max. allowable angle...

  • Page 47: Installation Of The Safedock Unit

    Chapter: 2 INSTALLATION Version: 2.7 3.1.5 Installation of the Safedock Unit (a) Check with the Project Manager for the exact height and alignment for every installation, as the stand requirements may differ. For example, verify alignment if mounted off-centre or if more than one centreline are to be used.

  • Page 48: Installation Of The Operator Panel

    3.1.7 Calibration Check (Auto Calibration) A Safedock system must be configured with two reference points. The system checks the calibration automatically for each docking or at regular intervals, according to the references and system settings. If fixed equipment at the aircraft stand cannot be used to obtain reference points (for example a fixed PBB section), a calibration plate can be installed to obtain reference points.
  • Page 49 SAFEDOCK® Manual Date: 6 February 2015 Chapter: 2 INSTALLATION Version: 2.7 The table below lists the scanning angles of the Safedock unit for the forward and the side scanning areas. Scanning Area Vertical Scanning Angle Horizontal Scanning Angle Forward area +15°;...

  • Page 50: Electrical Installation

    Version: 2.7 ELECTRICAL INSTALLATION GENERAL Cables for powering and operating the Safedock system must be run between the various sub-units of the system. It is also recommended to use UPS to avoid any power-down while a docking procedure commences, which is a critical time.

  • Page 51: Earthing The Safedock Housing

    The Safedock unit shall be connected to earth (the earth connection point is delivered by a third party), using an “earth bonding strap” with a conductor area of 25 mm , which shall be connected to the ground point on the rear of the Safedock housing. SAFEDOCK CONNECTION TO MAINS The mains supply should be routed from its conduit entry point via the routing channel to the pole circuit breaker (mains disconnect device).

  • Page 52: Communication Cable

    Cable Glands The Operator Panel unit includes three Ø20.5 mm holes, one with a cable gland for connection to the Safedock unit and two plugged holes for other connection options, if required. The Safedock unit includes two Ø20.5 mm holes with cable glands, one for connection to the Operator Panel and one for power.

  • Page 53: Cable Connection To Safedock Unit

    4.4.5 Cable Connection to Safedock Unit The cable from the Operator Panel shall be connected to terminals in the Safedock unit according to the drawings. Note: It is important to connect the shields directly to the chassis, where it enters the Safedock housing - or to a ground terminal.

  • Page 54: Other Connections (Options)

    Note: It is assumed that the PBB in question is capable to signal PBB location safe as well as to make use of the signal from Safedock that docking is in progress. It is recommended to use shielded twisted pair cabling (2x2x0.5 mm...

  • Page 55: System Configuration

    The set-up procedure at each stand is carried out using the Safedock Maintenance Tool. The Safedock Maintenance Tool can also be used to document each stand set- up. A copy per installed stand shall be stored for the customer’s approval during commissioning.
  • Page 56 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 2 INSTALLATION Version: 2.7 Aircraft Stop-Positions Stand/Gate Name/Number: Stop Distance - nose Aircraft Type(s) Stop Distance - nose Aircraft Type(s) wheel (unless noted) wheel (unless noted) Note: If notes are made on this page, please forward a copy to site management for safe keeping.
  • Page 57 Date: 6 February 2015 Chapter: 2 INSTALLATION Version: 2.7 5.3.2 Prepare the Maintenance Computer The following are required for a local connection to a Safedock system via an Operator Panel (supplied by Safegate, if requested):  Maintenance Computer – a portable computer ...
  • Page 58 5.4.1 Configuration of Ethernet Converter Build In on Control Card If communication to Superior System is required, each Safedock must be given an IP address and the corresponding network parameters. This is manually edited directly in the Operator Panel under the Test menu. See Chapter 2A Operator Panel Softkey Setup.
  • Page 59 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 2A Operator Panel Softkey Setup Version: 2.7 CHAPTER 2 INSTALLATION - APPENDIX A OPERATOR PANEL SOFTKEY SETUP (OPTION) CONTENTS Section Description Page No. SCOPE .......................... 3 CONTRAST ADJUSTMENT ..................3 NAVIGATING MENUS ....................4 ENTERING SETUP MODE ................
  • Page 60 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 2A Operator Panel Softkey Setup Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 2 of 8...

  • Page 61: Scope

    Emergency Stop message. When the contrast is as desired, press the Save key to store the value to non-volatile storage. If there are multiple Operator Panels connected to the same Safedock system, they all display the same text. However, each unit is managed separately; for example a contrast change only affects the unit on which keys are being pressed and settings are saved.

  • Page 62: Navigating Menus

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 2A Operator Panel Softkey Setup Version: 2.7 NAVIGATING MENUS ENTERING SETUP MODE To enter the setup menus: (a) Open the Operator Panel box and disconnect the J1 connector, to power off the unit.

  • Page 63: Lcd Contrast

    Valid addresses use variables: 1-4 (the default value is set to 1). Note: Each Operator Panel must have its own unique address. Using the same address in two or more units (extra Operator Panels) connected to a Safedock system gives unpredictable results. This parameter only affects Operator Panel units with software version 1.2 or later.

  • Page 64: Com2 Test (Not In Use)

    Chapter: 2A Operator Panel Softkey Setup Version: 2.7 Note: Com1 Test can only be performed when the Safedock software is not running as Safedock data interferes with the test. A connection to the Loader using SMT is required before starting this test. 3.6.3 Com2 Test (not in use) Note: Com2 test is not currently in use or supported by software.

  • Page 65: Extra Operator Panel (Option)

    Chapter: 2A Operator Panel Softkey Setup Version: 2.7 EXTRA OPERATOR PANEL (OPTION) The Operator Panel can be connected to an extra Operator Panel, to control Safedock from another place. The extra Operator Panel must also be set with a unique Com1 address. For example, if Operator Panel1 Com1 address is 1 (default) then Operator Panel2 Com1 address is to be set to 2.

  • Page 66: Operation And Maintenance Modes

    Chapter: 2A Operator Panel Softkey Setup Version: 2.7 OPERATION AND MAINTENANCE MODES The Safedock system can be equipped with several operation/ maintenance mode options, if required. Modes are set via key switches built into the Operator Panel. OPERATION MODES The Safedock system operation modes include: ...
  • Page 67 Continuous Test Procedure ..............9 2.3.4 Indication of Power Failure ............... 9 SAFEDOCK STATISTICS ................9 2.4.1 View Safedock Statistics ................9 SUPERIOR SYSTEM CONNECTIVITY STATUS .......... 11 2.5.1 View Superior System Connectivity Status and Activity ..... 11 TECHNICAL DESCRIPTION ..................12 SYSTEM UNITS....................
  • Page 68 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 DISCREPANCIES FROM THE DESCRIBED DOCKING ROUTINE ..... 18 GENERAL WARNING ..................18 MANUAL EMERGENCY-STOP ..............18 ITEMS TO CHECK BEFORE ENTERING THE STAND AREA ..... 19 THE SBU MESSAGE ..................19 ERRORS OR MALFUNCTIONS ..............

  • Page 69: Introduction

    SYSTEM OVERVIEW The Safedock system is designed to provide fast and safe guidance during the aircraft’s approach into the stand area. It is based on laser scanning and distance measuring technology, and it tracks the lateral and longitudinal position of the aircraft.

  • Page 70: Operating Details

    1. The docking procedure can be activated from any one of the following three options: (i) Safedock operator selecting the aircraft type to be docked from the Operators Panel. (ii) Remote selection of aircraft type by operator from the Superior System.
  • Page 71 Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 9. During the approach the aircraft type assigned will be verified by the Safedock system. When the aircraft type has been verified, the Operator Panel will show IDENTIFIED. 10. If the aircraft speed exceeds the configured maximum value, the message SLOW will be displayed to the pilot.

  • Page 72: The Docking Procedure In Abnormal Conditions

    Version: 2.7 THE DOCKING PROCEDURE IN ABNORMAL CONDITIONS If an object is blocking the view from the Safedock laser scanning unit toward the stop-position of the selected aircraft type, the system will be unable to perform the docking procedure. When an object is detected between the laser scanning unit and the stop-position, the system will halt the docking procedure and display a GATE BLOCK warning and a WAIT message.
  • Page 73 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 2-65 m or 6.5-213 ft 2 m or 6.5 ft 9 m or 30 ft 15 m or 49 ft 50-95 m or 164-312 ft FIGURE 3.2 – THE DOCKING PROCEDURE (OPTION/TYPE 1 DISPLAY)

  • Page 74: Docking Safety Features

    ERROR or ERR depending on display type (see below figure 3.3). . The type of the system error will be shown on the Operator Panel in clear text. The Safedock cannot be activated, if the system is not fully functional.

  • Page 75: Aircraft Profile Check

    Error Log. The system automatically performs auto calibration test at regular time intervals (every thirty minutes). Before the Safedock system gets activated, it checks if the latest auto calibration test was successful or not. If successful, the system starts-up without performing a new test, thus, reducing start-up time.
  • Page 76 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 From the Operator Panel, Test select Test key. SAFEDOCK SYSTEM READY Park Start Dock FIGURE 3.6 – OPERATOR PANEL TEST Press the right arrow button Walk View...

  • Page 77: Superior System Connectivity Status

    Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 SUPERIOR SYSTEM CONNECTIVITY STATUS Safedock can display Superior System connectivity status. 2.5.1 View Superior System Connectivity Status and Activity From the Test menu, press he right arrow button → start Program version SOS 1.1.2...

  • Page 78: Technical Description

    FIGURE 3.19 – SAFEDOCK SYSTEM SUB-UNITS 3.1.1 Control Unit The Control Unit is the processing heart of the Safedock system. It will accept user input commands from the Safedock Operator Panel or via the Superior System Interface. Alphanumeric information and aircraft position data are presented on the Pilot Display.

  • Page 79: Operator Panel

    3.1.5 Superior System Interface (Option) The Superior System Interface is the optional link between the Safedock system and a central control and monitoring system, the Superior System. It is also used as a gateway to other external systems and to receive information about scheduled arrivals and departures from FIS.

  • Page 80: Display Unit

    Chapter 3 Appendix A Operating Procedures. 1. In the Safedock system a number of aircraft types are defined by a set of parameters such as: nose, height and optionally aircraft geometry. At start of docking the operator assigns an aircraft.

  • Page 81: Software Programmes

    Calibration and Stand Configuration etc. It can also be used locally on a maintenance PC, connected to the Operator Panel’s service outlet or via the network. 9. SLV - utility program, Safedock Log Viewer is used to view log files from the system. SOFTWARE FUNCTIONS This section is a brief description of functions performed by software.

  • Page 82: Software Flowchart

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 5. Calibration Control function 6. Storage of data (i) Aircraft parameters (ii) Stand parameters (iii) Log files etc SOFTWARE FLOWCHART The software state diagram on next page illustrates the docking process from state READY to state PARKED.
  • Page 83 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 FIGURE 3.20 – SOFTWARE FLOWCHARTS Page 17 of 22...

  • Page 84: Safety Procedures

    DOCKING OK and the Pilot Display shows STOP (in red). GENERAL WARNING The Safedock system has a built-in error detection program to inform the aircraft pilot of impending dangers during the docking procedure. WARNING! IF THE PILOT IS UNSURE OF THE INFORMATION BEING SHOWN ON THE PILOT DISPLAY UNIT, HE MUST IMMEDIATELY STOP THE AIRCRAFT AND OBTAIN FURTHER INFORMATION FOR CLEARANCE.
  • Page 85 GUIDANCE! ERRORS OR MALFUNCTIONS If for any reason the Safedock system fails or reports an error, please take note of any details that may have caused the problem and report the error and supporting details to the appropriate maintenance personnel.
  • Page 86 Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 STAND ADJACENCY RULES Standalone Safedock operations can be enhanced with a Superior System to further improve safety and efficiency. Safedock units connected in a Superior System network with adjacent gate status provide: ...
  • Page 87 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 (c) Operator Panel display Airport personnel can start an aircraft docking locally at the gate, from an Operator Panel, or from a Superior System workstation. INTERLOCKED BY: When an aircraft docking is started, the selected aircraft type <Aircraft type>...
  • Page 88 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3 OPERATION Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 22 of 22...
  • Page 89 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 CHAPTER 3 OPERATION – APPENDIX A OPERATING PROCEDURES CONTENTS Section Description Page No. LOCAL START OF DOCKING – REGULAR CONDITIONS ........3 AIRCRAFT DOCKING ACTIVATION..............3 SELF-TEST .......................
  • Page 90 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 2 of 30...

  • Page 91: Local Start Of Docking - Regular Conditions

    Chapter: 3A Operating Procedures Version: 2.7 The following description covers both the local control procedures of Safedock and the optional operation of Safedock on commands from Superior System. For security reasons some Safedock systems are configured with a password feature for the authorisation of commands.

  • Page 92: Self-Test

    Check that the correct aircraft type is displayed on the Pilot Display. The lead-in line is to be followed. Note: If the Safedock system is still in Active mode when the aircraft nose reaches the Passenger Boarding Bridge cab, press the...

  • Page 93: Tracking

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 TRACKING Description Position The system has captured the aircraft and is actively tracking and verifying it. The floating arrows are replaced by a yellow centreline indicator and floating arrow.

  • Page 94: Closing Rate

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 CLOSING RATE Description Position The closing rate is the final countdown from a specific distance to the stop-position. A yellow vertical closing rate bar/centreline indicator appears, optionally with a digital countdown indication, depending on the configuration.

  • Page 95: Aligned To Centre

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 ALIGNED TO CENTRE Description Position The aircraft is at the displayed distance from the stop-position. The absence of any direction arrow indicates an aircraft on the centreline.

  • Page 96: Slow (Decrease Speed)

    Version: 2.7 SLOW (DECREASE SPEED) Description Position The Safedock system is configured with a slowdown active zone. Aircraft continues approach into gate. The limit speed for slow down indication is configurable per aircraft type in the 0-10m range from the stop-position, with a default setting of 2m/s.

  • Page 97: Azimuth Guidance

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 AZIMUTH GUIDANCE Description Position The aircraft is at the displayed distance from the stop-position. If the aircraft is not aligned to centre, a yellow arrow indicates an aircraft’s position to the centreline, and a red flashing arrow indicates the direction to turn.

  • Page 98: Stop Position Reached

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 STOP POSITION REACHED Description Position When the correct stop-position is reached, the Pilot Display will show STOP with a red border or with red lights. If the aircraft is found standing still but has not reached the intended stop-position, a Stop Short condition occurs (see §...

  • Page 99: Docking Completed

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 1.10 DOCKING COMPLETED Description Position When the aircraft has parked, the message OK will be displayed. If the aircraft rolls too far past the stop-position, the message TOO FAR appears (see §...

  • Page 100: Status Info

    STATUS INFO Description Position If the Safedock system is provided with optional support of CHOCKS ON, GPU On (for Ground Power Unit or 400Hz), PCA ON (for PC-Air) or other status messages, they will be displayed on the Pilot Display...
  • Page 101 Version: 2.7 Check that the PARKED message is displayed on the Operator Panel display Image Image Pilot Display Operator Panel T1-42 T2-18 T2S-24 T3-9 T3-15 Test SAFEDOCK SYSTEM READY Park Start Dock Illy- usin Donal Park on Select aircraft Air- Boe-...

  • Page 102: Park Off

    Position When an aircraft has departed, a PARK OFF command may be given by the Marshal, if the Safedock system by any reason did not detect the departure of the aircraft automatically and came to a READY state. The sequence is started with the Operator Panel showing the PARKED message.

  • Page 103: Local Start Of Docking - Abnormal Conditions

    Version: 2.7 LOCAL START OF DOCKING – ABNORMAL CONDITIONS If an object is blocking the view from the Safedock laser scanning unit toward the stop-position of the selected aircraft type, the system will be unable to perform the docking procedure. When an object is detected between the laser scanning unit and the stop-position, the system will halt the docking procedure and display a GATE BLOCK warning message.

  • Page 104: Bad Weather Conditions

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 BAD WEATHER CONDITIONS Description Position During heavy fog, rain or snow, the visibility for the docking system can Aircraft proceeds into the be reduced. gate area at a reduced...

  • Page 105: Overshoot

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 OVERSHOOT Description Position If the aircraft overshoots the stop-position with a configurable distance, the Pilot Display displays STOP (with RED border/bars) followed by TOO FAR after the aircraft comes to a complete stop.

  • Page 106: Stop Short

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 STOP SHORT Description Position If the aircraft is found standing still, within a configurable distance up to 5 m short of the stop-position, the message STOP and OK will be shown after a configurable amount of time.

  • Page 107: Failed Aircraft Verification (Id Fail)

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 FAILED AIRCRAFT VERIFICATION (ID FAIL) Description Position After capture of the aircraft, its geometry is checked against a stored Gate area: Empty profile. If, for any reason, aircraft verification is not confirmed 15m...

  • Page 108: Event Or Fault Diagnosis

    Diagnosis/resolution of an event/fault improves:  operational efficiency (future docking procedures)  safety (understand/avoid potential risks)  maintenance (pro-active troubleshooting) For more information, see:  the Maintenance, Troubleshooting or Configuration sections  the Safedock Manual  www.safegate.com or contact support. Page 20 of 30...

  • Page 109: Power Failure

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 POWER FAILURE Description Position In case of a power failure, the display will be completely black. A manual Aircraft stops and waits as backup procedure must be used for docking guidance.

  • Page 110: Emergency-Stop

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 EMERGENCY-STOP Description Position When the Emergency-Stop button on the Operator Panel is activated, Aircraft stops and waits as the Pilot Display shows STOP (with red border/bars).

  • Page 111: Gate Blocked

    2.10 GATE BLOCKED Description Position If an object is found to be blocking the view from the Safedock unit Aircraft stops and waits as towards the aircraft, and closer than the stop-position, this will be directed by the Pilot Display.

  • Page 112: Configuration Error

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 2.12 CONFIGURATION ERROR Description Position Any error related to system configuration that occurs during the docking Aircraft stops and waits as operation generates an error message in the Operator Panel and an directed by the Pilot Display error in the Pilots Display.

  • Page 113: Remote Start Of Docking - From Superior System (Option)

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 REMOTE START OF DOCKING – FROM SUPERIOR SYSTEM (OPTION) 2.13 Basic docking procedures are complemented with Superior System. All basic docking commands can be controlled remotely via Superior System or locally, if required.

  • Page 114: Start Of Docking With Activation

    Position A docking procedure is prepared by sending the aircraft information to Safedock, and to have the Safedock operator confirming that the stand is ready to accept an aircraft. (a) If the Safedock operator confirms the stands readiness before the...
  • Page 115 SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3A Operating Procedures Version: 2.7 Image Image Pilot Display Operator Panel T1-42 T2-18 T2S-24 T3-9 T3-15 SAFEDOCK SYSTEM READY-OPEN Shut Park Start down Dock PREPARED <Aircraft type> <Flight> (ii) Shut down SCHEDULED <Aircraft type> <Flight>...
  • Page 116 2.13.2.2 Docking Abort Command Description Position The Safedock operator may abort the scheduled/prepared docking, when the operator understands that the approaching aircraft is not according to the type assigned. (a) The Abort docking command is initiated by pressing the Shutdown key.

  • Page 117: Remote Start Of Docking - From Fids (Option)

    FIDS as well as basic docking commands controlled remotely via Superior System or locally, if required. Note: <Flight> indicated in the windows below, will be displayed at Safedock only if available from FIS, and if docking is not started locally. 2.14.1...

  • Page 118: Docking Abort Command

    2.14.3 Docking Abort Command Description Position The Safedock operator may abort the scheduled/prepared docking, when he understands that the approaching aircraft is not according to the type assigned. (a) The Abort docking command is initiated by pressing the Shutdown key.
  • Page 119 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3B Safedock Features Version: 2.7 CHAPTER 3 OPERATION - APPENDIX B SAFEDOCK FEATURES (OPTIONS) CONTENTS Section Description Page No. SAFEDOCK OPTIONS ....................3 DATA ENTRY ........................ 4 PASSWORD ENTRY ..................4 2.1.1...
  • Page 120 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3B Safedock Features Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 2 of 16...

  • Page 121: Safedock Options

    Safedock system. In sections describing a feature, it is usually stated that the Safedock system “is equipped” or “is configured” in a particular way. However, not all these statements may be relevant for a particular customer system. They are merely options and/or alternatives.

  • Page 122: Data Entry

    Manual Date: 6 February 2015 Chapter: 3B Safedock Features Version: 2.7 DATA ENTRY To control the Safedock system, the following options for manual data entry are available: (a) User passwords (b) System access (c) The ‘Open Stand’ command PASSWORD ENTRY The Safedock system can be equipped to use password protection for operations.

  • Page 123: Park Off Scan

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3B Safedock Features Version: 2.7 PARK OFF SCAN Once every minute (unless changed by a connected Superior System) while in PARKED status the system will perform a Park OFF scan. During the Park OFF scan, the system will try to match the profile for the currently parked aircraft with the aircraft in front of the system.

  • Page 124: Displayed Information During And After Docking

    CHOCK ON message. STAND SIGN The display of the Safedock system can be utilised as a general-purpose Stand Sign display between docking procedures. The information that can be displayed includes: Stand ID, Current Time and alternating Time/Stand ID.

  • Page 125: Uninterruptable Power Supply

    An information message will be displayed – Blocked by UPS  No more docking operation can be activated until mains power is restored.  After running on UPS while Safedock is idle is the default setting 5 min. Page 7 of 16...

  • Page 126: Centreline

    CENTRELINE MULTIPLE CENTRELINES The Safedock system is configured to use multiple centrelines. Up to three centrelines per system can be defined and used. The centrelines need not be parallel. The centreline to be used is determined individually per aircraft type. This configuration is described in Chapter 4A Stand Configuration Utility.

  • Page 127: Aircraft Safety Check

    Version: 2.7 AIRCRAFT SAFETY CHECK The Safedock system includes the Aircraft Safety Check feature, which is a further enhancement of its safety performance. Aircraft geometry is analysed by means of a true 3D measuring technique, thus bringing safety risk to a minimum.

  • Page 128: Interaction With External Equipment

    PUSHBACK DATA TRANSMISSION The Safedock system can be equipped with a feature to track an aircraft during the pushback procedure. The distance information gathered during pushback is forwarded Page 10 of 16...

  • Page 129: Manual Activation

    ON/OFF button. 8.5.2 Automatic Activation The bridge and GPU supply systems are connected to the Safedock system, allowing the Safedock system to automatically start the pushback procedure when it detects that the bridge is retracted and the GPU supply is disconnected.

  • Page 130: Apron Scan

    Version: 2.7 APRON SCAN The purpose of the apron scan functionality is to enhance normal Safedock T1 A-VDGS stand safety verification by scanning the stand area for unidentified or foreign objects. The function detects and locates objects before a docking is about to be initiated and an aircraft arrives at the stand.

  • Page 131: Operation During Capture

    During operation, the area being scanned corresponds the area from the nose position of the expected aircraft type when parked and further out. The boundaries from the stop position and further out, length and width are defined in the Safedock Maintenance Tool per configured centreline.
  • Page 132 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3B Safedock Features Version: 2.7 Image examples Minimum detection 100.0 meters point: 2 * laser height. Minimum detection distance Scanning area 30° 30° 100 meters / 328 feet Minimum detection point...

  • Page 133: Operational Scan

    Detectable object size Object size detection in primary area:  Full scan during start-up, before Safedock goes to ACTIVE: 1.0 m x 1.0 m.  Reduced scan during capture, before TRACKING: 1.0 m x 1.0 m. Object size in secondary area: ...
  • Page 134 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 3B Safedock Features Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 16 of 16...
  • Page 135 MAINTENANCE CONTENTS Section Description Page No. INTRODUCTION ......................5 SCOPE ......................5 SAFEDOCK SET-UP..................... 5 SET-UP PROCEDURES .................. 5 PLANNED MAINTENANCE ..................6 MAINTENANCE SCHEDULE ................6 WEEKLY CHECK....................6 3.2.1 Laser Unit Windows ................... 6 MONTHLY CHECK ................... 6 3.3.1...
  • Page 136 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 FAULT EVALUATION ..................16 ERRORS AND WARNINGS ................17 REPLACEMENT OF MALFUNCTIONING UNITS ............22 RENEWAL OF STEPPER MOTOR ..............25 6.1.1 Motor Disassembly .................. 25 6.1.2 Inspection ....................
  • Page 137 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 RE-CYCLING ....................51 7.2.1 Local Authority Re-cycling ..............51 7.2.2 Safegate Re-cycling ................. 51 7.2.3 Packaging ....................51 SPARE PARTS ....................52 Page 3 of 52...
  • Page 138 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 4 of 52...

  • Page 139: Introduction

    Workstation on the LAN can be used as a configuration tool. SAFEDOCK SET-UP The Safedock system has to be set up and configured at mainly the following events: (a) After initial installation at a stand (configuration and calibration) (b) After certain corrective activities/ maintenance (recalibration)

  • Page 140: Planned Maintenance

    Chapter: 4 MAINTENANCE Version: 2.7 PLANNED MAINTENANCE The Safedock system has been specifically designed to minimise maintenance downtime. The following maintenance schedules detail the maintenance requirements on a weekly, monthly, six monthly and twelve monthly basis. The system does not require any further scheduled maintenance, as proving operations are always done automatically prior to any start-of-docking procedure.

  • Page 141: Six Monthly Check

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 SIX MONTHLY CHECK 3.4.1 Laser Scanning Unit Door (a) Examine the Laser Scanning unit door seal for signs of perishing and security of attachment. (b) Renew carefully the seal if required. Use a sharp knife and clean with alcohol after removal.

  • Page 142: Corrective Maintenance

    Units shall be followed. TEST EQUIPMENT The test equipment used for the set-up of the Safedock system is the Server of the Safedock Central Computer System, provided that the connection to Superior System is established. The software SMT.EXE shall be used for this purpose.

  • Page 143: Mirror Position Detector Test

    Soft-labelled Connection to Maintenance touch keys computer Walk View Light Temp Test Test Logs Test Sens Sens Safedock SYSTEM User-friendly Safedock SYSTEM PROGRAM VERSION: READY illuminated graphic Soft Key 6.08-Zhr Mirr Mirr Laser Disp Scan display; one layout per Start...

  • Page 144: Scan Test

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 Walk View Light Temp Test Logs Test Sens Sens Program version SOS 1.0.0 L: Hor OK Ver OK Mirr Mirr Laser Scan Disp Test Test Test Test FIGURE 4.4 –...

  • Page 145: Walk-Test

    Walk-test is a system wide test function that exercises all the major features of the Safedock system. It is used to verify the operation of the system, and shall be performed whenever a modification to the system has been made.

  • Page 146: View Logs

    Next Panel keys to select which panels input should be displayed. 4.3.9 Light Sensor Test This test function is used to check the function of the light sensor that controls the intensity of the Safedock display. Page 12 of 52...

  • Page 147: Temperature Sensor Test

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 Walk View Light Temp Test Logs Test Sens Sens ‘kk’ is the light intensity Program version measured, and ‘nn’ is the SOS 1.0.0 control parameter used. Light: nn (kk)

  • Page 148: Set Ip

    Activate the modified setting for the system by pressing the Apply key. The system will restart using the new settings. 4.3.15 Restart The restart function can be used to restart the Safedock system. Back CONFIRM RESTART Accep FIGURE 4.20 – RESTART Press Accept to confirm the restart operation, press CANCEL or Back to resume normal operation.

  • Page 149: Operator Panel Setup And Test Functions Menu

    (b) Remove the J1 connector. (c) Press and hold the CANCEL button. (d) Insert the J1 connector. Alternatively, the Safedock system including Operator Panel can be powered off/on using the main switch in the display unit. This would require two people, one to turn off/on the display unit and one to press and hold the Operator Panel unit.

  • Page 150: Troubleshooting

    If a malfunction occurs within a Safedock system, error numbers appear on the Pilot Display and their equivalent error messages appear on the Operator Panel display.

  • Page 151: Errors And Warnings

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 ERRORS AND WARNINGS PD – OP messages, symptom Possible cause Action to rectify ERROR - Failed to load aircraft data Aircraft data missing in Add the aircraft to the The requested aircraft data could not be loaded.
  • Page 152 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 PD – OP messages, symptom Possible cause Action to rectify ERROR - Clip too short The clip distance is set to a distance that is Badly configured...
  • Page 153 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 PD – OP messages, symptom Possible cause Action to rectify STOP / SBU – SBU STOP Safety Backup behaviour. Common error message for issues that may require human intervention or restarted docking procedure after visual inspection of the stand area.
  • Page 154 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 PD – OP messages, symptom Possible cause Action to rectify WAIT – Stand equipment interlock The bridge or other stand equipment is not in a Incorrect Passenger...
  • Page 155 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 PD – OP messages, symptom Possible cause Action to rectify ERROR - WALKTEST REQUIRED A walk-test is required by the system. The configuration for Perform a walk-test...

  • Page 156: Replacement Of Malfunctioning Units

    Chapter: 4 MAINTENANCE Version: 2.7 REPLACEMENT OF MALFUNCTIONING UNITS This chapter describes the disassembly, inspection and the assembly of Safedock units. The following figures show the different types of Safedock units. WARNING: TO PREVENT ELECTRIC SHOCK, ISOLATE THE POWER SUPPLY PRIOR TO UNDERTAKING ANY MAINTENANCE WORK WITHIN THE UNIT.
  • Page 157 Version: 2.7 Power Supply CU Circuit Board Stepper Motor Service Drivers Power Outlet Surge Surge Arrestors Arrestors (primary (secondary side) side) Circuit Stepper Breaker Motors Laser Range Finder FIGURE 4.29 – OVERVIEW SAFEDOCK UNIT TYPE 2 Page 23 of 52...
  • Page 158 Version: 2.7 Power Supply CU Circuit Board Stepper Motor Service Drivers Power Outlet Surge Surge Arrestors Arrestors (primary (secondary side) side) Circuit Stepper Breaker Motors Laser Range Finder FIGURE 4.30 – OVERVIEW SAFEDOCK UNIT TYPE 3 Page 24 of 52...

  • Page 159: Renewal Of Stepper Motor

    Scanning Unit. Horizontal Stepper Motor Vertical Stepper Motor FIGURE 4.31 – SAFEDOCK T1 STEPPER MOTORS OF LASER SCANNING UNIT Vertical Stepper Motor Horizontal Stepper Motor FIGURE 4.32 – SAFEDOCK T 2/3 STEPPER MOTORS OF LASER SCANNING UNIT Page 25 of 52...

  • Page 160: Inspection

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 (a) Switch OFF the main power switch. (b) To gain entry to the Laser Scanning Unit, undo the cabinet lock and open the hinged door. (c) Turn off the power in the system (d) Loosen the two 3-mm socket head screws, on the axle adapter, which secures the scanning mirror (smaller) to the motor drive shaft (stem).

  • Page 161: Assembly

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 6.1.3 Assembly (a) Connect the stepper motor electrical connections to the terminal block (make sure to follow the colour codes). (b) Connect the connector to the motor position sensor.

  • Page 162: Renewal Of Calibration Mirror

    The calibration mirror is mounted on a bracket, situated above the laser range finding unit, see the figure below. Calibration Mirror FIGURE 4.33 – SAFEDOCK T1 CALIBRATION MIRROR Calibration Mirror FIGURE 4.34 – SAFEDOCK T2/3 CALIBRATION MIRROR Page 28 of 52...

  • Page 163: Inspection

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 (a) Switch power OFF and isolate the power supply unit. (b) To gain entry to the Laser Scanning Unit, undo the cabinet lock, and open the hinged door.

  • Page 164: Renewal Of Scanning Mirror

    The large mirror is used for the vertical scan on T2/T3, horizontal scan for T1. Horizontal Scanning Mirror FIGURE 4.35 – SAFEDOCK T1 SCANNING MIRRORS Horizontal Scanning Mirror FIGURE 4.36 – SAFEDOCK T 2/3 SCANNING MIRRORS Page 30 of 52...

  • Page 165: Inspection

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 (a) Switch power OFF and isolate the power supply unit. (b) To gain entry to the Laser Scanning Unit, undo the cabinet lock, and open the hinged door.

  • Page 166: Renewal Of Laser Range Finder

    Range Finder Disassembly The figure below illustrates the position of the Laser Range Finder. Laser Range Finder Unit FIGURE 4.37 – SAFEDOCK T1 LASER RANGE FINDER Laser Range Finder Unit FIGURE 4.38 – SAFEDOCK T2/3 LASER RANGE FINDER Page 32 of 52...

  • Page 167: Inspection

    6.4.5 Reset Laser Statistics Note: This operation is to be performed whenever a laser unit is replaced. (a) From the Operator Panel, select Test. Test Gate Sign Safedock SYSTEM READY Open Park Start Stand Dock FIGURE 4.39 – OP TEST (b) From the Test menu, press the right arrow for the next page and select Statistics.

  • Page 168: Scan Test

    (b) Dumping the CU memory contents to the PC will be done automatically, as soon communication between the CU and the PC is established. To make a disk copy, use the function “SAVE” in the Safedock Stand Configuration Dialogue Box. The current configuration will be saved onto disk in the maintenance PC.

  • Page 169: Control Unit Disassembly

    Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 6.5.3 Control Unit Disassembly The figure below illustrates the position of the Safedock Control Unit/CU. Stepper Motor Drivers Circuit Board Cover FIGURE 4.42 – SAFEDOCK T1, T2 AND T3 CONTROL UNIT...
  • Page 170 (a) Verify the system starts up correctly: Operator Panel contact is re-established and the emergency stop function is operational. (b) If it was possible to save the configuration file using the Safedock Maintenance program (SMT) then the configuration can be loaded to the system once again.
  • Page 171 This information is a basic step by step guide for authorized personnel to replace a Control Unit (CU) Docking Board. Safedock T1/2/3 (system design from Spring 2008) - CU circuit includes a docking board (connections) and a carrier board (CPU).
  • Page 172 (a) Verify the system starts up correctly: Operator Panel contact is re-established and the emergency stop function is operational. (b) If it was possible to save the file using the Safedock Maintenance program (SMT) then the configuration can be loaded to the system once again.
  • Page 173 This information is a basic step by step guide for authorized personnel to replace a Control Unit (CU) circuit board. Safedock T1/2/3 (system design from Spring 2008) - CU circuit includes a docking board (connections) and a carrier board (CPU).
  • Page 174 (a) Verify the system starts up correctly: Operator Panel contact is re-established and the emergency stop function is operational. (b) If it was possible to save the configuration file using the Safedock Maintenance program (SMT) then the configuration can be loaded to the system once again.

  • Page 175: Renewal Of Power Supply

    RENEWAL OF POWER SUPPLY 6.6.1 Power Supply Disassembly The figure below illustrates the position of the Safedock power supply. WARNING: DANGER OF ELECTRIC SHOCK! ISOLATE THE POWER SUPPLY PRIOR TO UNDERTAKING ANY MAINTENANCE! IF A BATTERY BACKUP IS INSTALLED, ALSO THE 24 VOLT DC CURRENT TO...
  • Page 176 FIGURE 4.51 – POWER SUPPLY RELEASE REMOVAL Renewal (a) Locate the upper DIN rail in the Safedock Pilot Display cabinet. (b) Carefully place the new power supply unit into position. (c) Apply gradual pressure until the spring latch catches on the DIN rail.

  • Page 177: Renewal Of Stepper Motor Drivers

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 RENEWAL OF STEPPER MOTOR DRIVERS 6.7.1 Stepper Motor Driver Disassembly The figure below illustrates the position of the two motor control boards, connected directly to the Control Unit.

  • Page 178: Assembly

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 WARNING! DANGER OF ELECTRIC SHOCK. THE ELECTRICAL CONNECTIONS MAY BE LIVE. DO NOT PLACE ANY TOOL INSIDE THE CONTROL RACK. (a) Switch power OFF and isolate the power supply unit.

  • Page 179: Renewal Of Led Module

    The figure below illustrates the LED matrix boards’ connection to the mounting plate. LED Module FIGURE 4.55 – SAFEDOCK T1 LED MODULE Note: The front glass is hinged at the top of the display unit. (a) To gain access to the inside of the display unit, undo and lift the front glass of the cabinet.

  • Page 180: Renewal Of Operator Panel Film (Softkey)

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 RENEWAL OF OPERATOR PANEL FILM (SOFTKEY) Renewal of Operator Panel Film (Softkey) This information is a basic step by step guide for authorized personnel to replace an old type, a damaged or worn film on the front cover, with a new one.
  • Page 181 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 (e) On the Operator Panel front, lift up a corner of the film using a knife. (f) Carefully start to cut at the film (bottom layer) adhesive and simultaneously detach the film.

  • Page 182: Renewal Of Surge Arrestors

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 6.10 RENEWAL OF SURGE ARRESTORS Renewal of surge arrestor (primary or secondary side) This information is a basic step by step guide for authorized personnel to replace an old type, a damaged or worn film on the front cover, with a new one.

  • Page 183: Renewal Of Display Fan And/Or Filter (T1 Only)

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 6.11 RENEWAL OF DISPLAY FAN AND/OR FILTER (T1 ONLY) Renewal of display Fan/Filter This information is a basic step by step guide for authorized personnel to replace display fan or filter.

  • Page 184: Support

    Our experienced engineers are available for support and service at all times, 24 hour/7 days a week. They are part of a dynamic organization making sure the entire Safegate Group is committed to minimal disturbance for airport operations. Safegate Support...
  • Page 185 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 RE-CYCLING 7.2.1 Local Authority Re-cycling The disposal of Safegate products is to be made at an applicable collection point for the recycling of electrical and electronic equipment. The correct disposal of equipment prevents any potential negative consequences for the environment and human health, which could otherwise be caused by inappropriate waste handling.
  • Page 186 Manual Date: 6 February 2015 Chapter: 4 MAINTENANCE Version: 2.7 SPARE PARTS For a complete and updated list of spare parts for Safedock system, please see www.safegate.com or contact Safegate for assistance with ordering spare parts. Page 52 of 52...
  • Page 187 SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 CHAPTER 4 MAINTENANCE - APPENDIX A STAND CONFIGURATION UTILITY (SAFEDOCK MAINTENANCE TOOL) CONTENTS Section Description Page No. SCOPE .......................... 3 LICENSE INSTALLATION AND SELECTION ............. 3 SOFTWARE OVERVIEW ....................4 SOFTWARE DESCRIPTION ..................
  • Page 188 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 4.8.5 Customizing the Operator Panel Layout ..........20 4.8.6 Creating Generic Aircrafts ..............21 4.8.7 Legacy A/C-id (GOS)................22 ISSUES ......................23 4.10 CONFIGURATION APPLIED ................24 4.11...

  • Page 189: Scope

    Chapter: 4A Stand Configuration Utility Version: 2.7 SCOPE This is a presentation of the Safedock Maintenance Tool (SMT) describing the procedures of how to configure and calibrate a Safedock system. LICENSE INSTALLATION AND SELECTION To start, the application requires at least one license file to be present in the license folder.

  • Page 190: Software Overview

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 SOFTWARE OVERVIEW On the left side each task that needs to be performed is represented by a red, yellow or green marker, where the colours have the following meanings: ...

  • Page 191: Software Description

    You need to have a configuration open to access most parts of the application. Some parts will be disabled when not connected to a Safedock system. When connecting to a system without an existing configuration, a dialog will appear that prompts for a selection of one of the possible actions.

  • Page 192: System Configuration

    SYSTEM CONFIGURATION SMT comes with a series of features that can be adjusted to your needs. The availability of these features depends on both the version of the Safedock system and also the license in use. You must apply the configuration to the system after changing the type of scanner being used, otherwise the system calibration will be invalid;...

  • Page 193: Gate Sign

    Use Prepared: The default scheduling procedure is changed to an alternative, site specific procedure. The message appears when the scheduled flight information is made available for the Safedock system. The system is then awaiting activation of the docking procedure. The only operation available to the local operator at this time is to abort the prepared flight.

  • Page 194: Interlock

    Use Superior System Interlock: This activates a blocking scheme, whereby two adjacent Safedock systems will lock each other out, allowing only one of the systems to be active at a time, or allow for operational use up to a pre-defined size of aircraft depending on the aircraft parked at adjacent stand.

  • Page 195: Ldm Type (Laser Distance Meter)

    Version: 2.7  Channel 1-4: If checked, Safedock will act as a TCP/IP client and Modbus master, connecting to the Modbus server specified by the parameter IP Address on port Port number with a poll update frequency as specified by the Poll time parameter.

  • Page 196: Docking Procedure

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 4.2.16 Docking Procedure  Use rolling arrows in downgrade: If checked, the system will allow the rolling arrows to be displayed even in downgrade mode; by default the system is preventing this type of signal in downgrade mode.

  • Page 197: Support Functions

    This step prepares the configuration of the system regarding the stand area in front of the Safedock unit. It is important to be thorough while calibrating the system because everything relies on the calibration being correct. All values in this view are relative to the position of the laser, meaning that if the system is mounted with a laser height of 5m;...

  • Page 198: Alternate Calibration Procedure

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 how the mirrors are mounted on the axis of the mirror motor. Negative values are to the left/up, positive to the right/down, from the system point of view.

  • Page 199: Feature Buttons

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 3. Press the “Save Calibration” button. 4. Verify that the silhouette of the apron corresponds to the imaginary line between the placed markers. Only a single point will be displayed for each marker.

  • Page 200: Centreline

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 3. Find a suitable object to use as a reference for calibration. It should be a flat surface located at least 3m from the system and preferably with its edges within the view.
  • Page 201 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 To define a centreline, follow the steps below: 1. Click on the appropriate centreline button on the right side, then press the “Edit” button. 2. Press and hold Ctrl and left-click along the centreline to place the centreline markers.

  • Page 202: Apron Scan

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 APRON SCAN Apron Scan configuration is done once for each centerline. The goal is to tell the system which area should be scanned and which should not. Please note that a proper apron scan setup can only be achieved using a high quality image (taken during the system calibration) of the area in front of the system.

  • Page 203: Aircraft

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 AIRCRAFT Here you can configure the centrelines, stop-positions and Operation Panel menu layout. FIGURE 4A.11 – AIRCRAFT FEATURE On the left is where the centrelines and stop-positions are shown. The middle part displays the properties for the currently selected aircraft.

  • Page 204: Changing Multiple Settings On Multiple Aircrafts

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 4.8.4 Changing multiple settings on multiple aircrafts Below the centreline/stop positions, there is a button labelled “Change all…”. Pressing this button brings up the dialog to change one or many settings on one or many aircrafts at the same time.

  • Page 205: Creating A Stop Position On A Centreline

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7  Docking procedure:  Too far distance: The maximum distance the aircraft may have travelled past the stop-position before the system will signal a TOO FAR condition.

  • Page 206: Customizing The Operator Panel Layout

    The Aircraft Menu shows the aircraft types that will be available for direct selection from the Operator Panel. The correspondence between the two is shown in the figure below: A321 A330 A340 Safedock SYSTEM Safedock SYSTEM Safedock SYSTEM Safedock SYSTEM READY READY...

  • Page 207: Creating Generic Aircrafts

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 On the Operator Panel display you can see ten items (folders/aircrafts) at a time. The first position (for the first item and the 11 item) will appear in the left lower corner and...

  • Page 208: Legacy A/C-Id (Gos)

    This tab shows a list of all aircrafts (column 1) and their GOS-ids (column2) available in the old version of Safedock together with the name (column 3) of the profile in the current configuration that matches (through GOS id) and the configuration id (column 4) that goes with it.

  • Page 209: Issues

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 ISSUES The application looks for certain conditions, such as missing and out-dated profiles, in the configuration. If any of the conditions are met, this view will present the user with an item for each detected issue.

  • Page 210: Configuration Applied

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4A Stand Configuration Utility Version: 2.7 4.10 CONFIGURATION APPLIED Here you can see the configuration history of the system, send a new configuration to the system and also set the time of the system.

  • Page 211: Updating The System

    UPDATING THE SYSTEM Occasionally you may want to update the software/data files in the system. This is done through the menu option Safedock -> Apply update. When clicked, you are asked to select an update (.spkg) package provided by Safegate. Once selected, press the Open button and a message will show you the purpose of the update package and also ask for permission to continue.

  • Page 212: Importing Configurations

    Importing Legacy Configuration Using the menu File > Import Legacy Configuration, a configuration from an older Safedock can be imported. The items that are imported are aircrafts, stop positions and operator menu (menu-based version only). The behaviour for creations of new centerlines are the same as when importing a modern configuration.
  • Page 213 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4B Safedock Log Viewer Version: 2.7 CHAPTER 4 MAINTENANCE - APPENDIX B SAFEDOCK LOG VIEWER CONTENTS Section Description Page No. INTRODUCTION ......................3 OVERVIEW ........................3 DOCKING VIEW ......................4 DOCKING VIEW ....................4 EVENT INDICATOR ..................
  • Page 214 Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4B Safedock Log Viewer Version: 2.7 Note: This page is blank for convenient double-sided printing. Page 2 of 6...

  • Page 215: Introduction

    Chapter: 4B Safedock Log Viewer Version: 2.7 INTRODUCTION The Safedock Log Viewer (SLV) is a tool that can be used to explore the content of log files from the Safedock system. SLV can be used to view both Safedock docking logs from individual docking operations and event logs from the system.

  • Page 216: Docking View

    Each range bar has a distance scale that indicates the distance from the Safedock to the tracked object. The distances are indicated in meters.

  • Page 217: Event Indicator

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4B Safedock Log Viewer Version: 2.7 EVENT INDICATOR Special events that occur during the tracking will be marked with ‘balloons’ surrounding the track. Specific information about the event can be seen as a ‘tooltip’...

  • Page 218: Short Log View

    Safegate Group SAFEDOCK® Manual Date: 6 February 2015 Chapter: 4B Safedock Log Viewer Version: 2.7 SHORT LOG VIEW The short log view is a textual representation of all the major events that occur in a docking operation. Each line in the shortlog represents a specific event, with timestamp.
  • Page 219 590222 - Cable Entry Cover Plate (3 hole) ASSEMBLY SG590222-001-01 590222 - Cable Entry Cover Plate SG590222-201-01 590222 - Cable Entry Cover Plate (3 hole with gasket) SG590222-202-01 590253 – Safedock T1 Cabinet SG590253-002-01_RVB 590253 – Safedock T1S Cabinet SG590253-219-01_RVB 590255 - HEATER SG590255-106-01_RVA...
  • Page 220 Safegate Group SAFEDOCK® Drawings List Date: 6 February 2015 Chapter: 5 Drawings List Version: 2.7 Drawing Title Drawing Number 590487 - Calibration Mirror SG590487-001-01_RVA 590495 - Soft Key Operator Panel COMPONENT PART LIST SG590495-010-01_RVG 590495 - Soft Key Operator Panel ASSEMBLY CONNECTION...
  • Page 221 Safegate Group SAFEDOCK® Drawings List Date: 6 February 2015 Chapter: 5 Drawings List Version: 2.7 Drawing Title Drawing Number 590621 - Control & Power Assembly *SG590621-001-01_RVU 590621 – DGS Connection Diagram SG590621-004-01_RVO 590621 – DGS Connection Diagram (Options) SG590621-004-02_RVO 590621 – CONTROL CABLE VERTICAL SCANNING MOTOR *SG590621-101-01 590621 –...
  • Page 222 Safegate Group SAFEDOCK® Drawings List Date: 6 February 2015 Chapter: 5 Drawings List Version: 2.7 Drawing Title Drawing Number 590982 - T2 Assembly *SG590982-001-01_RVE 590984 - T3 Assembly *SG590984-001-01_RVE Page 4 of 4...
  • Page 223 Safegate Group SAFEDOCK® Drawings List Date: 6 February 2015 Chapter: 5 Drawings List Version: 2.7 Drawing Title Drawing Number ACCESSORIES 590221 - U-CLAMP AND FASTENERS FOR Ø139.7 MM POLE SG590221-001-01 590353 - SDK3 INSTALLATION HARDWARE FOR Ø143 MM POLE SG590353-001-01 590353 - CLAMP FOR Ø143 MM POLE...
  • Page 224 Safegate Group SAFEDOCK® Drawings List Date: 6 February 2015 Chapter: 5 Drawings List Version: 2.7 Drawing Title Drawing Number 590557 - U-CLAMP FOR Ø100 MM PIPE SG590557-001-01 590561 - U-CLAMP FOR Ø214 MM PIPE SG590561-001-01 590595 - U-CLAMP – FOR Ø6 IN PIPE...
  • Page 297 35,5 10,5 30,5 MATERIAL: ALUMINIUM SHEET, EN1050A H14 Sharp Edges Unless otherwise indicated, all tolerances are according to SAFEGATE Surface Coating Weight G R O U P LAMP HOLDER BRACKET Safegate International AB MALMÖ, SWEDEN Drawn by: Date drawn: Checked by: G.O.
  • Page 348 Malmö, Sweden. Safegate Group has more than 70 partners around the globe in order to be close to its customers. Earlier members of Safegate Group include Thorn AFL and Idman, who both have over 40 years of experience in airfield lighting solutions for airports and heliports.

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