A330-200/300 Differences From A318/A319/A320/A321 Training Manual PDF
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Uploaded by EminentAspen
UAntwerp
2019
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Summary
This document is a training manual for the A330-200/300 aircraft, covering differences from other models, and autoflight systems. It is intended for training purposes only and should not be used for any other purpose.
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A330-200/300 DIFFERENCES FROM A318/A319/A320/A321 (CFM56/V2500) TRAINING MANUAL AUTOFLIGHT THIS MANUAL IS FOR TRAINING PURPOSES ONLY AND SHOULD NOT BE USED FOR ANY OTHER PURPOSE THESE NOT...
A330-200/300 DIFFERENCES FROM A318/A319/A320/A321 (CFM56/V2500) TRAINING MANUAL AUTOFLIGHT THIS MANUAL IS FOR TRAINING PURPOSES ONLY AND SHOULD NOT BE USED FOR ANY OTHER PURPOSE THESE NOTES ARE NOT UPDATED B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT Auto Flight Line Maintenance Briefing (2)..................... 2 FLIGHT ENVELOPE Flight Envelope General Description (3)...................... 36 Flight Envelope Protection D/O (3).......................... 42 FLIGHT MANAGEMENT Navigation Back-Up D/O (3)............................... 54 AUTO FLIGHT SYSTEM Power Interruptions and Power Up Tests D/O (3)............... 58 G7508471 - G7UT0TU CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) TABLE OF CONTENTS Nov 21, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 11 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) GENERAL This module describes the operational use of the Automatic Flight System (AFS) and the Flight Management Guidance and Envelope Computers (FMGECs) in a normal operation with total availability of the concerned functions. The short-term pilot orders are normally entered through the Flight Control Unit (FCU) while the long-term pilot orders are entered through the MCDUs. Four key words for the control principle and both types of guidance have to be kept in mind in order to avoid handling errors. Aircraft control is: - either automatic, that means AutoPilot (AP) or AutoTHRust (A/THR), - or manual, that means pilot action on side sticks or thrust levers. Aircraft guidance is: - either managed, that means targets are provided by the Flight Management (FM) functional part, - or selected, that means targets are selected by the pilots through the FCU. POWER-UP TEST FD ENGAGEMENT As soon as electrical power is available, the Flight Director (FD) is automatically engaged provided that the power-up test is successful. No G7508471 - G7UT0TU - FM22B1000000001 FD guidance symbols are displayed on the EFIS PFDs until take- off. CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 22 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 GENERAL & POWER-UP TEST FD ENGAGEMENT CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 33 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) MCDU INITIALIZATION The pilots use the MCDU for flight preparation, which includes: - choice of the data base, - flight plan initialization, - radio navigation entries and checks, - performance data entry such as V1 (decision speed), VR (rotation speed), V2 (take-off reference speed) and FLEX TEMP (flexible temperature) and weights. Entry of the flight plan (lateral and vertical) and V2 into the MCDU is taken into account by the FM part and confirmed by the lighting of the related lights on the FCU to indicate that the system is in managed mode. An altitude also has to be selected through the FCU. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 44 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 MCDU INITIALIZATION CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 55 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) A/THR ENGAGEMENT A/THR engagement depends on the position of the thrust levers for take-off. For take-off, the thrust levers are set to either the Take-Off/Go-Around (TO/GA) gate or the FLEXible-Maximum Continuous Thrust (FLEX-MCT) gate if a flexible temperature has been entered on the MCDU. When the pilot moves the thrust levers to the TO/GA gate, the FMGECs automatically engage the take-off operational modes for yaw and longitudinal guidance. The A/THR function is engaged (but it is not active) and the FD guidance symbols appear on the PFDs. At the thrust reduction altitude, the FM part warns the pilot to set the thrust levers to the CLimB gate. NOTE: Note: The thrust levers will not normally leave this position until a RETARD audio message tells the pilots to set the thrust levers to the IDLE gate before touch-down. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 66 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 A/THR ENGAGEMENT CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 77 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) AP ENGAGEMENT Either AP can only be engaged 5 seconds after lift-off. Only one AP can be engaged at a time, the last in being the last engaged. After the normal climb, cruise and descent phases, the selection of automatic landing through the APProach FCU P/B lets the second AP be engaged. After touch-down, during roll-out, APs remain engaged to control the aircraft on the runway centerline. The pilots disengage APs at low speed or when the A/C is stopped. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 88 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 AP ENGAGEMENT CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES Page 99 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) DATA BASE LOADING The navigation and performance data base must be loaded and updated to keep the system operational. Only the navigation data base is periodically updated (every 28 days). This module gives information related to the uploading and crossloading of the elements of the FM part of the FMGECs. The uploading is done using the Multipurpose Disk Drive Unit (MDDU). The FM part of each FMGEC operates thanks to: - the Flight Management System (FMS) operational software, - the PERFormance and NAVigation data bases aid, - the OPerational control Configuration (OPC), - and the Airline Modifiable Information (AMI) configuration files which are mandatory loadable elements. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 10 Page 10 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 DATA BASE LOADING CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 11 Page 11 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC AIRCRAFT MAINTENANCE CONFIGURATION Make sure that the FM source selector is in the NORM position. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 12 Page 12 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - AIRCRAFT MAINTENANCE CONFIGURATION CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 13 Page 13 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC (continued) CHECK OF THE LOADABLE ELEMENTS P/N REFERENCE The check of the P/N reference of the loadable elements is done through the applicable P/N STATUS page. Make sure that the software P/N reference, displayed on the related P/N STATUS page, is different from the P/N on the related floppy disk. To determine which elements need to be loaded: Push the DATA mode key on the MCDU and get access to the A/C STATUS page. Then select the SOFTWARE STATUS/XLOAD indication to display the P/N XLOAD page. To get access to the FM operational software (page 2/6), push the line key adjacent to the NEXT PAGE of the page 1/6. Make sure that the P/N reference is not the same as the P/N reference on the disk. Otherwise the uploading is not necessary. Make sure that the P/N reference is not the same as the P/N reference on the disk. Otherwise the uploading is not necessary. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 14 Page 14 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CHECK OF THE LOADABLE ELEMENTS P/N REFERENCE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 15 Page 15 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CHECK OF THE LOADABLE ELEMENTS P/N REFERENCE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 16 Page 16 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CHECK OF THE LOADABLE ELEMENTS P/N REFERENCE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 17 Page 17 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CHECK OF THE LOADABLE ELEMENTS P/N REFERENCE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 18 Page 18 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL This Page Intentionally Left Blank G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 19 Page 19 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC (continued) UPLOADING OF THE FMGEC Open one of the two FMGECs C/Bs on the RESET panel. On the Data Loading Selector (DLS) select the applicable FMGEC. Insert the applicable disk into the MDDU. Close the applicable FMGEC C/B. Monitor the data transfer and make a check on completion on the MDDU. Remove the disk and deselect the FMGEC through the DLS. Reset the loaded FMGEC. Check through the related P/N STATUS page that the displayed software P/N reference is identical to the P/N reference read on the relevant disk. NOTE: When the FMGEC power-up is completed, and if the opposite FMGEC is not yet uploaded, the amber IND annunciator comes on both MCDUs, and the INDEPENDENT OPERATION indication appears on each MCDU scratchpad. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 20 Page 20 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - UPLOADING OF THE FMGEC CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 21 Page 21 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - UPLOADING OF THE FMGEC CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 22 Page 22 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - UPLOADING OF THE FMGEC CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 23 Page 23 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - UPLOADING OF THE FMGEC CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 24 Page 24 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL This Page Intentionally Left Blank G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 25 Page 25 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC (continued) CROSSLOADING PROCEDURE When the uploading of the first FMGEC is completed, the XLOAD function can be used for the loading of the opposite FMGEC. In our example, we will XLOAD the FMGEC2 from the FMGEC1. If all the elements have to be crossloaded, a Flight Management System (FMS) UPDATE can be done through the P/N XLOAD page. Otherwise, use the P/N STATUS page related to the element, which has to be crossloaded. In both cases, the crossloading will be done from the MCDU related to the FMGEC already uploaded (MCDU 1 in our example). On the applicable P/N STATUS page, make sure that FMS1 and FMS2 have different P/Ns. Push the START XLOAD key to activate the loadable elements compatibility check. Then confirm your selection to activate the crossloading process. When the crossloading is completed, reset the loaded FMGEC. Make sure that both FMGECs are no longer in independent mode operation. The amber IND annunciator and the INDEPENDENT OPERATION indication go off. Check through the related P/N STATUS page that the displayed software P/N reference is identical to the P/N reference read on the relevant disk. The procedure is now G7508471 - G7UT0TU - FM22B1000000001 completed; you know how to upload and crossload data from a disk to the FMGEC, via the MDDU, the DLS and the MCDU. CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 26 Page 26 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CROSSLOADING PROCEDURE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 27 Page 27 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CROSSLOADING PROCEDURE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 28 Page 28 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CROSSLOADING PROCEDURE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 29 Page 29 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 UPLOADING (WITH THE MDDU/DLS) AND CROSSLOADING OF DATA TO THE FMGEC - CROSSLOADING PROCEDURE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 30 Page 30 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL This Page Intentionally Left Blank G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 31 Page 31 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) MAINTENANCE TIPS DELETE A FLIGHT PLAN FROM THE MCDU INIT A PAGE To carry out some maintenance actions, it can be necessary to enter a basic flight plan, for example to make an engine run-up. The process below explains how to delete such a flight plan, leaving the "INIT A" page in its initial condition. On MCDU 1 or 2, press the "DATA" mode key, "DATA INDEX page 1" appears. Select "A/C STATUS" page, select "SECOND DATA BASE", wait a few seconds: ACTIVE and SECOND DATA BASE dates and numbers are transposed. The flight plan data is deleted. Select "SECOND DATA BASE" again (the data base lines are retransposed). Verify the "ACTIVE DATA BASE" is valid (not out of date). Press "INIT" mode key and verify that "INIT A" page is erased. G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 32 Page 32 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 MAINTENANCE TIPS - DELETE A FLIGHT PLAN FROM THE MCDU INIT A PAGE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 33 Page 33 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22B1000000001 MAINTENANCE TIPS - DELETE A FLIGHT PLAN FROM THE MCDU INIT A PAGE CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 34 Page 34 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL This Page Intentionally Left Blank G7508471 - G7UT0TU - FM22B1000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) AUTO FLIGHT LINE MAINTENANCE BRIEFING (2) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 35 Page 35 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL FLIGHT ENVELOPE GENERAL DESCRIPTION (3) GENERAL In addition to the acquisition of the aircraft parameters used by the Auto Flight System (AFS), the Flight Envelope (FE) function basically consists of the speed envelope computation and the detection of abnormal flight conditions. G7508471 - G7UT0TU - FM22DB000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE GENERAL DESCRIPTION (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 36 Page 36 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22DB000000001 GENERAL CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE GENERAL DESCRIPTION (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 37 Page 37 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL FLIGHT ENVELOPE GENERAL DESCRIPTION (3) aircraft gross weight and the CG position from the FCMC. If both FCMCs ACQUISITION AND MONITORING are lost, the Flight Envelope function selects its own computations. The Flight Envelope function ensures the acquisition and monitoring of SPEED ENVELOPE COMPUTATION the various aircraft parameters used by the Flight Envelope, Flight Guidance (FG) and Flight Management (FM) functions except those The Flight Envelope function computes the speed envelope consisting specific to the Flight Management. of the characteristic speeds, these being the maneuvering speeds and In particular, the Flight Envelope function acquires the alphafloor speed limits. These speeds are used either by the crew or by the Flight detection signal computed from the Flight Control Primary Computers Guidance automation to safely fly the aircraft within the speed envelope. (FCPCs) and, if valid, sends it to the Flight Guidance function for Note that most of these speeds are obtained from VS (stall speed) alphafloor protection. delivered by the FCPCs. The speeds are displayed on the speed scale of Dialog between the three functional parts takes place via two common the EFIS PFDs. memories, one between the Flight Envelope and the Flight Guidance part, another between the Flight Guidance and the Flight Management ABNORMAL FLIGHT CONDITIONS DETECTION part. The Flight Envelope function detects the presence of several abnormal AIRCRAFT CONFIGURATION flight conditions. AFT CG The Flight Envelope function determines the aircraft configuration specifically for the Flight Envelope and Flight Guidance functions. The two FCMCs control the aft CG by transferring fuel to and from For that purpose, the Flight Envelope function acquires the ground/flight the trim tank to reduce drag. The Flight Envelope function monitors conditions from the Landing Gear Control and Interface Units (LGCIUs), aft CG limit overshoot by a computation fully independent of the the slat/flap configuration from the Slat Flap Control Computers (SFCCs) FCMCs. In case of aft CG limit overshoot, a warning is generated. and the engine on/off data from the Full Authority Digital Engine Control This computation is active in clean configuration over 20,000 feet. G7508471 - G7UT0TU - FM22DB000000001 (FADEC) computers. LATERAL ASYMMETRY WEIGHT AND CG The Flight Envelope function ensures the detection of lateral asymmetry by comparing the left and right engine thrusts. This The aircraft gross weight and Center of Gravity (CG) position data are condition is used for the Flight Envelope computations and Flight computed in parallel by the Fuel Control and Monitoring Computers Guidance function. (FCMCs) and the Flight Envelope function itself. The Flight Envelope function ensures the selection of this data, which is then used by the Flight WINDSHEAR Envelope, Flight Guidance, Flight Management and the flight controls. The Flight Envelope function computes a signal to provide a visual If at least one FCMC is valid, the Flight Envelope function uses the windshear warning on the PFDs and an audio warning through the CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE GENERAL DESCRIPTION (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 38 Page 38 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL loudspeakers. Note that it has no authority on the autothrust and is only active if slats and flaps are extended. G7508471 - G7UT0TU - FM22DB000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE GENERAL DESCRIPTION (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 39 Page 39 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22DB000000001 ACQUISITION AND MONITORING... ABNORMAL FLIGHT CONDITIONS DETECTION CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE GENERAL DESCRIPTION (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 40 Page 40 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL This Page Intentionally Left Blank G7508471 - G7UT0TU - FM22DB000000001 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE GENERAL DESCRIPTION (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 41 Page 41 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL FLIGHT ENVELOPE PROTECTION D/O (3) GENERAL The Flight Envelope (FE) part detects A/C configurations outside the normal flight envelope such as windshear conditions and aft Center of Gravity (CG) out of tolerated limit. The FE part also acquires and transmits the alphafloor signal from the Flight Control Primary Computers (FCPCs) to the Flight Guidance (FG) part. FE processing is autonomous. A single detection by one of the two Flight Management Guidance and Envelope Computers (FMGECs) is enough to activate one of these three functions. The FE function computes the limit and manoeuvering speeds which are displayed on the speed scale of the PFD. DETECTION AVAILABILITY Windshear detection, aft CG detection or alphafloor detection depend on flight conditions. Windshear detection is available during 30 seconds after take-off under 250 feet Radio Altimeter (RA) and from 1300 feet RA to 50 feet RA in approach. It is inhibited in clean configuration. Alphafloor acquisition is available from take-off to a radio altitude of 100 feet before landing. G7508471 - G7UT0TU - FM22D1000000002 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 42 Page 42 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22D1000000002 GENERAL & DETECTION AVAILABILITY CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 43 Page 43 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL FLIGHT ENVELOPE PROTECTION D/O (3) WINDSHEAR DETECTION If windshear is detected, the FE function computes a windshear warning. A visual indication is given on the PFD and an aural warning can be heard from the cockpit loudspeakers. This signal computation is based on an algorithm taking into account longitudinal shears, vertical acceleration, wind components given by the Air Data and Inertial Reference Unit (ADIRU) and slat/flap position given by the Slat Flap Control Computer (SFCC). WINDSHEAR WARNING The warning is triggered depending on the shear intensity and a minimal safe A/C energy (according to speed and flight path). NOTE: Note that if both RAs have failed, the windshear warning is not available. This warning loss is displayed on the ECAM status page. G7508471 - G7UT0TU - FM22D1000000002 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 44 Page 44 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22D1000000002 WINDSHEAR DETECTION - WINDSHEAR WARNING CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 45 Page 45 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL FLIGHT ENVELOPE PROTECTION D/O (3) AFT CENTER OF GRAVITY DETECTION In order to improve A/C performance, the Fuel Control and Monitoring Computer (FCMC) controls the CG position by transferring fuel forward. The FE function monitors the non-overshoot of the aft CG limits by a computation fully independent of the FCMC. AFT CG OVERSHOOT If the FE GC is greater than the aft CG caution limit, the information is transmitted to the FCMC which stops fuel transfer during a time limit. AFT CG WARNING The FE function provides the Flight Warning Computers (FWCs) with a CG monitoring availability signal. If the CG is greater than the limit CG, the FE function sends an aft CG warning signal followed by an ECAM message to the FWCs. Aft CG warning and caution are computed with CG and weight estimations made by the FE part, independently of the FCMC, mainly by using THS deflection. G7508471 - G7UT0TU - FM22D1000000002 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 46 Page 46 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22D1000000002 AFT CENTER OF GRAVITY DETECTION - AFT CG OVERSHOOT & AFT CG WARNING CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 47 Page 47 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL FLIGHT ENVELOPE PROTECTION D/O (3) ALPHAFLOOR ACQUISITION The FE part only acquires the Alphafloor detection/activation signal coming from the FCPC. This creates the Alphafloor condition. The FE part is involved as a letter box between the FCPCs and the FG part. The alphafloor condition is used by the FG part and the opposite FMGEC. ALPHAFLOOR PROTECTION OF THE AUTOTHRUST The alphafloor protection of the autothrust function is active when the detection is performed by at least one of the three FCPCs. The Alphafloor acquisition function has full authority on the autothrust via the FG part. It forces the autothrust to Take-Off/Go-Around (TO/GA) thrust even if the autothrust was not previously engaged. The full thrust signal is sent to the engines via the Flight Control Unit (FCU), the Engine Interface and Vibration Monitoring Unit (EIVMU) and the Electronic Engine Controls (EECs). ALPHAFLOOR WARNING MESSAGES Warning messages are displayed on the PFD and on the EWD. The FE function provides the Display Management Computers (DMCs) via the FCU with a Flight Mode Annunciator (FMA) amber message A. FLOOR in the autothrust zone and an EWD amber message A FLOOR at the top left of the screen. G7508471 - G7UT0TU - FM22D1000000002 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 48 Page 48 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22D1000000002 ALPHAFLOOR ACQUISITION - ALPHAFLOOR PROTECTION OF THE AUTOTHRUST & ALPHAFLOOR WARNING MESSAGES CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 49 Page 49 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL FLIGHT ENVELOPE PROTECTION D/O (3) green dot) is limited by the maximal operational speed (VMAXOP) OPERATIONAL SPEED COMPUTATION AND DISPLAY and the VLS. VMAN is available when the A/C is in flight and in clean configuration. Now the operational speeds will be explained. It is represented on the PFD by a green dot on the speed scale. F SPEED VMAXOP F speed is the minimum flap retraction speed and corresponds to the VMAXOP is the maximum operational speed used as a limit in the speed at which flaps can be retracted. FG part. F speed is available on the PFD one second after shock absorber extension and when the slat/flap lever is in positions 3 or 2. F speed NOTE: Note that it is not represented on the PFD. is represented by a green F on the speed scale. In clean configuration, the maximal operational speed corresponds to S SPEED the buffeting limit at 0.2 g with respect to weight and altitude. It is S speed is the minimum slat retraction speed: it corresponds to the limited by the maximal speed (VMAX) minus 5 kts and the VLS in speed at which slats can be retracted. clean configuration. S speed is available on the PFD one second after shock absorber With flaps and slat extended, VMAXOP is limited by the maximum extension and when the slat/flap lever is in position 1. S speed is Flap Extended Speed (VFE) and VLS. represented by a green "S" on the speed scale. VMAX VLS VMAX speed is the maximum speed and it is used by the AFS in The Lowest Selectable Speed (VLS) is the minimum selectable speed order to prevent excessive speed. for the actual slat and flap configuration taking into account the control The maximum speed (VMAX) corresponds to the Maximum Operating lever position, the real surface position and the speedbrake Speed/Mach (VMO/MMO) in clean configuration and L/G retracted. configuration. The VLS provides a safety margin in order to avoid In clean configuration but with L/G extended, VMAX corresponds G7508471 - G7UT0TU - FM22D1000000002 stalling at low speed and buffeting during cruise (throughout the FE). to the Maximum Landing Gear Extended Speed (VLE). With slats It is used by the Automatic Flight System (AFS) in order to prevent and flaps extended, VMAX corresponds to the Maximum Flap speed undershoot. Extended Speed (VFE). VLS is displayed one second after shock absorber extension and for It is defined on the PFD by the lower end of a red and black strip in all slat/flap configurations. It is represented by the top of an amber the upper part of the speed scale. strip in the lower part of the speed scale. VFEN VMAN GREEN DOT VFEN corresponds to the maximum flap and slat extension speed of The Manoeuvering Speed (VMAN) is a function of the weight, the the next slat/flap configuration. The predictive maximum flap extended altitude and the number of engines running. It is the optimum speed speed at the next slat/flap position depends only on the slat/flap control in the event of one engine failure. VMAN (manoeuvering speed or lever position. CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 50 Page 50 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL VFEN is displayed on the PFD below 14,625 ft except when flaps are fully extended and it is indicated by two amber dashes. VCTREND VCTREND represents the airspeed tendency, that means the A/C acceleration or deceleration. The airspeed tendency is computed to represent the speed that the A/C would have 10 seconds later if the acceleration remained constant. VCTREND is displayed on the PFD if VC is higher than 30 kts and it is defined by a yellow pointer initiating an A/C actual speed symbol. G7508471 - G7UT0TU - FM22D1000000002 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 51 Page 51 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22D1000000002 OPERATIONAL SPEED COMPUTATION AND DISPLAY - F SPEED... VCTREND CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 52 Page 52 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL This Page Intentionally Left Blank G7508471 - G7UT0TU - FM22D1000000002 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) FLIGHT ENVELOPE PROTECTION D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 53 Page 53 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL NAVIGATION BACK-UP D/O (3) GENERAL NAVIGATION The MCDU BACK-UP NAV (B/UP NAV) must be used as a back-up The BACK-UP NAV function is based on Inertial Reference (IR) inputs system when both Flight Management (FM) parts are failed, supplying from the ownside IR or IR3 which provide position, ground speed, track, the crew with limited information, which can be used to complete the heading, altitude and wind. The selected IR depends on pilot selection, current flight. through the IR source selector, to be consistent with the current displayed The MCDU B/UP NAV is activated through the "SELECT NAV B/UP" IR data on the corresponding PFD and ND. The MCDU B/UP NAV prompt on the MCDU MENU page. This prompt is available at all times, provides, the crosstrack error and the bearing/distance/time to go to the regardless of the status of FM1 or FM2, provided the FM SOURCE active waypoint, depending on the aircraft latitude/longitude and on the selector is set to the NORM position. active leg of the flight plan. It supplies the automatic leg change when If the FM source selector is moved from the NORM position to one of the TO waypoint is reached. the other two positions, BACK-UP NAV is deactivated. Finally, there is It is very important to note that all this data is only for display, there is no interconnection between MCDU1 and MCDU2, so the B/UP NAV no steering order issued by the MCDU, and the NAV mode cannot be functions work independently and may be activated separately. engaged. NOTE: Note that MCDU3 does not have this option, even when it is ND DISPLAY used to replace MCDU1 or MCDU2. The MCDU transmits the BACK-UP F-PLN to the NDs. It consists of FLIGHT PLANNING active F-PLN vectors and waypoints related to the fixed aircraft position in ROSE or ARC modes, or to the moving aircraft reference in PLAN Before activation of the BACK-UP NAV function, a condensed form of mode. In all cases, the flight plan line is dashed in green (as NAV mode the flight plan is transferred from the FM part to the MCDU. This cannot be engaged). Options selectable on the EFIS control panel are not downloading is updated in case of: allowed (WayPoinT, AiRPorT, VOR.D, Non-Directional Beacon, G7508471 - G7UT0TU - FM22DAF22MJ0102 - FM primary F-PLN changes, ConSTRaint). - FM lateral leg sequencing, - FM long power off, MCDU PAGE AVAILABILITY - FM source selector change, All flight planning operations are directly applied through the B/UP - FM resynchronization. F-PLN page. It displays each leg of the active route, providing position Downloading includes waypoint position, waypoint identifier, leg type, information for each waypoint, as well as computed course, time and discontinuity, overfly and turn direction information in a maximum of distance for the connecting legs. The revisions, available on the B/UP 150 legs. F-PLN page, are: At BACK-UP NAV activation, a last updating is performed and then any - waypoint insertion, other updating is ignored. A reduced capability is given to the MCDU - waypoint deletion, B/UP NAV function compared to the FM function. CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) NAVIGATION BACK-UP D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 54 Page 54 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL - discontinuity deletion, - overfly deletion/insertion. Pressing the DIR key enables the selection of a waypoint to join it directly. The B/UP F-PLN/DIR TO page is similar to the F-PLN page but line 1 is reserved for waypoint entry. Pressing the PROGress key gives navigation information. The B/UP PROG page displays the aircraft position with identification of the selected IR. It also provides ground speed, active leg track with aircraft track. The top line displays the waypoint identifier and altitude at the last sequenced waypoint, also called overhead (OVHD). The bottom line enables access to the B/UP IRS pages. The B/UP IRS pages correspond to IR1 or 2, function of MCDU1 or 2, and IR3. IR provides, for display information about position, the true track, the true and magnetic headings, the ground speed and the wind. DEACTIVATION When the BACK-UP NAV function is voluntarily left, the return is performed on the MCDU MENU page. DESELECT NAVB/UP prompt must be pressed to return to normal operation. G7508471 - G7UT0TU - FM22DAF22MJ0102 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) NAVIGATION BACK-UP D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 55 Page 55 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL G7508471 - G7UT0TU - FM22DAF22MJ0102 GENERAL... DEACTIVATION CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) NAVIGATION BACK-UP D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 56 Page 56 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL This Page Intentionally Left Blank G7508471 - G7UT0TU - FM22DAF22MJ0102 CMQ - SA family to A330-200/300 - T1+T2 (Lvl 2&3) (RR Trent 700) NAVIGATION BACK-UP D/O (3) Nov 20, 2008 22 - AUTO FLIGHT B1/B2_A330_DIFF_FR_A320 DVIATION TRAINING SERVICES 57 Page 57 REV. 1 FOR TRAINING PURPOSES ONLY DATE: 01.06.2019 A330-200/300 TECHNICAL TRAINING MANUAL POWER INTERRUPTIONS AND POWER UP TESTS D/O (3) battery, the FM retrieves the flight plan data for display on the INTERRUPTION < 10 MS MCDU whatever the interruption time. For the Flight Management Guidance and Envelope Computer (FMGEC), POWER-UP TEST Flight Control Unit (FCU) or MCDU, the transparency time may be around 10 ms and these interruptions do not affect the system. The only Power-up tests are performed when the A/C is on the ground, following effect is on the MCDU Cathode Ray Tube (CRT) wh
