Flight Operations Safety Awareness Seminar (FOSAS)
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1 Open space to put your own picture Flight Operations Safety Awareness Seminar (FOSAS) Technical solutions and design enhancements Airbus Flight Operations Support and Training Standards Nairobi, Sep. 2017
2 Technical solutions and design enhancements Soft Go-Around ROPS / RAA Harmonized PFD AED (A350) EFB Weather On Board Future Aircraft Projects 2
3 Technical solutions and design enhancements Soft Go-Around ROPS / RAA Harmonized PFD AED (A350) EFB Weather On Board Future Aircraft Projects 3
4 Soft Go-Around Function Why a SOFT Go-Around? Developed to reduce during go-around: + High vertical Speed + High Pitch angle + High Longitudinal acceleration To Reduce Flight Crew Workload To Reduce Flight Crew Spatial Disorientation 4
5 Soft Go-Around Function Why a SOFT Go-Around? ROTATION...PERFORM According to Go-Around survey + More than 13% of the Go-Arounds with TOGA selection are performed with an initial Pitch below 12 Incorrect Pitch Management 5
6 Soft Go-Around Function Why a SOFT Go-Around? ROTATION...PERFORM +When flying manually, rotate towards the Go-Around pitch target: Know your Go-Around Initial Pitch Target 6 A320 A330 A / o A380/A350 A /300 A300/A o 18 o
7 Soft Go-Around Function Why a SOFT Go-Around? ROTATION...PERFORM + If during a manual go-around the required pitch is not reached or maintained: + Linear acceleration will result, + This could induce, false climb illusion Pilot illusion Actual 7 Possible pilot reaction based on somatogravic illusion Fly the correct pitch
8 Soft Go-Around Function Principle : Thrust Mode All Engines Operative (AEO) only GA SOFT Manual thrust mode Same thrust management Available during goaround Pre-computed engine thrust If 2000 ft/min cannot be reached (e.g. overweight) Same engagement conditions Rate of Climb: Approx. 2000ft/min Cockpit Indications GA soft thrust = TOGA thrust 8
9 Soft Go-Around Function How to activate? +TOGA detent then FLEX/MCT detent 1 2 GA initiation: TOGA (no change) 9
10 Soft Go-Around Function Procedure New 10
11 Soft Go-Around Function Availability A300/A310 family A340 A320 family A330 A380 A350 XWB Not planned Optional on the A320neo (2015), not planned on the A320ceo Optional for A330 aircraft delivery (2015) Optional Basic 11
12 Technical solutions and design enhancements Soft Go-Around ROPS / RAA Harmonized PFD AED (A350) EFB Weather On Board Future Aircraft Projects 12
13 Preventing Runway Overruns and Incursions: The Airbus Solutions 13
14 Preventing Runway Overruns and Incursions: The Airbus Solutions 14 Page 14
15 Preventing Runway Overruns and Incursions: A Global Offer 15
16 Preventing Runway Overruns: Runway Overrun Prevention System 16 Page 16
17 Preventing Runway Overruns: ROPS Objectives 17 Page 17
18 Preventing Runway Overruns: ROPS Principles 18 Page 18
19 Preventing Runway Overruns: ROPS Principles ROW ROP Transition Point 19
20 Preventing Runway Overruns: ROW Principle (A380 & A350 only _ Above 500 ft) 500 ft ND ND: Mode PLAN Zoom 2 NM SOP: DES preparation (Runway selected) Assumptions: Normal landing, Max. Braking, Idle Rev. on dry runway / Max Rev on wet runway Predictive ROW (Above 500 ft) available on ND = Minimum achievable landing distance (+ 15%) ND 20 Page 20
21 Preventing Runway Overruns: ROW Principle (A320, A330, A340, A380) Transition Transition Point Point 21
22 Preventing Runway Overruns: ROW Principle (A320, A330, A340, A380) Transition Transition Point Point PFD (Below 500 ft) Aural Pilot Action (Below 500 ft) None Go-around decision if runway condition is not DRY 22 Page 22
23 Preventing Runway Overruns: ROW Principle (A380) Transition Transition Point Point PFD (Below 500 ft) Aural Pilot Action (Below 500 ft) None Go-around decision if runway condition is not DRY 23 Page 23
24 Preventing Runway Overruns: ROW Principle (A380) Transition Transition Point Point PFD (Below 500 ft) Aural Pilot Action (Below 500 ft) ND (A380) None Go-around decision if runway condition is not DRY 24
25 Preventing Runway Overruns: ROW Principle (A320, A330, A340, A380) Transition Transition Point Point 25 Page 25
26 Preventing Runway Overruns: ROW Principle (A320, A330, A340, A380) Transition Point PFD (Below 500 ft) Aural (Below 200 ft) Pilot Action (Below 500 ft) "RWY TOO SHORT!" Go-around decision regardless of runway condition 26 Page 26
27 Preventing Runway Overruns: ROW Principle (A380) Transition Point PFD (Below 500 ft) Aural (Below 200 ft) Pilot Action (Below 500 ft) "RWY TOO SHORT!" Go-around decision regardless of runway condition 27 Page 27
28 Preventing Runway Overruns: ROW Principle (A380) Transition Point PFD (Below 500 ft) Aural (Below 200 ft) Pilot Action (Below 500 ft) ND (A380) "RWY TOO SHORT!" Go-around decision if runway condition is not DRY 28 Page 28
29 Preventing Runway Overruns: ROW Principle (A350 only) 200 ft PFD (Below 500 ft/above 200 ft) Aural Pilot Action (Below 500 ft/above 200 ft) ND (A350) None No pilot action. Be ready to initiate a Go-around. 29 Page 29
30 Preventing Runway Overruns: ROW Principle (A350 only) 200 ft Transition Point PFD (Below 200 ft) Aural (Below 200 ft) Pilot Action (Below 200 ft) ND (A350) "RWY TOO SHORT!" Go-around 30 Page 30
31 ROP Principle (A320, A330, A340, A380, A350) Transition Point PFD (On ground) Aural (On ground) BRAKE MAX BRAKING MAX BRAKING - If Max Braking applied and Max Reverse not selected, "MAX REVERSE - - If there is still a risk of runway excursion at 80 kt "KEEP MAX REVERSE" Pilot Action (On ground) Max Braking Max Reverse 31 Page 31
32 ROP Principle (A380, A350) Transition Point PFD (On ground) Aural (On ground) BRAKE MAX BRAKING MAX BRAKING - If Max Braking applied and Max Reverse not selected, "MAX REVERSE - - If there is still a risk of runway excursion at 80 kt "KEEP MAX REVERSE" Pilot Action (On ground) Max Braking Max Reverse 32 Page 32
33 ROP Principle (A380, A350) Transition Point PFD (On ground) Aural (On ground) Pilot Action (On ground) ND (A350, A380) Autobrake modes BRAKE MAX BRAKING MAX BRAKING - If Max Braking applied and Max Reverse not selected, "MAX REVERSE - - If there is still a risk of runway excursion at 80 kt "KEEP MAX REVERSE" Max Braking Max Reverse 33 Page 33
34 Preventing Runway Overrun: Illustration 34 Page 34
35 ROPS 35
36 Preventing Runway Overrun: Availability on the Airbus Fleet Aircraft Family A300/A310 A320/A320neo A330/A340 A380 A350 XWB Status Not applicable Available as an Option/Retrofit Option/Retrofit A330: 2015 A340: 2016 Option associated with BTV/Retrofit Basic associated with BTV 38 Page 38
37 Preventing Runway Incursion: RAA 39 Page 39
38 Preventing Runway Incursion: Challenging Airport Situations Taxiing at night Taxiing with low visibility Fog Taxiing with low visibility Heavy rain Complex airport network Taxiing during sunset/sunrise Heavy traffic 40 Page 40
39 Preventing Runway Incursion: Runway Approaching Advisory 41 Page 41
40 Preventing Runway Incursion: RAA Principle 42 Page 42
41 Preventing Runway Incursion: RAA Principle PFD ND 43 Page 43
42 Preventing Runway Incursion: RAA Illustration (1/2) 60 m 7 s 44 Page 44
43 Preventing Runway Incursion: RAA Illustration (2/2) RWY AHEAD RWY AHEAD PFD ND ND 45 Page 45
44 Preventing Runway Incursion: Availability on the Airbus Fleet Aircraft family A300/A310 A320/A320neo A330/A340 A380 A350 XWB Status Not applicable Available as an Option/Retrofit Basic 46 Page 46
45 Preventing Runway Overruns and Incursions: Conclusion 47 Page 47
46 Technical solutions and design enhancements Soft Go-Around ROPS / RAA Harmonized PFD AED (A350) EFB Weather On Board Future Aircraft Projects 48
47 Harmonized PFD (hpfd) Operational Advantage Flight references on PFD appear similar to HUD when TRK/FPA mode is selected Help the transition from Head up to Head down Symbology consistent with future Enhanced/Synthetic Vision Systems TRK-FPA mode 49
48 Harmonized PFD (hpfd) Interface +Flight Director pitch bar at takeoff +Flight Path Director (or Donut FD) +Energy Chevrons +Speed Delta (on left FPV wing) +Display of the selected FPA 50
49 Harmonized PFD (hpfd) Availability
50 Technical solutions and design enhancements Soft Go-Around ROPS / RAA Harmonized PFD AED (A350) EFB Weather On Board Future Aircraft Projects 52
51 Automatic Emergency Descent (AED) Operational Benefit Flight Crew Workload Reduction (but the conventional EMER DES technique still possible) If flight crew incapacitated (hypoxia): The aircraft automatically descends Level B Training Availability A : Q A : Baseline 53
52 Automatic Emergency Descent (AED) Interface + New EMER DESCENT pushbutton on center pedestal + New AP/FD EMER DES mode and PFD messages + Flight crew can interact at any time + In case of RA during AED, AP/FD TCAS mode 54 automatically engages until RA resolutions. AED resumes if EMER DES conditions are still present
53 Automatic Emergency Descent (AED) Manual Operation + The flight crew presses the EMER DESCENT pb 55
54 Automatic Emergency Descent (AED) Manual Operation 3 NM side step TCAS BLW mode + The flight crew extends the speed brakes + Automatic squawk
55 Automatic Emergency Descent (AED) Automatic Operation + Countdown if CAB ALT > ft within15 s 57
56 Automatic Emergency Descent (AED) Automatic Operation 3 NM side step + Without crew action: Automatic engagement of AP/FD EMER DES & HDG modes TCAS BLW mode + Automatic squawk
57 Automatic Emergency Descent (AED) Memory Items + No change. +But 2 techniques now available to initiate EMER DESCENT 59
58 Technical solutions and design enhancements Soft Go-Around ROPS / RAA Harmonized PFD AED (A350) EFB Weather On Board Future Aircraft Projects 60
59 EFB - Weather On Board Principle EFB APPLICATIONS PLATFORM FLYSMART Deployment in Progress WEATHER PROVIDERS DATA CENTER AIRCRAFT - GROUND COMMUNICATION ON-BOARD MODULE Flight Crew SUPPLIER MODULE GROUND MODULE Dispatcher Very useful strategic tool, to anticipate before the weather radar s range 61
60 EFB - Weather On Board Key Features OBSERVATIONS FORECASTS ESSENTIAL AIRPORT METAR/SPECI AIRPORT TAF, CB TOPS, ICING, SIGMET CLEAR AIR TURBULENCE (CAT) PREMIUM **INCLUDES ESSENTIAL** SATELLITE IR, GROUND RADAR, LIGHTNING, PIREP WIND DISPLAY INTERACTIVE MAP BACKGROUND, TIME SCALE DISPLAY OF NAVAIDS, WAYPOINTS, AIRPORTS, AIRPORT SEARCH VERTICAL SECTION CB TOPS, CAT, ICING FLIGHT PLAN DISPLAY MAP CENTERING (CLASS 2 ONLY) AIRPORTS GROUND: DISPATCHER APPLICATION 62
61 EFB - Weather On Board Weather on Board Lightning Observations & SIGMET Forecasts Deployment in Progress 63
62 EFB - Weather On Board Weather on Board Clear Air Turbulence & Winds Forecasts Deployment in Progress 64
63 EFB - Weather On Board Weather on Board CB Tops Forecasts & Satellite Observations Deployment in Progress 65
64 EFB - Weather On Board Principle ESSENTIAL PREMIUM EFFECTIVITY FLYSMART INTEGRATION CLASS 1 EFBS CLASS 1 EFBS CLASS 2 EFBS OPERATING SYSTEM WINDOWS & IOS WINDOWS & IOS WINDOWS MARKET AVAILABILITY AVAILABLE AVAILABLE Q
65 Technical solutions and design enhancements Soft Go-Around ROPS / RAA Harmonized PFD AED (A350) EFB Weather On Board Future Aircraft Projects 67
66 Aircraft as a Weather Sensor Principle Mid-Term Flight Path + Destination 10X project launched by Airbus Safety Department (Ref. to 2017 Flight Safety Conference in Santiago) Turbulences Temperatures Volcanic Ash Lightening strikes Humidity Ice Crystals Winds 68
67 Aircraft as a Weather Sensor Areas of Research Long -Term Fusion of Radar & Uplinked Data 3D Weather Analysis & Automatic Re-routing 69
68 Ice Crystals Detection 70
69 Spot on Ice Crystals Today s Status Ice Crystals Icing (ICI) + No possible detection with existing radars (too low reflectivity) + Creation of a new FCTM chapter to explain the phenomenon ICI always above or downwind of convective clouds: Classical radar operational recommendations are useful (prefer lateral, upwind deviation) Clues to identify ICI: Appearance of rain at very low T, Surprizing TAT around 0 C, etc. Recall of good practices in the case of an event because of ICI: Follow Airbus sensed and not-sensed procedures 71
70 Spot on Ice Crystals Ice Crystals Detection Mid-Term project + International Collaboration since Icing wind tunnels, flight tests +3 campaigns of 26 flights in deep convective clouds +Specific instrumentation developed +Outcomes: + Ice Crystals Detectors + Enhanced Weather Radars + Spaceborne Retrieval 72
71 Airbus S.A.S. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof. AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks. AIRBUS S.A.S All rights reserved. Confidential and proprietary document
72 Preventing Runway Incursion: Retrofit 79 Page 79
73 Preventing Runway Incursion: Training A/C Family A320 A330/A340 A380 A350 XWB Minimum Training Requirement System Knowledge Module 80 Page 80
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