Flight Operations Safety Awareness Seminar (FOSAS)

Transcription

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