Airbus Operational Landing Distances International Air Safety Seminar – Singapore November 1-3, 2011 Operational Landing Distances Implementing the TALPA ARC proposals Presented by Lars KORNSTAEDT / Performance Expert, Airbus Flight Operations Support International Air Safety Seminar 2011 International Air Safety Seminar 2011 Airbus Operational Landing Distances TALPA ARC Concepts Common rules Page 2 • For all airports • For all manufacturers • For all operators Shared operational landing performance computation • Realistic Air Distance • Representative Friction • All physical effects considered Standardized performance to match reported conditions • Standardized runway condition assessment • Allow performance determination for all types of reports International Air Safety Seminar 2011 Airbus Operational Landing Distances FAA TALPA ARC – Runway Assessment Matrix Reporting Code Code 2 Measured Friction Runway Contaminant Greater than 1/8” of: •Water •Slush Primary Assessment Differentiation by Temperature Mu (µ) Reported Braking Action Deceleration and Directional Control Observation Brake deceleration and controllability is between Medium and Poor. Potential for hydroplaning exists. PiRep DOWNGRADE ONLY ~29-21µ PiRep Guidelines Medium to Poor Airbus Operational Landing Distances International Air Safety Seminar 2011 Procedure • Always start assessment with contaminant type and depth • Use additional information to • Degrade to lower friction code • Never upgrade • Careful with friction reports • May be optimistic on fluid contaminants • Do not hesitate to request additional information from ATC International Air Safety Seminar 2011 Airbus Operational Landing Distances Examples Compact Snow Braking Action Medium Wet in Heavy Rain Storm Cells above Airport MEDIUM MEDIUM TO POOR Dry Snow over Ice, Braking Action Medium Compact Snow OAT 1ºC Dewpoint 1ºC NIL MEDIUM TO POOR International Air Safety Seminar 2011 Airbus Operational Landing Distances TALPA Rules in a Nutshell • Provide Runway Status Reports • Using Matrix and associated methodology • In a performance oriented way • Publish Realistic Landing Performance Data • In accordance with agreed rules • For all supported aircraft types • Make Systematic Landing Performance Check • In all cases except for dry runway • Apply a 15% margin to the result Airbus Operational Landing Distances International Air Safety Seminar 2011 Situation for Airbus – BEFORE • Publication for in-flight use • • • • Unfactored certified reference distances used for dispatch For incomplete list of contaminant types and depths Coverage of loose snow by equivalence only Inconsistent assumptions between dry/wet and contaminants for airborne phase • Operators must define their own margins • Pilots have difficulty in using published data with diverse runway condition reporting methods Airbus Operational Landing Distances Airbus Situation – AFTER • For all Airbus aircraft • At least “Minimum Compliance” with TALPA ARC • Cover all 6 friction levels • Accountability for • Temperature effect • Runway slope effect • Matrix as entry-point • All Performance data sources • • • • • Flight Ops Engineer Software Flight Manual Operational Documentation Electronic Flight Bag Training Material International Air Safety Seminar 2011 International Air Safety Seminar 2011 Airbus Operational Landing Distances A320 in Tegucigalpa / Honduras MHTG/TGU RWY 02 LDA 5410ft / 1649m Elevation 3287ft CONF FULL / VREF+5 / no wind / OAT 20ºC OLD LW FOLD Dry 64.5t Dry 1330m 1520m (no rev) Wet 59.9t Good 1600m 1830m (all rev) Standing Water 53.8t Med to Poor 1910m 2200m (all rev) Limited by MLW / Dispatch International Air Safety 21-24 March 2011 Seminar 2011 17th Flight Airbus Operational Safety Conference Landing Distances Airbus Implementation Schedule Feb 2010 Presentation of Octopus specification to EASA Aug 2010 Communication to Airlines Q1 2011 Start of PEP/LPC Validation Apr 2011 PEP/FM Approval by EASA Q2 2011 Finalisation of Publication Method and Format Q3 2011 Start of Production of Documentation Q4 2011 OCTOPUS v28 Certification by EASA Mid 2012 Publication for A318/319/320/321/330/340 Q3 2012 Publication for A306/310/380 Page 10 Airbus Operational Landing Distances Operational Documentation - QRH International Air Safety Seminar 2011 Airbus Operational Landing Distances EFB Landing Application International Air Safety Seminar 2011 Airbus Operational Landing Distances EFB Landing Application International Air Safety Seminar 2011 Airbus Operational Landing Distances EFB Landing Application International Air Safety Seminar 2011 Airbus Operational Landing Distances International Air Safety Seminar 2011 Conclusion • Airbus adopts TALPA ARC standard for in-flight landing performance including for non-normal and in ROPS • Realistic computation basis for all winter runway conditions • In current environment, pilot must compensate for non yet compliant Runway Condition Reporting • Major safety step change requires