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EASA- HighIWC Final Meeting

EASA HighIWC (EASA.2011.OP.28). Presented by Airbus - CNRS (LATMOS/BOM – LaMP – SAFIRE). EASA- HighIWC Final Meeting. Contingency Plan & Way Forward. EASA- HighIWC Final Meeting Content. Context HIWC – Key Facts & Status Contingency Plan(s) Conclusion & Way Forward.

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EASA- HighIWC Final Meeting

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  1. EASA HighIWC (EASA.2011.OP.28) Presented by Airbus - CNRS (LATMOS/BOM – LaMP – SAFIRE) EASA-HighIWC Final Meeting Contingency Plan & Way Forward EASA.2011.OP.28

  2. EASA-HighIWC Final MeetingContent EASA.2011.OP.28 • Context • HIWC – Key Facts & Status • Contingency Plan(s) • Conclusion & WayForward

  3. EASA-HighIWC Final MeetingContent EASA.2011.OP.28 • Context • HIWC – Key Facts & Status • Contingency Plan(s) • Conclusion & WayForward

  4. EASA-HighIWC Final MeetingContext CDP-ROBUST 2D-S CPI Imager PIP Nevzorov & RICE EASA.2011.OP.28 • Motivation to use F20 in addition to G-II • Retrieve in situ IWC on F20 flight level (-50°C, -30°C, -10°C). • Validate the Doppler cloud radar estimates of IWC in HighIWC regions (retrieved from reflectivity and Doppler velocity) using G-II and Falcon 20 in situ data. • And use the validated radar estimates to take advantage of the vertical resolution of the cloud radar to extrapolate the IWC & PSD in situ data (G II & F20 trajectories) for the new icing envelope calculations.

  5. EASA-HighIWC Final MeetingContent EASA.2011.OP.28 • Context • HIWC – Key Facts & Status • Contingency Plan(s) • Conclusion & WayForward

  6. EASA-HighIWC Final MeetingHIWC National Aeronautics and Space Administration Federal Aviation Administration High Ice Water Content (HIWC) Flight Campaign Status EASA.2011.OP.28 • Status in July/August 2012 • Primary Campaign delayed by one year (2013 -> 2014) because workmanship and QA lapses at FTA led to stop work and investigation/corrective action planning • Planning • A/C Modification completed by end January 2013 • Instrumentation checks, calibrations, … (Jan-April, 2013) • Ground testing (April 2013) • Qualification Flights (April-June 2013) • Trial Campaign (Florida, August 2013) • Instrumentation repair/modification period (Sept-Nov, 2013) • Primary Campaign (Darwin, Jan-March 2014)

  7. EASA-HighIWC Final MeetingHIWC National Aeronautics and Space Administration Federal Aviation Administration High Ice Water Content (HIWC) Flight Campaign Status EASA.2011.OP.28 • Status in September 2012 • On September 18th NASA management, procurement and legal personnel visited FTA. They briefed NASA on FTA's financial capability as it relates to its ability to perform the contract. • On September 25th FTA communicated to their employees not to report to work until further notice. • To reduce risk exposure to NASA and its partners all government (and partner) provided equipment at FTA were moved to the fullest extent possible to NASA DFRC for storage. Shipment of equipment started on September 26th. • Note: EASA-HighIWC / HIWC / HAIC meeting held on September 24th, 2012 with the objective to reviewcontingency plan(s) and definewayforward

  8. EASA-HighIWC Final MeetingHIWC National Aeronautics and Space Administration Federal Aviation Administration High Ice Water Content (HIWC) Flight Campaign Status EASA.2011.OP.28 • Status in October 2012 • On October 19, 2012 NASA issued a contract termination notice to Flight Test Associates. • NASA and Environment Canada have secured all equipment on the aircraft including the instrument racks and associated avionics. Some items were not removed from the aircraft (i.e. satcom antenna) as they were too integrated into the aircraft. • Threshold Aviation Group (TAG) ferried the Gulfstream N81RR to the ChinoAirport on November 3rd, 2012

  9. EASA-HighIWC Final MeetingHIWC National Aeronautics and Space Administration Federal Aviation Administration High Ice Water Content (HIWC) Flight Campaign Status EASA.2011.OP.28 • Status in November 2012 • HIWC Progress meeting held on 01/11/2012 • HIWC Progress meeting held on 08/11/2012 • NASA/FAA Top Management meeting held on November 20th, 2012 • No viable options for the G-II, or other NASA A/C, to support a 2014 fieldcampaign • The only viable option for a backup to the G-II contract aircraft is the High Altitude Ice Crystal (HAIC) European Union project Falcon 20 atmospheric research platform pending IKP re-design and additional F/H • Although the Falcon-20 will address many HIWC objectives, the G-2 is also required to fulfill un-addressed or incompletely addressed objectives as defined in Engine Harmonization WG meetings and the HIWC Science Plan

  10. EASA-HighIWC Final MeetingHIWC National Aeronautics and Space Administration Federal Aviation Administration High Ice Water Content (HIWC) Flight Campaign Status EASA.2011.OP.28 • Status in November 2012 • NASA/FAA Top Management meeting held on November 20th, 2012 / CONCLUSION • BothAssociateAdministrators ( FAA- Aviation Safety and NASA- Aeronautics) support the objectives of the HIWC flight researchproject and the continueddevelopment of an aircraft option (the G-II is the mostlikely candidate) for a full complement of instruments to conduct a fieldcampaign in icecrystalenvironments.  It ispresumedatthis time thatpathwilltakeat least until 2015 and could have more than one deployment. • The outcome of the Falcon 20 contingency discussions isthatboth the AssociateAdministratorswantsomeadditional information before a final decisioncanbe made

  11. EASA-HighIWC Final MeetingContent EASA.2011.OP.28 • Context • HIWC – Key Facts & Status • Contingency Plan(s) • Conclusion & WayForward

  12. EASA-HighIWC Final MeetingContingency Plan(s) EASA.2011.OP.28

  13. EASA-HighIWC Final MeetingContingency Plan(s) EASA.2011.OP.28

  14. EASA-HighIWC Final MeetingContingency Plan(s) Weight: 57kg External Diam: 225mm Length: 1.85m Power: 5kW Weight: 30kg External Diam: 176mm Length: 1.00m Power: 2.5kW EASA.2011.OP.28 IKP Re-design Status: NRC completed assessment of IKP re-design to meet Falcon 20 pylon structural, drag, and electrical limits: IKP re-design can meet Falcon 20 constraints to operate on their aircraft Issue: FAA/NASA AssociateAdministratorswantsomeadditional information before a final decisioncanbe made regardingadditionalfunding

  15. EASA-HighIWC Final MeetingContingency Plan(s) EASA.2011.OP.28

  16. EASA-HighIWC Final MeetingContingency Plan(s) Weight: 57kg External Diam: 225mm Length: 1.85m Power: 5kW Weight: 30kg External Diam: 176mm Length: 1.00m Power: 2.5kW EASA.2011.OP.28 IKP Re-design Status: NRC completed assessment of IKP re-design to meet Falcon 20 pylon structural, drag, and electrical limits: IKP re-design can meet Falcon 20 constraints to operate on their aircraft Issue: FAA/NASA AssociateAdministratorswantsomeadditional information before a final decisioncanbe made regardingadditionalfunding

  17. EASA-HighIWC Final MeetingContingency Plan(s) EASA.2011.OP.28 • HIWC position • Two international partners stated that if NASA cannot complete a 2014 field campaign, they do not think their management will support further delays. These partners are critical to the HIWC team success • HAIC Position • HAIC agreed to support the 2014 Darwin Campaign • Associated delay mitigated thanks to further use of Airbus F/T campaign (Darwin, Cayenne, Chile) • Furtherdelaywill not be acceptable

  18. EASA-HighIWC Final MeetingContingency Plan(s) EASA.2011.OP.28 • HIWC position • Two international partners stated that if NASA cannot complete a 2014 field campaign, they do not think their management will support further delays. These partners are critical to the HIWC team success • HAIC Position • HAIC agreed to support the 2014 Darwin Campaign • Associated delay mitigated thanks to further use of Airbus F/T campaign (Darwin, Cayenne, Chile) • Furtherdelaywill not be acceptable

  19. EASA-HighIWC Final MeetingContingency Plan(s) EASA.2011.OP.28 • Remaining Scenarios / Option C.1 • IKP Redesignfeasibilitycompleted • NRC confirmedthat IKP re-design canmeet F20 requirements • IKP shouldbeavailable in Summer 2013 for installation and certification on F20 • Support from HAIC and HIWC teams • Preliminary F20 payloaddefined • Open Points • FAA fundingfor IKP re-design • Re-affirmthat the FAA sponsors still support the flight campaign and the mitigation strategiesbeingdeveloped. • Review how those mitigation strategieswillbeimplemented/supportedwithin the FAA • Workwith HIWC science team members to provide a complete description of what the Falcon 20 woulddeliver in 2014 to both the new rulemakingAppendix D for icecrystals and how this flight campaigncouldaddresscurrentfleet issues for mitigating the icecrystalthreat • Fundingfor additional F/H

  20. EASA-HighIWC Final MeetingContingency Plan(s) EASA.2011.OP.28 • Remaining Scenarios / Option D.1 • Support from HAIC and HIWC teams • Preliminary F20 payloaddefined • Open Points • Fundingfor additional F/H

  21. EASA-HighIWC Final MeetingContent EASA.2011.OP.28 • Context • HIWC – Key Facts & Status • Contingency Plan(s) • Conclusion & WayForward

  22. EASA-HighIWC Final MeetingConclusion & Way Forward EASA.2011.OP.28 • Conclusion • Major changes wrtassumptionstaken to build EASA-HighIWC and HAIC project • Summer 2012: Darwin Field campaign, originallyplanned in Q1 2013, postponed to 2014 due to FTA QA issue • November 2012: NASA G-II not available in Q1 2014 due to contractterminationwith FTA • 2014 Field campaigniscritical for HAIC projectand can’tbefurtherpostponed. • Contingency plan: F20 to be the primary A/C in Q1 2014 • The 2014 fieldcampaign has to besecured

  23. EASA-HighIWC Final MeetingConclusion & Way Forward EASA.2011.OP.28 • Option C.1 is the prefered scenario • WayForward • IKP feasibilitystudycompleted: NRC confirmedthat IKP re-design canmeet F20 requirements • Open points • FAA funding to besecured • Action to provide a complete description of what the Falcon 20 woulddeliver in 2014 to both the new rulemakingAppendix D for icecrystals and how this flight campaigncouldaddresscurrentfleet issues for mitigating the icecrystalthreat • Funding to besecured for addtional F/H

  24. EASA-HighIWC Final MeetingConclusion & Way Forward EASA.2011.OP.28 Actions to secure the Option C.1

  25. Ice Water Content of clouds at High altitude (EASA HighIWC, EASA.2011.OP.28) This document and the information contained are EASA HighIWC Contractors’ property and shall not becopied or disclosed to any third party without EASA HighIWC Contractors’ prior written authorization Project funded by the European Aviation SafetyAgency(EASA) EASA.2011.OP.28

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