{"id":657,"date":"2019-07-21T13:38:55","date_gmt":"2019-07-21T11:38:55","guid":{"rendered":"https:\/\/htps.aero\/?page_id=657"},"modified":"2025-05-08T12:31:14","modified_gmt":"2025-05-08T10:31:14","slug":"projects","status":"publish","type":"page","link":"https:\/\/htps.aero\/?page_id=657&lang=en","title":{"rendered":"Projects"},"content":{"rendered":"\t\t
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Flight Validation of PBN LFN airways in Austria<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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Flight validation of three airways of a newly developed Performance Based Navigation (PBN) Low Flight Network (LFN) for helicopters in Austria.<\/p>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t

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Flight Validation of PinS IFP at LOBE and LODC<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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Flight validation of the Point-in-Space (PinS) helicopter Instrument Flight Procedures (IFP) developed for the LOBE (Frauenkirchen) and LODC (St. Michael in der Obersteiermark) helicopter bases.<\/p>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t

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ADOA Flight Test Operations Manual<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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Creation of a Flight Test Operations Manual (FTOM) for a German design organization with Alternative Procedures to Design Organization Approval (ADOA).<\/p>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t

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A\u00e9rospatiale AS332 L1 BPKC<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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Supplemental Type Certificate (STC) for a Basic Protection Kit Cockpit (BPKC) developed for the A\u00e9rospatiale AS332 L1 Super Puma of the German Federal Police.<\/p>

It included category 2 flight tests in reference to EASA CS-29. The ground and flight test evaluation included the following areas:<\/p>

  • Pilot Compartment and Anthropometry<\/li>
  • Safety of Crew Accommodation<\/li>
  • Normal and Emergency Entry and Egress<\/li>
  • Pilot Field of View<\/li>
  • Flight Control Evaluation<\/li>
  • Lighting Environment<\/li>
  • Accessibility of Safety Equipment<\/li>
  • Vibration Measurement and Assessment<\/li><\/ul>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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    F-Light Line EC-135 T3H FTD Level 3<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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    Development and qualification of the Synthetic Training Device newly developed by Reiser Simulation and Training GmbH and RS Flight Systems GmbH for the Austrian Approved Training Organization Rotorsky GmbH:<\/p>

    • Flight Training Device (FTD) Level III (Type Rating H135 VFR\/IFR)<\/li>
    • Flight and Navigation Procedure Trainer (FNPT) for ab-initio training programs (PPL, \u00a0CPL, IR, MCC)<\/li>
    • Helicopter Emergency Medical Services (HEMS) operation including Technical Crew Member (TCM) training<\/li><\/ul>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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      Airbus Helicopters EC-135 T3H NVIS<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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      Supplemental Type Certificate (STC) for a Night Vision Imaging System (NVIS) compatible external and internal lighting of the EC-135 T3H (Helionix cockpit configuration).<\/p>

      It included category 2 flight tests in reference to EASA CS-27 and RTCA DO-275. The ground and flight test evaluation included the following areas:<\/p>

      • Daylight control\/display readability<\/li>
      • Night unaided control\/display readability<\/li>
      • NVG compatibility<\/li>
      • Reflections and glare<\/li>
      • Operational suitability<\/li><\/ul>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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        MBB BO-105 Utility Mount<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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        Supplemental Type Certificate (STC) for a newly developed „utility-mount“ used for a Shotover camera system on a MBB BO-105S helicopter.<\/p>

        It included category 2 flight tests in reference to EASA CS-27 for verification of<\/p>

        • Flying Qualities<\/li>
        • Performance<\/li>
        • Vibration and Flutter<\/li>
        • VNE<\/sub><\/li><\/ul>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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          Agusta Bell 212 \/ Bell 412 FastFin\u00ae<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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          Aim of the project was to verify the proposed statements including<\/p>

          • improved hover out of ground effect (HOGE) loads,<\/li>
          • improved hover-hold in challenging crosswinds,<\/li>
          • improved stability in all hover operations and<\/li>
          • elimination of loss of tail rotor effectiveness (LTE).<\/li><\/ul>

            It included category 4 flight tests of the BLR Aerospace FastFin\u00ae in reference to EASA CS-29 for verification of<\/p>

            • Flying Qualities<\/li><\/ul>
              • Performance<\/li><\/ul>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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                Agusta Bell 212 Mid-Life Update<\/h2>\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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                Aim of the project was the issuance of a supplemental type certificate (STC) for the Agusta Bell 212 Mid-Life Update. The focus was on reducing the pilot\u00b4s work load while increasing the situational awareness and flight safety.<\/p>

                It included software development, cockpit layout definition and category 2, 3 and 4 ground and flight tests in reference to EASA CS-29, RTCA DO-229C, RTCA DO-200A and ARINC 424-18 for evaluation and verification of the new<\/p>

                • Avionics systems<\/u>\u2013 Mission management system, communication and integrated navigation systems<\/li>
                • Helmet Mounted Display (HMD)<\/u> \u2013 Symbology development, HMD-design with respect to operational requirements<\/li><\/ul>
                  • Night Vision Goggles (NVG)<\/u> \u2013 Helicopter interior and exterior lighting to meet NVG lighting specifications<\/li><\/ul>\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t
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                    <\/div>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t\t\t\t<\/div>\n\t\t","protected":false},"excerpt":{"rendered":"

                    Flight Validation of PBN LFN airways in Austria Flight validation of three airways of a newly developed Performance Based Navigation (PBN) Low Flight Network (LFN) for helicopters in Austria. Flight Validation of PinS IFP at LOBE and LODC Flight validation of the Point-in-Space (PinS) helicopter Instrument Flight Procedures (IFP) developed for the LOBE (Frauenkirchen) and…<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":686,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":[],"_links":{"self":[{"href":"https:\/\/htps.aero\/index.php?rest_route=\/wp\/v2\/pages\/657"}],"collection":[{"href":"https:\/\/htps.aero\/index.php?rest_route=\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/htps.aero\/index.php?rest_route=\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/htps.aero\/index.php?rest_route=\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/htps.aero\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=657"}],"version-history":[{"count":42,"href":"https:\/\/htps.aero\/index.php?rest_route=\/wp\/v2\/pages\/657\/revisions"}],"predecessor-version":[{"id":1367,"href":"https:\/\/htps.aero\/index.php?rest_route=\/wp\/v2\/pages\/657\/revisions\/1367"}],"up":[{"embeddable":true,"href":"https:\/\/htps.aero\/index.php?rest_route=\/wp\/v2\/pages\/686"}],"wp:attachment":[{"href":"https:\/\/htps.aero\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=657"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}