{"id":106107,"date":"2025-09-08T14:44:34","date_gmt":"2025-09-08T12:44:34","guid":{"rendered":"https:\/\/ilot.lukasiewicz.gov.pl\/offer\/manufacturing\/przyrzady-i-systemy-pokladowe\/"},"modified":"2025-12-09T15:16:38","modified_gmt":"2025-12-09T14:16:38","slug":"on-board-instruments-and-systems","status":"publish","type":"page","link":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/offer\/manufacturing\/on-board-instruments-and-systems\/","title":{"rendered":"On-board instruments and systems"},"content":{"rendered":"\t\t
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On-board instruments and systems<\/h1>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t
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Home<\/a> <\/i><\/span> Page<\/span><\/div>\t\t<\/div>\n\t\t\t\t\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\t\t<\/div>\n\t\t
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Avionics equipment and systems <\/h2><\/span>\n\t\t\t\t\t\t\t\n\t\t\t<\/i><\/span>\n\t\t\t<\/i><\/span>\n\t\t<\/span>\n\n\t\t\t\t\t\t<\/summary>\n\t\t\t\t
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CRW\u201313 digital radio altimeter<\/h3>\n

Electronic block (2500 ft)<\/p>\n

Digital radio altimeter \u2013 features.<\/strong><\/p>\n

    \n
  • Digital altitude signal processing based on the FFT algorithm.<\/li>\n
  • Transmitter-receiver device built together with antennas.<\/li>\n
  • Installation without antenna cables and shock absorbing frame.<\/li>\n
  • Low height allows installation in a low hull profile.<\/li>\n<\/ul>\n

    CRW\u201313 has analog output and ARINC 429 for cooperation with GPWS, TCAS, Autopilot systems.<\/p>\n

    CRW\u201313 \u2013 specification<\/b><\/p>\n

      \n
    • dimensions without flange: 3,15\u201dW x 1,77\u201dH x 7,09\u201dL (80 x 45 x 180 mm);<\/li>\n
    • weight: 1.05 kg,<\/li>\n
    • power supply: 14 V DC \/ 0.5 A nominal to 28 V DC \/ 0.3 A;<\/li>\n
    • altitude: 55,000 ft;<\/li>\n
    • operating temperature range: -45\u2070C to +60\u2070C;<\/li>\n
    • transmitter output: 150 mW FMCW, 100 Hz modulation;<\/li>\n
    • operating frequency: 4300 \u00b120 MHz;<\/li>\n
    • AID height: 2 ft to 20 ft (0,6 m to 6 m);<\/li>\n
    • accuracy: \u00b12 ft or \u00b12% from to 500 ft, \u00b13% from 500 to 2500 ft.<\/li>\n<\/ul>\n
        \n
      • Rwl\u2013750m AA\u2013E7 radio altimeter<\/li>\n
      • Electronic block (750 m)<\/li>\n
      • AA\u2013E4 electronic block (2500 ft)<\/li>\n<\/ul>\n

        Electronic block \u2013 features<\/b><\/p>\n

          \n
        • The AA\u2013E4 can work with the AA\u2013W4 indicator in the range up to 2500 ft;<\/li>\n
        • The AA\u2013E7 can work with the AA\u2013W7 indicator in the range up to 750 m;<\/li>\n
        • cooperation with two S67\u20132002 antennas (Sensor Systems);<\/li>\n
        • requires AA\u2013R4 shock absorbing frame;<\/li>\n
        • has an analog output and ARINC 429 for cooperation with GPWS, TCAS, Autopilot systems.<\/li>\n<\/ul>\n

          Electronic block \u2013 specification<\/b><\/p>\n

            \n
          • dimensions: 3,58\u201dW x 3,46\u201dH x 10,04\u201dL (91 x 88 x 255 mm);<\/li>\n
          • weight: 1.9 kg,<\/li>\n
          • power supply: 27,5 V DC \u00b120% 0,7A nominal;<\/li>\n
          • altitude: 55,000 ft;<\/li>\n
          • temperature: -45\u2070C to +60\u2070C;<\/li>\n
          • transmitter output: 250 mW FMCW, 100 Hz modulation;<\/li>\n
          • frequency: 4300 \u00b120 MHz;<\/li>\n
          • AID height: 20 ft to 60 ft (6 m to 19 m);<\/li>\n
          • accuracy AA\u2013E4: \u00b12 ft 3% from to 500 ft, \u00b13% from 500 to 2500 ft;<\/li>\n
          • accuracy AA\u2013E7: \u00b10.6 m or \u00b13% from to 100 m, \u00b13% from 100 to 750 m.<\/li>\n<\/ul>\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/details>\n\t\t\t\t\t\t
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            Measuring and diagnostic devices <\/h2><\/span>\n\t\t\t\t\t\t\t\n\t\t\t<\/i><\/span>\n\t\t\t<\/i><\/span>\n\t\t<\/span>\n\n\t\t\t\t\t\t<\/summary>\n\t\t\t\t
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            Radio altimeter tester T4S<\/strong><\/p>\n\n

            T4S \u2013 features:<\/p>\n

              \n
            • easy connection to the RWL\u2013750M radio altimeter installation through two antenna couplers;<\/li>\n
            • A 1000 ft radio altitude simulator incorporating Teledyne Company precision delay line;<\/li>\n
            • manually adjustable attenuation of the simulator to measure the sensitivity of the radio altimeter with an accuracy of 2 dB;<\/li>\n
            • the possibility of connecting the simulator directly to the transceiver block<\/li>\n
            • the possibility of using the simulator to check other radio altimeters operating in the 4.3 GHz band. The built-in tuned calibrator generates a differential frequency signal, fed through the diagnostic cable of the RWL\u2013750M radio altimeter, allowing to check the decision altitude, fixed altitudes and altitude data transferred to EWGPS;<\/li>\n
            • all RWL\u2013750M outputs:\n
                \n
              • ARINC 429,<\/li>\n
              • precise analog output,<\/li>\n
              • indicator outputs are decoded,<\/li>\n
              • measured and displayed;<\/li>\n <\/ul>\n <\/li>\n
              • monitoring of the fixed altitudes, decision altitude and FCS Warn signal (performance signal). Using the tester, you can also check the indicator of the RWL\u2013750M tester;<\/li>\n
              • designed to work with all versions of the RWL\u2013750.<\/li>\n<\/ul>\n\n

                T4S<\/strong> \u2013 specification:<\/p>\n

                  \n
                • dimensions: 18,42\u201dW x 13,86\u201dH x 8,27\u201dL (468 x 352 x 210 mm);<\/li>\n
                • weight: 26 lbs (11.8 kg);<\/li>\n
                • power supply: 27,5 V DC \u00b120%, 0,15A nominal.<\/li>\n<\/ul>\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/details>\n\t\t\t\t\t\t
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                  Manufacturing Organization <\/h2><\/span>\n\t\t\t\t\t\t\t\n\t\t\t<\/i><\/span>\n\t\t\t<\/i><\/span>\n\t\t<\/span>\n\n\t\t\t\t\t\t<\/summary>\n\t\t\t\t
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                  Manufacturing Organization, approved by the Civil Aviation Authority under Regulation (EC) No 216\/2008 of the European Parliament and of the Council and Commission Regulation (EC) No 1702\/2003 in accordance with Annex (Part 21), Section A, Subpart G, is authorized to manufacture products, parts and accessories listed in its list of approval, and to issue a production certificate in the EASA FORM 1.<\/p>\n\n

                  Currently, the range of products manufactured by the \u0141ukasiewicz Manufacturing Organization \u2013 Institute of Aviation includes:<\/p>\n\n

                  In terms of EASA approval:<\/p>\n

                    \n
                  • For PZL M28 Bryza and Skytruck aircraft:\n
                      \n
                    • PPM\u20131, PPM\u20131B fuel gauge (including analog-digital indicators, digital indicators, electronic blocks, transmitters and fuel level indicators);<\/li>\n
                    • SN1C\/5 fuel level indicators;<\/li>\n
                    • BRO\u20132 lighting blocks.<\/li>\n <\/ul>\n <\/li>\n
                    • For I\u201323 aircraft:\n
                        \n
                      • SR\/2 remaining fuel indicators.<\/li>\n <\/ul>\n <\/li>\n<\/ul>\n\n

                        Beyond approval (ISO\/AQAP):<\/p>\n

                          \n
                        • For PZL M28 Bryza aircraft:\n
                            \n
                          • radio altimeter RWL\u2013750M (including analog indicators \u2013 servo mechanical and electronic blocks);<\/li>\n
                          • TPPM\u20131 fuel meter testers;<\/li>\n
                          • radio altimeter testers.<\/li>\n <\/ul>\n <\/li>\n
                          • For the PZL\u2013130 Orlik aircraft:\n
                              \n
                            • RWL\u2013750M\/O radio altimeter;<\/li>\n
                            • SR\/2remaining fuel indicators;<\/li>\n
                            • rudder automatic trim tab \u2013 ATSK.<\/li>\n <\/ul>\n <\/li>\n
                            • For the PZL W3 Sok\u00f3\u0142 helicopter:\n
                                \n
                              • radio altimeter RWL\u2013750M (including analog indicators \u2013 servo mechanical and electronic blocks);<\/li>\n
                              • torque meter testers.<\/li>\n <\/ul>\n <\/li>\n<\/ul>\n\n

                                Certificate of the approved Manufacturing Organization of the \u0141ukasiewicz Research Network \u2013 Institute of Aviation No. PL.21G.034 (Part 21).<\/p>\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/details>\n\t\t\t\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t

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                                We carry out scientific and research and design-construction work, as well as small-batch manufacturing in the fields of avionics equipment and systems, measurement and diagnostic equipment, and electrical installations and systems for airplanes, helicopters and unmanned aerial vehicles.<\/p>\n

                                We offer design and construction works in the following scope:<\/p>\n

                                  \n
                                • Systems related to the movement of aircraft and RPAS in civil airspace, in all phases of flight.<\/li>\n
                                • Avionic systems, in particular stabilization and classic, indirect and automatic control of the aircraft, RPAS, satellites and other control systems.<\/li>\n
                                • Avionics devices for measuring motion parameters (e.g.: CDA, radio altimeter), spatial position (e.g.: INS, AHRS) and operating parameters (e.g. fuel gauge).<\/li>\n
                                • Mathematical modeling of aircraft flight dynamics.<\/li>\n
                                • Designing microprocessor systems as calculators dedicated to measuring systems and devices, stabilization, control and diagnostic systems, with particular emphasis on avionics equipment of aircraft, RPAS, satellites, as well as other devices and system components that require the use of a computing platform for the implementation of numerical algorithms.<\/li>\n
                                • Rapid prototyping of avionic devices, their assembly and certified production for a commercial user.<\/li>\n
                                • Testing of resistance and strength to mechanical and climatic factors of the technical devices and installations.<\/li>\n
                                • Expert opinions and tests as well as assessment of aeronautical\u00a0 <\/span>equipment, systems and installations completed with the issuance of a certificate of compliance with aviation standards and regulations: RTCA, ARINC, MIL, TSO.<\/li>\n
                                • Prototyping and manufacturing of small batch precision equipment:
                                  measuring, indicating and diagnostic.<\/li>\n<\/ul>\n

                                  We perform expertise, testing and evaluation of aeronautical equipment, systems and installations, culminating in the issuance of a certificate of compliance with aviation standards and regulations: RTCA, ARINC, MIL, TSO. We have a workshop base that allows prototyping and small batch production of precision equipment: measuring, indicating and diagnostic. We have workstations and apparatus that allow us to carry out comprehensive testing of the devices and products made.<\/p>\n

                                  The products developed and made by us are on the outfit of many Polish aircraft and laboratories. Particularly noteworthy are:<\/p>\n

                                    \n
                                  • fuel gauges for the following aircraft: Iryda, M28 Bryza\/Skytruck and the W-3 Sok\u00f3\u0142 helicopter;<\/li>\n
                                  • RWL\u2013750M radio altimeters used on-board of the Iryda and Bryza aircraft and Anakonda helicopters;<\/li>\n
                                  • a torque meter unit used on-board of the W-3 Sok\u00f3\u0142 helicopter;<\/li>\n
                                  • signaling and lighting systems used on-board of the Iryda and Skytruck aircraft;<\/li>\n
                                  • autonomous control system of an unmanned aerial vehicle;<\/li>\n
                                  • analog-digital RAC recorder, designed to record analog and\/or digital data, record data from the GPS receiver, store the recorded values in the internal memory and read the recorded data on a personal computer;<\/li>\n
                                  • GPPA-3, GPPA\u20134 transients generators, GWE-2 electrostatic discharge generators;<\/li>\n
                                  • AROS autonomous recorder of fatigue loads;<\/li>\n
                                  • testers for TRS 6113-2 radio station, TPPM-1 fuel gauge, T4S radio altimeter, UD-100M torque meter gauge, MRT-3 radio navigation devices and systems;<\/li>\n
                                  • rudder trim tab controller for the \u201cOrlik\u201d aircraft.<\/li>\n<\/ul>\n

                                    ATSK \u2013 rudder automatic trim tab for the PZL\u2013130 Orlik aircraft<\/b><\/p>\n

                                    ATSK is designed for automatic trim of the rudder in the aircraft. It improves the flight characteristics of the aircraft and increases the safety and comfort of the pilot\u2019s work. Structurally, it is one device with three connectors, which generates signals controlling the rudder trim on the basis of input data concerning the engine operating parameters, speed and configuration of the aircraft.<\/p>\n

                                    Basic technical data:<\/p>\n

                                      \n
                                    • 182+(50 ) x 126 x 66.5 mm;<\/li>\n
                                    • weight: 800 g \u00b1100 g (without connectors and harnesses);<\/li>\n
                                    • power supply: 27.5 V DC;<\/li>\n
                                    • power consumption: < 0.5 A no current in loads;<\/li>\n
                                    • operating temperatures range: \u2012<\/span>35 \u00f7 +70\u2070<\/span>C;<\/li>\n
                                    • survival temperature range: \u2012<\/span>55 \u00f7 +85\u2070<\/span>C.<\/li>\n
                                    • operating conditions: operation in any spatial position of the aircraft;<\/li>\n
                                    • standby time: no more than 60 s after power supply;<\/li>\n
                                    • storage conditions:
                                      \n
                                        \n
                                      • recommended temperature range +10 \u00f7 +30\u2070<\/span>C,<\/li>\n
                                      • humidity < 80%;<\/li>\n<\/ul>\n<\/li>\n
                                      • environmental qualification:
                                        \n
                                          \n
                                        • according to DO\u2013160,<\/li>\n
                                        • according to NO 06\u2013A\u2013101.<\/li>\n<\/ul>\n<\/li>\n<\/ul>\n<\/div>\n<\/div>\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t","protected":false},"excerpt":{"rendered":"

                                          Home Strona Avionics equipment and systems CRW\u201313 digital radio altimeter Electronic block (2500 ft) Digital radio altimeter \u2013 features. Digital altitude signal processing based on the FFT algorithm. Transmitter-receiver device built together with antennas. Installation without antenna cables and shock absorbing frame. Low height allows installation in a low hull profile. CRW\u201313 has analog output […]<\/p>\n","protected":false},"author":208,"featured_media":0,"parent":106094,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_acf_changed":false,"_seopress_robots_primary_cat":"","_seopress_titles_title":"","_seopress_titles_desc":"","_seopress_robots_index":"","inline_featured_image":false,"footnotes":""},"class_list":["post-106107","page","type-page","status-publish","hentry"],"acf":{"czas_czytania":"3","wyroznij":"0"},"publishpress_future_action":{"enabled":false,"date":"2026-05-13 11:31:40","action":"change-status","newStatus":"draft","terms":[],"taxonomy":"translation_priority","extraData":[]},"publishpress_future_workflow_manual_trigger":{"enabledWorkflows":[]},"_links":{"self":[{"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/pages\/106107","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/users\/208"}],"replies":[{"embeddable":true,"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/comments?post=106107"}],"version-history":[{"count":4,"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/pages\/106107\/revisions"}],"predecessor-version":[{"id":106112,"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/pages\/106107\/revisions\/106112"}],"up":[{"embeddable":true,"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/pages\/106094"}],"wp:attachment":[{"href":"https:\/\/ilot.lukasiewicz.gov.pl\/en\/wp-json\/wp\/v2\/media?parent=106107"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}