{"id":201898,"date":"2023-02-26T20:32:47","date_gmt":"2023-02-26T11:32:47","guid":{"rendered":"https:\/\/kikakumaster.com\/mil-spec\/air-vehicle-technical-description-report-for-rotorcraft-and-propeller-driven-fixed-wing-aircraft\/"},"modified":"2023-03-03T17:08:53","modified_gmt":"2023-03-03T08:08:53","slug":"di-sess-82291","status":"publish","type":"mil-spec","link":"https:\/\/kikakumaster.com\/ja\/mil-spec\/di-sess-82291\/","title":{"rendered":"DI-SESS-82291 &#8211; Air Vehicle Technical Description Report for Rotorcraft and Propeller-Driven Fixed-Wing Aircraft"},"content":{"rendered":"<p>This Data Item Description (DID) specifies the technical data and supplementary technical data necessary for Government assessments of the flight performance, stability and control, handling qualities, rotor dynamics, airframe dynamics, engine\/drive system response characteristics, and transportability characteristics of new design or derivative rotary-wing and propeller-driven fixed-wing aircraft. These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62 (Copies of this AR are available from armypubs.army.mil.), and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e). (Copies of this reference are available from www.acquisition.gov\/browse\/index\/far.)<\/p><div id=\"kikak-3013034180\" class=\"kikak- kikak-entity-placement\"><p><a href=\"https:\/\/click.linksynergy.com\/fs-bin\/click?id=tuVq3VflqQM&amp;offerid=208750.10000028&amp;subid=0&amp;type=4\"><img class=\"lazyload\" decoding=\"async\" src=\"data:image\/gif;base64,R0lGODlhAQABAAAAACH5BAEKAAEALAAAAAABAAEAAAICTAEAOw==\" data-orig-src=\"https:\/\/ad.linksynergy.com\/fs-bin\/show?id=tuVq3VflqQM&amp;bids=208750.10000028&amp;subid=0&amp;type=4&amp;gridnum=16\" alt=\"American National Standards Institute Inc.\" border=\"0\" \/><\/a><\/p>\n<\/div>\n<p><a href=\"https:\/\/quicksearch.dla.mil\/qsDocDetails.aspx?ident_number=283282\">Go to DI-SESS-82291 at DAPS Quick Search ASSIST<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p>This Data Item Description (DID) specifies the technical data and supplementary technical data necessary for Government assessments of the flight performance, stability and control, handling qualities, rotor dynamics, airframe dynamics, engine\/drive system response characteristics, and transportability characteristics of new design or derivative rotary-wing and propeller-driven fixed-wing aircraft. These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62 (Copies of this AR are available from armypubs.army.mil.), and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e). (Copies of this reference are available from www.acquisition.gov\/browse\/index\/far.)<\/p>\n","protected":false},"featured_media":0,"template":"","categories":[3244],"tags":[],"sdo":[1337],"topic":[],"fsc":[3566],"document_type":[3246],"class_list":["post-201898","mil-spec","type-mil-spec","status-publish","hentry","category-data-item-description","sdo-us-dod","fsc-sess","document_type-data-item-description"],"acf":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.2 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>DI-SESS-82291 - Air Vehicle Technical Description Report for Rotorcraft and Propeller-Driven Fixed-Wing Aircraft - \u898f\u683c\u30de\u30b9\u30bf\u30fc<\/title>\n<meta name=\"description\" content=\"Air Vehicle Technical Description Report for Rotorcraft and Propeller-Driven Fixed-Wing Aircraft - This Data Item Description (DID) specifies the technical data and supplementary technical data necessary for Government assessments of the flight performance, stability and control, handling qualities, rotor dynamics, airframe dynamics, engine\/drive system response characteristics, and transportability characteristics of new design or derivative rotary-wing and propeller-driven fixed-wing aircraft. These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62 (Copies of this AR are available from armypubs.army.mil.), and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e). 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These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62 (Copies of this AR are available from armypubs.army.mil.), and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e). 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These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62 (Copies of this AR are available from armypubs.army.mil.), and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e). 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These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62 (Copies of this AR are available from armypubs.army.mil.), and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e). 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These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62 (Copies of this AR are available from armypubs.army.mil.), and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e). 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