DOU 01/11/2024 - Diário Oficial da União - Brasil

TEXTO OFICIAL · ÍNTEGRA

Documento assinado digitalmente conforme MP nº 2.200-2 de 24/08/2001, que institui a Infraestrutura de Chaves Públicas Brasileira - ICP-Brasil. Este documento pode ser verificado no endereço eletrônico http://www.in.gov.br/autenticidade.html, pelo código 05152024110100240 240 Nº 212, sexta-feira, 1 de novembro de 2024 ISSN 1677-7042 Seção 1 ÓRGÃO: 20000 - Presidência da República UNIDADE: 20204 - Instituto Nacional de Tecnologia da Informação - ITI ANEXO II Outras Alterações Orçamentárias PROGRAMA DE TRABALHO ( REDUÇÃO ) Recurso de Todas as Fontes R$ 1,00 .P R O G R A M ÁT I C A .P R O G R A M A / AÇ ÃO / LO C A L I Z A D O R / P R O D U T O .FUNCIONAL .E S F .G N D .R P .M O D .I U .F T E V A LO R 2301 Transformação do Estado para a Cidadania e o Desenvolvimento 313.973 .At i v i d a d e s 2301 217Z Gestão do Sistema Nacional de Certificação Digital da Infraestrutura de Chaves Públicas - ICP - Brasil e de outras tecnologias de segurança da informação e identificação digital 04 125 313.973 2301 217Z 0001 Gestão do Sistema Nacional de Certificação Digital da Infraestrutura de Chaves Públicas - ICP - Brasil e de outras tecnologias de segurança da informação e identificação digital - Nacional 04 125 313.973 F 3- ODC 2 90 0 1050 283.096 . . . .F .3- ODC .2 .90 .0 .1052 30.877 .TOTAL - FISCAL 313.973 .TOTAL - SEGURIDADE 0 .TOTAL - GERAL 313.973 Ministério de Portos e Aeroportos AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL SUPERINTENDÊNCIA DE AERONAVEGABILIDADE PORTARIA Nº 15.760, DE 31 DE OUTUBRO DE 2024 O SUPERINTENDENTE DE AERONAVEGABILIDADE, no uso das atribuições que lhe conferem o art. 35 do Regimento Interno, aprovado pela Resolução nº 381, de 14 de junho de 2016, e considerando o que consta do processo nº 00058.073662/2023-38, resolve: Art. 1º Tornar público, nos termos do Anexo desta Portaria, o documento de Critérios de Aeronavegabilidade de Classe Especial para a aeronave Modelo EVE-100 da EVE SOLUÇÕES DE MOBILIDADE AÉREA URBANA LTDA. Art. 2º Esta Portaria entra em vigor na data de sua publicação. ROBERTO JOSÉ SILVEIRA HONORATO ANEXO CRITÉRIOS FINAIS DE AERONAVEGABILIDADE EVE-100 SUBPART A - GENERAL EVE.2000 - Applicability and definitions. (a) These airworthiness criteria prescribe airworthiness standards for the issuance of a type certificate, and changes to that type certificate, for the EVE Soluções de Mobilidade Aérea Urbana LTDA, Model EVE-100. (b) For purposes of these airworthiness criteria, the following definitions apply: (1) Continued safe flight and landing - (i) for "essential performance" means the aircraft is capable of continued controlled flight and landing, possibly using emergency procedures, without requiring exceptional pilot skill, strength, or alertness (ii) for "increased performance" means the aircraft is capable of climbing to a safe altitude, on a flightpath clear of obstacles, and maintaining level flight to a planned destination or alternate landing, possibly using emergency procedures, without requiring exceptional pilot skill, strength, or alertness. (2) Phases of flight means ground operations, takeoff, climb, cruise, descent, approach, hover, and landing. (3) Source of lift means one of three sources of lift: thrust–borne, wing–borne, and semi-–thrust–borne. Thrust–borne is defined as when the weight of the aircraft is predominately supported by lift generated by engine-driven lift devices. Wing–borne is defined as when the weight of the aircraft is predominately supported by aerodynamic lift from fixed airfoil surfaces. Semi–thrust–borne is the combination of thrust–borne and wing–borne, where both forms of lift are used to support the weight of the aircraft. (4) Controlled emergency landing means the aircraft design allows direction and area of touchdown to be chosen while reasonably protecting occupants from serious injury, without requiring exceptional piloting skill or strength. Upon landing, some damage to the aircraft may be acceptable." (5) Critical change of thrust means the most adverse effects on performance or handling qualities resulting from failures of the flight control or propulsive system, either singular or in combination, not shown to be extremely improbable. (6) Local events are failures of aircraft systems and components, other than the engine control system, that may affect the installed environment of the engine or propeller control system. (7) Approved flight envelope means the flight envelope composed of (i) the flight envelope associated to routine operational and/or prescribed conditions and (ii) the flight envelope associated to warning onset cases excluding situations associated to aircraft design limits or hard protection limits. EVE.2005 - Reserved. EVE.2010 - Accepted means of compliance. (a) An applicant must comply with this regulation using a means of compliance, which may include consensus standards, accepted by the ANAC. (b) An applicant requesting acceptance of a means of compliance must provide the means of compliance to ANAC in a form and manner acceptable to A N AC . SUBPART B - FLIGHT PERFORMANCE EVE.2100 - Weight and center of gravity (a) The applicant must determine limits for weights and centers of gravity that provide for the safe operation of the aircraft. (b) The applicant must comply with each requirement at critical combinations of weight and center of gravity within the aircraft's range of loading conditions using tolerances acceptable to ANAC. (c) The condition of the aircraft at the time of determining its empty weight and center of gravity must be well defined and easily repeatable. EVE.2105 - Performance data (a) Unless otherwise prescribed, the aircraft must meet the performance requirements of this subpart in still air and standard atmospheric conditions. (b) Unless otherwise prescribed, the applicant must develop the performance data required for the following conditions: (1) Altitudes from the minimum to the maximum altitude for which certification is being sought; and (2) Temperatures above and below standard day temperature that are within the range of operating limitations, if those temperatures could have a negative effect on performance. (c) The procedures used for determining takeoff and landing performance must be executable consistently by pilots of average skill in atmospheric conditions expected to be encountered in service. (d) Performance data determined in accordance with paragraph (b) of this section must account for losses due to atmospheric conditions, cooling needs, installation losses, downwash considerations, and other demands on power sources. (e) The hovering ceiling, in and out of ground effect, must be determined over the ranges of weight, altitude, and temperature, if applicable. (f) Continued safe flight and landing must be possible from any point within the approved flight envelope following a critical change of thrust. (g) Following a condition when the aircraft can no longer provide the commanded power or thrust for continued safe flight and landing, the aircraft must be capable of a controlled emergency landing without requiring exceptional pilot skill, strength, or alertness. EVE.2110 - Minimum safe speed. The applicant must determine the aircraft minimum safe speed for each flight condition encountered in normal operations, including applicable source(s) of lift and phase(s) of flight, to maintain controlled safe flight. The minimum safe speed determination must account for the most adverse conditions for each flight configuration. EVE.2115 - Takeoff performance. (a) The applicant must determine takeoff performance accounting for: (1) All sources of lift for each takeoff flight path for which certification is sought; (2) Minimum safe speed safety margins; (3) Climb requirements; and (4) Obstacle Clearance. (b) For aircraft approved for essential performance, the applicant must determine the takeoff performance to a safe height above the takeoff. Additionally, the aircraft must perform a continued safe flight and landing according to EVE.2105(f) at any point along the takeoff flight path. (c) For aircraft approved for increased performance, the takeoff performance must be determined so that, following a critical change of thrust: (1) Prior to reaching the takeoff decision point: (i) A rejected takeoff resulting in a safe stop and landing can be made. The takeoff decision point may be a speed, an altitude, or both; and (2) After passing the takeoff decision point: (i) Continue the takeoff and climb to a safe height above the takeoff surface; (ii) The aircraft can achieve the configuration and airspeed used in compliance with EVE 2120(d)(1); and (iii) The aircraft must perform a continued safe flight and landing according to EVE.2105(f). EVE.2120 - Climb requirements (a) The applicant must demonstrate minimum climb performance out of ground effect at each weight, altitude, and ambient temperature within the operating limitations using the procedures published in the flight manual. (b) For aircraft approved for essential and increased performance, the applicant must determine the following all engines operating (AEO) climb performance requirements: (1) The aircraft must have a minimum steady climb gradient at sea level in the initial takeoff configuration(s) and a climb speed selected by the applicant or Vy, and (2) For a balked landing, the aircraft must be able to maintain a minimum steady climb gradient without creating undue pilot workload in the landing configuration(s). (c) For aircraft approved for essential performance, the climb performance after a critical change of thrust must be determined: (1) Using applicable sources of lift along the takeoff flight path for which certification is being sought at the speeds and configurations selected by the applicant; and (2) For the transition from the takeoff to the enroute configuration. The total altitude loss must be determined for the weight, altitude, and ambient temperature where level flight cannot be maintained. (d) For aircraft approved for increased performance, the climb performance after a critical change of thrust must be such that during climb: (1) Takeoff phase or following a balked landing: (i) The trajectory must clear all obstacles by sufficient margins for takeoff or landing and reach the Takeoff Safety Speed (VTOSS) at a safe height above the takeoff or landing surface with a positive rate of climb; (ii) The minimum rate of climb at initial takeoff height above the takeoff or landing surface in VTOSS is assured; (iii) The minimum rate of climb at final takeoff height above the takeoff or landing surface in Final Takeoff Speed (VFTO) is assured; (iv) From the initial takeoff height above the takeoff or landing surface, the aircraft path must be level or positive until the VFTO or the final takeoff height is attained, whichever is higher, with available rate of climb not less than the required by (d)(1)(iii). (2) Enroute: (i) Where applicable, the steady rate of climb (or descent) must be determined at each weight, altitude, temperature and sources of lift at which the aircraft is expected to operate for which certification is requested. EVE.2125 - Climb information (a) The applicant must determine climb performance at each weight, altitude, and ambient temperature within the operating limitations using the procedures published in the flight manual.