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

                            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.

                            

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