EMBRAER EMB-505: certification basis
Basis entries as written on the TCDS
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REG
EA-2009T12
State of Design Authority Type Certificate No.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
RBHA 23 - Requisitos de Aeronavegabilidade. Aviões Categoria Normal, Utilidade, Acrobática e Transporte Regional (Airworthiness Standards. Normal, Utility, Acrobatic, and Commuter Category Airplanes), corresponding to U.S. 14 CFR Part 23 including amendments 23-1 through 23-57; and additional requirements as per ANAC FCAR HT-01, additionally: For aircraft equipped with Autothrust System (Current Speed Control – CSC or Autothrottle – AT), for the components and areas affected by the system installation: RBAC 23 (“Requisitos de Aeronavegabilidade: Aviões Categoria Normal”), which is equivalent to 14 CFR Part 23, amendment: [23-]64 (23.2010, 23.2500(b), 23.2510, 23.2600(b) and 23.2605(b) and (c)).
ANAC Certification Basis
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
CS 23 – “Normal, Utility, Aerobatic and Commuter Category Aeroplanes” of 14 November 2003, as applicable to Commuter Category Certification; and additional requirements as per EASA CRI A-01.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
CS-ACNS (Subpart D, section 4) - initial issue of 17/12/2013 (see note 10)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
Additionally, for aircraft equipped with Autothrust System (Current Speed Control – CSC), for the components and areas affected by the system installation the following additional regulations apply: CS 23 at amendment 5 (23.2010, 23.2500(b), 23.2510, 23.2600(b) and 23.2605(b) and (c))
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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◆ SPECIAL
Part 23 Jets - Handling and Performance Requirements High Speed Characteristics Part 23 Jets - Stall Speed Determination Human Factors - Integrated Avionics System Performance Credit for APR during Go-Around Sonic Fatigue Pressurization into Non-Pressurized Areas Speed Margins Yawing Maneuver Dynamic Response Out of Trim Characteristics (Structures)
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◆ SPECIAL
Take-Off Warning System Extension and Retraction System Wheels Brakes and Braking Systems Doors Bird Strike Steering Systems Operation above 41.000 ft Belted Toilet Seat – Single Place Side facing Seat (for applicable areas affected by DCA 0505-025-00077-2010/EASA when embodied in the aircraft)
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◆ SPECIAL
Sideward Seating Arrangement (for applicable areas affected by DCA 0505-025-01013- 2010/EASA when embodied in the aircraft)
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◆ SPECIAL
Inflatable Restraints (for applicable areas affected by DCA 0505-025-01013-2010/EASA when embodied in the aircraft)
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◆ SPECIAL
Fuel Tank Crashworthiness Fuel System Hot Weather Operation, Turbine Fuel Lines, Fittings and Components Powerplant Fire Extinguishing Systems Negative Acceleration Fuel Tank Ignition Prevention Cold Soaked Fuel Battery Endurance Requirement (High Altitude)
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◆ SPECIAL
Hydraulic Systems Interaction of Systems and Structures Protection from effect of HIRF FADEC Integration Lithium Battery Installations Ice Protection, Special Condition for Auto-Activated Anti-ice Systems Security Protection of Aircraft System and Networks (for applicable areas affected by DCA 0505-046-00212-2019/EASA when embodied in the aircraft)
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◆ SPECIAL
Data link services for single European Sky. (for applicable areas affected by DCA 0505- 023-00059-2011/EASA or 0505-023-00060-2011/EASA when embodied in the aircraft)
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◆ SPECIAL
Flight recorders including data link recording. (for applicable areas affected by DCA 0505-023-00059-2011/EASA or 0505-023-00060-2011/EASA when embodied in the aircraft)
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◆ SPECIAL
Flight Guidance System – Autothrottle under Part 23 (for applicable areas affected by DCA 0505-022-00111-2017/EASA when embodied in the aircraft).
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◆ SPECIAL
Effects Reference take-off speed for part 23 jets noise certification Steep Approach and Landing (for applicable areas affected by DCA 0505-000-00057- 2011/EASA when embodied in the aircraft).
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◆ SPECIAL
Towbar less towing (for applicable areas affected by DCA 0505-032-00051-2012/EASA when embodied in the aircraft).
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ELOS
Motion and Effect of Cockpit Controls (for applicable areas affected by DCA 0505-025- 00124-2017/EASA when embodied in the aircraft)
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ELOS
Ditching emergency exit for passenger Video Monitors Deployed from Aisle Ceiling (for applicable areas affected by DCA 0505-000-00057-2011/EASA when embodied in the aircraft).
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ELOS
Digital only N2 and Fuel Flow Usable Fuel Quantity Markings
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ELOS
ELOS ATR/ APR Use of LED for Navigation Lights and Anti-Collision Lights Powerplant Instruments – Normal Operation Range Color Powerplant Instruments - Normal Operating Range Color and CSC Authority Indication (for applicable areas affected by DCA 0505-022-00075-2020/EASA when embodied in the aircraft)
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OTHER
CS 34 - Aircraft Engine Emissions and Fuel Venting, of 17 October 2003
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OTHER
CS 36 - Aircraft Noise, of 17 October 2003
- Exemptions: none recorded.