2.7 RADIO TECHNICAL COMMISSION FOR AERONAUTICS (RTCA) DOCUMENTS

2.8 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. DOCUMENTS

2.9 REFERENCE DOCUMENTS

3. TECHNICAL REQUIREMENTS

3.1 PROPULSION SYSTEM DEFINITIONS

3.1.1 Propulsion Pod System Definition

3.1.1.1 Engine (FAR Part 33 Certified)

3.1.1.2 Nacelle

3.1.1.3 Engine Mounts

3.1.1.4 Engine BuildUp (EBU)

3.1.1.5 Pylon

3.1.2 Airframe Modifications

3.1.2.1 Cockpit Modifications

3.1.2.1.1 Auto Throttle Compatibility

3.1.2.2 Avionics Modifications

3.1.2.3 Wing Modifications

3.1.3 Definition of Terms and Abbreviations Used

3.2 PERFORMANCE

3.2.1 Design Life

3.2.2 Propulsion System General Criteria and Operating Envelope

3.2.3 Propulsion System Operation Characteristics

3.2.3.1 Takeoff Thrust

3.2.3.2 Maximum Continuous Thrust

3.2.3.3 Thrust-Specific Fuel Consumption

3.2.3.4 Warm-up Time

3.2.3.5 Engine Operating Time

3.2.3.6 Noise

3.2.3.7 Emissions

3.2.3.8 Infrared Emissions

3.2.3.9 Electrical Power

3.2.3.10 Engine-Driven Hydraulic Pump

3.2.3.11 Bleed Air

3.2.3.11.1 Engine-Generated Substances

3.2.3.11.2 Ozone

3.2.3.11.3 Pneumatic System Performance

3.2.3.11.3.1 ECS Bleed Air System (EBAS)

3.2.3.11.3.1.1 Bleed Air Pressure

3.2.3.11.3.1.2 Overpressure Control and Indication

3.2.3.11.3.1.3 Bleed Air Temperature

3.2.3.11.3.1.4 Overtemperature Control and Indication

3.2.3.11.3.1.5 Bleed Flow

3.2.3.11.3.1.6 Pressure Drop

3.2.3.11.3.1.7 Stability

3.2.3.11.3.2 Wing Thermal Anti-Ice (WTAI)

3.2.3.11.3.2.1 Bleed Air Pressure

3.2.3.11.3.2.2 Bleed Air Temperature



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