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ARP217D
Testing of Airplane Installed Environmental Control Systems (ECS)
Testing of Airplane Installed Environmental Control Systems (ECS)
2011-06-01
有效
【范围】 This document deals with ground and flight test of airplane installed Environmental Control Systems (ECS), Figure 1. The ECS provide an environment, controlled within specified operational limits of comfort and safety, for humans, animals, and equipment. These limits include the following: pressure, temperature, humidity, ventilation air velocity, ventilation rate, wall temperature, audible noise, vibration, and environment composition (ozone, contaminants, etc.). The ECS are composed of equipment, controls, and indicators that supply, distribute, recycle and exhaust air to maintain the desired environment. 1.1 Purpose: This document defines recommended tests and test procedures for airplane installed ECS. The purpose of these tests is to: a. verify system pressure integrity (leakage), b. verify integration and compatibility of ECS with other airplane systems, and c. determine overall system performance in conditions representative of those which may be encountered during operations. {c6ae4349365ab2f5f00b9507788e16f4.jpg} 1.2 Field of Application: These tests (and procedures) may be used for commercial and military airplane certification (test of first article) or for production airplane (to ensure built as design) tests. The selection of the appropriate test conditions, instrumentation, and test procedures depends on a large number of variables (airplane configuration, system concept, hardware, integration with other on-board systems, certification or production airplane, etc.). Thus, these are addressed in general terms. This document is intended to serve as a guide in the planning and conduct of tests. The specification or contractual or regulatory (Federal Aviation Regulations (FAR), Joint Airworthiness Regulations (JAR)) requirements should be considered. The test plan and procedure should be coordinated with the appropriate agency. Test data may be used to show compliance with the applicable airplane specification, contractual, or regulatory requirements and to verify analytical simulation models. If the former is intended, it is extremely important to obtain prior approval of the test plan and procedure from the appropriate agency.strRefField
【与前一版的变化】

包含缩略语

ACM
AFB
APU
ARP
ATA
BITE
CFR
DER
DMIR
ECS
EGT
EICAS
EPR
FAA
FAR
JAA
JAR
OBOGS
OBIGGS
PRSOV
TAI

替代标准

引用文件/被引文件

Measurement of Exterior Noise Produced by Airplane Auxiliary Power Units and Associated Equipment during Ground Operations
Type Measurement of Airplane Interior Sound Pressure Levels in Cruise
Air Conditioning Design Information for Cargo and High Density Passenger Transport Planes
Fault Isolation in Environmental Control Systems of Commercial Transports
The Advanced Environmental Control Systems (AECS) Computer Program for Steady State Analysis and Preliminary System sizing
Transient ECS Computer Program
Airplane Environmental Systems Acoustical Design Considerations
Air Conditioning Equipment
Temperature Control Equipment
Air Conditioning
High Temperature Pneumatic Duct Systems for Airplane
General Requirements for Application of Vapor Cycle Refrigeration Systems for Airplane
Airplane Pressurization Control Criteria
Engine Bleed Air Systems for Airplane
Air Cycle Air Conditioning Systems for Military Air Vehicles
General Design Specification Environmental Control
Demonstration Requirements for Airplanes
Environmental Control Systems
Test Procedures for Airplane Environmental Systems
Extreme Climate Conditions and Derived Conditions for Use in Defining Design/Test Criteria for NATO Forces

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(R) Control of Water Carryover from the Environmental Control System and Condensation on the Structure
Construction and Calibration of Parallel Plate Transmission Line for Electromagnetic Interference Susceptibility Testing
Installation of Liquid Oxygen Systems in Civil Aircraft
Fault Isolation in Environmental Control Systems of Commercial Transports
Identification and Coding of Fluid and Electrical Piping System Functions

包含图表

Environmental Contro
Typical Pneumatic Sy
Typical Air Cycle Ai
Typical Vapor Cycle

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