Electric Power Generating and Control Equipment, Aircraft, Testing, General Specification

• Electric Power Generating and Control Equipment, Aircraft, Testing, General Specification
• Standard Conditions
• Temperature Stabilization
• Rework and Resubmission
• Table I. Test Plans for Three Samples
• Table II. Test Plans for Four Samples
• Failure Criteria
• Oil Saltwater Ingestion
• Minimum Temperature Altitude Criteria
• Figure 1. Temperature Altitude Requirements for Self-Cooled Components
• Figure 2. Temperature Altitude Requirements for Blast Cooled Components
• Electromagnetic Compatibility
• Engine Mounted Components
• Figure 3. Vibration Test Curve for Engine Mounted Components
• Non-Engine-Mounted Components
• Figure 5. Endurance Test Curve for Non-Engine-Mounted Components
• Figure 6. Typical Burn In Test Cycle
• Determination of Temperature Stabilization
• Inclusions in Equipment Specifications
• Standardization Document Improvement Proposal
• Postage and Fees Paid
• Blank Page

Electric Power Generating and Control Equipment, Aircraft, Testing, General Specification

Privacy Statement - Press Release - Copyright Information. - Contact Us