Power Unit Auxiliary, S-3A Aircraft Equipment Specification

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Power Unit Auxiliary, S-3A Aircraft Equipment Specification

Power Unit Auxiliary, S-3A Aircraft Equipment Specification
APU Components
Specifications and Standards
Specifications and Standards -Cont.
Other Government Documents
APU System Data Submittal and Approval
APU Configuration and Envelope Figure
Gyroscopic Moments
Heat Rejection and Cooling
Air and Gas Leakage
Compressed Air Connection
Compressed Air Contamination
Government Loaned Property List
Perfromance Presentation Steady-State
Documentation Requirements
Output Parameters
Performance Curves
Operating Limits
Fuel Flow Limits
Transient Conditions
Start Reliability
Environmental Conditions
Storage Temperature Range
Corrosive Atmosphere Conditions
Atmospheric Liquid Water
Materials and Processes
Nameplate and Product Marking
Drawing Revision Marking
Structural Performance
Strength and Life Analysis
Disc Burst Speeds
Design Standards
Design and Construction Changes
Service and Accessibility
Anti-Icing Interface
Shutdown Conditions
APU Overspeed System
Fuel Contamination
Permanent Magnet Generator
Ignition Power Source
Temperature Sensing Systems
Lubricating System Interface
Lubrication System Components and Features
Oil Drain
Oil Pressure Sensor
Automatic Starting
Engineering Evaluation Tests
Manner of Test and Reporting
Test Stand Dynamic Characteristics
Accreditable Test Time
Transient Data
Barometer Reading
Summary Reports
APU Heat Rejection and Oil Cooling
APU Pressure Balance Verification
Material Corrosion Test
Endurance Test Procedure
Endurance Test Schedule
APU Disassembly and Inspection
Explosion Proof Test
Altitude Tests
Altitude Test Completion
Rotor Structural Integrity
Overspeed Control Test
Endurance Test Procedure
Endurance Test Schedule
APU Disassembly and Inspection
APU Component Tests
Component Test Cycles
APU Control System Test Cycle
Ignition System Test Cycle
Salt Water
Room Temperature
APU Control System
Fuel Pump Cavitation
Component Test Completion
Component Test Procedures
Ignition System Fouling
Heat Exchangers
Altitude Tests
Altitude Test Procedure
Altitude Test Completion
Low Temperature Test
Environmental Icing Test
Bird Ingestion Test
Sand Ingestion Test
Noise Survey
Vibration
Emergency Fuel Test
Rotor Structural Integrity
Vibration and Stress Test
Gyroscopic Test
Test Apparatus
Fuel Servicing
Test Records
Transient Data
Test Procedure
Maximum Hours of Running
Sampling Tests
APU Axes
Center of Gravity
Gulping Volume
Maximum Allowable Rotor Speed
Power Section
APU Failures Chargeable
Standard Condition
Procurement Requirements
Radar Cross Section Report
Vibration and Stress Report
APU Electrical Power Failure Test
Approval Status
Verification Table
General Description
Specific Features
Specific Features -Cont.
Utilization
Appendix I. S-3A Generator
Start of the Second Engine
Figure 1. S-3A Generator Heat Rejection
Figure 2. Generator Input Shaft Power Versus Output KW
Figure 3. Power Transfer System
Appendix II. Electronic Control Unit, APU, Requirements
Master Caution Panel
Safety Provisions
Logic Voltage Levels
Environmental Conditions
Design and Construction
Nameplates and Product Marking
Personnel and Training
Disassembly and Inspection
Speed Signal
Appendix II. Miscellaneous Environmental Tests
Maintainability Assurance Program
Acceptance Tests
Figure 1. Interface Control Drawing, S-3A ECU
Figure 2. Electrical Interface, S-3A ECU
Appendix III. S-3A Aircraft APU Hydraulic Start System
Return System
Performance Characteristics
Figure 1. S-3A Modified Hydraulic APU Starting System
Figure 2. Start Valve Characteristic (Valve Opening Rate)
Appendix IV. Analysis and Test Summary
Appendix IV. Analysis and Test Summary -Cont.
Appendix IV. Analysis and Test Summary -Cont.
Appendix IV. Analysis and Test Summary -Cont.
Numerical Index
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Numerical Index -Cont.
Alphabetical Index
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Alphabetical Index -Cont.
Numerical Index of Figures
Numerical Index of Tables and Appendices
Figure 1. Interface Control Drawing, S-3A APU
Figure 2. Externally Applied Forces
Figure 3. Ambient Temperature Extremes
Figure 3. Ambient Temperature Extremes -Cont.
Figure 4. Uninstalled APU Performance
Figure 5. Droop Characteristics and Combined Loads
Figure 6. APU Starting Operating and Nonoperating Envelopes
Figure 7. Operating Attitude and Storage Limits
Figure 8.Continous Maximum Icing Conditions
Figure 9. Intermittent Maximum Icing Conditions
Figure 10. APU Test Points and Altitude Ranges
Table I. Minimum Uninstalled Sea Level Static Performance
Table II.Minimum Uninstalled Altitude Performance
Table III. APU Characteristics Summary
Table IV. Gearbox Pads and Drives
Table V. Sea Level Anti-Icing Conditions
Table VI. Mission, Mission Mix and Component Life
Table VI. Mission, Mission Mix and Component Life -Cont.
Table VII. Fuel Contaminants
Table VIII. Data Recording
Table IX. Corrosion Susceptibility 48 Hour Test Cycle Schedule
Notes for Table IX
Notes for Table IX -Cont.
Standardization Document Improvement Proposal
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Power Unit Auxiliary, S-3A Aircraft Equipment Specification

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