SAE ARP 5089 : 2011
SAE ARP 5089 : 2011
COMPOSITE REPAIR NDT/NDI HANDBOOK
SAE International
1 SCOPE
2 REFERENCES
3 DEFINITIONS
3.1 Glossary of Terms Used in Nondestructive
Testing of Composites
4 DESIGN OF COMPOSITE STRUCTURES
4.1 Honeycomb Sandwich Construction
4.2 Monolithic Construction
4.3 Fiber Reinforced Plastic Materials
5 COMPOSITE STRUCTURE APPLICATIONS
5.1 OEM Design Details
5.2 Avion de Transport Regional Parts
5.3 Aerospatial/British Aerospace Parts
5.4 Airbus Industrie Parts
5.5 Boeing Aircraft Parts
5.6 De Havilland
5.7 Douglas Aircraft Parts
5.8 Fokker Aircraft Parts
5.9 Saab
6 EXAMPLES OF IN-SERVICE DAMAGE AND PROCESSING
ANOMALIES
6.1 Visible Damage Assessment
6.2 Inspection procedure
6.3 Acceptance Criteria
7 INSPECTION TECHNIQUES
7.1 PE/TTU Ultrasonic
7.2 High Frequency Bondtesters
7.3 Low Frequency Bondtesters
7.4 MIA Inspectors
7.5 Tap Test Method
7.6 Radiographic Inspection
7.7 Thermography for Fluid Ingress
8 GENERAL TECHNIQUE HINTS, ALL REPAIRS
8.1 Ultrasonics
8.2 High Frequency Bondtesters
8.3 Low Frequency Bondtesters
8.4 MIA Testers
8.5 Tap Test of Metallic and Nonmetallic Structures
8.6 Radiographic Methods
8.7 Thermography for Fluid Ingress
8.8 Repair Processing Anomalies and Applicable
Inspection Methods
8.9 Repair Examples and Expected Instrument Responses
Gives background information on the design, application, repair and inspection of composite structure, including metal bonding, used on civil transport aircraft. Intended to help inspectors to know where to expect composite and metal bonded parts on the aircraft, providing understanding of current NDT methods and to interpretation of inspection results.
Document Type | Standard |
Status | Current |
Publisher | SAE International |