Guidance
Index of historic papers produced by the MASAAG
Updated 17 June 2022
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| MASAAG Paper No | TITLE |
|---|---|
| 1 | THE JAC MATERIALS SUB-COMMITTEE - PAST, PRESENT AND FUTURE |
| 2 | A SINGLE STRENGTH AND FATIGUE REQUIREMENT FOR COMBAT AEROPLANES AND HELICOPTERS |
| 3 | REVISION OF STRUCTURAL ASPECTS OF AvP970 PART 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT |
| 4 | PROPOSALS FOR THE REVISION OF THE UK STRUCTURAL AIRWORTHINESS REQUIREMENTS FOR MILITARY AIRCRAFT |
| 5 | PROGRESS IN THE REVISION OF THE UK MILITARY AIRWORTHINESS REQUIREMENTS FOR FATIGUE AND DAMAGE TOLERANCE |
| 6 | US TOUR - PRELIMINARY DIGEST OF FINDINGS |
| 7 | MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP RESEARCH OBJECTIVES OF REQUIREMENTS SECTION MS1 DIVISION |
| 8 | PROGRESS IN THE REVISION OF THE UK MILITARY AIRWORTHINESS REQUIREMENTS ON FATIGUE AND DAMAGE TOLERANCE |
| 9 | REQUIREMENTS SECTION MS1 DIVISION |
| 10 | A discussion paper comparing the requirements of AvP 970 with those of JAR 25 for large transport aircraft |
| 11 | PROPOSALS FOR A COMMON INTERNATIONAL APPROACH TO STRUCTURAL AIRWORTHINESS CERTIFICATION |
| 12 | FIRST ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP (MASAAG) DRAFT |
| 13 | FIRST ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP (MASAAG) |
| 14 | Summary of BAe's experience todate on the testing of carbon fibre composites. |
| 15 | GR5 Structural Airworthiness |
| 16 | RESEARCH OBJECTIVES AND PRIORITIES IN THE FIELD OF STRUCTURAL AIRWORTHINESS |
| 17 | STRUCTURAL IMPLICATIONS OF ACT: A NOTE INVITING GUIDANCE ON THE PREPARATION OF REQUIREMENTS |
| 18 | A SURVEY OF ACCIDENTS TO BRITISH MILITARY AIRCRAFT FROM 1961 TO 1982 WITH PARTICULAR REFERENCE TO STRUCTURAL FAILURES |
| 19 | AIRWORTHINESS CONSIDERATIONS OF PRIMARY BONDED STRUCTURES |
| 20 | Major Bonding Applications for Helicopters |
| 21 | DRAFT PROPOSALS FOR A REVISION OF STATIC AIRWORTHINESS FACTORS |
| 22 | LOADS AND STRENGTH - ARE THEY IN BALANCE? |
| 23 | COMMENTS ON RAE PROPOSALS FOR A REVISION OF STATIC AIRWORTHINESS FACTORS |
| 24 | Evaluation of Operational Loads to Verify Structural Design |
| 25 | n/a |
| 26 | COMMENTS ON "EVALUATION OF OPERATIONAL LOADS TO VERIFY STRUCTURAL DESIGN" BY H STRUCK |
| 27 | THE USE OF THE SAFE S-N CURVE AND ITS IMPACT ON SAFE-LIFE |
| 28 | n/a |
| 29 | n/a |
| 30 | FATIGUE DAMAGE TOLERANCE - AN OPPORTUNITY THAT MUST NOT BE MISSED |
| 31 | MASAAG: INTERIM REPORT, NOVEMBER 1984 |
| 32 | AREAS FOR DEBATE AND RESEARCH IN ACHIEVING AN INTERNATIONAL STRAGEGY FOR STRUCTURAL AIRWORTHINESS |
| 33 | MAINTENANCE COST IMPLICATIONS OF STRUCTURAL FAILURES IN SAMPLE AIRCRAFT |
| 34 | AIRWORTHINESS ASPECTS OF ALUMINIUM-LITHIUM ALLOYS AND OF SUPERPLASTIC FORMING/DIFFUSION BONDING |
| 35 | MASAAG 35 RESEARCH TOPICS IN COMPOSITES |
| 36 | VARIABILITY AND CUMULATIVE DAMAGE DATA PROGRAMME FOR STRUCTURAL FEATURES OF CARBON FIBRE COMPOSITE (VALID) |
| 37 | PROGRESS IN PREPARING JOINT STRUCTURAL REQUIREMENTS FOR COMBAT AIRCRAFT |
| 38 | Flight Clearance of Prototype Aircraft |
| 39 | n/a |
| 40 | LIGHTNING STRIKE AIRWORTHINESS CLEARANCE PROGRAMME FOR E A P |
| 41 | FABRICATION AND QUALITY ASSURANCE OF COMPOSITES |
| 42 | QUALITY ASSURANCE OF COMPOSITES STRUCTURES |
| 43 | CONSIDERATIONS AFFECTING THE FACTOR ON STRESS TO BE USED IN DERIVING SAFE S-N CURVES |
| 44 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP (MASAAG) |
| 45 | CLEARANCE OF EXPERIMENTAL AIRCRAFT/DEF STAN 00-970 |
| 46 | THE INFLUENCE OF ASYMMETRIC LOADS ON THE FATIGUE DESIGN AND CLEARANCE OF MILITARY FIGHTER AIRCRAFT |
| 47 | RECOMMENDATIONS FOR A REAPPRAISAL OF THE ROLE OF ANALYSIS IN THE AIRWORTHINESS CERTIFICATION PROCESS |
| 48 | A FINITE ELEMENT USER ACCREDITATION SCHEME |
| 49 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP |
| 50 | A STRATEGY FOR UK STRUCTURAL REQUIREMENTS ACTIVITY TO THE YEAR 2000 |
| 51a | PRINCIPAL RESEARCH OBJECTIVES IN THE FIELD OF STRUCTURAL AIRWORTHINESS |
| 51b | PRINCIPAL RESEARCH OBJECTIVES IN THE FIELD OF STRUCTURAL AIRWORTHINESS |
| 52 | ON THE USE OF 'B' VALUES FOR STATIC STRENGTH CERTIFICATION |
| 53 | A SURVEY OF ACCIDENTS TO RAF AIRCRAFT FROM 1983 TO 1985 WITH PARTICULAR REFERENCE TO STRUCTURAL FAILURES |
| 54 | STRUCTURAL DESIGN REQUIREMENTS FOR AIRCRAFT INCORPORATING ACTIVE CONTROL TECHNOLOGY |
| 55 | ON THE USE OF A LOAD FACTOR OF 1.2 TO ENHANCE THE EFFECTIVENESS OF MAJOR FATIGUE TESTS |
| 56 | THE SAFE S-N POLICY - AN INITIAL ASSESMENT OF THE IMPLICATIONS OF TEST DATA |
| 57 | MILITARY SPECIFICATION AIRCRAFT STRUCTURES GENERAL SPECIFICATION FOR |
| 58 | FATIGUE DAMAGE TOLERANCE |
| 59 | CERTIFICATION OF COMPOSITES FOR AIRCRAFT |
| 60 | DEF STAN 00-970 AND THE FUTURE RELATIONSHIP WITH US MIL SPECS/MIL PRIMES |
| 61 | A Draft Letter to European Specialists Who Are Responsible For The Structural Airworthiness Requirements For Future Military Aircraft |
| 62 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP |
| 63 | A COMPARISON OF THE FATIGUE DAMAGE TOLERANCE REQUIREMENTS FOR ENGINES WITH THOSE FOR AIRFRAMES |
| 64 | THE STRUCTURAL MIL PRIME - POINTS OF POLICY FOR DEBATE WITH THE USAF |
| 65 | STRUCTURAL REQUIREMENTS FOR FUTURE PROJECTS - THE UK POSITION |
| 66 | FATIGUE LIFE FACTORS |
| 67 | FATIGUE LIFE FACTORS |
| 68 | Application Of The Safe S-N Policy To Alluminium Alloy Structure Subject To Combat Aeroplane Wing Bending Spectra |
| 69 | THE USE OF RELIABILITY TECHNIQUES TO IMPROVE STRUCTURAL EFFICIENCY |
| 70 | REQUIREMENTS FOR THE TOLERANCE OF COMPOSITE STRUCTURE TO IMPACT |
| 71 | PRINCIPAL RESEARCH OBJECTIVES IN THE FIELD OF STRUCTURAL AIRWORTHINESS REQUIREMENTS DEVELOPMENT AND INTERPRETATION |
| 72 | A SURVEY OF ACCIDENTS TO RAF AIRCRAFT FROM 1986-1987 WITH PARTICULAR REFERENCE TO STRUCTURAL FAILURES |
| 73 | n/a |
| 74 | COMMENTS ON USAF COMPOSITE CERTIFICATION REQUIREMENTS |
| 75 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP |
| 76 | USE OF LOWER TEST FACTORS FOR HIGH LIFE AIRCRAFT DESIGN |
| 77 | AN APPRAISAL OF THE FATIGUE LIFE FACTORS ARISING FROM A FAILURE RATE APPROACH |
| 78 | AIRWORTHINESS OF HOT AIR DUCTING IN AIRCRAFT |
| 79 | ON THE USE OF AN ENHANCED-AND-TRUNCATED SPECTRUM TO ACCELERATE FULL-SCALE FATIGUE TESTS OF AIRFRAME STRUCTURES |
| 80 | FACTORS AT INCREASED LIVES |
| 81 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP 1989 |
| 82 | Report of the FAA Conference on Ageing Aircraft held in Atlanta, March 20-22, 1990 |
| 83 | RECOMMENDATIONS FOR A REVIEW OF THE EFFECTS OF AGEING ON THE CONTINUING STRUCTURAL INTEGRITY OF SERVICE AIRCRAFT |
| 83b | RECOMMENDATIONS FOR A REVIEW OF THE EFFECTS OF AGEING ON THE CONTINUING STRUCTURAL INTEGRITY OF SERVICE AIRCRAFT |
| 84 | MULTIPLE-SITE DAMAGE (MSD) AND INSPECTION-DEPENDENT STRUCTURE - DESIGN REQUIREMENTS |
| 85 | A SURVEY OF ACCIDENTS TO RAF AIRCRAFT FROM 1988-1989 WITH PARTICULAR REFERENCE TO STRUCTURAL FAILURES |
| 86 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP 1990 |
| 87 | ON THE ROLE OF FATIGUE REQUIREMENTS IN ACHIEVING IMPROVED STRUCTURAL RELIABILITY AND MAINTAINABILITY |
| 88 | SPENDING NOW TO SAVE LATER - HOW CAN MASAAG CONTRIBUTE TO IMPROVED R&M? |
| 89 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP 1991 |
| 90 | REQUALIFICATION OF STRUCTURAL COMPONENTS |
| 91 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP 1992 |
| 92 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP 1993 |
| 93 | ANNUAL REPORT OF THE MATERIALS AND STRUCTURES AIRWORTHINESS ADVISORY GROUP 1994 |
| 94 | n/a |
| 95 | n/a |
| 96 | n/a |
| 97 | n/a |
| 98 | n/a |
| 99 | n/a |
| 100B | The application of a numerical reliability requirement to airframes and mechanical systems |
| 101A | The role of structural analysis in the certification of military airframes |
| 102C | TORQUE TIGHTENING OF BOLTS |
| 103 | Structurally Significant Items and their use in Reliability Centred Maintenance schedules for British military aircraft |
| 104 | Recommendations for the future shape of the Ageing Aircraft Structural Audit |
| 105 | Teardown Inspections Ð Guidance and best practice |
| 106 | REPAIR ASSESSMENT PROGRAMME FOR MILITARY TRANSPORT AIRCRAFT |
| 107 | Proposed Defence Standard 00-970 Structural Monitoring Systems Using Non-Adaptive Prediction Methods |
| 108 | Military Version of Appendix K to CS-25 |
| 109 | Guidance for Aircraft Operational Loads Measurement Programmes |
| 110 | Carriage of Stores |
| 111 | A revised requirement for probabilistic gust load analysis |
| 112 | IMPACT DAMAGE RESISTANCE OF COMPOSITE MATERIAL STRUCTURES |
| 113 | FATIGUE SERVICE MONITORING |
| 114 | Airframe Structural Integrity Research and Development Strategy |
| 115 | Def-Stan 00-970 Clause 3.2 - Fatigue and Associated Leaflets |
| 116 | Widespread fatigue damage in military aircraft |
| 117 | NOT ISSUED |
| 118 | The interaction of corrosion and fatigue in aircraft structures |
| 119 | Mechanism for Introduction of New Non-Destructive Testing Capability |
| 122 | Development of a protocol for acceptance of new NDT capability in the air domain. |
| 123 | Development, Validation, Verification and Certification of Structural Health Monitoring Systems for Military Aircraft |