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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