117A Cladding thickness. Requirements per material specification
116A Macrostructure. Requirements per material specification
115A Decarburization check. Requirements per material specification
114A Grain size. Requirements per material specification
113A Flattenability test. Requirements per material specification
112A Hardness per BAPS 168-013. Hardness Testing on receipt may be waived, provided that all parts manufactured from each lot are 100% tested per BAPS 168-013 requirements and are fully traceable to the raw material lot.
111A Evaluation per material specification requirements
110A Visual inspection. Requirements per material specification
109A Grain flow. Requirements per material specification
108A Microstructure. Requirements per material specification
107A Bend test. Requirements per material specification
106A Flare test. Requirements per material specification
105A Fracture toughness test. Requirements per material specification
104A Exfoliation corrosion test. Requirements per material specification
103A Stress corrosion test. Requirements per material specification
102A Tensile testing. Requirements per material specification
101A Conductivity per BAPS 168-013 - Sheet and plate less than 0.500": Six random locations on one side of top sheet or plate. - Plate 0.500" or thicker: Three random locations on each end of each plate. - Extrusions bars or forgings: Three random locations on each length or piece. For all cases, conductivity values of any one part shall not vary by more than 2.0% IACS. Conductivity testing on receipt may be waived provided that all parts manufactured from each lot are 100% conductivity tested per BAPS 168-013 requirements. All parts must be fully traceable to the raw material lot.
100A Chemical composition requirement per material specification
127A Lap Shear Strength per BATS 3460
126A Corrosiveness. If conditioner is purchased separately from ink, no testing is required.
124A Breaking strength, stretch limits and permanent set per material specification
123A Fracture Toughness Evaluation. Requirements per material specification
125A All acceptance tests per specification except for prepreg chemical properties
122A Hardness per BAPS 168-013 Using Material Specification Requirements
121A Wire size and mesh size per ASTM E437
120A Izod impact. Requirements per material specification
02A Perform all the Quality Assurance / Batch or Lot Acceptance / Conformance / Initial Acceptance tests required of the manufacturer as per the material specification, unless purchaser acceptance tests are specified.
16A Examine first 6 feet for tack and ease of unwind
22A Honeycomb node delamination
24A Resistance to drying and ageing
29A Specific gravity, water content, particle count, acid number, chlorine content
30A Condition in container, dry time, appearance
31A Dry time, appearance, gloss and color
34A Corrosion resistance (salt spray)
35A Condition in container, gloss, adhesion
36A Conductivity per application specification
39A Appearance. The material shall be uniform in quality and condition, and free of foreign materials and from imperfections detrimental to usage of the material. When applicable, specification controlled materials shall also meet the appearance/visual requirements listed in the specification.
40A Test for sediment and suspended matter ("clean and bright"), water, total solids, density and electrical conductivity per material Specification requirements. Testing may be waived if a test report is supplied showing that the specific truckload of fuel meets the requirements specified above.
44A Verify certificate of conformance
51A Application life, dry time and cure time
53A Tensile strength and modulus
54A Flexibility and knife test
59A Color, viscosity and application
60A Check for adequate propellant in aerosol container
61A Check that product is dry, powdery and contains no lumps
62A Check that, by spraying on a clean metal surface, product deposits evenly and smoothly
70A Check for a good fluidity and homogeneity by visual inspection
74A Test per ASTM D2095. Perform the test using one aluminum rod of any alloy. Requirement: 1000 psi minimum. BLS 9403 specimens are permitted.
75A Cured Hardness and Tack Free Time per MIL-A-46106
77A Test per FAR 25.853(b) Flammability
78A Test per FAR 25.853(a) Flammability
82A Standard Cure Time (Hardness) and Tack Free Time per AMS-S-8802
86A Test for crazing as per AS5127/1 at a stress of 3000 psi on MIL-PRF-5425 substrate
88A Test per MIL-S-81733 Ty II
89A Test per MIL-S-81733 Ty III
90A Test per MIL-S-81733 Ty IV
92A Test per British Aerospace S26-1001
96A Inspect per IGC 04.36.100 and IGC 04.84.100
98A Test per IGC 04.37.100 Chart 3
02B Compression strength plus modulus calculations
03B Fire resistance per MIL-T-9046
08B Test per FAR 25.853(b) Flammability
10B Test per FAR 25.853 b2 and/or b3 flammability
11B Verify paperwork and two containers for fill, closure and marking
15B Lapshear per specification (no immersion)
17B Test for grain size in the -T62 temper by the Heyu volumetric lineal intercept procedure per ASTM E112. Grain size shall be 5.0 or finer
18B Shear strength and modulus
20B Flammability per specification
21B Melt Flow Index per ASTM D1238
23B Add Red Dye as per BAPS 140-013
26B Quantitator inhibitor analysis
27B Lapshear, A1/A1 Room Temperature, no conditioning
28B Fluid resistance per specification
31B After successful completion of acceptance tests per BAMS 532-020, material is to be re-identified as BAMS 532-020 by Receiving Quality.
32B After successful completion of acceptance tests per BAMS 532-019, material is to be re-identified as BAMS 532-019 by Receiving Quality.
33B After successful completion of acceptance tests per BAMS 551-007 Class I Grade II material is to be re-identified as BAMS 551-007 Classes I & II Grade II by Receiving Quality.
34B After successful completion of acceptance tests per BAMS 551-009 Type II, material is to be re-identified as BAMS 551-009 Type II by Receiving Quality.
96B For Inspection on receipt, refer also to IGC 04.31.207
01C Materials consisting of two or more components shall be shelf-lifed and maintained at all times in the form of the original procured kit.
11C Lapshear Strength 1000 psi
12C Lapshear strength 1200 psi
13C Lapshear strength 1500 psi minimum
14C Lapshear strength 2000 psi minimum at 70 ± 5°F
15C Lapshear strength 2250 psi
16C Lapshear strength 2500 psi. Test per BATS 3460
18C Lapshear strength 3000 psi
19C Lap shear 23°C. 15% by weight aluminum powder 0.4 mm bondline, requirements per ASN-B-85680
25C Core Spice shear Strength 660 psi minimum
35C Core Spice shear strength 3000 psi minimum
36C Interlaminar Shear is 7.3 ksi minimum when tested
40C Tensile strength (weak directional CD) 2000 psi min.
50C Cure Hardness 65-90 BARCOL
60C Cure Hardness 20 Shore "A"
65C Cure Hardness 30 Shore "A" in 24 hours
66C Cure Hardness 30 Shore "A" in 48 hours
68C Cure Hardness 33 shore "A" in 24 hours
70C Cure Hardness 35 Shore "A" in 7 days at R.T.
79C Cure Hardness 30+/-5 Shore "D" per ASTM D2240 after 72 hours cure at RT
80C Cure Hardness 75 ± 5 Shore "D" in 30 min. at 150°F
81C Cure Hardness 75 ± 5 Shore "D" in 24 hours at 70 ± 5°F plus 2 hours at 250 ± 5°F plus 30 mins. at 70 ± 5°F
82C Flow 50 ± 10% per material spec.
83C Compression, Ambient Condition
84C Expansion when cured at 170°C with a 10°C/minute max. Heat-up Rate, Expansion shall be 100%-200% cure for 30 minutes at 170°C
88C Tack Free Time 5 hours at 72°F and 50% RH
89C Cure Hardness and Tack Free Time per MIL-A-46146
91C Response to Heat Treatment
92C Evaluation per Material Specification Requirements, except screening tolerances to be MIL-S-13165 and hardness C55 to C65 acceptable when specifically so ordered.
02D Tack Free Time 15 minutes minimum at 72 +/- 5 F and 58 +/- 10% Relative Humidity
03D Tack Free Time 15 ± 5 minutes at 72°F and 58% Relative Humidity
05D Tack Free Time, maximum 60minutes at 72 F and 50% Relative Humidity
06D Tack Free Time 10 minutes at room temperature
08D Tack Free Time 30 minutes minimum at 75 +/- 5 F and 50 +/- 10% Relative Humidity
09D Tack Free Time 8 hours at 75 +/- 5F & 50 +/- 10% Relative Humidity
10D Tack Free Time, 24 hours maximum. Test per BATS 4317.
11D Tack Free time 24 hours, maximum
20D Density 11.13 to 12.67 lbs/ft³
21D Density 1.56 to 2.44 lbs/ft³
30D Application time 14 gr/minutes
43D Gel Time 60-110 seconds at 325°F
44D Gel Time 80-100 seconds at 325°F
47D Gel Time 1 to 5 minutes at 325°F
48D Gel Time 30 to 120 minutes at 325°F
50D Gel Time 9 ± 2 minutes per BATS 4764 Method-B (250 F)
52D Gel time 15 minutes at 350°F minimum
60D Viscosity 4500 centipose max.
62D Viscosity base to be 6,000 to 12,000 poises
65D Viscosity 17 to 55 seconds use FORD CUP #4
66D Viscosity 5-10 centipoises (Cannon-FENSKE)
70D Volume Resistivity 0.005 ohm-cm
71D Volume Resistivity 0.006 ohm-cm
72D Volume Resistivity 0.025 ohm-cm maximum
75D Volume Resistivity 0.1 ohm-cm
83D Expansion Ratio 100% at 350°F for 30 minutes
84D Viscosity 10 minutes at 38°C per ASTM D445.
86D Flash Point 130°C minimum per ASTM D92.
03E Mix Ratio by weight 1.1A/1B
09E Mix Ratio by weight 26A/1B
11E Mix Ratio by weight 50A/100B
15E Mix Ratio by weight 100A/6B
20E Mix Ratio by weight 100A/18B
24E Mix Ratio by weight 100A/20B
26E Mix Ratio by weight 100A/22B
30E Mix Ratio by weight 100A/33B
32E Mix Ratio by weight 100A/35B
37E Mix Ratio by weight 100A/40B
48E Mix Ratio by weight 100A/58B
70E Mix Ratio by weight 100A/100B
73E Mix Ratio by weight 100A/6.5B
80E Transparent liquid - dry time of thin, uniform layer at 72°F is 15 minutes
85E Self Extinguishing in 30 seconds maximum after 15 seconds exposure to a 1500°F flame.
87E Thickness reduced not more than 7% per BATS 4469
88E Compressibility 15 to 35% and recovery 40% minimum
01F Cure Cycle A per BATS 6203
02F Cure Cycle B per BATS 6203
03F Cure Cycle C per BATS 6203
05F Flow 9 to 22% at 50 psi per BATS 4763 Method-E
07F Flow 12 to22% at 50 psi and 325°F and 10 minutes
09F Flow 10 to 24% at 50 psi and 325°F and 10 minutes
12F Flow 14 ± 6% at 50 psi and 275°F
14F Flow 14 to 46% at 50 psi and 350°F
17F Flow 20 to 27% at 50 psi and 260°F
35F Resin Content 42 ± 3% per BATS 4761
55F Accelerated cure 2 hours at 150 ± 10°F
56F Accelerated cure 30 minutes at 150°F
58F Glass Transition Temperature - test per BAER 3073 min. 200 °C
59F Non-crumbling Etched Surface
62F A sample from each lot of material less than 0.250" thickness in the T3, T4, T6, T73 and T81 tempers purchased as "MRS (Minimum Residual Stress) Quality", shall be tested to the requirements of BATS 2505 (Exception: Alcoa, Davenport - code 019 is exempt from MRS testing on receipt).
63F Water break on the etched side per ASTM F22 after BAPS 180-009 General Cleaning
65F GEL Time 1 to 5 minutes at 250°F
66F Density in kg/m³ (Required -64 ± 6.4 kg/m³)
67F Metal to metal shear at 23°C per IGC 04.26.345
68F Honeycomb-metal climbing drum peel at 23°C per IGC 04.26.270
70F All test requirements are per MPS 250-23
71F Cell size or cell count, as applicable per specification requirements
72F Compression Strength, unstabilized RTA on 0.5" thick specimens
73F Appearance as per specification
74F Tack free time per specification
75F Viscosity to be 110 to 150 poises, use Bubble Viscometer from Gardner.
77F Materials consisting of two or more components shall be receipt tested and maintained at all times in the form of the original procured kit.
78F All components shall be receipt tested at the same time in the proportions indicated in the Material Description.
79F Volume Resistivity 2.0 ohm-cm maximum
81F Appearance - Homogeneous and Fluid in the Can
82F If thinner is purchased separately from other components, no testing is required.
83F Honeycomb peel at 75F +/- 5F per specification
84F FAR 25.853 (b3) SAA Aluminum Sheet 0.06" min. thickness, primed with 22-5-16 & coated with plastisol X53A to 0.03" nominal thickness per BAPS 177-035
85F Uncured Resin Chemical Structure
03G Surface Appearance of Cured Film
05G Standard Curing Time / Curing Rate
06G Honeycomb Peel Strength at RT with 250F Cure per Specification
08G Material to be used on Bombardier Aerospace Program only, must be approved to BAMS 565-001 and needs to be tested only to the Batch Acceptance requirements of BAMS 565-001.
09G Strength at Standard Conditions
10G Fatigue Life. Requirements per Material Spec.
11G Ultrasonic Inspection. Requirements per Material Spec.
12G Lapshear strength 4000 PSI min. @ 75 F, no immersion/conditioning, specimens preparation and test per BAMS 551-009, Class II
13G Honeycomb peel strength 30 pound-inch/3 inch width min @ 75°F, no immersion/conditioning, specimens preparation and test per BAMS 551-009, Class II.
14G Verify supplier production test and inspection report as required per Quality Assurance provision of the Douglas Aircraft Company.
15G Verify supplier production test and inspection reports
16G As per the production tests requirements section under Quality Assurance Provisions
17G Static shear strength after room temperature curing.
18G Cured hardness per MIL-A-46146, Group I, Type I
19G Visual examination, water content, corrosiveness, pour point and specific gravity per military specification.
20G Tensile shear test adherends to be chromic acid anodized per BAPS 160-010 and primed with BAMS 565-001, Grade B primer per BAPS 138-043.
23G Test per FAR 25.853(a)(1)(ii) flammability
24G Bend test for bar up to and including 0.5 inch diameter. Requirements per material specification.
25G Cure hardness 80 minimum Shore "D" after curing for 7 days at R.T. or 1 hour at 180 F
26G Charpy Impact strength. Requirements per material specification
27G S.T.I.C. test Requirements per material specification
30G When grain flow photographs or radiographic films accompany the lot, submit to BAMPE Laboratory for evaluation
33G Certificate of Conformance for each batch must show compliance with FAR 25.853 (a) Amendment 25-83, Appendix F, Part I (a) (1) (ii).
36G Dry adhesion on chromic acid anodizing
37G Assembly time as per AMS-S-8802 (approved by J. Guignard from Airbus on May 24th 2004 by email)
38G Non-volatile content of the base shall be 60% +/- 3% for Color # 16473 Dark Gray only.
39G 180 degree Peel Adhesion Test per ASTM D 3330 on Stainless Steel
40G Cure Time per BATS 4315: Shore A 30 after 5 days at 75 F +/- 5 F + 50% R.H.
41G Gel Time at 250F per specification
42G Lap Shear at RT with 250F Cure per specification
43G Impregnation Material Areal Weight per specification
45G Initial viscosity and viscosity at the end of the pot life
46G Initial viscosity and viscosity after 3 hours, 6 hours and 8 hours pot life
47G Cure hardness 50 Shore "A" minimum after 14 days at R.T.
49G Lapshear strength per BATS 3460 shall be 3800 psi minimum individual. Panels shall be prepared per BATS 6203 and cured at 75F for 30 minutes with a pressure of 4 +/- 1 psi, followed by 24 hours without pressure.
50G Test per FAR 25.853, App. F, Part 1, (a)(1)(i), Flammability
51G Mechanical properties (UTS, YS, %E) in the Longitudinal direction shall meet latest MMPDS requirements.
52G Peel test per BATS 6304, set number 6, immersion (b). Requirement by material specification.
54G Peel test per BATS 6304, set number 7, immersion (d).
55G Flow at 350F per specification
56G Lap shear at RT with accelerated cure per specification
57G Fastener installation time
59G Specific Gravity (Accelerate cure 4 hours at standard conditions followed by 20 hours at 140 +/- 5 F)
61G Exotherm tested at 350 +/- 10 F
62G Beam shear at 75 +/- 5 F (250 F cure, 3 specimens)
63G Tube shear at 75 +/- 5 F (250 F cure, 5 specimens)
64G If primer is purchased without the associated basecoat and clearcoat for painting of detail parts, only the tests on primer by itself are required.
65G Compression strenght and modulus calculation with room temperature or accelerated cure per specification.
66G Omit non-volatile content of the thinner
67G Flow at 250F per specification
68G Omit non-volatile content of the hardener
69G Glass Transition Temperature
70G Acceptance tests conditions same as per supplier batch/lot acceptance tests. Acceptance test methods and requirements per section 7 of material specification.
71G Gel time 2-10 minutes at 250 F per BATS 4564
72G Gel time 2-15 minutes at 260 F per BATS 4564
73G Omit Solar Reflectance and Thermal Emittance
75G All batch acceptance tests specified in BAMS 532-040 Table 7, except Prepreg Chemical Properties. Requirements per BAMS 532-040, Type 2 Class I, II or III, as applicable. The curing details and test methods shall be as defined in BAMS 532-040.
76G All batch acceptance tests except HPLC, carbon fiber characterization properties, and 90 degree tension strenght & modulus at 350F/Dry
77G Lap Shear at RT with 350F Cure per specification
78G Requirements and test methods as defined in MAM-BA000-065
79G All batch acceptance tests specified in BAMS 565-012 Table 5. Requirements per BAMS 565-012 Type II Grade 2.
80G Warpage as per specification
81G Viscosity of base component
83G Test per 14 CFR part 25, Appendix F, Part I (a) (1) (iv)
84G Verify test report to ensure all batch acceptance tests have been performed and that they meet the material specification requirements.
85G Tack Free Time 4 hours at 75 +/- 5F & 50 +/-10% Relative Humidity
86G All purchaser/user batch acceptance tests specified in, and to the requirements of DHMS P1.22
87G All batch/lot acceptance tests required for the manufacturer as specified in the Bombardier approved Process Control Document (PCD)
88G Omit impact test on primer only.
89G Compression strength @ 2% deflection tested at RT
90G Perform the Batch Acceptance Tests required of the manufacturer for Mixed Materials properties only, as per the material specification