INDEX 1. REFERENCES ...................................................................................................
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INDEX 1.
REFERENCES ...................................................................................................... 2
2.
INTRODUTION.................................................................................................... 2
3.
SHEET PARTS ..................................................................................................... 3
3.1 3.2 3.3 3.4
BEND RADIUS ........................................................................................................................... 3 LIGHTENING HOLES ................................................................................................................ 4 TOOLING HOLES ...................................................................................................................... 5 VARIOUS .................................................................................................................................... 5
4.
MACHINED PARTS ............................................................................................ 6
4.1
TOOL RADIUS ................................................................................................................................ 6
4.1.1 4.1.2 4.1.3
Standard ..................................................................................................................................................................... 6 Specials ...................................................................................................................................................................... 7 Spherical tool ............................................................................................................................................................. 8
4.2
THICKNESS-HEIGHT RATIO IN STIFFENERS ...................................................................................... 9
4.2.1
Transitions / Changes in thickness ............................................................................................................................. 9
4.3 4.4 4.5 4.6
CHAMFER................................................................................................................................. 10 STIFFENERS ENDINGS ............................................................................................................... 11 MINIMUM MACHINED THICKNESS .................................................................................... 11 TAPPING ................................................................................................................................... 12
5.
JOINS ................................................................................................................... 13
5.1 5.2
STEP........................................................................................................................................... 13 FOR INSTALLATION ...................................................................................................................... 13
5.2.1 5.2.2
Drilling diameter ...................................................................................................................................................... 13 Other requirements .................................................................................................................................................. 18
5.3
EDGE DISTANCES .................................................................................................................. 20
5.3.1 5.3.2
New parts ................................................................................................................................................................. 20 Parts reused existing holes ....................................................................................................................................... 20
5.4 5.5 5.6 5.7 5.8
RIVET STEP .................................................................................................................................. 21
6.
TOLERANCES ................................................................................................... 23
6.1 6.2 6.3
METALLIC PARTS ......................................................................................................................... 23
TYPICAL VALUES FOR EDGE AND STEP DISTANCES .................................................... 21 SHIMS ........................................................................................................................................ 22 CLEARANCES ............................................................................................................................... 22 RIVETS REPLACEMENT ................................................................................................................. 22
COMPOSITE PARTS ....................................................................................................................... 23 NO MODEL ELEMENTS .................................................................................................................. 24
7. MATERIAS, PROCESSES AND APPLICABLE CODES……. PROTECTION .............................................................................................................. 25
1.
REFERENCES 1. NT-FA-ID-05006: Selection of materials, processes, and corrosion prevention codes applicable to A330-200-MRTT programme. 2. NT-FA-ANC-05006: Standard parts applicable for EADS-CASA to A330-200 MRTT
2.
INTRODUTION
The purpose of this document is to present and summarize the design principles used in the transformation to a commercial Airbus A330-200 in a tanker aircraft (MRTT) It is important to remember that change is a repair, it will replace, modify or strengthen parts as needed. In particular, special attention should be paid to existing riveted, which will determine some design decisions.
3.
SHEET PARTS
In general, bent sheet metal parts used only when the tolerances are not smalls (although the charges are not very high, if they are fit enough pieces, small tolerances are required.) When the tolerances are tight or the part must be copied double-curved, bent sheet metal part is not the choice. In that case, double-curved, it is possible to do like ruled surface. The preferred material is 2024 aluminum cladding (Clad) and the normal state T3. Preferred thicknesses are in the following table (to reduce weight without penalizing supplies). Sizes larger than the standard must be communicated immediately to manufacturing / materials for availability / timing
3.1
BEND RADIUS
The most used bend radius are shown in the I+D-P-212 for aluminum and I+D-P-206 for steel and titanium, for thickness, treatment and selected material. The typical values for this materials are shown in the following table: MATERIAL
STATE THK IN mm
2024 2024 Clad
0 T3 T4
7075 Clad
0 T6
MATERIAL
STATE THK IN mm
2,0
2,3
2,5
3,0
3,2
3,5
4
4,8
5
6
0
3,0
4
4
5
5
5,6
7,2
9,5
10
12
T3 T4
8
9
10
12
12
12,7
17
21,4
25
0
3
4
4,8
-
5,6
-
7,9
9,6
-
T6
12,7
14,2
16,8
-
21,3
-
27
35
-
2024 2024 Clad 7075 Clad
BEND RADIUS (Minimum) en mm 0,3
0,4
0,5
0,63
0,8
1,0
1,2
1,3
1,4
1,5
1,6
1,8
0,6 1,0 0,8 2,3
0,6 1,0 0,8 2,3
0,6 1,6 0,8 3
0,6 2,0 0,80 4
1,0 2,5 0,8 4,8
1,2 3 1,6 6,4
1,6 4 1,6 -
1,8 4,5 1,6 7,9
2,0 5 -
2,0 5 -
2,0 5 2,3 10,4
3,0 6,0 3 11,2
6,4
9,5
12,7
16
35
64
30
32
48
-
-
22,9
35
63,5
-
50,8
-
-
BEND RADIUS (Minimum) en mm
In general, the used bend radius should be the minimums, unless the cargos will be small and the bend radius standard should be used. If it bend in 0 state, and it will be processed to final state (T4 or T6), it is necessary to explain this like: 2024-0 2024T42 7075-0 7075T62
3.2
LIGHTENING HOLES
To lightening and provide access while it gives rigidity to the piece, lightening holes are used according to CAN 16070. The edge of the lightening hole will, if it is possible, on the side of the flap of the piece. The preferred type is BT, whose dimensions listed in the CAN are: :
Designación
BT20 BT25 BT30 BT35 BT40 BT42 BT50 BT60 BT70 BT80 BT90 BT100 BT120 BT140 BT160 BT180
A aprox. 20 25 30 35 40 42 50 60 70 80 90 100 120 140 160 180
C aprox. 17 22 26 32 36 39 46 56 65 75 84 94 112 131 150 169
E mín. 9 9 9,5 10 10 10 10 10 10,5 11 11,5 12 13 14 15 16
H aprox. 3 3 4,5 4,5 5 5,5 5,5 6 6,5 7 7,5 8 9 10 11 12
R ± 1mm 3 3 4 4 5 5 6 7 7 8 8 8 8 8 8 8
The minimum distances to edges, some folded, some lightening, etc. are also included in the CAN 16070 According
to
the
material
and
treatment,
Material Estado Espesor max W 2,5 2024 O 2,5 T42 1,6 W 2,5 2024 O 2,5 Clad T4 1,6 7075 W 2,5 Clad O 2,5
thickness
Diametro Min Max 20 180 20 180 20 180 30 180 30 180 30 180 30 180 30 180
and
maximum
sizes
are:
3.3
TOOLING HOLES
To hold the piece in useful during complex bending operations (piecework, lightening, or flanges snare a curved shape), often are required tooling holes The standard diameter is 6.1 mm. The minimum number of drills to use a piece is two, but depending on the size might be needed more. In any case, the distance between them should be as large as possible. His position must be agreed with manufacturing.
3.4
VARIOUS
Cutout radius: The best cutout radius are 8 mm (4mm if it not possible 8mm). Minimum length flap. The minimum length required to bend a flap is defined in the standard DIN9003, if in a particular case appear not to use 2.5 times the bending radius. This minimum distance must be respected in all areas near the tip radius.
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4.
MACHINED PARTS
4.1
TOOL RADIUS
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4.1.1 Standard Como compromiso adecuado entre velocidad de avance, profundidades habituales de mecanizado y obtención de detalles con vida en fatiga aceptable y peso no penalizado, la herramienta típica es: diameter = 16 mm. Cutter radius = 4 mm To avoid stalls during the machining tool, the modeling radio parts must be greater than the tool. Therefore: Drafting radius = 9 mm. Cutter radius= 4 mm
D/2+1 R
R
ØD
Tipical tool: D = 16, R = 4
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4.1.2 Specials
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4.1.3 Spherical tool In general, it is prefer the use of cylindrical tools. The spherical tools increase the costs, but it can be used in special cases. The most used are: R4 R5 R6 In the next pictures it can be seen in which cases can be used spherical tool, and which is the alternative with cylindrical.
1
Alternative solution with cylindrical tool
Cylindrical tool USUAL USE
Spherical tool EXCEPCIONAL USE
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4.2
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THICKNESS-HEIGHT RATIO IN STIFFENERS
The following table lists the maximum height of stiffeners depending on the thickness and length.
h 25 36 42 60 75 96 120
t 1,5 1,8 2,0 2,5 3,0 4,0 6,0
R 10 16 20 20 20 25 25
E 150 180 200 250 300 450 450
These values are met if the cutter diameter D satisfies: For Aluminum D ≥ h / 3 To Titanium & Steel D ≥ h / 2
4.2.1 Transitions / Changes in thickness Thickness transitions in the direction of the load must be done gently to avoid problems of fatigue. The value to use as a baseline to confirm with fatigue, 70% t1
t2
t3
Recommended value 0.7 t2≈ 0.7 t1 t3≈ 0.7 t2 ~ 0.4 t1
To make a piecework in a machined part (see figure below) are recommended in the following table values (thickness zone ≈ 7 x depth of piecework). It will seek to install a rivet in the area of additional thickness to withstand torque produced by the misalignment of loads.
S M X
0,6
0,8
1,0
1,2
1,6
2,0
2,5
3,2
4,0
5,0
4,2
5,6
7
8,4
11,2
14
17,5
22,4
28
35
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4.3
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CHAMFER
To attach machined parts, the preferred method is to chamfer the inner part. The chamfer is 1 mm greater than the radius of machining the part on which it rests (R1 +1). The inner radius R2 should be large enough to keep the throat, causing the thickness of the thin wing, ie, w ≥ min. (t1, t2)
Gap for sealant. Parts were designed, leaving a gap of 0.2 mm between the pieces. This gap is due to the thickness of sealant applied to the assembly between the bearing faces of the pieces.
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4.4
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STIFFENERS ENDINGS
Stiffeners that end not attached to another wing or stiffener, should be cut at an angle to improve the discharge. When the load is tension, the angle that produces the best allowable fatigue is 15 º. If compression, cutting two planes 15 and 30 º is recommended 1 1 5
r
P u e d e c o n tin u a rs e e lc o rte c o n 3 0 º .A lg o p e o r
1 5 º
4.5
r
1
3 0 º
MINIMUM MACHINED THICKNESS
The minimum thickness depends on the material, the size of the area to be machined, the support on the table and technology. The minimum values are
Tecnology Material Aluminium Titanium - steel
Conventional
High speed
One face
Two faces
One face
Two faces
1,2
1,5
0,7
0,8
1,5
1,7
-
-
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4.6
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TAPPING
In exceptional cases, with the consent of fatigue can be used tappings to allow the seat of the head of bolts or rivets. If you make will be made according to the following diagrams. By request of fatigue, the tapping fillet radius will be 2.5 mm.
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5.
JOINS
5.1
STEP
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The typical step of riveting will be between 5 and 8 D (D = diameter of rivet) For joints staggered, the distances between rivets also apply. For sealing, at least one staggered riveted joint must be used
5.2
FOR INSTALLATION
5.2.1 Drilling diameter It will be identified and it will be used drill diameters and adjustments from CAN40027 for fixed joints: Hi-Loks
Typical drills (like I+D-P-117) AA
Drills with more tightening than AA (strong requirement for fatigue) A
Solid rivets
Drills presure limit ( like I+D-L-113) FF
Drills with greater ease than FF (without pressure limit) F
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For removable elements, are used preferably screws of 4.8 mm. The holes are as follows (see CAN16030 for drill rivet nut installation):
2D
5D**, 8D* D+1
D is the maximum diameter needed for bolt, according with CAN16030. For not anchor nuts it will be used the LOCK NUTS column. The diameter for anchor nuts only is necessary to apply in the part where nut is riveted, in the other(s) join part(s) the diameter will be LOCK NUTS column. Anchor nuts will be modeled with nominal diameter and measured with tolerances +/- 0,1; for not anchor nuts will be modeled with minimum diameter and measured with tolerances – 0,0 / +0,1.
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ANCHOR NUTS IN PRIMARY STRUCTURE, ACCORDING WITH CAN16030 Hole Min edge Min hole Min radius Bolt diameter diameter (D) distance(mm.) distance(mm.) distance (mm.) 2D 5D D+1 inch mm mm. .1120 2,84 3,3 -3,5 7 18 5 .1380 3,50 4,0 - 4,2 8 21 6 .1640 4,17 4,7 - 4,9 10 25 6 .1900 4,83 5,3 - 5,5 11 28 7 .2500 6,35 6,8 - 7,0 14 35 8 .3125 7,94 8,4 - 8,6 17 43 10 .3750 9,52 10,0 - 10,2 20 51 12 .4375 11,11 11,6 - 11,8 24 59 13 .5000 12,70 13,2 - 13,4 27 67 15
ANCHOR NUTS IN SECUNDARY STRUCTURE, ACCORDING WITH CAN16030 Hole Min edge Min hole Min radius Bolt diameter diameter (D) distance(mm.) distance(mm.) distance (mm.) 2D 5D D+1 inch mm mm. .1120 2,84 4,4 – 4,6 9 23 6 .1380 3,50 5,0 – 5,2 10 26 7 .1640 4,17 5,7 – 5,9 12 30 7 .1900 4,83 6,4 – 6,6 13 33 8 .2500 6,35 7,9 – 8,1 16 41 10 .3125 7,94 9,5 – 9,7 19 49 11 .3750 9,52 11,0 – 11,2 22 56 13 .4375 11,11 12,6 – 12,8 26 64 14 .5000 12,70 14,2 – 14,4 29 72 16
NOT ANCHOR NUTS, ACCORDING WITH CAN16030 Hole Min edge Min hole Min radius Bolt diameter diameter (D) distance(mm.) distance(mm.) distance (mm.) 2D 5D D+1 inch mm mm. .1120 2,84 3,0 – 3,1 6 16 5 .1380 3,50 3,7 – 3,8 8 19 5 .1640 4,17 4,3 – 4,4 9 22 6 .1900 4,83 5,0 – 5,1 10 26 7 .2500 6,35 6,5 – 6,6 13 33 8 .3125 7,94 8,1 – 8,2 16 41 10 .3750 9,52 9,7 – 9,8 20 49 11 .4375 11,11 11,3 – 11,4 23 57 13 .5000 12,70 12,9 – 13,0 26 65 14
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Countersink the minimum thickness, according to the following tables: Fastener Diam. 4 4,8 6,4 8 9,6 11,1 12,7
Fastener Diam. 4 4,8 6,4 8 9,6 11,1 12,7
DAN6 H 1,041 1,194 1,549 1,727 1,981 2,461 2,713
t 1,6 1,8 2,3 2,6 3,0 3,7 4,1
FASTENER TYPE DAN8 NAS1097 H t H t 1,778 2,7 0,945 1,4 2,045 3,1 1,168 1,8 2,743 4,1 1,524 2,3 3,429 5,1 4,115 6,2 4,813 7,2 5,486 8,2
NAS1581 H
t
1,25 1,6 1,79 2,07 2,55 2,83
1,9 2,4 2,7 3,1 3,8 4,2
FASTENER TYPE ASNA0077 NASM 20426 H t H t 1,4 2,1 1,402 2,1 1,78 2,7 1,785 2,7 2,44 3,7 2,422 3,6 2,703 4,1 3,417 5,1
FASTENER Fastener TYPE Diam. NAS1153 4,8 NAS1154 6,4
H 2,04 2,703
t 3,1 4,1
H ≤ 2/3 t
Min 0,5 mm
H
“Knife edge”
t
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5.2.2 Other requirements Distance to the nearest wall: The rivet head should not be on the radio. It should also be checked in the piece to which it binds. Typical values indicated in the diagram below. Taking into account the provision for the case of reusing existing holes (paragraph 5.3.2 below) Max. of
(Inst. Req; R+D+2; Rhead + 1)
1 min R
D
Check installation possibilities, especially for blind rivets.
NO OK
OK
Check access hi-lok/hi-lite Installation In general, to allow the pass from the pilot holes to final diameter and the installation of the Hi-Loks with automatic tool, it should be left a free space. For Hi-Lok installation should be left on the side where it will go the collar, a clearance of 10 mm radius (not taking into account the radius of the piece) and 50 mm in height for automatic installation or 30 mm in height for manual installation. Should be left free access to one of the two sides of the junction (on the side of pilot if exists) for drilling. 20
50 mm automatic 30 mm manual
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The relation between the diameter of the rivet and junction thickness should be between 2.5 (for solid rivets in single shear) and 4 (for bolts in double shear)
D
t
Solid rivets t/D 2,5. Hi-Loks y structural bolts t/D 4* * In areas of high load transfer stress department should be consult by the convenience of used steel hi-loks.
CONTOURING CRITERIA Ø Fastener inch 3/32 4/32 5/32 3/16 7/32 1/4 5/16 7/16 1/2
mm. 2,38 3,2 3,96 4,82 5,56 6,35 7,94 9,52 11,11
Maximum thickness to join HI-LOKS Y BOLTS
Maximum thickness to join RIVETS
10 13 16 19 22 25 32 38 44
6 8 10 12 14 16 20 24 28
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5.3
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EDGE DISTANCES
5.3.1 New parts Typical values:
Metal, all directions: 2D+1mm
Composites:
Perpendicular to principal load or compression: 2.5D+1mm Parallel to principal load: 3D + 1mm
5.3.2 Parts reused existing holes When it is reusing existing holes, the distances to edge should be considered sufficient additional margin to see the original assembly tolerances. The actual position of the drilling could oscillate a few mm from the original theoretical position. When reusing existing holes shall be increased by 2mm to-edge distances typical. The impact on weight, should be analyzed case by case basis
D+4
2D+4
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5.4
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RIVET STEP
General values for structural joints: Min: 4D Max: 8D Optimum step for structural joints: Metal: 5D Composites: Fibra Alto Módulo: 4,5D Fibra alta resistencia: 5D For non-structural joints, the maximum is used to 10D For removable joints, the typical step is 10D
5.5
TYPICAL VALUES FOR EDGE AND STEP DISTANCES
EDGE DISTANCE METAL Fastener Dia. 4 4,8 6,4 8 9,6
EDGE DISTANCE
METAL
COMPOSITE
FASTENER PITCH (P)
COMPOSITE
Std Shear/Comp. Tension Std Shear/Comp. dFastener et = des = 2 d Det +=1d des==22,5 D 1+ 1des =d2,5 et = 3 D + 1 D + D+1 es Dia. 11 4 9 9 1113 15,5 4,8 11 11 13 13 20,5 6,4 14 14 17 17 8 17 17 21 2125 9,6 20 20 25 2530
FASTENER PITCH (P)
Nominal Minimum Maximum Tension Nominal MetalMinimum (4D) Composite (4,5D) ( 4D ( 6D ) det = )3 D + 1 Metal (4D) Composite (4,5D) ( 4D ) 16 16 16 1816 24 18 13 19,2 19 19,2 2219 28,8 22 15,5 25,6 26 25,6 2926 38,4 29 20,5 25 32 32 32 3632 48 36 30 38,4 38 38,4 4438 57,6 44
P
P des
des det
det
Ma (
2 3
5
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5.6
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SHIMS
For easer installation or to take into account manufacturing tolerances and assembly, in some places it is necessary to consider the use of shims. The application to this program are:
Liquid shim allowed to 0.5 mm Solid shim allowed to 1.0mm (standard solid shim LN29557-3.0255.32Axx, XX thickness)
Shim aplication rule: I+D-P-061
5.7
CLEARANCES
In the absence of other documents that define specific values for an installation, the following values are used for parts to be designed with security clearances or distances:
5.8
Between joint parts but with relative movement between them: 6.5mm (1/4”) Between non-joint parts but with relative movement between them : 13 mm (1/2”) Between non-joint parts, relative movement between them and possible vibration: 25mm (1”)
RIVETS REPLACEMENT
The criteria for the replacement of rivets or other fasteners are: Solid rivet replaced by solid rivet: Use the same diameter Solid rivets replaced by hi-lok: Use oversized hi-lok Hi-lok replaced by Hi-lok: Use oversized hi-lok
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6.
TOLERANCES
6.1
METALLIC PARTS
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The typical values for machining parts are following as shown. In the drawings wil be indicated (always with the manufacturing agreement) those values that are required for assembly 0,15
BORE AND NERVE THICKNESS LENGHTS
30 mm l 30 < l 100 100 < l 500 500 < l 1000 1000 < l < 2000
0,2 0,3 0,5 1 1,2
ANGLES
30 31 < 120 120 < 315º
1º 0,5º 0.25º
ACCORDING RADIUS
+ 1,0 - 0,5
DEPTH RADIUS
0,5
ROUND OF EDGES
R = 0,3
+ 0,2 -0
FLATNESS
0,5 / 100 mm. Max. 1.0mm
PARALLELISM SQUARENESS
0,3 / 100 mm. Max. 1.0mm
RIGHTNESS
0.1 / 100 mm. Max. 1.0mm
6.2
COMPOSITE PARTS
Tolerances in manufacturing parts depends of manufacturing methodology, material and the number of plies. Typical values are:
UD Tape Prepreg Fabric Prepreg Glass Fibre Prepreg
Thickness tolerance (CASA values) Less than 20 ply 20 - 40 ply +/- 6% Max of (+/- 5% , +/-0,22) +/- 7% Max of (+/- 4,5% , +/-0,20) +/- 7% Max of (+/- 6% , +/-0,14)
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6.3
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NO MODEL ELEMENTS
Primer and paint, tedlar, adhesives, bronze net and fiberglass patch are not modeled in CATIA but should be considered for the calculation / determination of the gaps between parts. For the clearance calculation, following values are used:
Primer: Paint: Sealant: Fiberglass (for ply): Tedlar, bronze net and adhesives:
N/A N/A 0,2 mm 0,1 mm 0,3 mm
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7. MATERIAS, PROCESSES AND APPLICABLE CODES……. PROTECTION
EADS-CASA DESIGNATION
SEMIFINISHED PRODUCT STANDARD
AIRBUS MATERIAL SPECIFICATION
MATERIAL DESCRIPTION
ANTICORROSIVE PROTECTIONS (See 2.2.1) Z11.502
---
AIMS09-08-001Gr.2
Z11.505
---
AIMS09-08-003
CORROSION INHIBITING COMPOUND CORROSION INHIBITING COMPOUND
PRIMERS AND TOP COATS (See 2.2.2) Z12.113
---
AIMS04-04-004
Z12.129
---
AIMS04-04-002
FUEL TANK COATING NON CORROSION INHIBITING PRIMER
Z12.132
---
AIMS04-04-002
PRIMER FOR ANTIEROSION PAINT
Z12.201
---
---
EPOXY FILLER
Z12.210
---
---
EPOXY FILLER
Z12.211
---
AIMS04-04-011
Z12.380
---
AIMS04-04-003
POLYURETHANE PORE-FILLER INTERNAL PAINT SYSTEM (TOP COAT)
Z12.402
---
AIMS04-04-009
VARNISH FOR TOUCH-UP
Z12.412
---
AIMS04-04-023
U.V. RESISTANT VARNISH
Z12.512
---
AIMS04-04-024
ANTISLIP PAINT
Z12.520
---
AIMS04-04-007
Z12.524
---
AIMS04-04-010
ABRASION RESISTANT PAINT SEALANT BEAD PROTECTION PAINT
PLASTIC MATERIALS (See 2.2.3) Z14.501
LN9298
WL-5.1129.10
PTFE MOLDED (SHEETS)
Z14.502
---
Z14.510
---
AMS3652 L-P-1040B TYPE II, GRADE B, CLASS 1
PTFE SKIVED (FOILS) POLYVINYL FLUORIDE FILM (GREY)
Z14.512
---
L-P-1040B TYPE II, GRADES B AND C, CLASS 1
POLYVINYL FLUORIDE FILM (WHITE)
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EADS-CASA DESIGNATION
SEMIFINISHED PRODUCT STANDARD
AIRBUS MATERIAL SPECIFICATION
Pág. 26
MATERIAL DESCRIPTION
RESIN AND ADHESIVE MATERIALS (See 2.2.4) Z15.101
---
MMM-A-121
ELASTOMERIC ADHESIVE (NEOPRENE)
Z15.104
---
MIL-C-4003
ELASTOMERIC ADHESIVE (NITRILE)
Z15.201
---
I+D-N-200
EPOXY ADHESIVE
Z15.205
---
I+D-N-200
EPOXY ADHESIVE
Z15.209
---
DAN1284-01
EPOXY ADHESIVE
Z15.213
---
I+D-N-200
EPOXY ADHESIVE
Z15.301
---
I+D-N-200
SILICONE ADHESIVE
Z15.415
ABS5337
AIMS10-02-003
Z15.429
---
I+D-N-200
Z15.601
---
A-A-3097 TYPE I CL.2
Z15.915
---
I+D-N-200
BONDING PRIMER
Z18.115
---
I+D-N-200
EPOXY CORE FILLER (LOW VISCOSITY)
Z18.144
---
I+D-N-200
EPOXY CORE FILLER (R.T. CURING)
Z18.179
---
DAN1206-01
EPOXY CORE FILLER (HOT CURING)
CORE SPLICING ADHESIVE EPOXY FILM ADHESIVE (300 g/m2, 115 ± 5°C CURE) CYANOACRYLIC ADHESIVE
SEALANTS (See 2.2.5) Z11.903
---
AIMS04-05-005 TYPE I
Z16.101
---
AIMS04-05-002 INTERFAY
FAYING SURFACE SEALANT
MIL-PRF-81733 TYPE II-2
CORROSION INHIBITING COMPOUND
Z16.113 Z16.156 Z16.157 Z16.160 Z16.161 Z16.302 Z16.912
---
NON HARDENING JOINTING COMPOUND
AIMS04-05-002 BRUSH
INTEGRAL FUEL TANK SEALANT
AIMS04-05-002 FILLET
INTEGRAL FUEL TANK SEALANT
AIMS04-05-006 TYPE A
LOW ADHESION SEALANT
AIMS04-05-006 TYPE B
LOW ADHESION SEALANT
---
MIL-A-46106B GROUP I, TYPE I
SILICONE SEALANT
---
---
---------
ADHESION PROMOTER
HONEYCOMB CORES (See 2.2.6) Z17.607 Z17.622
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I+D-P-176 Class 1, Type 1
ARAMID HONEYCOMB CORE 3.0-1/8
I+D-P-176 Class 1, Type 1
ARAMID HONEYCOMB CORE 6.0-3/16
Edic./Issue A
NT-FA-ASO-05-087
AIRBUS MATERIAL SPECIFICATION
SEMIFINISHED PRODUCT STANDARD
EADS-CASA DESIGNATION
Pág. 27
MATERIAL DESCRIPTION
RESIN AND ADHESIVE MATERIALS (See 2.2.4) A-A-3097 TYPE I CLASS 2
---
Z15.601
CYANOACRYLIC ADHESIVE
AIMS10-02-003
ABS5337
Z15.415
CORE SPLICE ADHESIVE
Z18.179
EPOXY CORE FILLER (HOT CURING)
Z15.201
EPOXY ADHESIVE
Z15.205
EPOXY ADHESIVE
Z15.209
EPOXY ADHESIVE
Z15.213
EPOXY ADHESIVE
Z15.301
SILICONE ADHESIVE
Z15.429
EPOXY FILM ADHESIVE (300 g/m2, 115 ± 5°C CURE)
Z15.915
BONDING PRIMER
Z18.115
EPOXY CORE FILLER (LOW VISCOSITY)
Z18.144
EPOXY CORE FILER (R.T. CURING)
Z15.104
ELASTOMERIC ADHESIVE (NITRILE)
Z15.101
ELASTOMERIC ADHESIVE (NEOPRENE)
DAN1206-01 I+D-N-200 I+D-N-200 I+D-N-200 I+D-N-200 I+D-N-200 I+D-N-200 I+D-N-200 I+D-N-200 I+D-N-200 MIL-C-4003 MMM-A-121
-------------------------
SEALANTS (See 2.2.5) Z16.101
FAYING SURFACE SEALANT
Z16.156
INTEGRAL FUEL TANK SEALANT
Z16.157
INTEGRAL FUEL TANK SEALANT
---
Z11.903
NON HARDENING JOINTING COMPOUND
AIMS04-05-006 TYPE A
---
Z16.160
LOW ADHESION SEALANT
AIMS04-05-006 TYPE B MIL-A-46106B GROUP I, TYPE I
---
Z16.161
LOW ADHESION SEALANT
---
Z16.302
SILICONE SEALANT
---
---
Z16.912
ADHESION PROMOTER
AIMS04-05-002 INTERFAY
---
AIMS04-05-002 BRUSH
---
AIMS04-05-002 FILLET
---
AIMS04-05-005 TYPE I
HONEYCOMB CORES (See 2.2.6) I+D-P-156 Class 1, Type 1
---
Z17.607
ARAMID HONEYCOMB CORE 3.0-1/8
I+D-P-156 Class 1, Type 1
---
Z17.622
ARAMID HONEYCOMB CORE 6.0-3/16
NT-FA-ASO-05-087
AIRBUS MATERIAL SPECIFICATION
SEMIFINISHED PRODUCT STANDARD
EADS-CASA DESIGNATION
Edic./Issue A
Pág. 28
MATERIAL DESCRIPTION
WET LAY-UP MATERIALS (See 2.2.7) AIMS08-02-001 AMS-C-9084 T.III C2 AMS-C-9084 T.VIII C2 I+D-N-200
---------
Z18.170
EPOXY RESIN, R.T. CURING, FOR GLASS WET LAYUP
Z17.201
GLASS FIBER FABRIC (120 style, 104 g/m2)
Z17.208
GLASS FIBER FABRIC (181 style, 293 g/m2)
Z18.142
EPOXY RESIN, HOT CURING, FOR FILLING AND POTTING
PREPREG MATERIALS (See 2.2.8) AIMS05-10-001
ABS5047
Z19.607
GLASS/PHENOLIC PREPREG (7781 TYPE, 135°C CURE)
AIMS05-10-009
ABS5047-01
Z19.605
GLASS/PHENOLIC PREPREG (120 TYPE, 135°C CURE)
I+D-P-250A, Group I
---
Z19.101
GLASS/EPOXY PREPREG (181 TYPE, 125°C CURE)
I+D-P-250A, Group I
---
Z19.111
GLASS/EPOXY PREPREG (181 TYPE, 125°C CURE)
I+D-P-250A, Group I
---
Z19.301
GLASS/EPOXY PREPREG (120 TYPE, 125°C CURE)
I+D-P-250A, Group I
---
Z19.311
GLASS/EPOXY PREPREG (120 TYPE, 125°C CURE)
MISCELLANEOUS (See 2.2.9) A-A-1689, Type I, Class 2
---
Z24.310
VINYL ADHESIVE TAPE
A-A-59163, Type I
ABS5334
Z22.127
SELF-ADHERING INSULATION TAPE
A-A-59474, Type I, Class 1
---
Z24.330
PTFE ADHESIVE TAPE
MIL-L-23398
---
Z21.305
SOLID FILM LUBRICANT
---
--
Z24.273
DOUBLE SIDED ADHESIVE TAPE