BACK COVER COVER - Rockwell Collinsbeaerospace.com/wp-content/uploads/2016/01/BE-Teklam_Product... · is an industry leader in the design and manufacture of advanced laminated honeycomb

B/E-TEKLAM High PerformanceComposite Panels

350 W. Rincon Street Corona, A 92880+1.951.278.4563 [email protected] beaerospace.com

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ABOUT USEstablished in 1990, TEKLAM, a B/E Aerospace company,

is an industry leader in the design and manufacture of

advanced laminated honeycomb panels.

With over two decades of experience, our superior quality products are designed for aerospace and commercial applications where a high strength to weight ratio is critical.

Our lightweight structural materials are produced to the most stringent requirements. TEKLAM honeycomb panels are designed for optimal performance in their specific applications. Utilizing materials including Carbon Fiber, Kevlar®, Fiberglass, Nomex® and aerospace aluminum alloys, TEKLAM provides unique and innovative solutions to satisfy the most demanding requirements. Through both Multiple Opening Presses (MOP) and vacuum processing we are capable of producing panels of a wide range of shapes, sizes and performance characteristics.

In 2011, TEKLAM was acquired by B/E Aerospace and shortly thereafter moved into a new 93,000 square foot production facility in Corona, California. Our site maintains ISO9001 / AS9100 certification.

PRODUCT DEVELOPMENT AND APPLICATION ENGINEERING SERVICESFrom concept design through qualification, first article inspection and production, our engineers are with you every step of the way. We frequently work with customers to evaluate the properties of the materials used in existing designs so that we can propose alternatives that reduce weight, increase strength and/or reduce cost. Through precise material selection and process variation, our application engineers take pride in making sure that the panel selected for your design is optimal. Whether you are looking for opportunities to reduce weight on an existing application or are working on a new design with demanding requirements, our engineers are available to assist in any way they can. Our established relationships with a wide variety of material suppliers help ensure that the panel materials are ideally suited for your unique application. Our R&D laboratory is equipped with two small scale lab presses and a full range of mechanical testing equipment. Product innovation in composite technology forms the cornerstone of our value proposition.

LAMINATED HONEYCOMB PANELS – FLAT PANELS AND CURVED SHAPESB/E-TEKLAM’s standard aerospace product line includes over 30 floor and interior panels with FAA approved test data available. Beyond these standard products, our R&D engineers are continually working to develop new, innovative designs for the most demanding applications. Standard panel thicknesses are held to an industry leading +/- 0.010 inch tolerance and are designed for durability that is superior to comparable products.

In addition to our line of flat panels, our oven cure vacuum bagging process enables us to produce shapes consisting of complex curves.

EMBEDDED PANELSMany of our advanced, space saving panel designs include components embedded within the panel itself. Hinges, hard points, latches and electrical conduits are only a few common embedded items. Proprietary processes ensure that embedded components maintain their precise location throughout the layup and press process.

VALUE ADDED SERVICESB/E-TEKLAM’s Value Added Services enable the delivery of finished parts or parts kits which are packaged and delivered ready for assembly. These services include the following:

• CNC routing• Edge closeouts and edge fill• Insert installation• Cut and fold

PRODUCTS & CAPABILITIES

ApplicationsB/E-TEKLAM’s extensive product family of laminated honeycomb panels are designed for optimal performance in their specific applications in:

• Aerospace Interiors• Spacecraft• Commercial (Marine, Rail, Automotive)

Within the Aerospace interiors sector, B/E-TEKLAM has been developing and delivering high end products to the following customer segments for 25 years:• OEMs• MROs• VIP• BizJet

PHONE: +1.951.278.4563

[email protected] beaerospace.com

350 W. RINCON STREETCORONA, CA 92880 USA



PHONE: +1.951.278.4563

The aeroFIBERTM family is comprised of sandwich panels with a Nomex® honeycomb core and fiberglass skin. Dependent upon the panel application, a woven fiberglass with a phenolic or epoxy resin is possible. Primarily used on aircraft interiors including monuments, partitions and ceiling panels, the fiberglass panels feature a combination of light weight with high strength, durability and corrosion resistance. The phenolic fiberglass panels provide superior flammability properties, heat release and low smoke emissions facilitating use in aircraft interiors.

Benefits• Available in multiple sheet sizes from 48” x 96” up to 60” to 144” (additional size options are available upon request through the aeroADDTM family)• Capability to produce panels at a thickness tolerance of ± 0.010”• Can be designed to meet all requirements of FAA CFR 25.853 Appendix F: Part I – 60 sec vertical; Part IV – OSU Heat Release; Part V – NBS Smoke Emission

• Uses Nomex® core that meets the AMS-C-81986 • FAA approved mechanical properties on select standard panels• Materials used in the aeroFIBERTM family are in accordance with industry standards for mechanical strength properties

Options • Phenolic Resin • Epoxy Resin• 1-Ply Fiberglass • 2-Ply Fiberglass

ApplicationsThe aeroFIBERTM family is primarily designed for aircraft interiors including:• Monuments • Partitions & bulkheads• Overhead bins & ceilings

THE BASICS DONE RIGHT

aeroFIBERTM

Performance• Minimum average Peel Strength of 6 in. lb/in with the capability of achieving values of 10 in.lb+ for select panels• Corrosion resistance• Service temperature: -67°F (-49°C) to 180°F (82°C)

EPOXY FIBERGLASS SKIN / NOMEX® CORE - AIRCRAFT COMPOSITE PANEL

Panel Part # Panel Thickness

Panel Weight

Long Beam Flexural Bending

Moment [Mean]

Long Beam Flexural Facing

Stress [Mean]

Short Beam Core Shear [Mean]

Climbing Drum Peel [Mean]

Stabilized Core Compression

[Mean]

FAA Allowables

in lbs/sf in-lbs/in psi psi in-lbs/in psiL W L W L W

NE1G1-02-125 0.125 0.25 21 20 20061 19254 186 113 10 503 Yes

NE1G1-02-250 0.250 0.28 77 75 35876 34450 157 85 15 438 Yes

NE1G1-02-375 0.375 0.31 124 110 37522 33384 136 80 14 342 Yes

NE1G1-02-500 0.500 0.35 146 138 33134 31119 131 79 13 323 Yes

NE1G1-02-625 0.625 0.38 178 167 32000 30000 175 100 10 325 No

NE1G1-02-750 0.750 0.41 237 213 35597 31797 108 77 14 313 Yes

NE1G1-02-875 0.875 0.44 249 233 32000 30000 175 100 10 325 No

NE1G1-02-1000 1.000 0.47 307 287 34391 32060 104 77 11 326 Yes

Flammability FAR 25.853 Appendix F: Part I - 60 second vertical;

Skins 0.010” Epoxy Fiberglass

Core NOMEX® 1/8” Cell, 3 lbs/ft³

Standard Dimensional Length & Width: ±0.500”

Tolerances Thickness: ±0.010”

Panel Dimension 48” x 96” (up to 60” x 144”)

Epoxy Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel

PHENOLIC FIBERGLASS SKIN / NOMEX® CORE - AIRCRAFT COMPOSITE PANEL


Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


NP1G1-02-125 0.125 0.24 33 31 32000 30000 175 100 8 325 No

NP1G1-02-250 0.250 0.27 69 65 32000 30000 175 100 8 325 No

NP1G1-02-375 0.375 0.30 105 98 32000 30000 175 100 8 325 No

NP1G1-02-500 0.500 0.34 142 133 32000 30000 175 100 8 325 No

NP1G1-02-625 0.625 0.37 178 167 32000 30000 175 100 8 325 No

NP1G1-02-750 0.750 0.40 213 200 32000 30000 175 100 8 325 No

NP1G1-02-875 0.875 0.43 249 233 32000 30000 175 100 8 325 No

NP1G1-02-1000 1.000 0.46 285 268 32000 30000 175 100 8 325 No

Flammability FAR 25.853 Appendix F: Part I - 60 second vertical; Part IV - OSU Heat Release; Part V - NBS Smoke Emission

Skins 0.010” Phenolic Fiberglass





Phenolic Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel

STANDARD PANELS

EPOXY FIBERGLASS SKIN / NOMEX® CORE - AIRCRAFT COMPOSITE PANEL


Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


NE2G1-02-125 0.125 0.47 36 38 18888 19512 379 238 10 935 Yes

NE2G1-02-250 0.250 0.50 155 122 37880 29466 200 104 10 473 Yes

NE2G1-02-375 0.375 0.53 265 153 42011 24293 170 85 17 360 Yes

NE2G1-02-500 0.500 0.57 315 191 36698 22080 168 86 16 343 Yes

NE2G1-02-625 0.625 0.60 349 273 32000 25000 175 100 10 325 No

NE2G1-02-750 0.750 0.63 443 279 33825 21161 141 77 15 291 Yes

NE2G1-02-875 0.875 0.66 493 386 32000 25000 175 100 10 325 No

NE2G1-02-1000 1.000 0.69 560 379 31744 21427 134 79 14 295 Yes

Flammability FAR 25.853 Appendix F: Part I - 60 second vertical;

Skins 0.020” Epoxy Fiberglass





Epoxy Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel



Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


NP2G1-02-125 0.125 0.45 62 48 32000 25000 175 100 8 325 No

NP2G1-02-250 0.250 0.48 152 106 36617 24821 165 84 6 357 Yes

NP2G1-02-375 0.375 0.51 218 144 34463 22766 146 80 8 336 Yes

NP2G1-02-500 0.500 0.55 273 190 31980 22064 137 78 7 305 Yes

NP2G1-02-625 0.625 0.58 350 273 32000 25000 175 100 8 325 No

NP2G1-02-750 0.750 0.61 374 266 28761 20172 134 73 7 305 Yes

NP2G1-02-875 0.875 0.64 493 386 32000 25000 175 100 8 325 No

NP2G1-02-1000 1.000 0.67 526 377 29810 21287 127 76 8 310 Yes








Low Weight, High Strength Interior PanelOur unique panel construction provides high strength in interior applications where weight savings is critical. aeroFEATHERTM provides the strength and performance of a double ply fiberglass / Nomex® design with the weight savings of a single ply panel.

Benefits*• Available in multiple sheet sizes from 48” x 96” up to

60” to 144” (additional size options are available uponrequest through the aeroADDTM family)

• Capability to produce panels at a thickness tolerance of± 0.010”

• Low Weight – 38% weight savings compared to

standard two ply fiberglass/Nomex® panel design• High Impact Strength – 300% improvement

in impact resistance• High Peel Strength – 8% improvement in peel strength• Superior Flexural Strength

*Benefits based on NP1G9-02-500 (TEKlam•LITETM)

Applications• Interior monument construction• Interior cabinetry• Galleys and lavatories• Seat surrounds and privacy dividers• Side ledges and side walls• Luggage bins

UP TO 38% WEIGHT REDUCTION

aeroFEATHERTM

PHONE: +1.951.278.4563





Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


NP1G9-02-125 0.125 0.26 42 38 40000 36000 175 100 8 325 No

NP1G9-02-250 0.250 0.29 87 78 40000 36000 175 100 8 325 No

NP1G9-02-375 0.375 0.32 132 118 40000 36000 175 100 8 325 No

NP1G9-02-500 0.500 0.35 175 159 44390 40271 138 93 10 466 No

NP1G9-02-625 0.625 0.38 222 199 40000 36000 175 100 8 325 No

NP1G9-02-750 0.750 0.41 267 240 40000 36000 175 100 8 325 No

NP1G9-02-875 0.875 0.44 312 281 40000 36000 175 100 8 325 No

NP1G9-02-1000 1.000 0.47 357 321 40000 36000 175 100 8 325 No

Flammability FAR 25.853 Appendix F: Part I - 60 second vertical; Part I - 45 Degree; Part IV - OSU Heat Release; Part V - NBS Smoke Emission







STANDARD PANELS

High Surface Finish Interior PanelB/E-TEKLAM has developed a proprietary process, which produces a panel eliminating the need for secondary surface preparation such as fill and fair or the application of peel plies and surfacing films. After a light sanding and solvent wipe, the panels are ready to be primed and painted.

Benefits• Available in multiple sheet sizes from 48” x 96” up to

60” to 144” (additional size options are available uponrequest through the aeroADDTM family)

• Capability to produce panels at a thickness tolerance of± 0.010”

• Elimination of labor and material costs associatedwith fill and fair operations, peel plies, andsurfacing films

• Reduced weight through the elimination of surfacepreparation materials

• Reduction in processing time• Panel is free from telegraphing of the honeycomb

core, pitting, dimpling, and waviness• Processing can be accomplished on a variety of

phenolic and epoxy panel constructions• If scratched during processing and handling, the panel

can still accept a fill and fair to eliminate the blemish

Applications• Any aircraft interior panel application where a painted

surface is required• Any aircraft interior panel application where a thin

veneer or tedlar is applied and panel surfaceinconsistency may be visible

Performance• Mechanical, physical, and flammability performance

of the panel is not affected

ALL YOU NEED IS PAINT

aeroREADYTM

PHONE: +1.951.278.4563



PHONE: +1.951.278.4563



An innovative panel construction that provides low weight, high strength, improved stiffness and shear in multiple floor panel applications where weight is critical. A Nomex® or Aluminum honeycomb core with a modified toughened epoxy resin system and unidirectional fiberglass or carbon skins yields superior durability performance when compared to the standard OEM floor panel requirements.

Benefits• Available in multiple sheet sizes from 48” x 96” up to 60” to 144” (additional size options are available upon request through the aeroADDTM family)• Capability to produce panels at a thickness tolerance of ± 0.010”• Superior flexural strength, stiffness, and shear which exceed OEM requirements• Low fray edges• Improved processing during secondary operations

such as machining, bonding, insert installation, edge potting, and decorative application

• Excellent performance in both hot and wet conditions• Eliminates the need for more frequent floor board replacements in the cabin and the cargo bay

STRONG, DURABLE FLOORS

aeroBASETMHigh Strength and Stiffness Multi-use Floor Panel

PerformanceB/E-TEKLAM’s most popular aeroBASETM product when compared with standard OEM requirements:• High Flexural Strength: 89% improvement • High Flexural Stiffness: 44% improvement • Excellent Shear Strength: 40% improvement in Panel Shear, 68% improvement in in-plane shear, and 140% improvement in Insert Shear • Hot/Wet Flexural Strength: 67% improvement • No degradation of bond strength in hot/wet conditions• Weight: 0.77 lbs/ft2

Applications• Aisles • Under seats • Entrances/Exits • Galleys• Cargo Bays

EPOXY COMPOSITE SKIN - AIRCRAFT FLOORING PANEL


Panel Weight


Moment [Mean]


Stress [Mean]

Short Beam Core Shear

[Mean]

Climbing Drum Peel

[Mean]

Stabilized Core

Compression [Mean]

FAA Allowables


AE201-22-400 (A401) 0.400 0.51 288 N/A 50000 N/A 340 220 12 570 No

AE203-22-400 (A402) 0.400 0.62 306 N/A 53754 N/A N/A 475 17 1712 Yes

AEU03-11-400 (A402H) 0.400 0.77 N/A 513 N/A 60215 N/A 476 19 1694 Yes

AEV03-11-400 (A402MD) 0.400 0.99 668 N/A 5538 N/A 826 526 12 1560 No

NE2G3-04-400 (N402) 0.400 0.52 266 N/A 35000 N/A 325 175 12 770 No

NE2G3-05-400 (N404) 0.400 0.64 286 N/A 37884 N/A N/A 306 20 Yes

NE1G19-05-400 (N404H) 0.400 0.79 375 N/A 40000 N/A 515 300 12 2100 No

NE1C7-05-400 0.400 0.57 273 N/A 69872 N/A 586 N/A 8.5 2146 No

NE1C7-04-400 0.400 0.44 277 259 70940 66453 406 N/A 12.5 910 No

Flammability FAR 25.853 Appendix F: Part I - 60 second vertical; Part I - 45 Degree;

Skins See List

Core See List



Thickness 0.400

Epoxy Composite Skin / See List - Aircraft Flooring Panel

EPOXY COMPOSITE SKIN - AIRCRAFT FLOORING PANEL

Panel Part # Core Description Skin Upper Spec Skin Lower Spec

AE201-22-400 (A401) 5052 Alum. 1/8” Cell, 4.5 lbs/ft³ 0.015” Epoxy Composite

AE203-22-400 (A402) 5052 Alum. 1/8” Cell, 8.1 lbs/ft³ 0.015” Epoxy Composite

AEU03-11-400 (A402H) 5052 Alum. 1/8” Cell, 8.1 lbs/ft³ 0.022” Epoxy Composite

AEV03-11-400 (A402MD) 5052 Alum. 1/8” Cell, 8.1 lbs/ft³ 0.044” Epoxy Composite 0.022” Epoxy Composite

NE2G3-04-400 (N402) NOMEX® 1/8” Cell, 5 lbs/ft³ 0.015” Epoxy Composite

NE2G3-05-400 (N404) NOMEX® 1/8” Cell, 9 lbs/ft³ 0.015” Epoxy Composite

NE1G19-05-400 (N404H) NOMEX® 1/8” Cell, 9 lbs/ft³ 0.022” Epoxy Composite

NE1C7-05-400 NOMEX® 1/8” Cell, 9 lbs/ft³ 0.010” Epoxy Carbon Fiber

NE1C7-04-400 NOMEX® 1/8” Cell, 5 lbs/ft³ 0.010” Epoxy Carbon Fiber

STANDARD PANELS

A QUALITY CLASSIC IN AEROSPACE

aeroMETALTMB/E-TEKLAM provides a wide range of Aluminum Sandwich panels of the highest industry levels of quality and durability. This aircraft grade panel family can be used in multiple interior and structural applications. It offers the flexibility to customize the sheet size, skin Aluminum type and treatment options. These panels comply with FAA flammability requirements.

Benefits• Available in multiple sheet sizes from 48” x 96” up to 60” to 144” (additional size options are available upon request through the aeroADDTM family)• Capability to produce panels at a thickness tolerance of ± 0.010”• Available in a wide range of Aluminum alloys such as 2024-T3, 7075-T6 with sheet treatment options such as Clad, Anodized/Chem. film, Primer, Alodine, Bare, etc.• Compliant with FAA CFR 25.853 Appendix F: Part I – 60 sec vertical; Part IV – OSU Heat Release; Part V – NBS Smoke Emission • The aeroMETALTM panels use: - An Aluminum skin that meets the applicable AMS- QQ-A-250 Specifications - An Aluminum core that meets the AMS-C-7438 Specifications - A Film adhesive that meets the AMS-A-25463 type 1 Specifications• FAA approved mechanical properties on select standard panels• OEM qualification on select panels

ApplicationsThe aeroMETALTM family is mainly designed for aircraft interiors such as:• Monuments and Shelving• Partitions & bulkheads

PHONE: +1.951.278.4563

Performance• Service temperature: -67°F (-55°C) to 180°F (82°C)• Superior Elasticity• Combination of consistency to cost effectiveness



2024-T3 CLAD SKIN / 5052 ALUM. CORE - AIRCRAFT ALUMINUM PANEL


Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


AA207-33-125 0.125 0.70 120 116 57000 55000 460 300 12 770 No

AA207-33-250 0.250 0.76 263 253 57000 55000 460 300 12 770 No

AA207-33-375 0.375 0.82 405 391 57000 55000 460 300 12 770 No

AA207-33-500 0.500 0.88 609 586 63186 60488 470 293 17 916 Yes

AA207-33-625 0.625 0.94 690 666 57000 55000 460 300 12 770 No

AA207-33-750 0.750 1.00 934 876 63350 59649 456 297 14 957 Yes

AA207-33-875 0.875 1.06 975 941 57000 55000 460 300 12 770 No

AA207-33-1000 1.000 1.12 1228 1193 62370 60688 417 274 17 841 Yes

Flammability FAR 25.853 Appendix F: Part I - 60 second vertical; Part IV -OSU Heat Release; Part V - NBS Smoke Emission

Skins 0.020” 2024-T3 CLAD

Core 5052 Alum. 3/16” Cell, 5.7 lbs/ft3




2024-T3 CLAD Skin / 5052 Alum. Core - Aircraft Aluminum Panel



Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


AA207-55-125 0.125 1.04 169 163 57000 55000 460 300 12 770 No

AA207-55-250 0.250 1.10 398 383 57000 55000 460 300 12 770 No

AA207-55-375 0.375 1.16 626 603 57000 55000 460 300 12 770 No

AA207-55-500 0.500 1.22 853 823 57000 55000 460 300 12 770 No

AA207-55-625 0.625 1.28 1082 1043 57000 55000 460 300 12 770 No

AA207-55-750 0.750 1.34 1445 1384 62562 60264 482 287 11 802 Yes

AA207-55-875 0.875 1.40 1538 1483 57000 55000 460 300 12 770 No

AA207-55-1000 1.000 1.46 1766 1703 57000 55000 460 300 12 770 No








STANDARD PANELS



Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


AA209-33-125 0.125 0.69 120 116 57000 55000 235 150 12 320 No

AA209-33-250 0.250 0.72 263 253 57000 55000 235 150 12 320 No

AA209-33-375 0.375 0.76 401 382 56105 54092 358 177 13 426 Yes

AA209-33-500 0.500 0.79 547 503 56706 52425 302 169 17 405 Yes

AA209-33-625 0.625 0.83 690 666 57000 55000 235 150 12 320 No

AA209-33-750 0.750 0.86 851 721 58210 49217 233 140 19 391 Yes

AA209-33-875 0.875 0.90 975 941 57000 55000 235 150 12 320 No

AA209-33-1000 1.000 0.93 1157 938 58720 47777 246 154 14 417 Yes










Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


AA805-11-125 0.125 0.40 86 83 75000 72000 210 130 12 270 No

AA805-11-250 0.250 0.43 180 173 75000 72000 210 130 12 270 No

AA805-11-375 0.375 0.46 273 263 75000 72000 210 130 12 270 No

AA805-11-500 0.500 0.49 413 388 75997 71118 285 170 14 393 Yes

AA805-11-625 0.625 0.53 462 443 75000 72000 210 130 12 270 No

AA805-11-750 0.750 0.56 555 533 75000 72000 210 130 12 270 No

AA805-11-875 0.875 0.59 648 623 75000 72000 210 130 12 270 No

AA805-11-1000 1.000 0.62 743 713 75000 72000 210 130 12 270 No










Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


AA810-22-125 0.125 0.47 102 98 75000 72000 320 210 12 480 No

AA810-22-250 0.250 0.51 214 206 75000 72000 320 210 12 480 No

AA810-22-375 0.375 0.56 327 313 75000 72000 320 210 12 480 No

AA810-22-500 0.500 0.60 439 422 75000 72000 320 12 480 No

AA810-22-625 0.625 0.65 552 529 75000 72000 320 210 12 480 No

AA810-22-750 0.750 0.69 600 510 73545 62481 344 207 11 658 Yes

AA810-22-875 0.875 0.74 777 746 75000 72000 320 210 12 480 No

AA810-22-1000 1.000 0.78 889 853 75000 72000 320 210 12 480 No








PHONE: +1.951.278.4563

comMETALTM consists of a wide range of commercial grade Aluminum Sandwich panels of the highest quality and durability. The comMETALTM family can be used in multiple structural applications. It offers the flexibility to customize the sheet size, skin Aluminum type and treatment options.

Benefits• Available in multiple sheet sizes from 48” x 96” up to 60” to 144” (additional size options are available upon request through the aeroADDTM family)• Capability to produce panels at a thickness tolerance of ± 0.020”• The comMETALTM panels use 5052-H32 skins

ApplicationsThe comMETALTM family is primarily designed for structural applications when a high strength to weight ratio is required.

Performance• Service temperature: -67°F (-55°C) to 180°F (82°C)• Superior Elasticity

A QUALITY CLASSIC IN COMMERCIAL APPLICATIONS

comMETALTM



ALUMINUM SKIN / ALUMINUM CORE - COMMERCIAL PANEL


Panel Weight


Moment [Mean]


Stress [Mean]




[Mean]

FAA Allowables


AA418-44B-125 0.125 0.84 78 73 31000 29000 210 130 12 325 N/A

AA418-44B-250 0.250 0.88 174 163 31000 29000 210 130 12 325 N/A

AA418-44B-375 0.375 0.92 271 254 31000 29000 210 130 12 325 N/A

AA418-44B-500 0.500 0.95 368 344 31000 29000 210 130 12 325 N/A

AA418-44B-625 0.625 0.99 465 435 31000 29000 210 130 12 325 N/A

AA418-44B-750 0.750 1.03 562 526 31000 29000 210 130 12 325 N/A

AA418-44B-875 0.875 1.07 658 616 31000 29000 210 130 12 325 N/A

AA418-44B-1000 1.000 1.10 756 707 31000 29000 210 130 12 325 N/A

Flammability N/A

Skins 0.025” 5052-H32 Gold Seal

Core 3003 Alum. 3/8” Cell, 3.6 lbs/ft³




Aluminum Skin / Aluminum Core - Commercial Panel

STANDARD PANELS

PHONE: +1.951.278.4563

In addition to a wide range of standard panels, B/E-TEKLAM has the capability to develop completely customized Sandwich Panel combinations that are tailored to specific customer needs. The B/E-TEKLAM team will review your requests or drawings and has the engineering expertise and in-house R&D department to review and test as required and produce complex non-standard panels.

Benefits• Available in multiple sheet sizes from 48” x 96” up to 60” to 144” (additional size options are available through the aeroADDTM family)• Capability to produce panels at a thickness tolerance of ± 0.010”• Customization capability to fit your needs• Can be designed to meet all requirements of FAA CFR 25.853 Appendix F: Part I – 60 sec vertical; Part IV – OSU Heat Release; Part V – NBS Smoke Emission• The Nomex®, Kevlar® and Aluminum honeycomb cores meet AMS industry and OEM specifications• Capability to Vacuum-bag Cure • Capability to run FAA approved test programs • Designed to meet all your mechanical properties with the best combination of durability and light weight• Ability to obtain OEM certification.

Options*Resin Options:• Phenolic • Epoxy Core Options:

• Nomex® • Aluminum • Kevlar®Skin Options: • Aluminum • Carbon • Fiberglass

*Typical options shown, possibilities are infinite.

INFINITE POSSIBILITIES, ONE SUPPLIER

aeroINFINITETM

ApplicationsThe aeroINFINITETM family can be used in: • Interiors• Structural applications • Cargo applications

PerformanceUpon selection of desired combination, B/E-TEKLAM can provide the resulting mechanical properties.



PHONE: +1.951.278.4563

For all panels, standard or custom, B/E-TEKLAM has full tooling capabilities to provide panels with value added operations. Equipped with CNC machines and ovens, a variety of secondary operations can be performed including insert installation, edge sealing, cut and fold, and embedded details within the panel. B/E-TEKLAM has extensive experience to manufacture hand layup curved panels and can procure custom tools or use customer furnished tools to generate the required shape and form.

Benefits*• On-site panel manufacturing and value added to enhance logistics, providing a one-stop shop for customers• The sealants used comply with the FAA CFR 25.853 Appendix F: Part I – 60 sec vertical requirements• Wide range of tools to enable - CNC routing - Hand Routing for complex shapes - Edge closeouts including edgefill, extrusions, bars, or tapes - Insert Installation - Cut and fold - Hand layup curved panels• Embedded Details• Available in custom sheet sizes

*For panel specifications, please refer to the B/E-TEKLAM aeroPANEL families.

ApplicationsThe aeroADDTM family is designed to meet a broad range of customer’s specific drawing requirements

PerformanceUpon selection of desired combination, B/E-TEKLAM can provide the resulting mechanical properties.

ABOVE AND BEYOND

aeroADDTM



PHONE: +1.951.278.4563



For Additional Product Information, Please Contact:

Teklam Sales DepartmentTeklam SalesB/E Aerospace | Teklam

350 W. Rincon Street | Corona, CA 92880 USAOffice +1.951.278.4563 | Fax [email protected]

Jiyoon BackManager, Sales & MarketingB/E Aerospace | Teklam

350 W. Rincon Street | Corona, CA 92880 USAOffice +1.951.356.8413 | Mobile [email protected]

Cindy MaysDirector, Technical SalesB/E Aerospace | Teklam

350 W. Rincon Street | Corona, CA 92880 USAOffice +1.951.356.8426 | Mobile [email protected]

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BACK COVER COVER - Rockwell Collinsbeaerospace.com/wp-content/uploads/2016/01/BE-Teklam_Product... · is an industry leader in the design and manufacture of advanced laminated honeycomb