BACK COVER
COVER
B/E-TEKLAM
High Performance
Composite Panels
350 W. Rincon Street
Corona, A 92880
+1.951.278.4563
Sales@Teklam.com
beaerospace.com
POCKET
ABOUT US
Established 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.
PRODUCTS & CAPABILITIES
PRODUCT DEVELOPMENT AND APPLICATION ENGINEERING SERVICES
From 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 SHAPES
B/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 PANELS
Many 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 SERVICES
B/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
Applications
B/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
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
aeroFIBER
TM
THE BASICS DONE
RIGHT
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
Performance
Options
• 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)
• Phenolic Resin
• 1-Ply Fiberglass
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
• Epoxy Resin
• 2-Ply Fiberglass
Applications
The aeroFIBERTM family is primarily designed for aircraft
interiors including:
• Monuments
• Partitions & bulkheads
• Overhead bins & ceilings
STANDARD PANELS
Epoxy Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel
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
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
L
W
L
W
L
W
FAA
Allowables
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
Phenolic Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel
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
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”)
PHENOLIC FIBERGLASS SKIN / NOMEX® CORE - AIRCRAFT COMPOSITE PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
Epoxy Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel
Flammability
FAR 25.853 Appendix F: Part I - 60 second vertical;
Skins
0.020” 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
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
Phenolic Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel
Flammability
FAR 25.853 Appendix F: Part I - 60 second vertical; Part IV OSU Heat Release; Part V - NBS Smoke Emission
Skins
0.020” Phenolic 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”)
PHENOLIC FIBERGLASS SKIN / NOMEX® CORE - AIRCRAFT COMPOSITE PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
aeroFEATHER
TM
UP TO 38% WEIGHT
REDUCTION
Low Weight, High Strength
Interior Panel
Our 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 upon
request 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
•
•
•
•
•
•
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
Interior monument construction
Interior cabinetry
Galleys and lavatories
Seat surrounds and privacy dividers
Side ledges and side walls
Luggage bins
STANDARD PANELS
Phenolic Fiberglass Skin / NOMEX® Core - Aircraft Composite Panel
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
Skins
0.010” Phenolic 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”)
PHENOLIC FIBERGLASS SKIN / NOMEX® CORE - AIRCRAFT COMPOSITE PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
L
W
L
W
L
W
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
aeroREADY
TM
ALL YOU NEED IS
PAINT
High Surface Finish Interior Panel
B/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 upon
request through the aeroADDTM family)
• Capability to produce panels at a thickness tolerance of
± 0.010”
• Elimination of labor and material costs associated
with fill and fair operations, peel plies, and
surfacing films
• Reduced weight through the elimination of surface
preparation 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 surface
inconsistency may be visible
Performance
• Mechanical, physical, and flammability performance
of the panel is not affected
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
aeroBASE
TM
STRONG, DURABLE
FLOORS
High Strength and Stiffness Multiuse Floor Panel
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
Performance
Applications
B/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
• Aisles
• Entrances/Exits
• Cargo Bays
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
• Under seats
• Galleys
STANDARD PANELS
Epoxy Composite Skin / See List - Aircraft Flooring Panel
Flammability
FAR 25.853 Appendix F: Part I - 60 second vertical;
Part I - 45 Degree;
Skins
See List
Core
See List
Standard Dimensional Length & Width: ±0.500”
Tolerances
Thickness: ±0.010”
Thickness
0.400
EPOXY COMPOSITE SKIN - AIRCRAFT FLOORING PANEL
Panel Part #
Core Description
Skin Upper 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
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
Skin Lower Spec
0.022” Epoxy Composite
EPOXY COMPOSITE SKIN - AIRCRAFT FLOORING PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam
Core Shear
[Mean]
Climbing
Drum Peel
[Mean]
Stabilized
Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
NE2G3-05-400 (N404)
0.400
0.64
286
N/A
37884
N/A
N/A
306
20
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
No
Yes
aeroMETAL
TM
A QUALITY CLASSIC
IN AEROSPACE
B/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
Performance
Applications
• Service temperature: -67°F (-55°C) to 180°F (82°C)
• Superior Elasticity
• Combination of consistency to cost effectiveness
The aeroMETALTM family is mainly designed for aircraft
interiors such as:
• Monuments and Shelving
• Partitions & bulkheads
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
STANDARD PANELS
2024-T3 CLAD Skin / 5052 Alum. Core - Aircraft Aluminum Panel
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
Standard Dimensional Length & Width: ±0.500”
Tolerances
Thickness: ±0.010”
Panel Dimension
48” x 96” (up to 60” x 144”)
2024-T3 CLAD SKIN / 5052 ALUM. CORE - AIRCRAFT ALUMINUM PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
2024-T3 CLAD Skin / 5052 Alum. Core - Aircraft Aluminum Panel
Flammability
FAR 25.853 Appendix F: Part I - 60 second vertical; Part IV OSU Heat Release; Part V - NBS Smoke Emission
Skins
0.032” 2024-T3 CLAD
Core
5052 Alum. 3/16” Cell, 5.7 lbs/ft3
Standard Dimensional Length & Width: ±0.500”
Tolerances
Thickness: ±0.010”
Panel Dimension
48” x 96” (up to 60” x 144”)
2024-T3 CLAD SKIN / 5052 ALUM. CORE - AIRCRAFT ALUMINUM PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
2024-T3 CLAD Skin / 5052 Alum. Core - Aircraft Aluminum Panel
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. 1/4” Cell, 3.4 lbs/ft3
Standard Dimensional Length & Width: ±0.500”
Tolerances
Thickness: ±0.010”
Panel Dimension
48” x 96” (up to 60” x 144”)
2024-T3 CLAD SKIN / 5052 ALUM. CORE - AIRCRAFT ALUMINUM PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
FAA
Allowables
AA209-33-125
0.125
0.69
120
116
57000
55000
235
150
12
320
AA209-33-250
0.250
0.72
263
253
57000
55000
235
150
12
320
No
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
7075-T6 CLAD Skin / 5052 Alum. Core - Aircraft Aluminum Panel
Flammability
FAR 25.853 Appendix F: Part I - 60 second vertical; Part IV OSU Heat Release; Part V - NBS Smoke Emission
Skins
0.010” 7075-T6 CLAD
Core
5052 Alum. 3/16” Cell, 3.1 lbs/ft3
Standard Dimensional Length & Width: ±0.500”
Tolerances
Thickness: ±0.010”
Panel Dimension
48” x 96” (up to 60” x 144”)
7075-T6 CLAD SKIN / 5052 ALUM. CORE - AIRCRAFT ALUMINUM PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
7075-T6 CLAD Skin / 5052 Alum. Core - Aircraft Aluminum Panel
Flammability
FAR 25.853 Appendix F: Part I - 60 second vertical; Part IV OSU Heat Release; Part V - NBS Smoke Emission
Skins
0.012” 7075-T6 CLAD
Core
5052 Alum. 1/4” Cell, 4.3 lbs/ft3
Standard Dimensional Length & Width: ±0.500”
Tolerances
Thickness: ±0.010”
Panel Dimension
48” x 96” (up to 60” x 144”)
7075-T6 CLAD SKIN / 5052 ALUM. CORE - AIRCRAFT ALUMINUM PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
W
L
W
L
W
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
comMETAL
TM
A QUALITY CLASSIC
IN COMMERCIAL
APPLICATIONS
TM
comMETAL consists of a wide range of
commercial grade Aluminum Sandwich
panels of the highest quality and
TM
durability. The comMETAL 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
Applications
The 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
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
STANDARD PANELS
Aluminum Skin / Aluminum Core - Commercial Panel
Flammability
N/A
Skins
0.025” 5052-H32 Gold Seal
Core
3003 Alum. 3/8” Cell, 3.6 lbs/ft³
Standard Dimensional Length & Width: ±0.500”
Tolerances
Thickness: ±0.020”
Panel Dimension
48” x 96” (up to 48” x 144”)
ALUMINUM SKIN / ALUMINUM CORE - COMMERCIAL PANEL
Panel Part #
Panel
Thickness
Panel
Weight
in
lbs/sf
Long Beam
Flexural Bending
Moment [Mean]
Long Beam
Flexural Facing
Stress [Mean]
in-lbs/in
L
W
Short Beam Core
Shear [Mean]
Climbing Drum
Peel [Mean]
Stabilized Core
Compression
[Mean]
psi
in-lbs/in
psi
psi
L
W
L
FAA
Allowables
W
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
aeroINFINITE
TM
INFINITE POSSIBILITIES,
ONE SUPPLIER
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
•
•
•
•
•
•
•
•
•
Options*
Applications
The aeroINFINITETM family can be used in:
• Interiors
• Structural applications
• Cargo applications
Performance
Upon selection of desired combination, B/E-TEKLAM can
provide the resulting mechanical properties.
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
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.
PHONE: +1.951.278.4563
Resin Options:
• Phenolic • Epoxy
Core Options:
• Nomex® • Aluminum
Skin Options:
• Aluminum • Carbon
• Kevlar®
• Fiberglass
*Typical options shown, possibilities are infinite.
aeroADD
TM
ABOVE AND
BEYOND
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.
Applications
The aeroADDTM family is designed to meet a broad range
of customer’s specific drawing requirements
Performance
Upon selection of desired combination, B/E-TEKLAM can
provide the resulting mechanical properties.
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563
For Additional Product Information, Please Contact:
Teklam Sales Department
Teklam Sales
B/E Aerospace | Teklam
350 W. Rincon Street | Corona, CA 92880 USA
Office +1.951.278.4563 | Fax +1.951.278.0389
Sales@Teklam.com
Jiyoon Back
Manager, Sales & Marketing
B/E Aerospace | Teklam
350 W. Rincon Street | Corona, CA 92880 USA
Office +1.951.356.8413 | Mobile +1.951.317.8646
Jiyoon_Back@beaerospace.com
Cindy Mays
Director, Technical Sales
B/E Aerospace | Teklam
350 W. Rincon Street | Corona, CA 92880 USA
Office +1.951.356.8426 | Mobile +1.626.367.8002
Cindy_Mays@beaerospace.com
beaerospace.com
Passion to Innovate. Power to Deliver.
350 W. RINCON STREET
CORONA, CA 92880 USA
Sales@Teklam.com
beaerospace.com
PHONE: +1.951.278.4563