FAA Approved
Fibrelam® Honeycomb Sandwich Panels
P/N BMS 4-17 Ty II
Hexcel Logo


Part Information
Hexcel P/N

Click for Data Sheet
Core Material
per AMS-C-7438
Top/Bottom Skin Alum per QQ-A-250
Part Thickness (inch)
Weight (lbs/sf)
BMS 4-17 Ty II
HexWeb Medium Density
0.015/0.015 (0.381/0.381)
0.400
0.63


Click Here for full Product Data Sheet

Inventory Information
Part Number Quantity on Hand Pricing Information
BMS 4-17 Ty II 0 Call for Pricing.
817-453-1900

 


FAA-APPROVED ALLOWABLE COMPOSITE PANELS
TEKLAM offers a large selection of panels with
FAA-approved 'A' and 'B' basis design allowables.

TEKLAM P/N



Click for Data Sheet

Core Material

Top/Bottom Skin
7781 Fiberglass

Part Thickness (inch)

Weight (lbs/sf)

NE1G102125

3.0
NOMEX®

H/C

1-Ply Epoxy

.125

.27

NE2G102125

3.0
NOMEX®

H/C

2-Ply Epoxy

.125

.50

NE1G102250

3.0
NOMEX®

H/C

1-Ply Epoxy

.250

.29

NE2G102250

3.0
NOMEX®

H/C

2-Ply Epoxy

.250

.52

NE1G102375

3.0
NOMEX®

H/C

1-Ply Epoxy

.375

.32

NE2G102375

3.0
NOMEX®

H/C

2-Ply Epoxy

.375

.56

NE1G102500

3.0
NOMEX®

H/C

1-Ply Epoxy

.500

.35

NE2G102500

3.0
NOMEX®

H/C

2-Ply Epoxy

.500

.57

NE1G102750

3.0
NOMEX®

H/C

1-Ply Epoxy

.750

.41

NE2G102750

3.0
NOMEX®

H/C

2-Ply Epoxy

.750

.64

NE1G1021000

3.0
NOMEX®

H/C

1-Ply Epoxy

1.000

.48

NE2G1021000

3.0
NOMEX®

H/C

2-Ply Epoxy

1.000

.70

NP2G102250

3.0
NOMEX®

H/C

2-Ply Phenolic

.250

.52

NP2G102375

3.0
NOMEX®

H/C

2-Ply Phenolic

.375

.54

NP2G102500

3.0
NOMEX®

H/C

2-Ply Phenolic

.500

.57

NP2G102750

3.0
NOMEX®

H/C

2-Ply Phenolic

.750

.64

NP2G1021000

3.0
NOMEX®

H/C

2-Ply Phenolic

1.000

.70

Teklam


FAA-APPROVED HONEYCOMB SANDWICH PANELS

TEKLAM offers a large selection of panels which have
previously received FAA-approval for 'A' and 'B' design allowables.


 



hexcel

HEXCEL FIBRELAM HONEYCOMB SANDWICH FLOOR PANEL

Meets FAR 25.853 & 855 Appendix F Part I

BMS 4-17 Ty II Image

Teklam
FAA-APPROVED ALLOWABLE ALUMINUM PANELS
TEKLAM offers a large selection of panels with
FAA-approved 'A' and 'B' basis design allowables.

TEKLAM P/N

Click for Data Sheet and Inventory Status
Core Material
per AMS-C-7438
Top/Bottom Skin Alum per QQ-A-250
Part Thickness (inch)
Weight (lbs/sf)
AA209-33-250
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.250
.68
AA209-33-375
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.375
.73
AA209-33-500
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.500
.78
AA209-33-750
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.750
.87
AA209-33-1000
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
1.000
.93
AA207-33-250
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.250
.75
AA207-33-375
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.375
.80
AA207-33-500
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.500
.85
AA207-33-750
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.750
.96
AA207-33-1000
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
1.000
1.06
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