TEKLAM - Providing the Industry with Laminated Solutions FAA APPROVED
P/N AA810-22-750
Product Data Sheet
  • Facings: .012" 7075T6 CLAD ALUMINUM PER QQ-A-250
  • Core: 5052-.0020-1/4-4.3 ALUMINUM HONEYCOMB PER AMS-C-7438
  • PANELS MANUFACTURED PER TEKLAM PROCESS SPECIFICATION TPS-A-A-500, REV. A
PROPERTY
TEST METHOD
UNIT
VALUE

Mean
'B'
Basis
'A'
Basis
Thickness ASTM C366 inch .750
Weight ASTM C29 lbs/sq ft .66
Long Beam Flexural ('L' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs.
AMS-STD-401

in-lbs/in
psi
inch

600
73,545
0.11

536
65,676

491
60,151
Long Beam Flexural ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs.
AMS-STD-401

in-lbs/in
psi
inch

510
62,481
0.12

430
52,576

373
45,621
Short Beam Core Shear ('L' Dir.) AMS-STD-401
psi
344 314
294
Short Beam Core Shear ('W' Dir.) AMS-STD-401
psi
207 202
199
Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 33
Flatwise Compression AMS-STD-401 psi 658 571 511
Insert Pull-Out (Tension)
NAS-1832-3-5 (Blind)
NAS-1834-3-750 (Through)
NAS-1836-3-14 (Blind)
TPS-SF-2000, Type II, Rev. B
lbs
lbs
lbs

897
1,032
685

766
935
547

674
867
451
Insert Shear
NAS-1832-3-5 (Blind)
NAS-1834-3-750 (Through)
NAS-1836-3-14 (Blind)
TPS-SF-2000, Type II, Rev. B
lbs
lbs
lbs

990
1,105
913

872
1,021
753

790
962
640
'A' and 'B' Basis design allowable data FAA-approved
per TEKLAM Test Plan TTP-1004 under FAA Project No. ST7145LA-T 3-22-00
Flammability – 60-Second Vertical FAR 25.853, Part I
Pass
OSU Heat Release FAR 25.853, Part IV
Pass
NBS Smoke Emission
FAR 25.853, Part V
Pass
  • STANDARD PANEL SIZES: 48" X 96", 48" X 144", OTHER SIZES AVAILABLE.
  • STANDARD DIMENSIONAL TOLERANCES: WIDTH AND LENGTH: +/- 1/2"; THICKNESS: +/- 0.010".
  • FLATNESS: MAX. DEVIATION, DELTA, INS.= (LxL) x .004/T, WHERE L=LENGTH IN FT, T=THICKNESS IN INS.
REV. NOV. 2005

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