TEKLAM - Providing the Industry with Laminated Solutions FAA APPROVED
P/N AA209-33-500 (A505)
Product Data Sheet
  • FACINGS: .020" 2024T3 CLAD ALUMINUM PER QQ-A-250
  • CORE: 5052-.0015-1/4-3.4 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 .500
Weight ASTM C29 lbs/sq ft .78
Long Beam Flexural ('L' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs.
AMS-STD-401

in-lbs/in
psi
inch

547
56,706
0.14

523
54,287

506
52,589
Long Beam Flexural ('W' Direction)
Bending Moment
Facing Stress
Deflection @ 100 lbs.
AMS-STD-401

in-lbs/in
psi
inch

503
52,425
0.15

492
51,212

484
50,360
Short Beam Core Shear ('L' Dir.) AMS-STD-401
psi
302 266
242
Short Beam Core Shear ('W' Dir.) AMS-STD-401
psi
169 163
160
Climbing Drum Peel ASTM D1781-76 in-lbs/3² width 52
Flatwise Compression AMS-STD-401 psi 405 313 248
Insert Pull-Out (Tension)
NAS-1832-3-3 (Blind)
NAS-1834-3-500 (Through)
NAS-1836-3-12 (Blind)
TPS-SF-2000, Type II, Rev. B
lbs
lbs
lbs

610
825
609

526
719
507

468
645
436
Insert Shear
NAS-1832-3-3 (Blind)
NAS-1834-3-500 (Through)
NAS-1836-3-12 (Blind)
TPS-SF-2000, Type II, Rev. B
lbs
lbs
lbs

1,278
1,550
1,080

1,113
1,324
928

999
1,166
821
'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.