Gillfab® 1369A

Overview

Gillfab® 1369 series laminates are high strength, low FST grade liners constructed using woven E- and/or S-glass cloth with a modified phenolic resin system and an optional 1 mil Polyvinyl Fluoride (PVF) film overlay on the face side for surface reflectivity and uniform appearance.

Applications

Cargo liners for cargo compartment, bulkhead facings and blowout panels for aircraft. Also used as backing material for non-textile floor mats used in wet areas of cabin interior (without PVF film overlay).

Features

  • High impact strength
  • Fire resistant
  • Corrosion resistant
  • Low moisture absorption
  • Low smoke and toxicity generation
  • Service temperature -40°F to 220°F (-40°C to 110°C)

Availability

Gillfab® 1369A
1-Sided PVF Film
Thickness inch (mm)0.013 (0.330)
0.020 (0.508)
0.025 (0.635)
0.030 (0.762)
0.040 (1.016)
0.045 (1.143)
0.060 (1.524)
LengthStandard 144 inch (3,658 mm)
Maximum 168 inch (4,267 mm)
WidthStandard 48 inch (1,219 mm)
Maximum 72 inch (1,829 mm)
SidesGillfab® 1369AAvailable Upon Request
ColorFace Side1 mil White PVF FilmGranite Grey
Misty Beige
ColorBack SideAmberAmber

Construction

Reinforcement: Woven fiberglass cloth

Resin System: Phenolic

Surface Finish: 1 mil white PVF film overlay for standard applications

Specifications

Gillfab® 1369A

  • Airbus AI 2550M1M000800 Types 13, 25, 40, 45, and 60
  • Airbus ABS 5777, AIMS05-11-001 Types 20, 40, 45, and 60, and AIMS05-11-004 Type 20
  • FAR 25.853 and 25.855 Appendix F Parts I, III, IV and V

Alternative Gillfab® 1369 Products

Gillfab® 1369 series are high strength, high impact and fire resistant fiberglass reinforced phenolic laminates for aircraft cargo liner applications.

TGC Product No.Difference
Gillfab® 1368AHigh strength, high impact, low FST, fiberglass reinforced phenolic laminate for aircraft cargo liner applications.
Gillfab® 1368BThinner and lighter than 1368A.
Gillfab® 1368E1368A with 1mil white PVF film bonded to both faces of the laminate.
Gillfab® 1368GExtremely thin, lightweight and superior impact strength to corresponding types.

Performance Properties, Typical

The following tests are run in accordance with BMS 8-223 specification requirements.

TGC Part Number1369A0131369A0201369A0251369A0301369A0401369A0451369A060
Thickness, inch (mm)0.013 (0.33)0.020 (0.51)0.025 (0.64)0.030 (0.76)0.040 (1.02)0.045 (1.14)0.060 (1.52)
Weight, psf (kg/m²) 0.12 (0.60)0.20 (0.98)0.24 (1.17)0.29 (1.42)0.38 (1.85)0.44 (2.15)0.57 (2.77)
Impact Strength¹, ft·lbf (N·m)9 (12)11 (15)11 (15)12 (16)18 (24)20 (27)23 (31)
Edge Bearing², kpsi (MPa)WarpN/A43 (300)
FillN/A38 (260)
Flexural Strength³, kpsi (MPa)WarpN/AN/AN/A40 (278)
FillN/AN/AN/A34 (234)
Flexural Modulus³, Mpsi (GPa)WarpN/AN/AN/A2.5 (17)
FillN/AN/AN/A2.2 (15)
Tensile Strength⁴, kpsi (MPa)Warp55 (380)
Fill50 (345)
Tensile Modulus⁴, Mpsi (GPa)Warp3.3 (23)
Fill3.0 (21)
Water Absorption⁵, %<1.0
FlammabilityMeets requirements of FAR 25.853 & 855 Appendix F Part I & III

Figures shown reflect typical values and should not be used as design specifications.
¹ – Calculated per ASTM D5420 using a modified dart and specimen test frame.
² – Tested per ASTM D953 using a modified test fixture.
³ – Tested per ISO 178.
⁴ – Tested per ISO 527-4
⁵ – Tested per ISO 62 Method 1.

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