Gillfab® 4422

Gillfab® 4422 image

Overview

Gillfab® 4422 is a light weight and low smoke cargo liner panel made from woven fiberglass reinforced phenolic facings boned to meta-aramid honeycomb core.

Applications

The panel is designed to use as cargo compartment lining in sidewalls, ceilings, partition walls, and as decompression panels in the lower cargo hold in all Airbus Industrie A300/A310/A300-600, A319/A320/A321, A330/A340 and A318 aircrafts.

Features

  • High impact strength
  • Corrosion resistant
  • Light weight
  • Low smoke generation
  • Good burn through resistance
  • Service temperature: 180°F (82°C)

Availability

4422-2954422-3074422-3154422-3314422-3464422-3664422-3864422-4134422-5084422-5474422-6104422-630
Thickness, inch (mm)0.295 (7.5)0.307 (7.80)0.315 (8.00)0.331 (8.4)0.346 (8.8)0.366 (9.30)0.386 (9.80)0.413 (10.50)0.508 (12.90)0.547 (13.90)0.610 (15.50)0.630 (16.00)
Facing, Face/back, inch (mm)0.013/0.013 (0.330/0.330)0.020/0.020 (0.508/0.508)0.020/0.020 (0.508/0.508)0.020/0.020 (0.508/0.508)0.020/0.020 (0.508/0.508)0.013/0.013 (0.330/0.330)0.020/0.020 (0.508/0.508)0.013/0.013 (0.330/0.330)0.013/0.013 (0.330/0.330)0.020/0.020 (0.508/0.508)0.013/0.013 (0.330/0.330)0.013/0.013 (0.330/0.330)
Length and width, inch (mm)Typical 48 x 144 (1,219 x 3,658)
Maximum 72 x 168 (1,829 x 4,267)

Construction

Adhesive: Modified phenolic

Core: Meta-aramid

Facings Reinforcement: Fiberglass cloth and/or Unidirectional

Facings Resin System: Phenolic

Specifications

  • Airbus Industrie Technical Specification No. 2550 M1M 0008 00
  • FAR Part 25, Appendix F, Parts I and III (burn through)
  • ABD 0031
  • The Gill Corporation Report No. AIM-2001 – Airline Instruction Manual for Cargo Liner Laminates and Panels

Performance Properties, Typical

The following tests are run in accordance with Airbus 2550 M1M 000800 specification requirements.

TGC Part Number4422-2954422-3074422-3154422-3314422-3464422-3664422-3864422-4134422-5084422-5474422-6104422-630
Weight, psf (kg/m2)0.452 (2.207)0.577 (2.817)0.580 (2.832)0.549 (2.682)0.548 (2.677)0.478 (2.334)0.606 (2.96)0.495 (2.417)0.530 (2.58)0.717 (3.50)0.568 (2.773)0.575 (2.807)
Long Beam Bending, lbs (N)107 (476)202 (899)193 (860)260 (1,157)250 (1,113)135 (601)269 (1,197)173 (770)182 (810) 337 (1,500)223 (992)235 (1,046)
Drum Peel, Face/Back,in-lbs/3″ width (N/76mm width)23/23 (204/204)23/23 (204/204)23/23 (204/204)48/48 (214/214)50/50 (223/223)23/23 (204/204)23/23 (204/204)23/23 (204/204)23/23 (204/204)23/23 (204/204)23/23 (204/204)23/23 (204/204)
Stabilized Core Compression, psi (N/cm2)601 (414)575 (396)592 (408)577 (398)537 (370)597 (411)596 (411)581 (401)594 (410)577 (398)577 (398)554 (382)
Impact Strength,ft-lbf (Nm)17 (23)17 (23)17 (23)21.83 (29.5)17.34 (23.4)17 (23)17 (23)17 (23)17 (23)26 (35)17 (23)17 (23)
Warpage, in/ft (mm/m)<0.036 (3.0)
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.

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