曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

core (8.0 pcf vs. 6.0 pcf)
Containerized Gillfab 4322* Gillfab 4522 Heavier density Nomex honeycomb
Cargo Flooring 5360 M1M 000100, Issue 6, 7 5360 M1M 000500, Issue 5 core (8.0 pcf vs. 6.0 pcf)
(CCC1)
Bulk Cargo Flooring Gillfab 4323 Gillfab 4223 Thicker top facing (0.045" vs. 0.030")
5360 M1M 000100, Issue 6, 7 5360 M1M 000500, Issue 3
(BCC2) Heavier density Nomex honeycomb core
(9.0 pcf vs. 6.0 pcf)
Main Deck Cargo Not applicable Gillfab 4123 Not applicable - new panel designation
Flooring - Freighter 5360 M1M 000500, Issue 5
Combi/Convertible (MDC2)
Airbus A300/A310/A300-600 Aircraft
TABLE 1
COMPARISON OF FLOOR PANEL CONSTRUCTIONS – ORIGINAL VS. NEW GENERATION
* Applicable to A319/A320/A321 aircraft only
Note: Airbus operators should consult the relevant Airbus Industrie Structural Repair Manual (SRM) to determine specific part installation.
FOR ADDED SSTRENGTH
Airbus A319/A320/A321/A330/A340 Aircraft
6
Based on a panel 0.374" thick with 0.030"/0.020" phenolic
facings and a 9 pcf 0.324" thick core.
Specification: AI 5360 M1M 000500, Issue 5 (MDC2)
Meets smoke and toxicity requirement of ABD 0031 1Chapter numbers in “Test Method” column refer to section in AIrbus specification. 2Chapter 5.5 and 5.4 relate to 4405 Ty 1 and Ty 2
Based on a panel 0.496" thick with 0.045"/0.020" phenolic
facings and a 9 pcf 0.431" thick core.
Specification: AI 5360 M1M 000500, Issue 3 (BCC2)
Weight, psf (kg/m2) ASTM C 29 0.789 (3.81) 0.973 (4.75)
In-plane Shear, lbs/in (N/mm) Chapter 9.21 782 (137) N/R
Long Beam Flexural Strength, lbs (N) ASTM C 393
Ultimate Load
Ribbon (L) Direction
Room Temperature 504 (2242) 788 (3505)
Humidity Aged, Tested at 40°C 493 (2193) N/R
Transverse (W) Direction N/R
Room Temperature 466 (2072)
Humidity Aged, Tested at 40°C 475 (2112)
Long Beam Deflection ASTM C 393
@ 445N (100 lbs), in (mm)
Ribbon (L) Direction
Room Temperature 0.545 (13.84) 0.277 (7.04)
Humidity Aged, Tested at 40°C 0.527 (13.29) N/R
Transverse (W) Direction N/R
Room Temperature 0.543 (13.79)
Humidity Aged, Tested at 40°C 0.519 (13.18)
Hard Point Shear Chapter 5.52/9.83 N/R N/R
Ultimate Load, lbs (N)
Room Temperature
Humidity Aged, Tested at 40°C
Panel Shear ASTM C 393 N/R
Ultimate Load, lbs (N)
Room Temperature 964 (4288)
Humidity Aged, Tested at 40°C 917 (4079)
Food Cart Roller, cycles Chapter 9.5 N/R
125.7 lbs/wheel (57 KG) Pass (No Damage)
165.3 lbs/wheel (75 KG) Pass (No Damage)
88 lbs/wheel (40 KG) N/R
Bending Under Static Load Chapter 9.6 N/R
F (Limit Corrected), lbs (N) 1512 (6727)
F (Ultimate Corrected), lbs (N) 6230 (27713)
Deflection @ F (Limit Corrected), in (mm) 0.657 (16.69)
Insert Shear Chapter 9.7 N/R
Ultimate Load, lbs (N)
Room Temperature 1921 (8546)
Humidity Aged, Tested at 40°C 1762 (7842)
Impact Strength, ft-lbs, (N-m) Chapter 9.84/ 9.95 ATSM D 3029 8.45 (11.46) 11.0 (15)
Indentation, lbs (N) Chapter 9.96/ 5.42/9.107 450 (2002) N/R
C.D. Peel, lbs (N) ASTM D 1781 N/R
Room Temperature 66.5 (295.8)
Humidity Aged, Tested at 40°C 64.6 (287.4)
Stabilized Core Compression psi(N/mm2) ASTM C 365 2234 (15.4) N/R
Flammability ABD 0031 N/R
60 Second Vertical AITM 2.0002A
Extinguishing Time, sec 1.8
Burn Length, in (mm) 0.5 (12.7)
Drip Extinguishing Time, sec 0.0
12 Second Vertical AITM 2.0002B
Extinguishing Time, sec 0.0
Burn Length, in (mm) 0.2 (5.1)
Drip Extinguishing Time, sec 0.0
30 Second 45 Degree AITM 2.0004
Extinguishing Time, sec 0.5
Afterglow, sec 0.0
Flame Penetration None
Flame Penetration Resistance FAR 25.855, App. F,
Flame Penetration Part III, Amend. 25-60 None
Temperature Rise, °F 150
Property Test Method Gillfab 4123 Gillfab 4223
TABLE 2 – TYPICAL AVERAGE
3Chapter 9.8 relates to 4505 4Chapter 9.8 relates to 4123 5Chapter 9.9 relates to 4505 6Chapter 9.9 relates to 4123 7Chapter 9.10 relates to 4505 and 4605 N/R means Not Required 7
Based on a panel 0.374" thick with 0.030"/0.024"
phenolic facings and a 8 pcf 0.320" thick core
Specification: AI TL53/5000/79, Issue 8, Annex A, Types 1 and 2 (PC3)
Based on a panel 0.374" thick with 0.020"/0.020" phenolic
facings and a 9 pcf 0.334" thick core.
Specification: AI 5360 M1M 000600, Issue 3 (PC3)
Based on a panel 0.374" thick with 0.020"/0.015" phenolic
facings and a 8 pcf 0.339" thick core.
Specification: AI 5360 M1M 000500, Issue 5 (CC1)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：航空資料2(47)