曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

A typical initial (first) panel installation using GORE™ SKYFLEX®
sealant takes up to 65 minutes for the first installation with no cure
time. Subsequent panel removal cycles requires no additional time
when using GORE™ SKYFLEX® sealant; no time is spent scraping
sealant, reapplying sealant, or waiting for the sealant to cure. The
typical time estimate is derived using the following:
• Scraping off and cleaning old sealant=45 minutes
• Installing GORE™ SKYFLEX® sealant=20 minutes
1st 2nd 3rd 4th 5th
600
500
400
300
200
100
0
Minutes
life cyle time savings
The sealant application per panel chart shows the cumulative time required to replace sealant for multiple panel removals.
By the fifth time the panel is removed and replaces using traditional sealants, the cumulative time required for this activity
is 600 minutes while the cumulative time for GORE™ SKYFLEX® Sealant is 65 minutes.
Panel Removals
Polysulfide
SKYFLEX Sealant
installation time analysis
gore™
traditional skyflex®
sealant sealant
Scraping off and
cleaning old sealant 45 min. 45 min.
Masking panel and 30 min. 0 min.
mixing polysulfide
sealant
Applying sealant 15 min. 20 min.
Cleanup 15 min. 0 min.
Cure time 6-48 hours 0 min.
4
aircraft technical order
Joint Services Tech. Manual NAVAIR 01-1A-509
T.O. 1-1-691
TM 1-1500-344-23
A-10 Thunderbolt 1A-10A-2-51JG-1
1A-10A-2-51MS-1
B-1B Lancer 1B-1B-23
B-52 Stratofortress 1B-52H-3
C-5 Galaxy 1C-5A-23
1C-5A-3
C-17 Globemaster III OEM Installation at factory
1C-17A-23
C-130 Hercules 1C-130A-23
1C-130B-2-2
1C-130H-2-2
1C-130(H)H-2-1
1C-130H-2-56JG-00-1
C-141 Starlifter 1C-141B-23
EA-6B Prowler 01-85ADC-3-3
ES-3A 01-S3AAA-3-4
E-2 Hawkeye 01-E2AAA-3-1.1
E-3 Sentry 1E-3A-2-28-1
NN1E3A-3-572
E-6 Tacamo 01-E6AAA-SRM-000
A1-E6AAB-SRM-200
Eurofighter OEM Specification
F-4 Phantom 1F-4-3-1-6
F-5 Tiger 1F-5E-3
F-15 Eagle 1F-15A-23
1F-15A/C/E-3-5
F-16 Falcon In process of approval by Lockheed Martin
H-53 A1-H53CE-110-000
A1-53AD-110-000
1H-53(M)J-2-1
KC-135 Stratotanker 1C-135(K)A-3-1
1C-135(K)A-3-4
PDM Work Specification
P-3 Orion 01-75PAA-2-2.1
S-3 Viking 01-S3AAA-3-4
T-45Goshawk A1-T45AB-SRM-100
V-22 Osprey OEM installation at factory
military technical order approvals
5
Skyflex®
aircraft sealant
aircraft applications service bulletin/manual/specification
Airbus A320 Wing leading edge access panels
Antennas
SB-A320-57-1052
SIL-A320-34-069
Airbus A300 Antennas
Main deck cargo loading system- floor panel sealing
SIL-A300-34-069
DASA specification 2250 MIC 0103 01
Airbus A330 Antennas
Horizontal stabilizer (spar)
Horizontal stabilizer (panels)- 200/300 series
Horizontal stabilizer (panels)- 500/600 series
Floor structure corrosion barrier
Floor structure corrosion barrier
Floor structure corrosion barrier
SIL-A330-34-069
ABS5311, ABS5311-01/ -02 & -03
F559-80032-200 & F551-82609-200
G551-80842-202 & G551-80843-202
ABS5631A25/ EADS number TBA
ABS5631A50/ EADS number 887 282 20
ABS5631A80/ EADS number 887 289 80
Airbus A340 Antennas
Horizontal stabilizer (spars)
Horizontal stabilizer (panels)- 200/300 series
Horizontal stabilizer (panels)- 500/600 series
Floor structure corrosion barrier
Floor structure corrosion barrier
Floor structure corrosion barrier
SIL-A340-34-069
ABS5311-01/ -02 & -03
F559-80032-200 & F551-82609-200
G551-80842-202 & G551-80843-202
ABS5631A25/ EADS number TBA
ABS5631A50/ EADS number 887 282 20
ABS5631A80/ EADS number 887 289 80
Airbus A380 Horizontal stabilizer fuel tank
Boeing 727 Sill plates entry way doors
Cargo floor
FEDEX EO 7-5321-7-3326
FEDEX SR27-51-001
Boeing 737 Passenger floors
Cargo floor
Cabin floor
Cargo tie downs
Engine struts
Landing lights
ECS access
Electrical panel access
Vertical stabilizer
Horizontal stabilizer
Gap cover panel
Reveal strip
737-SL-53-034-E
Production DWG 453A1600
Production DWG 452A1600
Production DWG 453A2600
Production DWG 311A-2539
Production DWG 116A1510
Production DWG 213A2330-1
Production DWG 214A0603
Boeing 747 Passenger floor panels 747-SL-53-090-E
Boeing 757 Passenger floor panels
　
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