曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
SERIAL NUMBER IS IN
ACCORDANCE WITH SERIAL
NUMBERS DESCRIBED IN
CHAPTERS 05-20-01,
05-20-04,05-20-05 OR
05-20-06, PERFORM A
THOROUGH EXAMINATION OF
THE SPAR FLANGE / SKINS
JUNCTION.
IF CORROSION IS DETECTED
ON THE SPAR FLANGES OR
WEB, CORROSION AT
SPAR / SKINS INTERFACE IS
HEAVILY SUSPECTED.
CORROSION
YES
I END OF EXAMINATION I
ASSESSMENT OF
THE DAMAGE
RECORDING OF THE
DEFECTS (POSITION AND
DIMENSIONS)
REPA R PER
MANUFACTURER'S
SOLUTION OR BY STATION
APPROVED FOR THIS TYPE
OF REPAIR
Corrosion inspection (box interior) - Visual examination
Figure 601
AAAA
Validity : S / N 1 - 9999 57-00-00Page 608
(EA) JUN 02
Corrosion inspection (spar / skins interfaces) - Thorough examination
Figure 602 (1/2)
AAAA
Validity : S / N 1 - 9999 57 00-00Page 609
(EA) JUN 02
CORROSION
YES
IF DEFECT DEPTH s 0.0118 IN
(0.3 MM) CONTAINED WITHIN A
MAXIMUM DIAMETER OF
2,36 IN (60 MM)
REPAIR PER MAINTENANCE
MANUAL, PAGE 801
IF DEFECT DEPTH
> 0,0118 IN (0,3 MM)
REPAIR PER
MANUFACTURER'S SOLUTION
OR BY STATION APPROVED
FOR THIS TYPE OF REPAIR
Corrosion inspection (spar / skins interfaces) - Thorough examination
Figure 602 (2/2)
AAAA
Validity : S / N 1 - 9999
57-00-00 Page 610
57
(EA) JUN 02
1 - Wing upper surface skin
2 - Spar flange
3 - Spar web
4 - Rivet
5 - Wing lower surface skin
6 - Visible corrosion
7 - Underlying corrosion
Corrosion inspection - Type of defect
Figure 604
WA
Validity : S / N 1 - 9999 57 00 00Page 11
(EA) JUN6 02
Corrosion inspection (spar / skins interfaces) - Wing upper surface
Figure 605
N3
1085 mm
3.56 ft 13 - Stiffener
14 - Core sample
N1
660 mm
2.16 ft
13
+ + +
+ + + + + + + -F
+ + + + + + + + + + +
Bord d'attaque 14
Leading edge
Corrosion inspection (spar / skins interfaces) - Wing lower surface
Figure 606
AAAA
Validity : S / N 1 - 9999 57-00-00Page 612
(EA) JUN 02
15 - Ruler
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址：TB20 MAINTENANCE MANUAL 57 机翼 TB20飞机维护手册(15)
| 
