CHAPTER 57
__________
WINGS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Sub-spars and Ribs 1 ALL Skins 4 ALL Access Panels 4 ALL
LEADING EDGE 57-41-00
INSPECTION/CHECK 601 ALL
Inspection of the Wing Leading 601 ALL
Edge
Detailed Visual Inspection of Slat 607 ALL
1, Tracks 1-4: Visible Part of
Roller Contact Area
Detailed Visual Inspection of the 612 ALL
Outer Wing Bottom Skin Lower
Surface at Drain Holes for Track
Cans 1, 2, 3 and 4 (Rib-bays 1-2,
2-3, 4-5 and 5-6)....
Detailed Visual Inspection of the 619 001-049, 051-099
Outer Wing Bottom Skin Lower 101-149, 151-199
Surface at Fuel Tank Water Drain 201-299, 401-499
Holes between RIBS 15-16 and 22-23
Detailed Visual Inspection of the 623 301-399,
Outer Wing Bottom Skin Lower
Surface at Fuel Tank Water Drain
Holes between RIB 22-23 and
Magnetic Level Indicator Position
Detailed Visual Inspection of Slat 629 ALL
2, Tracks 5 and 6: Visible Part of
Roller Contact Area
Detailed Visual Inspection of Slat 633 ALL
3, Tracks 7 and 8: Visible Part of
Roller Contact Area
Detailed Visual Inspection of Slat 637 ALL
4, Tracks 9 and 10: Visible Part
of Roller Contact Area
Detailed Visual Inspection of Slat 641 ALL
5, Tracks 11 and 12: Visible Part
of Roller Contact Area
Detailed Inspection of Outer Wing, 645 ALL
Fixed Leading Edge, Roller Pin
Holes and other Cutouts in Track
Rib 1 to 12
Special Detailed Inspection of the 651 ALL
Outer Wing Fixed Leading Edge
Forward Upper Roller Pin Holes in
Track Ribs 5, 6, 7, 8, 9, 10, 11
57-CONTENTS Page 17 Aug 01/05 R CES
CHAPTER 57
__________
WINGS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ and 12 Detailed Inspection of Outer Wing, 657 ALL Fixed Leading Edge, Bottom Attachment Joint on Track Rib 1 to 12 Detailed Visual Inspection of the 662 ALL Outer Wing Fixed Leading Edge Bottom Wing Skin Upper and Lower Surfaces Forward of Front Spar from RIB1 to RIB27 .... Detailed Visual Inspection of 668 ALL Outer Wing Fixed Leading Edge Top Wing Skin Upper and Lower Surfaces Forward of Front Spar from RIB1 to 27 Special Detailed Inspection of 673 ALL Outer Wing, Fixed Leading Edge Pinion Fitting Bolting and Actuator Bolting Lower Bolt Holes on Ribs 2, 3, 5, 6, 7, 8....
MOUNTINGS - SUPPORTS 57-41-33
REMOVAL/INSTALLATION 401 ALL Removal of the Slat-Track 401 ALL Vertical-Load Rollers Installation of the Slat-Track 407 ALL Vertical-Load Rollers
ACCESS PANELS AND COVERS 57-41-37
REMOVAL/INSTALLATION 401 ALL Removal of the Pressure-Relief 401 ALL Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Installation of the 404 ALL Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Removal of the Access Panel 412 ALL 522AT(622AT) Installation of the Access Panel 418 ALL 522AT(622AT) Removal of the NACA Duct Panel 424 ALL 521BB(621BB) Installation of the NACA Duct 428 ALL Panel 521BB(621BB) Removal of the Access Panels 431 ALL
57-CONTENTS Page 18 Aug 01/05 R CES
CHAPTER 57
__________
WINGS
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB) Installation of the Access Panels 440 ALL 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB) Removal of the Access Panel 451 ALL 522WB(622WB) Installation of the Access Panel 454 ALL 522WB(622WB) Removal of the Access Panel 457 ALL 521BT(621BT) Installation of the Access Panel 460 ALL 521BT(621BT)
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼1(29)
