Location of the Antennas, Probes and Sensors and Exterior Lights Figure 602/TASK 05-51-18-991-002- 12 (SHEET 1)
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 05-51-18Page 612 1 1 May 01/05 1 1 1CES 1
Location of the Antennas, Probes and Sensors and Exterior Lights Figure 602/TASK 05-51-18-991-002- 22 (SHEET 2)
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 05-51-18Page 613 1 1 May 01/05 1 1 1CES 1
Location of the Antennas, Probes and Sensors and Exterior Lights
Figure 602A/TASK 05-51-18-991-002-A12 (SHEET 1)
R 1EFF : 151-199, 401-499, 1 05-51-18Page 614 1 1 Aug 01/05 1 1 1CES 1
Location of the Antennas, Probes and Sensors and Exterior Lights
Figure 602A/TASK 05-51-18-991-002-A22 (SHEET 2)
R 1EFF : 151-199, 401-499, 1 05-51-18Page 615 1 1 Aug 01/05 1 1 1CES 1R Location of the Antennas, Probes and Sensors and Exterior Lights R Figure 602B/TASK 05-51-18-991-002-B12 (SHEET 1)
R 1EFF : 301-399, 1 05-51-18Page 616 1 1 May 01/04 1 1 1CES 1R Location of the Antennas, Probes and Sensors and Exterior Lights R Figure 602B/TASK 05-51-18-991-002-B22 (SHEET 2)
R 1EFF : 301-399, 1 05-51-18Page 617 1 1 May 01/04 1 1 1CES 1
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
| |CODE| | 1 | 2 | 3 |SIGN|FIG.|
|----|----|---------------------------------------|-----|-----|-----|----|----|
| A.| | Examine the nose landing gear and the | X | | | | |
| | | main landing gear: | | | | | |
| | | (1) Examine the LG structure and the | | | | | |
| | | points where it is attached for | | | | | |
| | | change of color, burn marks and | | | | | |
| | | other damage. | | | | | |
| | | (2) Examine the shock absorber for | | | | | |
| | | change of color and burn marks. | | | | | |
| | | (3) Examine all the components | | | | | |
| | | attached to the landing gear and | | | | | |
| | | fully examine the electrical looms| | | | | |
| | | and components for a change of | | | | | |
| | | color and burn marks. | | | | | |
| | | | | | | | |
|5. | | Inspection of the Belly Fairing | | | | | |
| | | | | | | | |
| A.| | Examine the belly fairing panels | X | | | | |
| | | (including the wing-to-fuselage | | | | | |
| | | fairings) for change of color, burn | | | | | |
| | | marks, puncturing and delamination. | | | | | |
| | | Examine fairing screws and fasteners | X | | | | |
| | | for burn marks. | | | | | |
| | | | | | | | |
|6. | | Inspection of the Fuselage | | | | | |
| | | | | | | | |
R | A.| | Examine externally all of the fuselage| X | | | | |
R | | | skin with rivets and screws for | | | | | |
| | | change of color, burns marks and | | | | | |
| | | small holes. | | | | | |
| | | | | | | | |
| B.| | Examine all the probes, sensors and | X | | | | |
| | | drain masts and the adjacent area for | | | | | |
| | | burn marks and change of color. | | | | | |
| | | | | | | | |
| C.| | Examine carefully all the | X | | | | |
| | | communication and navigation antennas | | | | | |
| | | and the adjacent area for burn marks, | | | | | |
| | | change of color, puncturing and | | | | | |
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