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Page 23
Feb 15/03
The beacon can be installed in any position (normal, upside down, right side, left side) with respect with the
G-Switch activation direction stated on figure 4.
The activation / identification assy of the beacon can be installed in four positions. Three alignment pins on
the beacon board allow to set it in the required position. A cap is installed in one of the four holes of the
activation / identification assy who is unused.
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Unstowed objects must be not able to impact the beacon.
Attach the beacon to the fuselage of the aircraft by means of four M4 bolts. Four 5 mm diameter holes at the
corners of a 210 mm x 45 mm rectangle are drilled in the beacon. Particular care must be taken with this
attachment. Standard industry means must be used to lock the screws. Use flat washer in order to avoid
paint damage.
The attachment points are similar to those of the ADT 406 AF/AP beacon.
Содержание ADT 406 AF
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Страница 16: ...86 5 6 1 22 Page 15 Apr 17 03 ELT ADT 406 AP Overall Dimensions Without optional protecting cover Figure 3...
Страница 36: ...Appendix A page 1 Feb 15 03 COSPAS SARSAT TYPE APPROVAL CERTIFICATE...
Страница 37: ...Appendix A page 2 Feb 15 03 JTSO 2C91a AND JTSO 2C126 APPROVAL...
Страница 38: ...Appendix A page 3 Feb 15 03 TSO C91a AND TSO C126 APPROVAL...
Страница 39: ...Appendix A page 4 Feb 15 03...
Страница 40: ...Appendix A page 5 Feb 15 03 Crash Sensor Response Curve...
Страница 41: ...2 22 Appendix B page 1 Feb 15 03 FACTORY SETTING NEXT BATTERY SERVICING MM YYYY...
Страница 42: ...2 22 Appendix B page 2 Feb 15 03 FACTORY SETTING...