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15) Remove the warning sign prohibiting main switch-breaker operation. 16) If connected, disconnect the ground power unit - refer to 24-40-00. AAAA Validity : S / N 1 - 9999 32-20-07 Page 203 (BA) JUN 02 Nose landing gear door - Removal / Installation Figure 201 AAAA Nose landing gear door - Adjustment / Test Figure 202 PAGE INTENTIONALLY LEFT BLANK WA Validity : S / N 1 - 9999 32-20-07 Page 206 (BA) JUN 02 EXTENSION AND RETRACTION DESCRIPTION AND OPERATION 1. GENERAL The landing gear maneuver system includes the following elements : - main landing gear actuating cylinder, - nose landing gear actuating cylinder, - main landing gear hinged strut, - nose landing gear hinged strut, - main landing gear compensating spring, - nose landing gear compensating actuator, - end of travel microswitch. 2. LOCATION COMPONENT QTY AREA ACCESS DOOR REFERENCE Main L / G actuating cylinder 2 730 - 740 / 32-30-01 Nose L / G actuating cylinder 1 100 131 32-30-02 Main L / G hinged strut 2 730 - 740 / 32-30-03 Nose L / G hinged strut 1 100 131 32-30-04 Main L / G compensating spring 2 730 - 740 / 32-30-00 Nose L / G compensating actuator 2 100 131 32-30-06 End of travel microswitch 8 100 - 730 - 740 131 32-30-07 3. DESCRIPTION (Figure 1) |