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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
~.......................................................................... | BIT TABLE | ............................................................................ | | Bit Condition | ............................................................................ | Switch | Port/Label | Bit | 0 | 1 | ............................................................................ | R BODY GR | E/099/272/00 | 14 | NOT DOWN | GEAR DOWN | | DOWN/LOCK ALT | | | | | ............................................................................ | L BODY GR | E/099/272/00 | 15 | NOT UP | GEAR UP | | UP/LOCK ALT | | | | | ............................................................................ | L WING GR | E/099/272/00 | 16 | NOT UP | GEAR UP | | UP/LOCK ALT | | | | | ............................................................................ | R WING GR | E/099/272/00 | 17 | NOT UP | GEAR UP | | UP/LOCK ALT | | | | | ............................................................................ | R BODY GR | E/099/272/00 | 18 | NOT UP | GEAR UP | | UP/LOCK ALT | | | | | ............................................................................ | NOSE GR | E/099/273/00 | 18 | NOT DOWN | DOWN | | DOWN/LOCK ALT | | | AND LOCKED | AND LOCKED | ............................................................................ | NOSE GR | E/099/273/00 | 19 | NOT UP | GEAR UP | | UP/LOCK ALT | | | AND LOCKED | AND LOCKED | 2................…...................…..........…............….............1
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(2) Remove the DO-NOT-CLOSE tags and close these circuit breakers on the
Overhead Circuit Breaker Panel, P7:
(a) 7F23 LANDING GEAR DSP & CONT ALTN
(b) 7F26 PSEU SECT 2
S 865-058
(3) Open these circuit breakers on the Overhead Circuit Breaker Panel,
P7 and install DO-NOT-CLOSE tags:
(a) 7F22 LANDING GEAR DSP & CONT PRI
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400 MAINTENANCE MANUAL
(b) 7F25 PSEU SECT 1
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(4)
Prepare the CMC for the test:
(a)
Push the line-select key, adjacent to the INPUT MONITORING display.
(b)
Push the CDU keys E/099/270/00, then push key 1L.
(c)
Push the NEXT PAGE key.
(d)
Push the CDU keys E/099/271/00.
(e)
Push the NEXT PAGE key.
(f)
Push the CDU keys E/099/272/00.
(g)
Push the NEXT PAGE key.
(h)
Push the CDU keys E/099/273/00.
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(5)
Do a test of the nose gear position indication:
(a)
Push the NEXT PAGE key as necessary to show the logic conditions of label 273/00.
(b)
Make sure the CDU display of label 273/00 is shown as follows:
(c)
Condition - Gear Down and Locked
~.............................................. | Sensor and Bit Location | Bit State | ................................................ |Nose Gear Down/Lock on Bit 18 | 1 | ................................................ |Nose Gear Up/Lock on Bit 19 | 0 | 2.................................…............1
(d)
Put a rectangular deactuator on the sensor, S424 (alternate nose gear lock sensor).
(e)
Make sure the CDU display of label 273/00 is shown as follows:
(f)
Condition - Gear Down and Unlocked
~.............................................. | Sensor and Bit Location | Bit State | ................................................ |Nose Gear Down/Lock on Bit 18 | 0 | ................................................ |Nose Gear Up/Lock on Bit 19 | 0 | 2.................................…............1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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