1EFF : ALL 1 32-00-00Page 23 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 32-00-00Page 24 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 32-00-00Page 25 1 1 Aug 01/05 1 1 1CES 1
R R R R R the NLG wheels. Two handwheel transmitters in the cockpit supply the primary steering inputs to the BSCU. The rudder pedals and the autopilot supply secondary input to the BSCU through the flight control primary computers. The system operation can be cancelled to let the nose wheels move freely during aircraft ground movement.
R **ON A/C ALL
F. Position and Warning (Ref. 32-60-00)
The position and warning system has two parts which are: - indicating and warning (Ref. 32-61-00) - L/G BITE (Ref. 32-69-00).
(1) Indicating and Warning (Ref. 32-61-00)
The indicating and warning system has proximity sensors on the L/G and L/G doors to give position data to the LGCIU. Indication is given to the flight crew on ECAM and: - L/G control lever - LDG gear annunicators on panel 402vu, if specified failures occur - a warning is given on the Engine Display Unit (EDU) (Ref. 31-66-00) - the fuel page on the SD - the flight warning computer (Ref. 31-52-00) gives an audible and visual warning to the flight crew.
(2) L/G BITE (Ref. 32-69-00)
Each LGCIU contains BITE which continuously monitors the system for failures. The BITE supplies data to the centralized fault display system (Ref. 31-30-00). The BITE functions: - to continuously monitor the system for failures - to do a test of related systems during power-up - to keep a record of failures and send this data to the Centralized Fault Display System (CDFS) and data recording system (Ref. 31-30-00) - to do a system test during ground maintenance - to simulate different L/G configuration during maintenance.
5. Power Supply____________ A. Electrical **ON A/C 001-049, 101-149, 151-199, 201-299,
(Ref. Fig. 008) **ON A/C 051-099,
R (Ref. Fig. 008A) **ON A/C 301-399, 401-499,
(Ref. Fig. 008B) **ON A/C ALL
R B. Hydraulic **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
R (Ref. Fig. 009) **ON A/C 401-499,
R R (Ref. Fig. 009A) **ON A/C ALL
6. Interface_________ (Ref. Fig. 010) 7. Operation/Control and Indicating________________________________ **ON A/C 001-049, 101-149, 151-199, 201-299,
(Ref. Fig. 011)
Landing Gear - Electrical Power Supplies Figure 008 (SHEET 1)
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Landing Gear - Electrical Power Supplies Figure 008 (SHEET 2)
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Landing Gear - Electrical Power Supplies Figure 008 (SHEET 3)
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INTENTIONALLY BLANK
R 1 1
32-00-00Page 29
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R Landing Gear - Electrical Power Supplies
R Figure 008A (SHEET 1)
R 1EFF : 051-099, 1 32-00-00 Page 30
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R Landing Gear - Electrical Power Supplies
R Figure 008A (SHEET 2)
R 1EFF : 051-099, 1 32-00-00 Page 31
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R Landing Gear - Electrical Power Supplies
R Figure 008A (SHEET 3)
R 1EFF : 051-099, 1 32-00-00 Page 32
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INTENTIONALLY BLANK
R 1 1
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Landing Gear - Electrical Power Supplies
Figure 008B (SHEET 1)
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Landing Gear - Electrical Power Supplies
Figure 008B (SHEET 2)
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Landing Gear - Electrical Power Supplies
Figure 008B (SHEET 3)
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Hydraulic Power Supply
Figure 009
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-00-00Page 37 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1
R Hydraulic Power Supply
R Figure 009A
R 1EFF : 401-499, 1 32-00-00 Page 38
1 1 Aug 01/05
1 1
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Interface Figure 010 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架1(76)
