1) Make sure the ANTI-SKID INOP light on the P2 panel stays on.
(j)
Close the ANTI-SKID OUTBD circuit breaker. 1) Make sure the ANTI-SKID INOP light goes off.
(k)
Put the ANTI-SKID switch to the OFF position. 1) Make sure the ANTI-SKID INOP light goes on.
(l)
Pressurize the hydraulic system A (AMM 29-15-00/201).
(m)
Put the ANTI-SKID switch to the ON position. 1) Make sure the ANTI-SKID INOP light goes off.
(n)
Open the ANTI-SKID FAIL WARN & PARK BK circuit breaker.
(o)
Remove the pressure from hydraulic system B (AMM 29-15-00/201). 1) Make sure the ANTI-SKID INOP light comes on.
NOTE: It is allowable for the light to come on within
____ 15 seconds after the time that you open the circuit breaker.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-42-00
ALL ú ú 01 Page 502 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(p)
Put the LIGHTS switch on the P2 panel to the DIM position. 1) Make sure the ANTI-SKID INOP light decreases.
(q)
Close the ANTI-SKID FAIL WARN & PARK BK circuit breaker.
(r)
Put the ANTISKID switch to the OFF position. 1) Make sure the ANTI-SKID INOP light stays on.
(s)
Move the LIGHTS switch to the BRT position. 1) Make sure the ANTI-SKID INOP light stays on and is bright.
(t)
Pressurize hydraulic system B (AMM 29-15-00/201).
(u)
Put the ANTI-SKID switch to the ON position. 1) Make sure the ANTI-SKID INOP light goes off.
(v)
Put the LIGHTS switch on the P2 panel to the TEST position. 1) Make sure the ANTI-SKID INOP light comes on.
(w)
Put the LIGHTS switch to the BRT position.
(x)
Put the ANTI-SKID switch to the OFF position. 1) Make sure the ANTI-SKID INOP light stays on.
(y)
Open the ANTI-SKID FAIL WARN & PARK BK circuit breaker. 1) Make sure the ANTI-SKID INOP light goes off.
(z)
Close the ANTI-SKID FAIL WARN & PARK BK circuit breaker. (aa) Put the ANTI-SKID switch to the ON position. 1) Make sure the ANTI-SKID INOP light stays off.
(ab) Push the ANTI-SKID INOP light. 1) Make sure the light comes on when it is pushed.
TASK 32-42-00-705-009
3. Antiskid System Diagnostic Test_______________________________
A. References
(1)
AMM 29-15-00/201, Hydraulic Systems
B.
Access
(1)
Location Zone
101 Control Cabin - Left
102 Control Cabin - Right
205 Electrical Compartment
310 Left Main Landing Gear
410 Right Main Landing Gear
C.
Quiescent Valve Test
S 735-010
(1)
Put the selector switch to LO and push the VALVE button for all of the valve test.
(2)
Make sure the center green LED comes on.
S 735-012
(3)
Do steps (1) and (2) with the selector switch moved to LI, RI, and RO positions.
(4)
Put the selector switch to the L ALT position.
S 735-011
S 735-013
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-42-00
ALL ú ú 01 Page 503 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CONTROL PANEL CONTROL PANEL
Antiskid System Controls Figure 501
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú ALL ú ú ú
ANTISKID
ANTISKID
CONTROL UNIT
32-42-00
01 Page 504Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 起落架 LANDING GEAR 3(53)
