(b)
Remove air supply.
(c)
If external air supply was used, determine if there is any further need for electrical power on airplane. If not, remove electrical power.
(d)
Install wing leading edge lower access panels.
504
30-11-0 Page 504 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Oct 20/84
D. Ground Operational Test with Engine Power
NOTE: You can also do this test with APU power. Paragraph E. provides a procedure, which uses this option.
(1) Prepare to Test Wing TAI System.
(a)
Start engines in accordance with engine start procedure (Ref Chapter 71, Power Plant).
(b)
With engines set idle and power available at 115V ac transfer bus No. 1 and No. 2, and 28V dc T/R bus No. 1, check that the following circuit breakers are closed: 1) ENG NO. 1 NACELLE & WING ANTI-ICE 2) ENG NO. 2 NACELLE & WING ANTI-ICE 3) ENG NO. 1 & WING ANTI-ICE CONTROL
(c)
On pilot's overhead panel P5, press to test the wing anti-ice left and right valve open annunciator lights for operation.
NOTE: Each light will come on when pressed and go off when released.
(2) Test Wing TAI System
(a)
Position left engine bleed valve to open and isolation valve to closed.
(b)
Hold wing TAI control switch in GRD-TEST position and check that both valve open lights glow brightly for one to three seconds and then continue to glow dim.
(c)
Increase left engine power slightly until both valve open lights glow brightly (left ground overheat switch actuates).
(d)
Reduce left engine power to idle, close left engine bleed valve and check that the valve open lights return to dim after a short interval.
(e)
Repeat steps (a), (c), and (d) for right side of system to check operation of right ground overheat switch.
Oct 20/91 30-11-0
Page 505
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
(f)
Release wing TAI control switch and check that both valve open lights glow brightly for 1 to 3 seconds and then go off.
(g)
Shut down engine.
E. Ground Operational Test with APU Power (alternative to test with Engine Power).
(1)
Provide electrical power (Ref Chapter 24, Electrical Power).
(2)
Start the APU (Ref Chapter 49, APU) and allow it to stabilize.
(3)
Make sure the VALVE OPEN indicator lights operate:
(a)
Push the L and R VALVE OPEN lights on the P5 overhead panel.
(b)
Make sure that each light comes on.
(c)
Release the VALVE OPEN lights.
(d)
Make sure that each light goes off.
(4)
Prepare for the test:
(a)
Set the BLEED 1 and 2 switches on the P5 panel to OFF.
(b)
Set the PACK L and R switches on the P5 panel to OFF.
(c)
Set the ISOLATION VALVE switch on the P5 panel to OPEN.
(5)
Do this test of the left wing TAI system:
(a)
Disconnect electrical connector D736 from the right wing ground thermal switch.
(b)
Set the WING ANTI-ICE switch to GND TEST. 1) Make sure that each VALVE OPEN light comes on bright for 1 to 3 seconds
(this shows that the valves are in transit). 2) Make sure that each VALVE OPEN light becomes dim after 3 seconds.
(c)
Set the APU BLEED switch to ON.
CAUTION: DO NOT LET THE WING TAI VALVE BE OPEN FOR MORE THAN 30 SECONDS. OPERATION FOR MORE THAN 30 SECONDS WITH HEATED AIR CAN CAUSE DAMAGE TO THE WING LEADING EDGE.
1) Make sure that each VALVE OPEN light comes on bright in approximately 10 to 30 seconds.
2) If the lights do not come on in 30 seconds, set the APU BLEED switch to OFF.
(d)
Set the APU BLEED switch to OFF.
1) Make sure that both VALVE OPEN lights become dim.
NOTE: It is possible that the lights will not become dim for up to 2 minutes after you set the APU BLEED switch to OFF.
(e)
Connect the electrical connector to the right wing ground thermal switch.
(6) Do a test of the right wing TAI system:
(a)
Disconnect electrical connector D738 from the left wing ground thermal switch.
(b)
Set the APU BLEED switch to GND TEST.
504
30-11-0 Page 506 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Feb 20/94
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機維護手冊 防冰和排雨 ICE AND RAIN PROTECTION(8)
