(b)
Replace the cap on the hose.
S 432-088
(16) Connect the air supply:
(a)
Remove the cap from the manifold which is in the electronics compartment on the forward right side.
(b)
Connect the dry filtered air supply to the manifold.
S 862-089
(17) Flush the auxiliary No. 1 static system at these locations:
(a)
The static hose disconnected from the cabin altimeter and differential pressure indicator in the P5 panel.
(b)
The static hose disconnected from the electronic pressure controller.
(c)
The static line disconnected from drain fitting No. 4 which is on the right side of the E1 rack.
(d)
The static line disconnected from drain fitting No. 12 which is at the forward end of the nose wheel well.
(e)
The static line disconnected from the lower right pitot static probe.
S 032-090
(18) Disconnect the air supply:
(a)
Disconnect the dry filtered air supply from the manifold which is in the electronics compartment on the forward right side.
(b)
Replace the cap on the manifold.
S 432-091
(19) Connect the air supply:
(a)
Remove the cap from the auxiliary No. 1 static system hose at the top left pitot-static probe.
(b)
Connect the dry filtered air supply to the hose.
S 862-158
(20) Flush the auxiliary No. 1 static system at these locations:
(a)
The static line disconnected from the bottom right pitot-static probe.
(b)
The static line disconnected from drain fitting No. 12 which is at the forward end of the nose wheel well.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
34-11-01
ú ú 09 Page 204 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 032-093
(21) Disconnect the air supply:
(a)
Disconnect the dry filtered air supply from the auxiliary static system hose that you disconnected from the top left pitot-static probe.
(b)
Replace the cap on the hose.
S 432-094
(22) Connect the air supply:
(a)
Remove the cap from the auxiliary No. 2 static system hose at the top right pitot-static probe.
(b)
Connect the dry filtered air supply to the hose.
S 432-116
(23) Connect the air supply:
(a)
Remove the cap from the static line that you disconnected from the right static port.
(b)
Connect the dry filtered air supply to the static line.
S 862-117
(24) Flush the alternate static system at these locations:
(a)
The static line disconnected from the left side port.
(b)
The static line disconnected from drain fitting No. 5 which is on the right side of the E1 rack.
(c)
The static hose disconnected from the combined standby altimeter/airspeed indicator.
E. Put the Airlane Back to Its Usual Condition
S 842-118
(1)
Connect all of the pitot and static hoses or lines, that you disconnected, to their related components.
S 842-119
(2)
Make sure that no unwanted material is in or around the static ports and pitot-static probe openings.
S 842-120
(3)
Make sure that no rough surfaces are in or around the static ports and pitot-static probe openings.
S 842-121
(4)
Do a leakage test of all of the systems (Ref 34-11-01, Pitot-Static System - Adjustment/Test).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
34-11-01
ú ú 10 Page 205 ú Jul 15/98
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 導航 NAVIGATION 1(38)
