(5) Flush captain's static system from capped fitting on static system manifold located forward of captain's instrument panel on inboard side to:
(a)
Static hose disconnected from altitude indicator.
(b)
Static hose disconnected from instantaneous vertical velocity indicator.
(c)
Static hose disconnected from airspeed indicator.
(d)
Static line disconnected from drain fitting 6 (Fig 301, sheet 1).
(e)
Static line disconnected from drain fitting 19 (Fig 301, sheet 3).
(f)
Static hose disconnected from central air data computer No. 1.
EFFECTIVITY
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(g) Disconnect and cap alternate static system tubing from captain's static source selector valve. Place selector valve toggle in ALTERNATE position and flush using reduced air pressure. Return selector valve toggle to NORMAL position but do not reconnect tubing.
(6)
Flush using reduced air pressure from captain's static pressure manifold to static line disconnected from drain fitting 1 (Fig. 301, sheet 1).
(7)
Replace cap on captain's static pressure manifold.
(8)
Flush captain's static system from captain's static hose disconnected from upper left pitot-static probe to:
(a)
Static line disconnected from drain fitting 1 (Fig 301, sheet 1).
(b)
On FREIGHTERS, static line disconnected from drain fitting 32 (Fig. 301, sheet 1).
(c)
Static line disconnected from drain fitting 29 (Fig 301, sheet 2).
(d)
Static hose disconnected from lower right pitot-static probe.
(9)
Flush first officer's static system from capped fitting on static system manifold located forward of first officer's instrument panel on the inboard side to:
(a)
Static hose disconnected from altitude indicator.
(b)
Static hose disconnected from instantaneous vertical velocity indicator.
(c)
Static hose disconnected from airspeed indicator.
(d)
Static line disconnected from drain fitting 10 (Fig. 301, sheet 2).
(e)
Static line disconnected from drain fitting 21 (Fig 301, sheet 3).
(f)
Static hose disconnected from central air data computer No. 2.
(g)
Disconnect and cap alternate static system tubing from first officer's static source selector valve. Place selector valve toggle in ALTERNATE position and flush using reduced air pressure. Return selector valve toggle to NORMAL position but do not reconnect tubing.
(10)
Flush using reduced air pressure from first officer's static pressure manifold to static line disconnected from drain fitting 2 (Fig. 301, sheet 2).
(11)
Replace cap on first officer's static pressure manifold.
(12)
Flush first officer's static system from first officer's static hose disconnected from upper right pitot-static probe to:
(a)
Static line disconnected from drain fitting 2 (Fig 301, sheet 2).
(b)
On FREIGHTERS, static line disconnected from drain fitting 35 (Fig. 301, sheet 2).
(c)
Static line disconnected from drain fitting 30 (Fig 301, sheet 1).
(d)
Static hose disconnected from lower left pitot-static probe.
EFFECTIVITY
ALL 22 Page 311 Apr 25/9734-11-00
(13)
Flush alternate static system from hose disconnected from right alternate static port to:
(a)
Static line disconnected from drain fitting 7 (Fig 301, sheet 1).
(b)
Static line disconnected from captain's static source selector valve. Do not allow any dirt to be blown into selector valve. Reconnect line to captain's static source selector valve.
(c)
Static line disconnected from first officer's static source selector valve. Do not allow any dirt to be blown into selector valve. Reconnect line to first officer's static source selector valve.
(d)
Static hose disconnected from left alternate static port.
(14)
Flush auxiliary static system No. 1 from static hose disconnected from lower right pitot-static probe to:
(a)
Static line disconnected from drain fitting 28 (Fig 301, sheet 2).
(b)
Static hose disconnected from upper left pitot-static probe.
(c)
On FREIGHTERS, static line disconnected from drain fitting 33. Refer to figure 301, sheet 1.
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本文链接地址：747飞机维护手册AMM CHAPTER 34 - NAVIGATION 第34章导航1(35)
