737 AMM 飞机维护手册 导航 NAVIGATION 2(23)

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B.  When a test step does not check out, follow the NOT OK line to the box containing the trouble symptom and continue to follow a single line by analyzing the results of each test step until the required corrective action is determined. Perform the specified corrective action; then repeat the step at which the failure was encountered.
C.  All trouble shooting procedures are based on the assumption that wiring is OK and that electrical power is available. If the corrective action in the procedure does not correct the problem, check wiring using the wiring diagram.
2.  Trouble Shooting Tips
A.  The malfunctions associated with the VOR/ILS navigation system can generally be divided into four groups: VOR/LOC deviation, glide slope deviation, VOR bearing and flag warning. First check for power to the defective system and establish that power is available.
B.  Verification of a navigation unit malfunction can usually be accomplished by observing for presence of flag warnings in the indicators and by self-test of the VOR/ILS navigation system. In the event of flag warnings, use the VHF NAV transfer switch to transfer to the opposite system for component isolation.
C.  To trouble shoot a VOR bearing malfunction, for example, if the VOR bearing displays are different when both systems are tuned to the same station, interchange the navigation units. If the problem follows, replace the malfunctioning navigation unit. If the problem remains in the same system, check the VOR/LOC antenna installation for corrosion at antenna feed cable connections and for physical damage to the cables and the antenna.
NOTE:  A nonsymmetrical ground station signal can also cause different bearing and deviation displays when tuned to the same frequency.
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3.  Prepare for Trouble Shooting
A.  Verify that all applicable VOR/ILS, compass, flight instrument and instrument transfer circuit breakers on panels P6 and P18, are closed.
B.  Apply electrical power.
C.  Position AFCS controller switches and controls (P7 panel) as follows:
Nav Mode - HDG SEL
All Others - OFF
Course Counter - 000
Heading Control -Position HSI heading marker under lubber line.
Verify that autopilot is disengaged.

D.  Position HSI transfer switches (P7 panel) to RADIO.
E.  Position VHF NAV transfer switch (P5 panel) to NORMAL.
F.  Position COMPASS transfer switch (P5 panel) to NORMAL.
G.  Select VOR mode for RDDMI VOR/ADF switches (P1 and P3 panels).
NOTE:  Throughout the trouble shooting NORMAL position of transfer switch implies captain on 1 and first officer on 2.
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VOR/ILS NAVIGATION SYSTEM - ADJUSTMENT/TEST
EFFECTIVITY
GJ B-2509 and B-2510

1.  VOR/ILS Navigation System Test
A.  Equipment and Materials
(1)  Ramp and Bench Test Set - Collins Type 972Q-4 or Instrument Flight Research Type NAV-401L
B.  Prepare to Test System
(1)  
Provide electrical power and energize panels P6 and P18.

(2)  
Check that circuit breakers for following systems are closed: compass, flight director, instrument, interphone, and VOR/ILS navigation systems.

(3)  
Position VHF NAV and COMPASS transfer switches to NORMAL.

(4)  
Set selected course to 000.

(5)  
Set compass system to indicate a heading of 0 degree.

(6)  
Check that autopilot system is not in radio mode.

(7)  
Position HSI transfer switches to RADIO.

(8)  
Position RDDMI VOR/ADF switches to VOR.

C.  Test VOR/ILS System
(1)  Test VOR/ILS System Self-Test Function
(a)  
Tune No. 1 VOR/ILS system to local VOR station and check that station identification code is audible over flight interphone system.

(b)  
Select 108.0 MHz on captains VHF NAV control panel. Check that captain's ADI and HSI glide slope flags and pointers are out of view and that the HSI NAV flag is in view.
　
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