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时间:2011-03-30 10:20来源:蓝天飞行翻译 作者:航空
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(b)  
Pull the three generator control circuit breakers C4, C5 and C6 on the load control center right (P6-4). See wiring diagram manual 24-21-11, -21 or -31 depending on generator number.

(c)  
Measure generator exciter field resistance. The field resistance measured from F to A terminals should be at least 8 ohms.


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Feb 15/70  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  24-21-0 Page 106A 


(3)  
Rotating rectifier has failed.

(a)  
Determine if generator rotates [Ref 4.C.(1)(a)].

(b)  
Determine that exciter field is not open or shorted [Ref step 4.C.(2)].

(c)  
Check voltage regulator by exchanging the generator control unit (GCU) for one that is known to function properly. Also check connections at voltage regulator terminals on the GCU for continuity and short circuits.

(d)  
If test equipment is available, check generator rotating rectifier (Ref 24-21-61).

 

(4)  
Shorted feeder lines.

(a)  
Remove generator feeder lines from generator terminals T1, T2 and T3.

(b)  
Check for open, or infinity on ohmmeter, between feeder lines, phase to phase, and phase to neutral. If continuity exists, the feeder lines are shorted.

 


D.  Constant Speed Drive
(1)  Input shaft has failed, generator shaft has sheared, disconnect has failed.
(a)  
With engine running, check residual voltage at generator terminals, and check that constant speed drive is not disconnected [Ref 4.C.(1)].

(b)  
If drive is connected and the residual voltage is zero, the input shaft or the disconnect unit has failed. If the low pressure light on the overhead panel is off and still no residual voltage, the generator shaft is sheared.

(c)  
If disconnect does not actuate properly, check circuit; if circuit checks, replace transmission. 1) Disconnect connector D6 from CSD wiring harness. 2) Measure resistance of CSD disconnect solenoid coil between pins 3 and 4 of


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24-21-0 Page 106B  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Feb 20/84 


wiring harness. Check that resistance is less than 100 ohms. 3) Check continuity to ground of pins 3 and 4 of connector D6. 4) Set meter to measure dc voltage and monitor voltage of pin 6 on D6. 5) Place BAT switch on P5 panel to ON. Set CSD DISCONNECT switch to ON. 6) Verify voltage on meter is approximately 28 volts while switch is held to ON and
zero when switch is released. 7) Remove meter, restore airplane to normal, and lockwire switch.
(d)  If disconnect does not reset properly, replace transmission.
(2)  
Disconnect unit has failed.

(a)  Ref 4.D.(1)(c) and (d).

(3)  
Drive has failed internally.


(a)  Remove and inspect magnetic drain plug. The presence of reasonably large pieces of bright metal on the magnetic plug indicates a drive failure.
NOTE: A small amount of fine or fuzzy granular material is normal.
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Feb 20/84  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  24-21-0 Page 107 


BTB  GCB  GCR  VOLT-METER  FREQ METER  ANNUNCI -ATOR SIGNAL  AC AM-METER READING  CIRCUITS* LOCKED OUT  CSD LOW PRESSURE LIGHT  CSD TEMP 
Closed  Open  Open  Zero  Zero  FF  Zero  Off  Safe 
Closed  Trip  Trip  Zero  Zero  FF_LV*  Zero  Off  Safe 
Trip  Trip  Closed  Zero  Zero  LV  Zero  LV  Off  Safe 
Closed  Trip  Trip  Above 129  400  HV  -- Off  Safe 
Closed  Trip  Trip  115  400  FF  -- Off  Safe 
Open  One Trip  Trip  Zero  LV  Zero  Off  Safe 
Closed  Open  Closed  Zero  Zero  No Signal  Zero  On  Safe 
Closed  Open  Closed  115  400  No Signal  Zero  Off  Safe 
Closed  Trip  Trip  -- -- LV  Zero  LV  Off  Safe 
Closed  Trip  Trip  Below 97  -- LV  -- LV  Off  Safe 
Closed  Open  Closed  115  400  No Signal  Zero  Off  Safe 
Open  Trip  Closed  115  400  LV  Zero  UF  Off  Safe 
Open  Closed  Trip  Zero  Zero  LV  Zero  LV  Off  Safe 
 
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