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9. MCP ALT DES AND FMC V/S CLB (0.5 SEC) 8. MCP ALT CLB AND FMC V/S DESCENT (0.5 SEC)10. FMC TARGET V/S NOT VALID 6. CLIMB CMD AND ALPHA WARN AND NOT CLIMBING AT MIN V/S AND NOT ON GRND (5 SEC) 7. DES CMD AND VMO/MMO AND NOT DES AT MIN V/S AND NOT ON GRND (10 SEC) X X  X X  X X  X X X 
11. INTENTIONAL BLANK15. VHF NAV XFR AND NEITHER A/P IN CMD AND BOTH F/D ON 14. LCL AC BUS XFR AND NEITHER A/P IN CMD AND BOTH F/D ON 13. ATT XFR AND NEITHER A/P IN CMD AND BOTH F/D ON 12. FLARE X  X X X X  X 
20. SELECTED IRU LONG ACCELERATION NOT VALID 19. SELECTED IRU VERTICAL ACCELERATION NOT VALID 18. SELECTED IRU PITCH ATTITUDE RATE NOT VALID 17. SELECTED IRU ROLL ANGLE NOT VALID 16. SELECTED IRU PITCH ANGLE NOT VALID  X X X X  X X  X X  X X  X X  X X  X X X  X X  X X  X X  X X X X  X X X X 
21. SELECTED IRU VERTICAL SPEED NOT VALID 25. BARO CORRECTED ALTITUDE NOT VALID 24. BARO UNCORRECTED ALTITUDE NOT VALID 23. TAS NOT VALID 22. STATIC PRESSURE NOT VALID  X X  X X  X X X  X X X  X X X X  X X X X  X X X X  X X  X X X X  X X X  X  X X 
30. F/D COMPARATOR 28. 115 VOLT AC (2.5 SEC) 29. AUTOTUNE 27. MACH NOT VALID 26. CAS NOT VALID  X X X  X  X  X  X X  X X  X X X  X  X  X  1 X X  X X X 

NEITHER A/P IN CMD, LOC ENGAGED,
GS ENGAGE AND LRRA LESS THAN 800 FEET

Pitch Bar Bias TableFigure 22
A737-300/400/500MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.AIRPLANES WITHOUT EFIS ú
 22-11-00
úú 12 Page 61 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (h)  
Event 8 - The mode control panel is set for a higher altitude, however, the FMC command is V/S descent.

 (i)  
Event 9 - The mode control is set for a lower altitude, however, the FMC command is V/S climb.

 (j)  
Event 10 - The FMC target V/S is not valid.

 (k)  
Event 12 - Flare mode is not used in conjunction with the F/D and the bars are biased out of view.

 (l)  
Event 13 - Attitude transfer (Attitude to Both on 2) from the normal position without either A/P in CMD and both F/D on.

 (m)  
Event 14 - Local AC bus transfer without either A/P in CMD and both FD on.

 (n)  
Event 15 - VHF NAV transfer from the normal position without either A/P in CMD and both F/D on.

 (o)  
Event 16 - Selected IRU pitch angle not valid.

 (p)  
Event 17 - Selected IRU roll angle not valid.

 (q)  
Event 18 - Selected IRU pitch attitude rate not valid.

 (r)  
Event 19 - Selected IRU vertical acceleration not valid.

 (s)  
Event 20 - Selected IRU longitudinal acceleration not valid.

 (t)  
Event 21 - Selected IRU vertical speed not valid.

 (u)  
Event 22 - ADC static pressure not valid.

 (v)  
Event 23 - ADC TAS not valid.

 (w)  
Event 24 - ADC Baro uncorrected altitude not valid.

 (x)  
Event 25 - ADC Baro corrected altitude not valid.

 (y)  
Event 26 - ADC CAS not valid.

 (z)
Event 27 - ADC mach not valid.
 (aa) Event 28 - A loss of the 115 volts power.
 (ab) Event 29 - The VHF navigation system is in autotune.
 (ac) Event 30 - F/D comparator 3° difference for more than 3 seconds

 

 between captain and first officer's F/D commands.
 I. Roll Axis Flight Control Operation (Fig. 23)
 (1)  The aileron and aileron trim flight control system provides airplane roll control. Roll control is assisted by the flight spoilers. Rotation of either aileron control wheel results in movement of the ailerons and movement of the flight spoilers. The ailerons are powered by two independent hydraulic power control roll units connected to separate hydrualic systems. Either power unit is capable of providing full power control response to aileron control system inputs. In the event of total hydraulic failure, roll control is maintained manually.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
　
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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 自動(dòng)飛行 AUTOFLIGHT 1(34)