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 ALL  ú ú 01 Page 7 ú Oct 20/83
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ~.............................................................................. | Air-Ground Sensing Functions | | Table 1 | ................................................................................ | SYSTEM | SAFETY SENSOR | TO SIMULATE | | | | FUNCTION | AIRPLANE-IN-AIR | PRECAUTIONS | ................................................................................ | Drain | Transfers power || Press and hold | If airplane power is being|| |
| | | mast| | source for heater| | |
| air sensing test| used, open drain mast |
 | heater | from 115 volt ac || switch | heater circuit breaker to || |
| |          |
|
| (air condition) to |
|| prevent overheating heater||          |
| 28 volt ac (ground| |
|| element. Close circuit |
         |
|
| condition) |
|| breaker when maintenance |
         |
|
|
|| is completed |
 ................................................................................| | | |
|
| Voice | Permits erasure of || Press and hold | None| |

| |
| recorder | tape after parking| | || ground sensing |
|
         |
|

| brake is set | test switch| |
|
 ................................................................................| | | |
|
| Landing | Prevents control || Cannot be | None| |

| |
| gear| | lever from being| || simulated |
|
 | control | placed UP position |
|
|

| |
| lever | when airplane is on || |
|

| |
| lock | ground |
|
|

| |
................................................................................| | | |

|
| Antiskid | Prevents applica-| | Press and hold| | None |

| |
| (inboard | tion of brakes| | || air sensing |
|
 | brakes)| | before touchdown| || test switch |
|
         |
| and loss of brakes| |
|
|
         |
| at low speed| |
|
|
 ................................................................................| | | |

|
| Wing | Prevents hot air || Press and hold | None| |

| |
| anti-ice | from entering| | || ground sensing |
|
         |
|

| anti-ice ducts | test switch| |
|
         |
| when airplane is| |
|
|
         |
| on ground| |
|
|
 ................................................................................| | | |
|
| Stall | Activates system || Press and hold | Avoid contact with angle| |

| |
| warning | when airplane is || air and ground | of airflow sensor vane as || |

| |
         |
| in air| | sensing test |

| | vane will be hot |
         |
|
| switches *[1]| |
|
 ................................................................................| | | |
|
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 32-00-00
 ALL  ú
 ú  01  Page 8
 ú  Mar 15/96 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ~..............................................................................
 | Air-Ground Sensing Functions |
 | Table 1 |
 ................................................................................
 | SYSTEM | SAFETY SENSOR | TO SIMULATE | |
 | | FUNCTION | AIRPLANE-IN-AIR | PRECAUTIONS |
 ................................................................................
 | Flight | Activates system || Press and hold | If electrical power is| |

| |
| recorder | when airplane is| | ground sensing| | being used, open flight |
　
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