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F. Pitot Probe Installation Test
SUBTASK 27-31-94-760-001
(1) Measure the resistance between the strut of the pitot probe [8] and the airplane skin with a
bonding meter, COM-1550.
(a) If the resistance is more than 0.010 ohms, do these steps:
1) Remove the pitot probe [8].
2) Clean the bonding surfaces, including the countersunk holes in the pitot probe [8]
(SWPM 20-20-00).
3) Replace the bolts with new bolts.
4) Re-install the pitot probe [8].
5) Measure the resistance between the strut of the pitot probe [8] and the airplane skin
with a bonding meter, COM-1550.
6) If the resistance is more than 0.010 ohms, do these steps:
a) Remove the pitot probe [8].
b) Replace the nutplates and rivets that attach the pitot probe [8] (SRM 51-40-02).
c) Reinstall the pitot probe [8] and make sure the bonding resistance is not more than
0.010 ohm.
SUBTASK 27-31-94-860-003
(2) For the left pitot probe,
Remove the safety tag and close this circuit breaker:
CAPT Electrical System Panel, P18-3
Row Col Number Name
C 4 C00236 HEATERS ELEV PITOT LEFT
SUBTASK 27-31-94-860-004
(3) For the right pitot probe,
Remove the safety tag and close this circuit breaker:
CAPT Electrical System Panel, P18-3
Row Col Number Name
D 4 C00237 HEATERS ELEV PITOT RIGHT
SUBTASK 27-31-94-710-001
(4) Do this task: Elevator Pitot System Leak - Test, TASK 27-31-17-790-801.
SUBTASK 27-31-94-710-002
(5) Do this task: Pitot Probe, AOA Sensor, and TAT Probe Heater Test, TASK 30-31-00-730-801.
------------------------- END OF TASK ---------------------------
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D633A101-GUN
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STALL WARNING SYSTEM - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
(1) Stall Warning System - Operational Test
(2) Stall Management Yaw Damper Test - Existing Faults
(3) Stall Management Yaw Damper Test - Fault History
(4) Stall Management Yaw Damper Test - Ground Test
TASK 27-32-00-710-801
2. Stall Warning System - Operational Test
(Figure 501)
A. References
Reference Title
24-22-00-860-813 Supply External Power (P/B 201)
24-22-00-860-814 Remove External Power (P/B 201)
B. Location Zones
Zone Area
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-32-00-860-001
(1) Do this task: Supply External Power, TASK 24-22-00-860-813
SUBTASK 27-32-00-710-001
(2) Do a test of the number 1 stall warning system:
NOTE: The amber SPD LIM light on the on-side Primary Flight Display will come on. The
MASTER CAUTION light will come on if the Yaw Damper switch is ‘‘disengaged/off’’.
This will not occur on 285A1010-7 SMYD units. A SPD LIM annunciation that stays on
more than 5 seconds after the stick shaker operates could be a problem.
(a) Push and hold the STALL WARNING TEST NO. 1 switch on the stall warning test module
(P5-18 panel).
(b) Make sure that the captain’s control column shaker operates.
(c) Release the switch.
(d) Make sure that the shaker stops.
SUBTASK 27-32-00-710-002
(3) Do a test of the number 2 stall warning system:
NOTE: The amber SPD LIM light on the on-side Primary Flight Display will come on. The
MASTER CAUTION light will come on if the Yaw Damper switch is ‘‘disengaged/off’’.
This will not occur on 285A1010-7 SMYD units. A SPD LIM annunciation that stays on
more than 5 seconds after the stick shaker operates could be a problem.
(a) Push and hold the STALL WARNING TEST NO. 2 switch on the stall warning test module
(P5-18 panel).
(b) Make sure that the first officer’s control column shaker operates.
(c) Release the switch.
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EFFECTIVITY
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(d) Make sure that the shaker stops.
SUBTASK 27-32-00-860-002
(4) If electrical power is no longer needed: do this task: Remove External Power,
TASK 24-22-00-860-814.
------------------------- END OF TASK ---------------------------
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Stall Warning System Test
Figure 501/27-32-00-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
　
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