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(Part #: 411B90, Supplier: 3DN12, A/P Effectivity: 737-ALL)
(Part #: DAD5013, Supplier: $0856, A/P Effectivity: 737-ALL)
(Part #: DFD5019, Supplier: $0856, A/P Effectivity: 737-ALL)
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B. Location Zones
Zone Area
323 Vertical Fin - Front Spar To Rear Spar
C. Pitot Probe Removal
SUBTASK 27-31-94-860-001
(1) For the left pitot probe,
Open this circuit breaker and install safety tag:
CAPT Electrical System Panel, P18-3
Row Col Number Name
C 4 C00236 HEATERS ELEV PITOT LEFT
SUBTASK 27-31-94-860-002
(2) For the right pitot probe,
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Open this circuit breaker and install safety tag:
CAPT Electrical System Panel, P18-3
Row Col Number Name
D 4 C00237 HEATERS ELEV PITOT RIGHT
SUBTASK 27-31-94-140-001
WARNING: MAKE SURE THAT THE PITOT PROBE [8] HEAT IS OFF. INJURY TO PERSONS CAN
OCCUR.
CAUTION: MAKE SURE THAT THE AREA AROUND THE PITOT PROBE [8] IS CLEAR OF
UNWANTED MATERIAL. CONTAMINATION OF THE PITOT SYSTEM CAN OCCUR.
(3) Use the sealant removal tool, COM-2481 to remove the sealant from around the baseplate [5] of
the pitot probe [8].
SUBTASK 27-31-94-020-001
(4) Remove the bolts [9] from the baseplate [5] of the pitot probe [8].
SUBTASK 27-31-94-020-002
CAUTION: MAKE SURE THAT THE PITOT PROBE HAS NO WEIGHT ON IT. THE PITOT PROBE [8]
CAN BEND OR TWIST OUT OF TOLERANCE.
(5) Do these steps to loosen the pitot probe [8] from the airplane skin:
(a) Hold the probe strut [7].
(b) Loosen the gasket [2].
(c) Pull the pitot probe [8] out from the airplane skin until you can get access to the pitot hose
fitting [10] and electrical connector [1] on the base of the pitot probe [8].
SUBTASK 27-31-94-020-003
CAUTION: USE WRENCHES TO APPLY COUNTER PRESSURE ON EACH SIDE OF THE FITTING
DURING DISASSEMBLY. DAMAGE TO THE TUBE OR FITTING CAN OCCUR.
(6) Disconnect the pitot hose fitting [10] at the base of the pitot probe [8].
SUBTASK 27-31-94-020-004
(7) Remove the long screw [6] from the pitot probe side of the electrical connector [1].
SUBTASK 27-31-94-020-005
(8) Disconnect the electrical connector [1].
SUBTASK 27-31-94-020-006
(9) Remove the pitot probe [8].
SUBTASK 27-31-94-420-001
(10) Install the long screw [6] in the electrical connector [1].
SUBTASK 27-31-94-020-007
(11) Temporarily attach the electrical connector [1] and pitot hose fitting [10] to the airplane structure
with tape so they do not fall inside vertical fin.
SUBTASK 27-31-94-020-008
(12) Put a cap on the pitot hose fitting [10] to keep out unwanted material.
SUBTASK 27-31-94-020-013
(13) Remove the elbow [11] from the pitot probe assembly [8].
(a) Remove the lockwire [12] and discard.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-31-94-020-009
(14) Remove the bolts [3], washers [4], and pitot probe [8] from the baseplate [5].
SUBTASK 27-31-94-020-010
(15) Keep the baseplate [5] for another installation.
SUBTASK 27-31-94-020-011
(16) Remove the gasket [2] and discard it.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Feel System Pitot Probe Installation
Figure 401/27-31-94-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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TASK 27-31-94-400-801
3. Feel System Pitot Probe - Installation
(Figure 401)
A. References
Reference Title
20-10-34-110-802 Clean Bare, Clad, or Plated Metal with Solvent (P/B 701)
　
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本文鏈接地址：737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊3(96)