曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

15.86 mm 15.88 mm 15.89 mm 0.0025 in
#2 BOLT O.D. 0.6230 in 0.6240 in 0.6226 in 0.06 mm
15.82 mm 15.85 mm 15.81 mm
#3 BEARING I.D. 0.6245 in 0.6250 in 0.6255 in
15.86 mm 15.88 mm 15.89 mm 0.0025 in
#3 BOLT O.D. 0.6230 in 0.6240 in 0.6226 in 0.06 mm
15.82 mm 15.85 mm 15.81 mm
SUBTASK 27-62-94-020-012
(4) Install the outboard ground spoiler actuator. To install it, do this task: Outboard Ground Spoiler
Actuator Installation, TASK 27-62-94-400-801.
------------------------- END OF TASK ---------------------------
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Outboard Ground Spoiler Actuator Wear Limits
Figure 601 (Sheet 1 of 2)/27-62-94-990-802
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Outboard Ground Spoiler Actuator Wear Limits
Figure 601 (Sheet 2 of 2)/27-62-94-990-802
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LEADING EDGE FLAP AND SLAT CONTROL SYSTEM - MAINTENANCE PRACTICES
1. General
A. This procedure contains these tasks for the leading edge (LE) flap and slat control system:
(1) A task to deactivate the leading edge flaps and slats
(2) A task to reactivate the leading edge flaps and slats
(3) A task to operate the leading edge flaps and slats with primary control
(4) A task to operate the leading edge flaps and slats with alternate control
(5) A task to extend the leading edge flaps and slats
(6) A task to retract the leading edge flaps and slats
(7) A task to install the leading edge flap and slat locks
(8) A task to remove the leading edge flap and slat locks
TASK 27-81-00-040-801
2. Deactivate the Leading Edge Flaps and Slats
A. General
CAUTION: MAKE SURE THE INBOARD FAN DUCT COWL AND THE INBOARD AND OUTBOARD
THRUST REVERSERS ARE CLOSED OR REMOVED BEFORE YOU EXTEND THE
LEADING EDGE FLAPS AND SLATS. THERE IS NOT SUFFICIENT CLEARANCE FOR
THE FLAPS AND SLATS TO EXTEND IF THE INBOARD FAN DUCT COWL AND THE
INBOARD AND OUTBOARD THRUST REVERSERS ARE IN THE OPEN POSITION. THIS
CAN CAUSE DAMAGE TO EQUIPMENT.
(1) Before you do maintenance on the leading edge flaps and slats, you must deactivate the leading
edge control surfaces. This is to prevent injury to persons and damage to equipment because of
accidental operation of the leading edge control surfaces.
B. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-860-805 Trailing Edge Flap System Operation With Leading Edge Flaps and
Slats Disabled (P/B 201)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
29-21-00-000-802 Standby Hydraulic System Power Removal (P/B 201)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
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Reference Description
SPL-1675 Assembly - Lock, Flight Controls
(Part #: F80049-18, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80049-12, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1734 Lockout Set - Leading Edge Slats and Krueger Flaps Actuators
(Part #: C27051-29, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
(Opt Part #: C27051-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -BBJ)
SPL-1746 Tool - Lockout, LE Shutoff Valves
(Part #: C27038-6, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
　
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