TASK 53-05-03-210-861
57. INTERNAL - GENERAL VISUAL: FLIGHT COMPARTMENT FROM STA 178 TO 270
NOTE: This procedure is a scheduled maintenance task.
A. References
Reference Title
25-11-21-210-801 Inspection Access - P18 Panel (P/B 601)
25-11-21-210-802 Inspection Access - P5 Panel (P/B 601)
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
221 Passenger Compartment - Aft of Control Compartment to Forward Entry Door - Left
222 Passenger Compartment - Aft of Control Compartment to Forward Entry Door -
Right
C. Access Panels
Number Name/Location
S2101 Flight Compartment Inspection
D. Inspection
SUBTASK 53-05-03-010-079
(1) Special Access:
Number Name/Location
S2101 Flight Compartment Inspection
NOTE: Remove glare shield, liners, overhead units and panels, forward galley and lavatory.
Remove/displace insulation blankets as required.
SUBTASK 53-05-03-020-001
(2) To access inspection area behind P18 panel, do this task: Inspection Access - P18 Panel,
TASK 25-11-21-210-801 up to Step 2. H.
SUBTASK 53-05-03-020-002
(3) To access inspection area behind P5 panel, do this task: Inspection Access - P5 Panel,
TASK 25-11-21-210-802 up to Step 3. H.
SUBTASK 53-05-03-210-049
(4) Do a General Visual inspection of the flight compartment, including skin panels (skins, frames,
stringers), circumferential skin and stringer splice, crew cabin window cutout structure, and
forward pressure bulkhead within the following areas: Forward side of frame at STA 259.5 and
structure 3 inches forward of STA 259.5; BL 0 + 4 inches (Left and Right); Forward and aft side
of Frame 259.5 and structure from STA 249 to STA 263 between floor and S-5L (excluding
window and window frame structure); Forward side of Frame 259.5 and structure 3 inches
forward of STA 259.5 between floor and S-3R; Structure forward of STA 203.8 to STA 178 and
from floor up to window frame; and skin, frames and stringers above P5 panel.
SUBTASK 53-05-03-910-077
(5) 737-6789 Basic Task Description, AMM Task 51-05-01-210-808.
SUBTASK 53-05-03-410-074
(6) To install the P18 panel, do this task: Inspection Access - P18 Panel, TASK 25-11-21-210-801,
Step 2. H.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-03
Page 298.96
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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