TAILCONE - REMOVAL/INSTALLATION
1. General
A. This procedure contains these tasks:
(1) Tailcone Removal
(2) Tailcone Installation
TASK 53-53-00-000-801
2. Tailcone Removal
A. General
(1) A power-off flight test may be necessary after the installation of the component. Check the
requirements in the “General” section at the beginning of the Elevator Power-Off Flight - Test,
TASK 27-31-00-710-803.
B. References
Reference Title
27-21-17-000-801 Rudder Index Plate Removal (P/B 401)
27-31-00-710-803 Elevator Power-Off Flight - Test (P/B 501)
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (P/B 201)
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-11-000-801 Elevator - Removal (P/B 401)
27-31-81-000-801 Elevator Index Plate Removal (P/B 401)
27-41-11-000-801 Horizontal Stabilizer - Removal (P/B 401)
49-91-71-000-801 Eductor Inlet Duct Removal (P/B 401)
55-10-11-000-801 Balance Bay Panels Removal (P/B 401)
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.
Reference Description
SPL-1672 Assembly - Lock, Stabilizer Trim
737-600, -700, -800
Part #: F71336-501 Supplier: 81205
D. Location Zones
Zone Area
315 APU Compartment - Left
316 APU Compartment - Right
E. Access Panels
Number Name/Location
318BR Tailcone Access Door
333AB Horizontal Stabilizer, Gap Cover, Horizontal Stabilizer to Body
333AT Horizontal Stabilizer, Gap Cover, Horizontal Stabilizer to Body
333AZ Horizontal Stabilizer, Access Panel, Inboard T.E. Closure Rib
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-53-00
Page 401
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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