Removal of the Cabin Floor Panels from FR12 to FR70 (Alternative Removal Procedure with the Skyflex Option)

TASK 53-00-00-000-801-A-02
Removal of the Cabin Floor Panels from FR12 to FR70 (Alternative Removal Procedure with the Skyflex Option)

NOTE: The Functional Item Numbers (FIN) for the cabin floor panels from FR12 to FR70 are given in description and operation 06-41-53-00.

ZONE: 220
ZONE: 230
ZONE: 240
ZONE: 250
ZONE: 260

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
220	FWD CAB UTILITY AREAS
230	FWD PASSENGER COMPARTMENT
240	MID PASSENGER COMPARTMENT
250	AFT PASSENGER COMPARTMENT
260	AFT CABIN UTILITY AREA

B. Referenced Information

REFERENCE	DESIGNATION
TASK 23-33-47-000-001-A	Removal of the Wall Disconnect Box (WDB)
TASK 24-42-00-861-001-A	Energize the Ground Service Network from the External Power
TASK 25-21-41-000-001-A	Removal of the Passenger Seats
TASK 25-21-61-000-001-A	Removal of the Seat-to-Seat Cables
TASK 25-22-42-000-001-A	Removal of the Free-Standing Cabin Attendant Seat (CAS)
TASK 25-22-43-000-001-A	Removal of the Cabin Attendant Swivel-Seat
TASK 25-23-45-000-002-A	Removal of the Door Frame Linings from the Right Forward Passenger/Crew Door
TASK 25-23-45-000-005-A	Removal of the Door Frame Linings from the Left Forward Passenger/Crew Door
TASK 25-26-42-000-001-A	Removal of a Partition
TASK 25-27-46-000-001-A	Removal of the Forward Doghouse
TASK 25-27-51-000-001-A	Removal of the Heated Floor Panels at the Emergency Exit Doors
TASK 25-27-51-000-002-A	Removal of the Heated Floor Panels at Door 1
TASK 25-28-41-000-001-A	Removal of the Textile Floor Covering
TASK 25-28-42-000-001-A	Removal of the Non-Textile Floor Covering (NTF)
TASK 25-28-43-000-001-A	Removal of the Moisture Barrier Foil (MYLAR)
TASK 25-30-00-00	BUFFET AND GALLEY - DESCRIPTION AND OPERATION
TASK 25-40-00-00	LAVATORIES - DESCRIPTION AND OPERATION
TASK 25-70-00-00	ACCESSORY COMPARTMENTS - DESCRIPTION AND OPERATION
Typical Installation of the Cabin Floor Panels - FR12 thru FR70 - Wet Sealant and Dry Sealant - Skyflex Option

3. Job Set-up
Subtask 53-00-00-861-052-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).

Subtask 53-00-00-010-056-A ** ON A/C NOT FOR ALL

B. Get Access
(1) If necessary, remove the passenger seats (Ref. AMM TASK 25-21-41-000-001).
(2) If necessary, remove the seat-to-seat cables (Ref. AMM TASK 25-21-61-000-001).
(3) If necessary, remove the galleys, the lavatories and/or the stowages. To do this, refer to paragraph Component Location in the applicable ATA 25 description and operation:

For the galleys (Ref. AMM D/O 25-30-00-00)
For the lavatories (Ref. AMM D/O 25-40-00-00)
For the stowages (Ref. AMM D/O 25-70-00-00).

(4) If necessary, remove the cabin attendant seats (Ref. AMM TASK 25-22-42-000-001) and/or (Ref. AMM TASK 25-22-43-000-001).
(5) If necessary, remove the partitions (Ref. AMM TASK 25-26-42-000-001).
(6) If necessary, remove the textile floor covering (Ref. AMM TASK 25-28-41-000-001).
(7) If necessary, remove the Non-Textile Floor covering (NTF) (Ref. AMM TASK 25-28-42-000-001).
(8) If necessary, remove the moisture barrier foil (Mylar) (Ref. AMM TASK 25-28-43-000-001).
(9) If necessary, remove the doghouse (Ref. AMM TASK 25-27-46-000-001).
(10) If necessary, remove the Wall Disconnect Box (WDB) (Ref. AMM TASK 23-33-47-000-001).
(11) If necessary, remove the door frame linings (Ref. AMM TASK 25-23-45-000-002) and (Ref. AMM TASK 25-23-45-000-005).

4. Procedure
Subtask 53-00-00-020-052-A ** ON A/C NOT FOR ALL

A. Removal of the Cabin Floor Panels

CAUTION: WHEN YOU REMOVE THE SCREWS, MAKE SURE THAT YOU RECORD THE CORRECT POSITION OF EACH OF THEM. THE SCREWS HAVE DIFFERENT LENGTHS.

(1) Remove the angles (1) and (8) from the left and right bottom corners of door 1, as follows:
(a) Hold the angle (1) that is attached to the structure.
(b) Remove the screws (6) and the washers (7).
(c) Remove the screws (3) and (5) and the washers (2) and (4).
(d) Remove the angle (1) from the structure.
(e) Hold the angle (8) that is attached to the structure.
(f) Remove the screw (5) and the washer (4).
(g) Remove the screws (3) and (6) and the washers (2) and (7).
(h) Remove the angle (8) from the structure.
(i) Hold the cover strip (11) that is attached to the structure.
(j) Remove the screws (9) and (10).
(k) Remove the cover strip (11) from the structure.
(2) Remove the cabin floor panels (18) (dry sealant) as follows:
(a) Remove the adhesive tape (17) from the cabin floor panels (18).
(b) Remove the screws (12) from the cabin floor panels (18).
(c) Remove the cabin floor panels (18).
(d) Put an identification label on each cabin floor panel (18) to make the installation procedure easier.
(e) Remove the damaged adhesive tape (19).
(f) Make sure that the clip nuts (15) are installed on the structure.
(3) Remove the cabin floor panels (16) (wet sealant) as follows:
(a) Remove the adhesive tape (17) from the cabin floor panels (16).
(b) Find the ends of the cords (13).
(c) Pull the cords (13) up to remove the sealant (22) from the floor panel joints.
(d) Remove the screws (12) from the cabin floor panels (16).
(e) Remove the cabin floor panels (16).
(f) Put an identification label on each cabin floor panel (16) to make the installation procedure easier.
(g) Remove the damaged adhesive tape (14) from the cabin floor panels (16).
(h) If the heated floor panels are installed, remove them (Ref. AMM TASK 25-27-51-000-001) and (Ref. AMM TASK 25-27-51-000-002).
(i) Make sure that the clip nuts (15) are installed on the structure.
(4) Remove the door-threshold floor panels (21) (wet sealant) as follows:
(a) Find the end of the cords (13).
(b) Pull the cords (13) up to remove the sealant (22) from the floor panel joints.
(c) Remove the screws (12) from the door-threshold floor panels (21).
(d) Remove the door-threshold floor panels (21).
(e) Remove the damaged adhesive tape (14) from the door-threshold floor panels (21).
(f) If the heated floor panels are installed, remove them (Ref. AMM TASK 25-27-51-000-001) and (Ref. AMM TASK 25-27-51-000-002).
(g) Make sure that the clip nuts (15) are installed on the structure.

[Rev.10 from 2021] 2026.04.01 01:49:39 UTC