Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
Material No. 19-002 USA MIL-T-713
SYNTHETIC FIBRE CORD (NYLON) 2.5MM DIA.
(Ref. 20-31-00)
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CES C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
11-00-00-400-007 20-21-11-911-001 24-42-00-861-001 Installation of the ESSO (Scotchcal Labels)Tightening Torques for Standard Threaded FastenersEnergize the Ground Service Network from the External Power
24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power
25-21-41-000-001 25-25-11-000-001 25-25-11-400-001 25-26-41-000-013 Removal of the Passenger SeatsRemoval of the Filler Panel(s) of the Passenger Service/Information Unit(s) (PSIU)Installation of the Filler Panel(s) of the Passenger Service/Information Unit(s) (PSIU)Removal of the Curtains
25-26-41-400-013 Installation of the Curtains
25-27-46-000-001 25-27-46-400-001 Removal of a DoghouseInstallation of a Doghouse
AMM 11-32-25 P.Block 001 INTERIOR PLACARDS (SEE ALSO 11-42-25) R **ON A/C 001-049, 101-105, 151-199,
25-26-42-991-005-A Fig. 401
**ON A/C 201-210,
25-26-42-991-005 Fig. 401A
**ON A/C 301-399,
25-26-42-991-005-B Fig. 401B
R EFF : 001-049, 101-105, 151-199, 201-210, 25-26-42Page 411 301-399, May 01/05
CES
R **ON A/C 001-049, 101-105, 151-199, 201-210, 301-399,
3. Job Set-up
__________ R **ON A/C 001-049, 101-105, 151-199, 201-210,
Subtask 25-26-42-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(2)
Make sure that the curtain from the Center Class Divider is removed (Ref. TASK 25-26-41-000-013).
**ON A/C 301-399,
Subtask 25-26-42-860-051-A
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(2)
Make sure that the curtain from the center class divider is removed (Ref. TASK 25-26-41-000-013).
(3)
Make sure that the passenger/information units (PSIU) are open (Ref. TASK 25-25-11-000-001).
(4)
Make sure that the seat-row forward of the partition is removed (Ref. TASK 25-21-41-000-001).
(5)
Make sure that the doghouse(s) is/are removed (Ref. TASK 25-27-46-000-001).
R EFF : 001-049, 101-105, 151-199, 201-210, 25-26-42Page 412 301-399, May 01/05
CES CES
R **ON A/C 001-049, 101-105, 151-199, 201-210, 301-399,
R 4. Procedure_________ **ON A/C 001-049, 101-105, 151-199,
(Ref. Fig. 401/TASK 25-26-42-991-005-A) **ON A/C 201-210,
(Ref. Fig. 401A/TASK 25-26-42-991-005) **ON A/C 301-399,
R (Ref. Fig. 401B/TASK 25-26-42-991-005-B) **ON A/C 001-049, 101-105, 151-199, 301-399,
Subtask 25-26-42-210-057-A
A. Preparation for Installation (1) Clean the component interface and/or the adjacent area. (2) Do an inspection of the component interface and/or the adjacent area. (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
R **ON A/C 001-049, 101-105, 151-199,
Subtask 25-26-42-420-054-A
B. Installation of the Partition. (Ref. Fig. 401/TASK 25-26-42-991-005-A) NOTE : Unless specified, TORQUE all nuts, bolts and screws (Ref. TASK 20-____ 21-11-911-001). NOTE : The installation for the left and/or right partition is the same.____
(1)
Install the partition:
(a)
Put the seat track fittings (4) in position as recorded in the removal procedure.
(b)
Put the shim plates (3) in position as recorded in the removal procedure.
(c)
Put the partition in (1) position. 1 Make sure that the partition is in a vertical position.
_
(d)
Lift the pins (8) together with the upper attachment tubes (7) up into the upper attachment panel (11).
(e)
Turn the pins (8) into the partition (1) until they engage.
(f)
Install the screws (2).
(g)
Install the cover plate (9) and the screws (10).
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