(5)
Remove the seat. Move the seat out of the cockpit.
(6)
Install the armrest (1) on the seat. Install the bolts (7) and TORQUE the bolts to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).
EFF : ALL
25-11-51Page 405
May 01/05
R
CES
TASK 25-11-51-400-001
Installation of the Captain/First Officer Seat (3MS, 4MS)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 16-007 COATING ELASTOMERIC, ULTRA LOW GLOSS (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
25-11-51-991-001-A Fig. 401
25-11-51-991-002-A Fig. 402
EFF : ALL
25-11-51Page 406
3. Job Set-up
__________
Subtask 25-11-51-010-051
A. Aircraft Maintenance Configuration
(1) Make sure that the access platform is near the access door 811 of the avionics compartment.
(2) Make sure that the access door 811 is open.
Subtask 25-11-51-865-054
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 3MS
122VU COCKPIT SEATS/SEAT CTL/CAPT 1MS1 U11 122VU LIGHTING/FLOOD/CAPT/SIDE 5LE Z05
FOR 4MS 122VU COCKPIT SEATS/SEAT CTL/F/O 1MS2 U14 122VU LIGHTING/FLOOD/F/O/SIDE 4LE Z06
4. Procedure
_________
(Ref. Fig. 401/TASK 25-11-51-991-001-A, 402/TASK 25-11-51-991-002-A)
Subtask 25-11-51-420-051
A. Installation of the Seat NOTE : It is necessary to remove the armrest on the side stick side to
____
enable passage of the seat in the cockpit.
(1) Remove the bolts (7). Remove the armrest (1) from the seat. R NOTE : Make sure the seat is in the stowed position before you remove
____ R the bolts (7).
(2)
Put the seat on the floor.
(3)
Install the washers (4) and the bolts (3) and tighten them.
(4)
Install the armrest (1) on the seat. Install the bolts (7) and TORQUE the bolts to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in)
(5)
Paint the bolts (3) with STRUCTURE PAINTS (Material No. 16-007).
(6)
Remove the blanking caps from the connectors (5) and (6).
EFF : ALL
25-11-51Page 407
(7) Connect the electrical connector (5) to the electrical connector (6).
Subtask 25-11-51-865-055
R R R R R B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 3MS 1MS1, 5LE FOR 4MS 1MS2, 4LE.
Subtask 25-11-51-861-051
C. Energize the aircraft electrical circuits. (Ref. TASK 24-41-00-861-002)
Subtask 25-11-51-710-050
D. Operational Test of the Seat
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the right side (left side) of
the seat pan.
- Set the control switch S2 to - the seat moves forward.
forward.
- Release the control switch S2. - the seat stays locked in this
position.
- Set the control switch S1 to - the seat moves up.
up.
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