C
OMPONENT
M
AINTENANCE
M
ANUAL
S
OAP
D
ISPENSERS
S
EIFENSPENDER
B82X
S
ERIES
No.: 25-40-01
Issue: D
Date: May 02/2022
25-40-01
May 02/2022
(5) If placard has been removed stick new placard onto cover.
NOTE:
No further assembly is recommendable because the unit can
not be installed into the aircraft as a complete assembled
unit.
D.
Assembly of B823 version (Ref. IPL, Fig. 1E to 1H and 2A)
(1)
Install PVC-tube (1-20) with cable tie (1-30) to piston assy
(1-10).
(2)
Attach assembled piston (1-10) with PVC-tube to the shank assy
(1-40).
(3)
Secure piston assy onto shank by turning cover (2-60)
clockwise until it stops.
(4)
Install tube (1-70) with clamps (1-60).
(5)
Install adapter (1-50) to container (1-80).
(6)
If placard has been removed stick new placard onto cover.
NOTE:
No further assembly is recommendable because the
unit can not be installed into aircraft as a
complete
assembled
unit.
E.
Assembly of B825 version (Ref. IPL, Fig. 1J to 1K and 2A)
See B828 version.
F.
Assembly of B828 version (Ref. IPL, Fig. 1J to 1K and 2A)
(1)
Install PVC-tube (1-20) with cable tie (1-30) to piston assy
(1-10).
(2)
Attach assembled piston (1-10) with PVC-tube to the shank assy
(1-40).
(3)
Secure piston assy onto shank by turning cover (2-60)
clockwise until it stops.
(4)
Install tube (1-80) with clamps (1-50) to shank assy (1-40).
(5)
Install flexible metal pipe (1-100) with sleeves (1-90).
(6)
Install tube assy (1-80) with clamp (1-50) to container
(1-60).
(7)
If placard has been removed stick new placard onto cover.
NOTE:
No further assembly is recommendable because the
unit can not be installed into aircraft as a
complete
assembled
unit.
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