(9) Remove the lockpin assembly from the valve/regulator assembly of the
 inflation reservoir (Ref. TASK 25-62-00-081-001). 
R  (10) FOR 7506MM
 (a) Install the access panel 151KW 
R  (11) FOR 7507MM
 (a) Install the access panel 152KW.
 (12) Set the AFT CARGO COMPT light switch 8LU to the OFF position.
 (13) Remove the access platform(s).
 (14) Close the AFT cargo-compartment door (Ref. TASK 52-30-00-860-002). 

 Removal of the Rigid Control Assembly
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
21-20-00-010-001 Removal of the Air-Conditioning Distribution Ducts 24-42-00-861-001 Energize the Ground Service Network from the External
 Power
 25-21-41-000-001 Removal of the Passenger Seats
 25-23-47-000-002 Removal of the Upper Sidewall Panel Assy 241LW,

 (242LW), 241CW, (242CW) and 241FW, (242FW)
 25-23-48-000-001 Removal of the Cove Light Panels
 25-62-00-481-001 Special Precautions before Work on the Offwing

 Escape-Slide Systems
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-209, 401-499,
 25-62-43-991-002 Fig. 402
 **ON A/C 106-149, 210-299,
 25-62-43-991-002-A Fig. 402A R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 3. Job Set-up
__________
 Subtask 25-62-43-861-052

 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

R  EFF : 001-049, 051-099, 101-149, 151-199, 25-62-43Page 415 201-299, 401-499, Aug 01/05
 CES  Subtask 25-62-43-010-051

 B. Get Access
 (1)
 Do the special precaution before work on the off-wing escape-slide system (Ref. TASK 25-62-00-481-001).

 (2)
 If necessary remove the passenger seats (Ref. TASK 25-21-41-000-001) in the area of the emergency exits.

 (3)
 Remove the cove light panels 241KW (242KW) and 241GW (242GW) (Ref. TASK 25-23-48-000-001).

 (4)
 Remove the emergency-exit frame linings 241JW (242JW) and 241FW (242FW) (Ref. TASK 25-23-47-000-002).

 (5)
 Remove the air conditioning duct if necessary to get access to the rigid control assembly (Ref. TASK 21-20-00-010-001).

 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-209, 401-499,
 (Ref. Fig. 402/TASK 25-62-43-991-002)
 **ON A/C 106-149, 210-299,

 (Ref. Fig. 402A/TASK 25-62-43-991-002-A) R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-209, 401-499,
 Subtask 25-62-43-020-054
 A. Disconnect the rigid control assembly, as follows:
 (1)
 Remove and discard the cotter pin (1).

 (2)
 Remove the pin (2), the spacers and space washers (3) and disconnect the rigid control assembly (4) from the latch lever (5).

 (3)
 Remove the bracket attach bolts (6) and the nuts (7).

 (4)
 Remove and discard the cotter pins (8).

R  EFF : 001-049, 051-099, 101-149, 151-199, 25-62-43Page 416 201-299, 401-499, Aug 01/05
 CES

 Rigid Control Assembly Figure 402/TASK 25-62-43-991-002 
R  EFF : 001-049, 051-099, 101-105, 151-199, 201-209, 401-499,  25-62-43 Page 417 Aug 01/05
 CES 

 Rigid Control Assembly Figure 402A/TASK 25-62-43-991-002-A 
R  EFF :  106-149, 210-299,  25-62-43 Page 418 May 01/05
 CES 

 (5)
 Remove the pins (9), the washers (10) and the handles (11) from the rigid control assembly (4).

 (6)
 Remove the flange attach bolts (12) and the nuts (13).

 (7)
 Remove the bolts (14), the nuts (15) and the clamps (16).

 (8)
 Remove the rigid control assembly (4) from the aircraft structure.

 (9)
 Remove the old sealant from the bolts (6) and (12) and the nuts (7) and (13).

 **ON A/C 106-149, 210-299,
 Subtask 25-62-43-020-054-A
 A. Removal of the Rigid Control Assembly
 (1)
 Remove and discard the cotter pin (1).

 (2)
 Remove the pin (2), the spacers and space washers (3) and disconnect the rigid control assembly (4) from the latch lever (5).
　
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