Passenger Compartment Floor Panels Figure 405/TASK 32-33-16-991-008
1EFF : 1 1R 1CES ALL 1 11 1 32-33-16 Page 422 Feb 01/03
(7)
Remove these passenger-compartment floor-panels as necessary (Ref. TASK 53-32-12-000-002):
-242BF, 241EF, 241FF, 242FF, 242GF, 242JF
-241KF, 242KF, 241LF, 242LF, 241MF, 242MF.
(8)
Remove the cockpit floor panels 212GF, 212NF (Ref. TASK 53-12-11-000-001).
(9)
Remove the forward fuselage floor panels 222CF, 222EF, 232DF (Ref. TASK 53-12-12-000-001).
R **ON A/C 151-199, 401-499,
Subtask 32-33-16-010-051-A
B. Get Access (Ref. Fig. 401/TASK 32-33-16-991-006, 402/TASK 32-33-16-991-001, 404A/TASK 32-33-16-991-007-A, 405/TASK 32-33-16-991-008)
(1)
Open the main gear doors (Ref. TASK 32-12-00-010-001).
(2)
Make sure that the GROUND LOCK SLEEVE (460005835) is on the applicable main gear door actuator.
(3)
Open the lateral avionics-compartment doors 822, 824 (Ref. TASK 52-41-00-010-002).
(4)
Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-001).
(5)
Remove the forward cargo-compartment ceiling-panels 131MC, 131NC.
(6)
Remove the forward cargo-compartment rear-partition 132PW.
(7)
Remove these cabin floor-panels as necessary (Ref. TASK 53-32-12-000-002):
-242BF, 241EF, 241FF, 242FF, 242GF, 241JF
-241KF, 242KF, 241LF, 242LF, 241MF, 242MF.
(8)
Remove the cockpit floor panels 212GF, 212NF (Ref. TASK 53-12-11-000-001).
(9)
Remove the cabin floor-panels 222CF, 222EF, 232DF (Ref. TASK 53-12-12-000-001).
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Subtask 32-33-16-869-054
C. Flight Configuration Precautions
(1)
If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2)
If the electrical power is necessary, do the precautions for flight configuration (Ref. TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
Subtask 32-33-16-865-053
D. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
Subtask 32-33-16-480-051
E. Installation of the Rigging Pins
(1)
For the cables (13), (15), (25) and (27): (Ref. Fig. 402/TASK 32-33-16-991-001, 406/TASK 32-33-16-991-003)
-
put a RIGGING PIN (98A27801001000) in the position Pin 1
-
put a RIGGING PIN (98DNSA20208150) in the position Pin 2.
(2)
For the cables (37), (38), (39) and (40): (Ref. Fig. 402/TASK 32-33-16-991-001, 407/TASK 32-33-16-991-004, 408/TASK 32-33-16-991-005, 409/TASK 32-33-16-991-009)
-
put a RIGGING PIN (98DNSA20208150) in the position Pin 2
-
put a RIGGING PIN (98DNSA20208060) in the applicable position Pin
3.
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Free-fall Extension Cables - MLG (FR 7 to FR 41) Figure 406/TASK 32-33-16-991-003
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Free-fall Extension Cables - MLG (FR 41 to FR 43) Figure 407/TASK 32-33-16-991-004
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Free-fall Extension Cables - MLG (FR 41 to FR 43) Figure 408/TASK 32-33-16-991-005
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Free-Fall Extension Cables - MLG (FR41 to FR43) Figure 409/TASK 32-33-16-991-009
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4. Procedure
_________ Subtask 32-33-16-020-051
A. Removal of the MLG Free-Fall Extension Cables (13) and/or (15)
(Ref. Fig. 406/TASK 32-33-16-991-003)
(1)
Remove these items as necessary:
-
the cotter pins (8) and (11)
-
the washers (9) and (12)
-
the tubes (7) and (10).
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