-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Material No. 05-002 Material No. 05-027
Material No. 09-005 Material No. 09-016
Material No. 11-016 Material No. 16-003
C. Expendable Parts
lockwire, corrosion-resistant steel dia 0.6 mm
(0.2362 in.)
USA MIL-P-8116
PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
USA MIL-L-81309
RUST INHIBITOR(FOR CORROSION USE 15-004)
(Ref. 20-31-00)
USA MIL-S-81733 CLASS C
CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
USA BOEING BAC 5000 BAC 5504 BAC 5750
CLEANING SOLVENT (Ref. 20-31-00)
F ASNB70720
COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
tab washer 52-33-32 03 -150
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-006 Open the Bulk Cargo-Compartment Door
52-30-00-860-008 Close the Bulk Cargo-Compartment Door
52-30-00-860-010 Open the Deactivated Bulk Cargo-Compartment Door
52-30-00-860-011 Close the Deactivated Bulk Cargo-Compartment Door
52-33-11-820-001 Adjustment of the Bulk Cargo-Compartment Door
52-71-00-710-001 Operational Test of the Door Warning System
53-22-14-000-001 Removal of the FWD Cargo-Compartment Floor-Panels
53-22-14-400-001 Installation of the FWD Cargo-Compartment
Floor-Panels
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-32Page 407 1224-224, 228-228, 1May 01/05 1 1 1CES 1
3. Job Set-up
__________ R **ON A/C 001-049, 051-099, 101-105,
Subtask 52-33-32-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position below the Bulk cargo-compartment door (referred to as Bulk door).
(2)
Make sure that the Bulk door is opened (Ref. TASK 52-30-00-860-006).
(3)
Make sure that the quick-release fasteners are released and the sidewall panels 162BW and 162EW are removed.
(4)
Make sure that the protection cover (20) together with the plate (39) and the gasket (40) are removed from the floor panel 162KF.
(5)
Make sure that the floor panels 162HF, 162GF, 162KF and 162LF are removed (Ref. TASK 53-22-14-000-001).
(6)
If necessary, disengage the disc fasteners and the VELCRO tapes to remove the insulation mats adjacent the bulk door frame.
R **ON A/C 106-149, 221-221, 224-224, 228-228,
Subtask 52-33-32-860-051-A
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position below the Bulk cargo-compartment door (referred to as Bulk door).
(2)
Make sure that the Bulk door is opened (Ref. TASK 52-30-00-860-010).
(3)
Make sure that the quick-release fasteners are released and the sidewall panels 162BW and 162EW are removed.
(4)
Make sure that the protection cover (20) together with the plate (39) and the gasket (40) are removed from the floor panel 162KF.
(5)
Make sure that the floor panels 162HF, 162GF, 162KF and 162LF are removed (Ref. TASK 53-22-14-000-001).
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-32Page 408 1224-224, 228-228, 1May 01/05 1 1 1CES 1
(6) If necessary, disengage the disc fasteners and the VELCRO tapes to remove the insulation mats adjacent the bulk door frame.
R **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
Subtask 52-33-32-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU EIS/SDAC1 AND 2/DOOR/DET/AVNCS 46WV P02
4. Procedure
_________
Subtask 52-33-32-910-052
A. Preparation for Installation
(1)
Make sure that the parts retained from the removed component are clean and in the correct condition.
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