A. Removal of the Check Valve R WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
_______ R - FLUSH IT AWAY WITH CLEAN WATER R - GET MEDICAL AID.
CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT
_______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER.
FOR 2170GM
(1)
Disconnect the coupling nuts (3) and (5) and remove the pipe (4).
(2)
Remove the check valve (2) from the coupling nut (1). FOR 2405GM
(3)
Cut, remove and discard the tie-wrap (6) then remove the support plug (7).
(4)
Remove the nuts (8), the spring washers (9), the sleeves (10), the bolts (12) and the clamp (11).
(5)
Disconnect the coupling nuts (3) and (5) and remove the pipe (4).
(6)
Remove the check valve (2) from the coupling nut (1).
(7)
For 2170GM and 2405GM:
(a)
Remove the container and correctly dispose of the hydraulic fluid.
(b)
Put blanking plugs on the disconnected line ends.
(c)
Remove the container and correctly dispose of the hydraulic fluid.
1EFF : ALL 1 29-12-37Page 416 1 1 Aug 01/02R 1 1 1CES 1
TASK 29-12-37-400-002
Installation of the Check Valve 2170GM(2405GM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice
No specific access platform 4 m (13 ft. 1 in.)
No specific container 5 l (1.3208 USgal)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 02-003 F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
FOR FIN 2405GMtie-cable 29-15-05 38A-010
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-009
27-51-00-710-001
27-60-00-866-002
27-80-00-866-005
29-00-00-864-001
29-00-00-910-002
29-10-00-863-003
29-10-00-864-003
29-14-00-614-001
R 57-51-37-000-004
R
R
29-12-37-991-002
R FOR FIN 2170GM
R 57-51-37-400-004
R
R
R FOR FIN 2405GM
R 57-51-37-400-004
R
R
Retraction of the Flaps on the GroundOperational Test of the Wing Tip Brake and the Pressure Off BrakeExtension-Retraction of the Spoilers for MaintenanceRetracting the Slats on the GroundPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionSafety Procedures of the Hydraulic SystemPressurize the Blue Hydraulic System with a Ground Power SupplyDepressurize the Blue Hydraulic SystemDepressurization of the Hydraulic Reservoirs Removal of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)Fig. 402
Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
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