(1) Make sure that the actuator (4) and the drive spindle are in the correct configuration.
R R NOTE : The roll pin on the drive spindle must be correctly aligned____ with the hole in the actuator driveshaft.
R (2) Put the V-band clamp (2) on the drive sub-assembly (1).
R R R R R R (3) Install the actuator (4) on the drive sub-assembly (1). Make sure that: - the actuator driveshaft engages correctly with the drive spindle slot and roll pin - the actuator housing engages correctly with the slot in the drive sub-assembly (1).
R R (4) Make sure that the actuator (4) is correctly positioned then fully tighten the V-band clamp (2).
R (5) Safety the V-band clamp (2) with MISCELLANEOUS (Material No. 19-010).
R (6) Remove the blanking cap from the electrical connector (5).
R (7) Install the electrical connector (5).
Subtask 28-26-51-410-050
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the applicable access door on the access panel: FOR 11QL - close 195AB FOR 12QL - close 196AB.
(3) Remove the access platform(s).
Subtask 28-26-51-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1QL, 2QL, 3QL.
E. Preparation For Test
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001).
(3)
On the ECAM Control Panel (CP), push (in) the FUEL pushbutton switch (P/BSW).
(4)
Make sure that the FUEL page is shown on the ECAM System Display Unit (SDU).
(5)
Refuel, defuel or transfer fuel (Ref. TASK 12-11-28-650-003) (Ref. TASK 28-25-00-650-001) (Ref. TASK 28-25-00-869-001) to get:
-between 1500 kg (3306.9330 lb) and 5500 kg (12125.4210 lb) in each wing tank
-a minimum of 1500 kg (3306.9330 lb) in the center tank.
Subtask 28-26-51-865-053
F. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FUEL/L WING TK/PUMP2 SPLY 7QA N26 121VU FUEL/L WING TK/PUMP1 SPLY 1QA N23 121VU FUEL/R WING TK/PUMP2 SPLY 8QA Q26 121VU FUEL/R WING TK/PUMP1 SPLY 2QA Q23 123VU L WING TK/PUMP 1/STBY SPLY 11QA AD12 123VU R WING TK/PUMP 1/STBY SPLY 12QA AE12
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G. Operational Test of the Fuel Control Valve Actuator(s) 11QL (12QL)
(1) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the panel 40VU: - make sure that the L and R TK PUMPS 1 and 2 P/BSWs are released (out) On the panel 40VU:- make sure that the OFF lights of theL and R TK PUMPS 1 and 2 P/BSWs areon
- make sure that the CTR TK L and CTR TK R XFR PUMP P/BSWs are released (out) - make sure that both the OFF lights ofthe CTR TK L and R XFR P/BSWs are on
- make sure that the MODE SEL P/BSW is released (out) - make sure that the MODE SEL P/BSW MANlight is on
- push (in) the L TK PUMPS 1 and 2 P/BSWs - the fault lights in the L TK PUMPS 1and 2 P/BSWs come on momentarily and then go off - when the P/BSW FAULT lights go off, the L TK PUMPS 1 and 2 OFF lights go off.
On the ECAM SDU:
- the indications for the LEFT pumps change from amber cross-line (pump not in operation) to green in-line (pump in operation).
- push (in) the CTR TK L XFR P/BSW. On the panel 40VU:- the OFF light of the CTR TK L XFR P/BSW goes off
- the fuel control valve opens.
On the ECAM SDU:
- the indication for the CTR LH pump changes from amber cross-line (pump not in operation) to green in-line (pump in operation).
1EFF : 301-399, 1 28-26-51Page 410 1 1 May 01/04 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
(pump in operation).
R 2. Let the L TK PUMPS 1 and 2 On the ECAM SDU make sure that:
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