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时间:2011-03-27 12:57来源:蓝天飞行翻译 作者:航空
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R to the hydraulic pressure caution switch.

R (54) At station 158, attach the ground wires to the ground studs with the
R nuts (60), lockwashers (65) and washers (70).
R (Ref. Fig. 414/TASK 71-51-43-991-308)
R WIRE GROUND
R
R GD9951DC/1 GD9951DC
R GD9951DC/2 GD9951DC
R GD9952DC/1 GD9952DC
R GD9952DC/2 GD9952DC
R GD9953DC/1 GD9953DC
R GD9953DC/2 GD9953DC
R GD9954DC/1 GD9954DC
R GD9954DC/2 GD9954DC
R GD9955DC GD9955DC
R GD9956DC GD9956DC
R GD9957DC GD9957DC

R NOTE : Make sure that the electrical resistance, from each ground

____ R wire to the terminal stud, is not more than 0.0025 ohms.
R (55) Put the harness (5) in the flip-lock clamp (33) and tighten the R captive screw.
R (56) Connect the electrical connector 4007EN-A to the oil chip detector. R (Ref. Fig. 415/TASK 71-51-43-991-309)
R (57) Connect the electrical connector 4002EN-A to the oil quantity R transmitter.
R (58) Put the harness (5) into the rubber supports for line blocks (40) and R (55).
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R  (59) Put the rubber supports in the line blocks (40) and (55) that attach 
R  the harness (5) to the brackets at stations 191 and 199. Close the 
R  line blocks and tighten the captive bolts. 
R  (60) Install the bolt, clamps and anti-rotation lug (49) that attach the 
R  harness (5) to the bracket at station 199. 
R  (61) Put the clamp (80) on the harness (5). Attach the clamp (80) to the 
R  bracket at station 199 with the bolt (75). 
R  (62) TORQUE the bolt (75) to between 20 and 25 lbf.in (0.22 and 0.28
 m.daN). 
R  (63) Connect the electrical connector 4000KC-A to the high pressure fuel 
R  shutoff. 
R  (64) Put the harness (5) into the rubber supports for line blocks (50) and 
R  (55) along station 158. 
R  (65) Make sure that the harness (5) is correctly installed on the engine. 
R  (66) Put the rubber supports in the line blocks (50) and (55) along 
R  station 158. Close the line blocks and tighten the captive bolts. 
R  (67) Install the bolt, clamps and anti-rotation lug (58) that attach the 
R  harness (5) to the bracket at station 158. 
R  (68) Install the bolt and clamp (107) that attach the harness (5) to the 
R  bracket at station 158. 
R  (69) TORQUE the bolts (17), (22), (32), (42), (43), (47), (49), (57), (58) 
R  and (107) to between 25 and 30 lbf.in (0.28 and 0.33 m.daN). 

R  END SPIB NO. CFM02255MW1 

R  (70) Put the clamp (100) on the harness (5). Attach the clamp (80) to the
 bracket on station 158 with the bolt (95). 
R  (71) TORQUE the bolt (95) to between 20 and 25 lbf.in (0.22 and 0.28
 m.daN). 
R  (72) Put the clamp (80) on the harness (5). Attach the clamp (80) to the 
R  bracket on the gearbox with the bolt (75) and the nut (85). 
R  (73) TORQUE the nut (85) to between 20 and 25 lbf.in (0.22 and 0.28
 m.daN).

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R  (74) Connect the electrical connector 4004EN-A to the oil temperature sensor. 
R  (75) Connect the electrical connector 4001EN-A to the oil differential pressure switch. 
R  (76) Connect the electrical connector 1030GK-A or 3030GD-A, as applicable, to the hydraulic pump bypass valve. 
R R  (77) Examine the harness installation and make sure that the flip-lock clamps, the line blocks and the clamps are installed correctly.
 Subtask 71-51-43-865-082
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3DA1, 3DA2, 3DA3, 4DA1, 4DA2, 4DA3, 5DA1, 5DA2, 5DA3, 1DB1, 1DB2, 4DG1, 4DG2, 1JH, 3801GX, 3802GX, 3803GX, 7TU, 2RK, 4RK FOR 1000EM1 2KS1, 4KS1, 2JH1, 3JH1, 1WE1, 2WE1, 7WD1, 8WD1, 2XU1 FOR 1000EM2 2KS2, 4KS2, 2JH2, 3JH2, 1WE2, 2WE2, 7WD2, 8WD2, 2XU2
 Subtask 71-51-43-861-057
 C. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)
 Subtask 71-51-43-860-078
 D. Do the EIS start procedure (for the lower display of the ECAM system only). (Ref. TASK 31-60-00-860-001).
 
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