(b) Engage the T5 sensor probe (10) in the recess of turbine frame boss. Install the bolts (110) and nuts (100). Tighten the nuts by hand.
(c) Lubricate the threads of the bolts (20, 60) with graphite grease (Material No. CP2101).
(d) Attach the T5 sensor (10) to the bracket (40) at flange T with the clamp (30), the bolt (20) and the nut (50). Tighten the nut by hand.
(e) Attach the T5 sensor (10) to the bracket (80) at flange S with the clamp (70), the bolt (60) and the nut (90). Tighten the nut by hand.
(f) Lubricate the threads of bolts (150) with graphite grease (Material No. CP2101)
(g) Attach the bracket (170) and the T5 sensor (10) assembly to the bracket (140), at flange R, with the bolts (150) and the nuts (130). Tighten the nuts by hand.
(h) Make sure the T5 sensor rigid lead is installed stress-free on the engine and, from rear to front:
- TORQUE nuts (100) to between 95 and 110 lbf.in (1.07 and 1.24 m.daN)
- TORQUE nuts (50, 90) to between 50 and 55 lbf.in (0.56 and 0.62 m.daN)
- TORQUE nuts (130) to between 95 and 110 lbf.in (1.07 and 1.24 m.daN).
(i) Connect the CJ13 harness connector to the T5 sensor connector.
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(j) TORQUE the coupling nut of CJ13 harness connector to between 150 and 160 lbf.in (1.69 and 1.80 m.daN). Safety the coupling nut with a lockwire 0.6 mm (0.0236 in.) dia. (Material No. CP8004) or lockwire 0.6 mm (0.0236 in.) dia. (Material No. CP8005).
Subtask 77-22-10-861-051
B. Energize the aircraft electrical circuits. (Ref. TASK 24-41-00-861-002).
Subtask 77-22-10-410-054
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the thrust reverser cowl doors: (Ref. TASK 78-36-00-410-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
(3) Remove the warning notice(s).
Subtask 77-22-10-440-051
D. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
Subtask 77-22-10-869-054
E. On the panel 50VU, make sure that the OFF legend of the FADEC GND PWR1(2) pushbutton switch is off.
Subtask 77-22-10-710-051
F. Do an operational test on the FADEC on the ground (with Engine Non Motoring) (Ref. TASK 73-29-00-710-040).
Subtask 77-22-10-869-055
G. Do the EIS start procedure (upper ECAM DU only) (Ref. TASK 31-60-00-860-001).
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H. Operational Test:
(1) On the left or right MCDU, get the SYSTEM REPORT/TEST page (Ref. TASK 31-32-00-860-012).
(2) Push the line key adjacent to the FADEC 1A(1B) for engine 1.
(3) Push the line key adjacent to the FADEC 2A(2B) for engine 2.
(4) Make sure that the message "T5 SENS, J13, ECU" is not in view. Subtask 77-22-10-860-051
J. Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
5. Close-up
________ Subtask 77-22-10-862-051
A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 77-22-10-410-055
B. Close the fan cowl doors: (Ref. TASK 71-13-00-410-040)
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
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T5 THERMOCOUPLE - INSPECTION/CHECK
__________________________________
TASK 77-22-10-210-002
Visual Inspection of the T5 Sensor
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific bristle brush No specific warning notice No specific access platform 1 m (3 ft. 3 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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