D. Check Electrical bonding.
(1) Measure the resistance value (Ohmic) (Ref. TASK 20-28-00-720-005). Make sure that the resistance between the engine and the pylon is not more than 1.5 milliohms.
R Subtask 71-00-00-820-071
R E. Do the adjustment of the LH or RH thrust reverser "J" ring (Ref. TASK 78-R 36-42-820-002). R Subtask 71-00-00-820-072 R F. Do the adjustment of the thrust reverser half door latches (Ref. TASK 78-
R 36-41-820-042). Subtask 71-00-00-440-068 R G. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
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Subtask 71-00-00-612-052
R H. Do a check of the oil levels
(1) Make sure that the IDG oil level is correct (Ref. TASK 24-21-00-210-046).
(2) Make sure that the starter oil level is correct.
(3) Make sure that the oil tank level is correct (Ref. TASK 12-13-79-610-002).
Subtask 71-00-00-614-051
R J. Pressurize the aircraft hydraulic systems FOR 1000EM1 Pressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-002). FOR 1000EM2 Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-002).
Subtask 71-00-00-942-057
R K. Remove the access platform(s).
Subtask 71-00-00-410-096
R L. Close the thrust reverser cowl doors : (Ref. TASK 78-36-00-410-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
Subtask 71-00-00-865-090
R M. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1DA1, 1DA2, 2DA1, 2DA2, 2DA3, 3DA1, 3DA2, 3DA3, 4DA1, 4DA2, 4DA3, 5DA1, 5DA2, 5DA3, 1DB1, 4DG1, 4DG2, 1JH, 1WE1, 2WE1, 1WE2, 2WE2, 7TU, 2RK, 4RK FOR 1000EM1 2KS1, 4KS1, 2JH1, 3JH1, 7WD1, 8WD1, 2XU1, 1DN1 FOR 1000EM2 2KS2, 4KS2, 2JH2, 3JH2, 7WD2, 8WD2, 2XU2, 1DN2, 3801GX, 3802GX, 3803GX
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Subtask 71-00-00-942-058
R N. Put the aircraft back to its initial configuration.
(1) Remove the warning notice(s).
(2) On the panel 114VU remove the locking tool from the flap and slat control lever. Subtask 71-00-00-861-074 R P. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). Subtask 71-00-00-869-187 R Q. Do the EIS start procedure (upper and lower ECAM DU's only) (Ref. TASK 31-60-00-860-001). Subtask 71-00-00-740-053 R R. Enter the engine hours and cycles data into the DMU for the installed engine (Ref. TASK 31-36-00-740-005).
Subtask 71-00-00-720-054 R S. Do the tests
(1) On the left or right MCDU, do this check:
(a) Get access to the screen of the SYSTEM REPORT/TEST ENG (Ref. TASK 31-32-00-860-012)
(b) Push the line key adjacent to the FADEC 1(2) A(B): The ENGINE MAIN MENU page comes into view.
(c) Do a functional test of the ECU (Ref. TASK 73-21-60-720-040).
(d) Read the LRU IDENTIFICATION Report of the engine 1(2) (Ref. TASK 73-21-60-740-006).
NOTE : The LRU identification check is only required on one
____ channel of the ECU A or B.
1 Push the line key adjacent to the LRU IDENT indication:
_ CHANNEL A(B) page comes into view.
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_ consistency with the actual engine configuration:
a Engine thrust rating and type:
_ - These inputs are available on the engine name plate. NOTE : The engine thrust rating must be the same as on
____ opposite engine and consistent with the Aircraft Model.
b "LRU PART NO" (ECU Part Number):
_
- The P/N is available on the ECU identification plate. c "N1 TRIM":
_
- The N1 trim level (0 through 7) is available on the engine name plate.
d "BUMP" option: must read "N".
_
e If "OVERBOOST" is displayed on the screen: must read "N".
_
f "PMUX" option:
_
- PMUX engine (4 hoses connected to the ECU) must read "Y"
- Non PMUX engine (2 hoses connected to the ECU) must read "N".
g If "CONFIG" is displayed on the screen:
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本文链接地址：A320飞机维护手册 AMM 动力装置 POWER PLANT 1(30)
