2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific access platform 3 m (9 ft. 10 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026  GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 1EFF : ALL 1 28-42-43Page A443 1 1 Feb 01/05 1 1 1CES 1 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-42-00-740-001 Status Report (BITE)
 28-46-00-740-001 Functional (BITE) Test

 **ON A/C 001-049, 051-061, 101-105, 201-203, 301-399,
 28-42-43-991-026-A Fig. 420
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Post SB 28-1087 For A/C 001-049,051-061,101-105,201-203, 28-42-43-991-026 Fig. 420A **ON A/C ALL
 3. Job Set-up
__________
 **ON A/C 001-049, 051-061, 101-105, 201-203, 301-399,

 (Ref. Fig. 420/TASK 28-42-43-991-026-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Post SB 28-1087 For A/C 001-049,051-061,101-105,201-203, (Ref. Fig. 420A/TASK 28-42-43-991-026) **ON A/C ALL
 Subtask 28-42-43-941-066
 A. Safety Precautions
 (1) Make sure that the safety barriers are in position.
 1EFF : ALL 1 28-42-43Page A444 1 1 Aug 01/05 1 1 1CES 1 Subtask 28-42-43-860-056

 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the access platform is below the applicable wing trailing edge at the false rear spar, zone 574(674).

 (2)
 Make sure that the applicable access panel is open:

 -
for the left wing, open 574BB

 -
for the right wing, open 674BB.

 Subtask 28-42-43-865-072
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHANNEL/1 AND 2 8QT L26 121VU FUEL/HI/LVL/SPLY 1QJ L25 121VU FUEL/FQI/CHAN/2 2QT M27
 4. Procedure
_________
 Subtask 28-42-43-420-099
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (2)
 Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 1EFF : ALL 1 28-42-43Page A445 1 1 Feb 01/05 1 1 1CES 1 **ON A/C 001-049, 051-061, 101-105, 201-203, 301-399,

 Subtask 28-42-43-420-100-A
 B. Installation of the Shorting Plug Connectors
 (1)
 Remove the blanking caps from the electrical connectors.

 (2)
 Install the shorting plug connectors (1) on the harness connectors (5).

 (3) Attach the lanyards (2) to the support bracket with the screws (3) and the nuts (4). R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Post SB 28-1087 For A/C 001-049,051-061,101-105,201-203,
 Subtask 28-42-43-420-100

 B. Installation of the Fused Plug Connectors
 (1)
 Remove the blanking caps from the electrical connectors.

 (2)
 Install the fused plug connectors (1) on the harness connectors (5).

 (3)
 Attach the lanyards (2) to the support bracket with the screws (3) and the nuts (4).

 **ON A/C ALL
 Subtask 28-42-43-865-073
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1QJ, 1QT, 2QT, 8QT.
 1EFF : ALL 1 28-42-43Page A446 1 1 Aug 01/05 1 1 1CES 1 Subtask 28-42-43-740-058

 D. Test
 (1)
 Do a status report (BITE) of the fuel-quantity indicating system (Ref. TASK 28-42-00-740-001).

 (2)
 Do a functional (BITE) test of the fuel-tank level-sensing system (Ref. TASK 28-46-00-740-001).
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUEL 燃油6(17)