(69)
 Push and hold the MEM READ button.

 S 985-080
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757 MAINTENANCE MANUAL
 S 985-081
 (70)
 Release the LOC TEST button. S 985-082

 (71)
 Release the MEM READ button. S 285-083

 (72)
 Make sure code 97 is shown. NOTE: Code 97 displays for 1 minute.

____
 S 985-038
 (73) Push and release the MEM CLR button while code 96 is shown. NOTE: If step 3.C.(71) is missed do the procedure again from
____
 3.C.(63) to 3.C.(70).

 S 285-039
 (74)
 Make sure code 25 or 75 is shown. S 985-040

 (75)
 Push and release the MEM CLR button. S 285-041

 (76)
 Make sure the display is blank. S 985-042

 (77)
 Push and release the MEM READ button. S 285-043

 (78)
 Make sure code 25 or 75 is shown. S 985-044

 (79)
 Push and release the MEM CLR button.

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 S 285-045
 (80)
 Make sure the display is blank.

 S 985-046

 (81)
 Push and release the MEM READ button.

 S 285-047

 (82)
 Make sure code 97 is shown.

 S 985-048

 (83)
 Push and release the MEM READ button.

 S 285-049

 (84)
 Make sure the display is blank.

 S 865-040

 (85)
 Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P6 panel.

 (a)
6C1 L FUEL COND CONT

 (b)
6C2 R FUEL COND CONT

 E. Put the airplane back to its initial condition.
 S 865-050
 (1)
Close the cover on the electrical system card file, P50.

 (2)
Remove electrical power if it is not necessary (AMM 24-22-00/201).

 S 865-015
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 DUCT LEAK DETECTOR - REMOVAL/INSTALLATION
_________________________________________
 1.  General (Fig. 401)_______
 A.  Duct leak detectors are installed next to the pneumatic air ducts in the wings and in the fuselage.
 B.  The removal/installation procedure is the same for all units except for access to the units.
 TASK 26-18-01-024-031
 2.  Remove Duct Leak Detector_________________________
 A.  Equipment
 (1)  
Main Gear Door Locks (AMM 32-00-15/201)

 (2)  
Caps to fit 35303-64 connectors

 (3)  
Bonding Meter, AVTRON T477W

 B.  References
 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 06-42-00/201, Empennage Access Doors and Panels

 (3)  
AMM 06-44-00/201, Wing Access Doors and Panels

 (4)  
AMM 25-50-02/401, Cargo Compartment Sidewall Panels

 (5)  
AMM 32-00-15/201, Landing Gear Door Locks

 (6)  
AMM 32-00-20/201, Landing Gear Downlocks

 C.  Access
 (1)  Location Zones
 133/134 Wing Center Section (Left and Right)
 310 Fuselage Body Section 48
 500/600 Wing (Left and Right)
 730/740 Main Landing Gear Wheel Well

 D.  Prepare for Removal of the Wing Detectors (Fig. 402)
　
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