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 (b)  11B21, FIRE DETECTION L ENGINE 2
 S 845-140
 (6)  AIRPLANES WITH ROLLS ROYCE ENGINES AND SYSTRON-DONNER FIRE DETECTORS; Return the detectors to the normal configuration.
 (a)  
Remove the jumper wire from pins A and D on electrical connectors D1406 and D1408.

 (b)  
Connect electrical connectors, D1406 and D1408, to the engine fire detectors, TS5037 and TS5036.

 S 845-143
 (7)  AIRPLANES WITH ROLLS ROYCE ENGINES AND GRAVINER FIRE DETECTORS; Return the detectors to the normal configuration.
 (a)  
Remove the jumper wire from the center conductor of fire detector TS5148 and ground.

 (b)  
Remove the jumper wire from the center conductor of the fire detector, TS5147, and ground.

 (c)  
Connect electrical connectors, D1450 and D1452, to the engine fire detectors, TS5148 and TS5147.

 S 415-108
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (8)  Close the thrust reversers (AMM 78-31-00/201).
 S 415-248
 WARNING: OBEY THE PRECAUTIONS FOR THE KEVLAR WRAPPING WHEN YOU CLOSE
_______ THE FAN COWL PANEL. IF THE PRECAUTIONS ARE NOT OBEYED, DAMAGE TO THE KEVLAR WRAPPING CAN OCCUR.
 (9)  
Close the fan cowl panels (AMM 71-11-04/201).

 S 865-065

 (10)
 Do the activation procedure for the thrust reverser (AMM 78-31-00/201).

 S 915-129

 (11)
 Do the Left Engine Fire Detection System Test again for the Right Engine Fire Detection System. Use the RIGHT system detectors and circuit breakers in Table 2 and make sure the RIGHT system indications occur.

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 ~............................................................................. | TABLE 2 | ............................................................................... | SYSTEM | DETECTOR (CONNECTOR) | CIRCUIT BREAKERS | ............................................................................... | R NACELLE OVHT| LOOP 1 - TS5073 (D2800) | 11B22, FIRE DETECTION R ENGINE 1 | | | LOOP 2 - TS5074 (D2804) | 11B23, FIRE DETECTION R ENGINE 2 | ........................................... | | R FIRE DETECT | LOOP 1 - TS5037 (D1406) | | | | LOOP 2 - TS5036 (D1408) | | 2...............….........................…...................................1
 F. Put the Airplane back to its Usual Condition.
 S 865-067
 (1)  Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P6 panel:
 (a)  
6C1, FUEL COND CONT L

 (b)  
6C2, FUEL COND CONT R

 (c)  
6H1, FIRE EXTINGUISHING ENG L BTL 1

 (d)  
6H2, FIRE EXTINGUISHING ENG L BTL 2

 (e)  
6H3, FIRE EXTINGUISHING ENG R BTL 1

 (f)  
6H4, FIRE EXTINGUISHING ENG R BTL 2

 S 865-068
 (2)  Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel:
 NOTE: Close the system 1 and 2 circuit breakers at the same time.
____
 (a)  
11B20, FIRE DETECTION L ENGINE 1

 (b)  
11B21, FIRE DETECTION L ENGINE 2

 (c)  
11B22, FIRE DETECTION R ENGINE 1

 (d)  
11B23, FIRE DETECTION R ENGINE 2

 (e)  
11B24, FIRE DETECTION APU 1

 (f)  
11B25, FIRE DETECTION APU 2

 (g)  
11B26, FIRE DETECTION CARGO 1

 (h)  
11B27, FIRE DETECTION CARGO 2

 (i)  
11D7, ENGINES STBY IGN LEFT 1

 (j)  
11D8, ENGINES STBY IGN LEFT 2

 (k)  
11D9, ENGINES STBY IGN RIGHT 1

 (l)  
11D10, ENGINES STBY IGN RIGHT 2

 (m)  
11D19, ENGINES START CONT LEFT

 (n)  
11D20, ENGINES START CONT RIGHT

 (o)  
　
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