S 015-032-C00

 (2)
Open the left fan cowl panel (AMM 71-11-02/201) for each engine.

 S 865-033-C00

 (3)
Make sure the two forward thrust levers are at the idle postion.

 S 495-106-C00

 (4)  
Do this step on the first engine.

 (a)  Install the rig pin 3 (F70207-23) in the "P" (part power stop) rig pin hole in the fuel control box (View B, Fig. 501).
 S 485-035-C00
 (5)  Attach the adaptor and the protractor to the thrust lever for the first engine (Fig. 502).
 NOTE: If the protractor is not available, refer to
____ AMM 76-11-00/201 for the conversion of angular position to linear position of the thrust lever.
 S 715-036-C00
 (6)  Move the first thrust lever forward to 30.0 (+1.0/-1.0) degrees from the idle stop.
 (a)  The power lever in the fuel control box on the first engine must touch the rig pin 3.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-00
 ALL  ú ú C01 Page 509 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b)  If necessary, adjust the turnbarrel on the push-pull cable to get the thrust lever travel and the rig pin condition specified (View B, Fig. 501).
 S 495-107-C00
 (7)  Do this step on the second engine.
 (a)  Install the rig pin 3 (F70207-23) in the "P" (part power stop) rig pin hole in the fuel control box (View B, Fig. 501).
 S 715-109-C00
 (8)  
Move the second thrust lever forward until the power lever in the fuel control box on the second engine touches the rig pin 3.

 S 825-038-C00

 (9)  
Adjust the turnbarrel on the push-pull cable for the second engine until the two thrust levers align within 0.06 inches (1.52 mm).

 S 215-040-C00

 (10)
 When the adjustments are complete, make sure the thread engagement witness holes in the turnbarrels are at least 50 percent covered.

 S 435-041-C00

 (11)
 Install lockwire on the turnbarrels.

 S 095-042-C00

 (12)
 Remove the rig pins.

 (13)
 Close the fan cowls (AMM 71-11-02/201).

 (14)
 Remove the adaptor and the protractor from the thrust lever.

 (15)
 Do the procedure: Put the Airplane Back to Its Usual Condition.

 S 415-043-C00
 S 085-044-C00
 S 845-103-C00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-00
 ALL  ú ú C01 Page 510 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
H. Put the Airplane Back to Its Usual Condition
 S 095-059-C00
 WARNING:_______BE CAREFUL WHEN YOU WORK NEAR THE LEADING EDGE FLAPS. LEADING EDGE FLAPS MOVE VERY QUICKLY. INJURY CAN OCCUR.
 (1)  
Remove the locks on the leading edge of the flap (AMM 27-81-00/201).

 S 445-095-C00

 (2)  
Do the activation procedure for the thrust reverser system (AMM 78-31-00/201).

 TASK 76-11-00-835-111-C00
 3. Engine Control Cables Tension Adjustment
________________________________________
 A. General
 (1)  This procedure describes the tension adjustment of the thrust control and start control cables. You must do this task after you replace an engine control cable.
 B. Equipment
 (1)  
Tensiometer, 0 to 125 pound (0 to 58 Kg) capacity
 (commercially available)

 (2)  
Kit - Rig Pin, F70207-93

 (a)  
Rig Pin - F70207-8 Optional: MS20392-4C pin (or equivalent 0.311 inch (7.9 mm) diameter, 3 inch (76 mm) long rod or bolt)

 (b)  
Rig Pin - F70207-23 (2 required). Optional: MS20392-3C pin (or equivalent 0.248 inch (6.29 mm) diameter, 3 inch (76.2 mm) long rod or bolt).

 ú (3) Rig Pin - C76001-9
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 發(fā)動(dòng)機(jī)控制 ENGINE CONTROLS(10)