• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-16 09:58来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

(PW4052, PW4056, PW4060, PW4060A, PW4060C AND ALL (-1C) INTERMIX MODELS WHICH INCLUDES PW4062-1C) 
0998 L-B6932 
Figure 506 (Sheet 3) Turbine Cooling Air Ratio Check Limits 

H93452
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú N03 Page 561 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
0.70
0.69

0.68
0.67
0.66
0.65
0.64
0.63
0.62
0.61
0
PS4I/PT3
OR 0.97 (PS4I/PS3)

THIS CURVE IS FOR ENGINES POST-PW-SB 72-662 NOTES: THE PERMITTED BAND IS NOT APPLICABLE_____ WITH TOBI DUCT PN's 50K362-01, 50K362-001, OR 50K372-01. TO THE IDLE POWER CONDITIONS. 
(PW4052-3, PW4056-3, PW4060-3, PW4062-3, AND ALL (-3B) INTERMIX MODELS) 
0998 L-B0049 
Figure 506 (Sheet 4) Turbine Cooling Air Ratio Check Limits 

H93532
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú N03 Page 562 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
0.74
0.73
0.72

0.71
0.70
0.69
0.68
0.67
0.66
0.65
0.64
PS4I/PT3
OR 0.97 (PS4I/PS3)

THIS CURVE IS FOR ENGINES PRE-PW-SB 72-662 NOTES: THE PERMITTED BAND IS NOT APPLICABLE_____ WITH TOBI DUCT PN's 50K137-01, OR 50K362-002. TO THE IDLE POWER CONDITIONS. 
ALL (-3B) INTERMIX MODELS) (PW4052-3, PW4056-3, PW4060-3, PW4062-3, AND 
0998 L-B6933 
Figure 506 (Sheet 5) Turbine Cooling Air Ratio Check Limits 

H93583
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú N03 Page 563 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
TEST NO. 9 - PERFORMANCE TEST
_____________________________
 S 715-057-N00
 (9)  Do a test of the engine acceleration/deceleration in the primary EPR mode with the steps that follow:
 NOTE: Before you do the acceleration test, let the engine become
____
 stable for 5 minutes at the minimum idle.

 (a)  Set the approach idle with the steps that follow:
 1)  For the applicable engine, open this circuit breaker and attach the DO-NOT-CLOSE tag: a) P6 Main Power Distribution Panel
 ~........................................ | 1 |6F10 ENG 1 IDLE CONT/TMC DISCRETE | .......................................... | 2 |6E10 ENG 2 IDLE CONT/TMC DISCRETE | .......................................... | 3 |6D10 ENG 3 IDLE CONT/TMC DISCRETE | .......................................... | 4 |6C10 ENG 4 IDLE CONT/TMC DISCRETE | 2...…....................................1
 2)  Open this circuit breaker and attach the DO-NOT-CLOSE tag:
 NOTE: The alternate mode will occur and the EPR display on
____ the EICAS performance page will go off.
 a) P414 Power Distribution Center - Left ~........................................ | 1 |414D25 ENG IDLE CONT ALT | 2...…....................................1
 (b)  Make a record of the approach idle N2 indication.
 1)  Make sure the approach idle N2 indication is in the permitted range (AMM 71-00-01/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú N03 Page 564 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
TEST NO. 9 - PERFORMANCE TEST_____________________________
 (c)  Make a record of the engine indications.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 动力装置 POWER PLANT 1(72)