71-00-02
Bracket Installation -Thrust Reverser Links
Figure 3-7 (Sheet 2)
71-00-02
ITEM NO. PART NUMBER NOMENCLATURE UC QTY
3-7 55 55 60 65 70 75 315N3007-6 315N3007-2 315N3008-7 NAS6704U22 NAS1149C0463R BACN10YR4C BRACKET INSTALLATION -THRUST REVERSER LINKS (FIGURE 3-7, SHEET 2) ATTACH HOOKS (55) TO ENGINE USING ITEMS (60 THRU 75). . HOOK . HOOK . PIN ASSY . BOLT . WASHER . NUT OPT 2 -2 2 2 2
71-00-02
PW2000 SERIES ENGINES
757
POWERPLANT BUILDUP MANUAL
FIGURE 4-1
STARTER INSTALLATION
REF QEC TASK NO.: 4
REF DWG: 332N3310
71-00-02
P/P BUILDUP FIGURE 4-1 Page 1 May 05/2009
PW2000 SERIES ENGINES
757
POWERPLANT BUILDUP MANUAL
Starter Installation
Figure 4-1 (Sheet 1)
71-00-02
P/P BUILDUP FIGURE 4-1 Page 2 May 05/2009
ITEM NO. PART NUMBER NOMENCLATURE UC QTY
4-1 STARTER INSTALLATION (FIGURE 4-1, SHEET 1) INSTALL ITEMS (1 AND 2) IN ADAPTER ASSY (5).
1 MS24391-6L . PLUG 1
2 2-112V884-75 . O-RING (V02697) VEN 1
2 2-112V747-75 . O-RING (V02697) REMOVE CLAMP (10) FROM QAD ADAPTER (5). ENSURING INDEXING PIN IS ALIGNED WITH THE GEARBOX INSTALL GASKET (15) AND QAD ADAPTER (5) ON GEARBOX USING NUT (20). TIGHTEN NUT (20) TO 260-320 LB-IN. CHECK BONDING RESISTANCE BETWEEN QAD AND GEARCASE. THE MAXIMUM ALLOWABLE RESISTANCE IS 0.0005 OHMS. OPT -
5 782475-2 . QAD ADAPTER ASSY (V73030) (BOEING S332T001-13) VEN -
5 S332T001-13 . QAD ADAPTER ASSY 1
10 . . CLAMP REF -
15 332T3323-2 . GASKET 1
15 332T3323-1 . GASKET OPT -
20 624AG5HD . NUT (V82831) LUBRICATE O-RING (25) WITH MIL-L-23699 OR MIL-L-7808 AND INSTALL ON STARTER (30) DRIVE SHAFT. VEN 6
25 AS3209-136 . O-RING 1
25 M83248-1-136 . O-RING OPT -
30 784750A6 . STARTER (V73030) (BOEING S332N108-102) VEN -
30 S332N108-102 . STARTER 1
30 784750A3 . STARTER (V73030) (BOEING S332N108-101) VEN -
30 784750A2 . STARTER (V73030) (BOEING S332N108-101) VEN -
30 S332N108-101 . STARTER (REPLACED BY S332N108-102)*[1] ALIGN INDEXING PIN ON STARTER (30) WITH SLOT ON QAD ADAPTER (5). SECURE STARTER (30) TO QAD ADAPTER (5) USING CLAMP (10). ROTATE CLAMP (10) TO THE 9:00 O’CLOCK POSITION AND TIGHTEN TO 60-65 LB-IN. *[1] S332N108-101 CAN REPLACE -102 FOR SPARES USAGE LTD -
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 动力装置安装手册 Powerplant Buildup Manual(59)
