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8-2 14TH-STAGE SURGE BLEED DUCT INSTALLATION (FIGURE 8-2, SHEET 4) TIGHTEN BOLTS (15 AND 20) TO 90-125 LB-IN. (10.2-14.1 N.m). FOLLOWING A TIGHTENING SEQUENCE AROUND BOLT FLANGE TO PREVENT SLIPPAGE OF SWIVEL FLANGE FROM UNLOADED POSITION. TIGHTEN TO AFT SUPPORT ROD BOLTS (35), THEN FORWARD SUPPORT ROD BOLTS (55) TO 125-150 LB-IN. (14.1-16.9 N.m). MAKE SURE TIGHTENING DOES NOT PRELOAD INSTALLATION. ENSURE ENGINE FASTENERS ARE TIGHTENED AT ALL FOUR ENGINE CLEVIS LOCATIONS. INSTALL LOCKWIRE TO AFT SUPPORT ROD ASSY AND TO FORWARD SUPPORT ROD ASSY.
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POWERPLANT BUILDUP MANUAL
FIGURE 9-1
ENGINE DRAIN INSTALLATION
REF QEC TASK NO.: 9
REF DWG: 332N3710 332N3150
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PW2000 SERIES ENGINES
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POWERPLANT BUILDUP MANUAL
Engine Drain Installation
Figure 9-1 (Sheet 1)
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ITEM NO. PART NUMBER NOMENCLATURE UC QTY
9-1 ENGINE DRAIN INSTALLATION (FIGURE 9-1, SHEET 1) THIS SHEET NOT USED
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Engine Drain Installation
Figure 9-1 (Sheet 2)
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ITEM NO. PART NUMBER NOMENCLATURE UC QTY
9-1 ENGINE DRAIN INSTALLATION (FIGURE 9-1, SHEET 2) INSTALL TEE (5), WASHERS (10, 15) AND NUT (16) ON LOWER BIFURCATION DISCONNECT PANEL.
5 BACT16BN060606J . TEE 1
10 NAS1149C0963R . WASHER (UNDER TEE) 1
15 NAS1149C0932R . WASHER (UNDER NUT) 1
16 AN924-6J . NUT INSTALL UNION (20) ABOVE LOWER BIFURCATION DISCONNECT PANEL AND SECURE WITH WASHER (21) AND NUT (22). 1
20 MS21924J10 . UNION 1
21 NAS1149C1490R . WASHER (UNDER NUT) 1
21 NAS1149C1432R . WASHER (REPLACED BY NAS1149C1490R) LTD -
21 NAS1149C0432R . DELETED DEL -
22 AN924-10J . NUT INSTALL TUBE ASSY (25) AND TEE (30) ON TEE (5). 1
25 332N3710-37 . TUBE ASSY 1
30 BACT16BL060606J . TEE 1
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POWERPLANT BUILDUP MANUAL
Engine Drain Installation
Figure 9-1 (Sheet 3)
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ITEM NO. PART NUMBER NOMENCLATURE UC QTY 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(77)
