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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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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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Engine Drain Installation
Figure 9-1 (Sheet 3)
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ITEM NO. PART NUMBER NOMENCLATURE UC QTY 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：757 動力裝置安裝手冊 Powerplant Buildup Manual(77)
