EasyManua.ls Logo

Boeing 737-600 - Subtask 47-11-02-420-001; Subtask 47-11-02-765-001; Subtask 47-11-02-390-001; Subtask 47-11-02-865-002

Boeing 737-600
2300 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
2) Install the coupling [5].
(d) Tighten the nut on the HFV muscle air duct [7] to 280 ±28 in-lb (31.6 ±3.2 N·m).
NOTE: Use two wrenches to tighten the nuts. This will release torque pressure on the
HFV muscle air duct [7] and the NEA duct [11].
(e) Tighten the nut on the NEA duct [11] to 280 ±28 in-lb (31.6 ±3.2 N·m).
NOTE: Use two wrenches to tighten the nuts. This will release torque pressure on the
HFV muscle air duct [7] and the NEA duct [11].
(f) Tighten the nut on the oxygen sensor tube [19] to 170 ±17 in-lb (19.2 ±1.9 N·m).
NOTE: Use two wrenches to tighten the nuts. This will release torque pressure on the
HFV muscle air duct [7] and the oxygen sensor tube [19].
SUBTASK 47-11-02-420-001
(3) Do these steps to finish the installation:
(a) Tighten the four bolts [3] to 109 ±6 in-lb (12.3 ±0.7 N·m).
(b) Connect the electrical connector [13] to the differential pressure sensor.
(c) Connect the electrical connector [13] to the high flow valve [1].
(d) Attach the bonding jumper [14] to the jumper tab [18] with the screw [15], washers [16],
and nut [17].
SUBTASK 47-11-02-765-001
(4) Use an intrinsically safe approved bonding meter, COM-1550, to measure the resistance
between the jumper tab [18] and bracket (SWPM 20-20-00)
(a) Make sure that the resistance is 0.010 ohm (10 milliohms) or less.
SUBTASK 47-11-02-390-001
(5) Apply BMS 5-45 sealant, A50337, to fully cover the screw [15], washers [16], nut [17], and
jumper tab [18].
I. Operational Test for the High Flow Valve
SUBTASK 47-11-02-865-002
(1) Do these steps to prepare for the operational test:
(a) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-3
Row Col Number Name
ILF 402, 452, 509, 510, 523, 525-528, 576, 577, 971; ILF 101, 151, 156-199, 301, 304, 308, 310,
314, 315, 317-319, 323, 331-399, 401, 405, 406, 409, 410, 412, 416, 424, 425, 427-429, 451,
501-504, 507, 508, 512-514, 516, 518, 524, 531-533, 535-537, 541, 542, 552-556, 560-562, 567,
571-575, 671, 672, 686, 703, 707-710, 803-813, 821, 822, 831, 832, 836, 837, 841, 842, 851, 852,
854-858, 861-863, 871-874, 947, 948, 968-970, 972, 973 POST SB 737-47-1003
D 17 C01657 NITROGEN GEN CONT
ILF 568, 569, 581, 583, 585, 588-590, 592-599, 601-603, 606, 607, 610-615, 620, 625-627,
691-699, 833-835, 838, 980-999; ILF 567, 973 POST SB 737-47-1003
D 17 C01657 NITROGEN GENERATION CONTROL
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
47-11-02
Page 409
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF 402, 452, 509, 510, 523, 525-528, 568, 569, 576, 577, 581, 583, 585, 588-590,
592-599, 601-603, 606, 607, 610-615, 620, 625-627, 691-699, 833-835, 838, 971, 980-999;
ILF 101, 151, 156-199, 301, 304, 308, 310, 314, 315, 317-319, 323, 331-399, 401, 405,
406, 409, 410, 412, 416, 424, 425, 427-429, 451, 501-504, 507, 508, 512-514, 516, 518,
524, 531-533, 535-537, 541, 542, 552-556, 560-562, 567, 571-575, 671, 672, 686, 703,
707-710, 803-813, 821, 822, 831, 832, 836, 837, 841, 842, 851, 852, 854-858, 861-863,
871-874, 947, 948, 968-970, 972, 973 POST SB 737-47-1003

Table of Contents

Related product manuals