Boeing 737-600 - Subtask 24-41-11-410-005; Task 24-41-11-200-803 - External Power Receptacle Neutral Pin to Ground Continuity Check

CAUTION
DO NOT USE TOO MUCH FORCE WHEN PUSHING THE WEAR GAGE
ONTO THE PINS. THE WEAR GAGE IS A GO/NO GO TOOL AND
SHOULD NOT FIT OVER THE PINS. THE USE OF TOO MUCH FORCE
COULD CAUSE DAMAGE TO PINS.
(a) Try to slide the wear gage set, SPL-1625 over the external power receptacle pins
NOTE: The F70284-1 is a gage set. Use the -2 on the four large pins A, B, C and N. Use
the -3 on the two small pins E and F.
(b) Make sure the gage does not slide over the pins. If the gage slides over the pins to within
0.50 inch of the face of the receptacle, do the applicable tasks:
ILF 686; ILF 101, 151, 156-199, 301, 304, 308, 310, 314, 315, 317-319, 323, 331-399, 401, 402, 405,
406, 409, 410, 412, 416, 424, 425, 427-429, 451, 452, 496, 498-504, 507-510, 512-516, 518-520,
523-528, 530-533, 535-537, 541, 542, 552-557, 560-562, 567-569, 571-577, 581, 583, 585, 671, 672,
703, 707-710, 803-813, 821, 822, 831, 832, 836, 837, 841, 842, 851, 852, 854-858, 861-863, 871-874,
947, 948, 968-971, 973 PRE SB 737-24-1198
1) External Power Receptacle Removal, TASK 24-41-11-000-801
External Power Receptacle Installation, TASK 24-41-11-400-801
ILF 491-495, 497, 559, 563, 564, 588-590, 592, 972, 980-999; ILF 101, 151, 156-199, 301, 304, 308,
310, 314, 315, 317-319, 323, 331-399, 401, 402, 405, 406, 409, 410, 412, 416, 424, 425, 427-429, 451,
452, 496, 498-504, 507-510, 512-516, 518-520, 523-528, 530-533, 535-537, 541, 542, 552-557, 560-562,
567-569, 571-577, 581, 583, 585, 671, 672, 703, 707-710, 803-813, 821, 822, 831, 832, 836, 837, 841,
842, 851, 852, 854-858, 861-863, 871-874, 947, 948, 968-971, 973 POST SB 737-24-1198
2) External Power Receptacle Removal, TASK 24-41-11-000-802-001
External Power Receptacle Installation, TASK 24-41-11-400-802-001
External Power Receptacle Pins Replacement, TASK 24-41-11-960-802-001
ILF 593-599, 601-603, 606, 607, 610-615, 620, 625-627, 691-699, 833-835, 838
3) External Power Receptacle Removal, TASK 24-41-11-000-803-002
External Power Receptacle Installation, TASK 24-41-11-400-803-002
ILF ALL
SUBTASK 24-41-11-410-005
(5) Close this access panel:
Number Name/Location
114AR External Power Receptacle Door
END OF TASK
TASK 24-41-11-200-803
5. External Power Receptacle Neutral Pin to Ground Continuity Check
(Figure 601 or Figure 602 or Figure 603)
A. General
(1) The External Power Receptacle is located on the lower right hand side of the airplane. It is
installed forward of the nose gear wheel well.
(2) The External Power Receptacle Neutral Pin to Ground Continuity Check uses a low resistance
ohm meter to measure the resistance between the neutral pin and a ground stud located on
the main landing gear wheel well.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Page 618
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL