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Boeing 737-600 - Subtask 53-51-21-400-005

Boeing 737-600
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c) Install the non-designated electrical bond fasteners for this access panel [34]:
Number Name/Location
193B Wheel Well Panel - Forward Inboard
d) Install the non-designated electrical bond fasteners for this access panel [32]:
Number Name/Location
193CL Wheel Well Panel - Aft Outboard
e) Install the non-designated electrical bond fasteners for this access panel [37]:
Number Name/Location
193CR Wheel Well Panel - Aft Outboard
f) Install the non-designated electrical bond fasteners for this access panel [35]:
Number Name/Location
193D Wheel Well Panel - Aft Inboard
3) Zone 195:
a) Install the non-designated electrical bond fasteners for this access panel [20]:
Number Name/Location
195AL Wing To Body Fairing - Left Side
b) Install the non-designated electrical bond fasteners for this access panel [21]:
Number Name/Location
195BL Wing To Body Fairing - Left Side
c) Install the non-designated electrical bond fasteners for this access panel [22]:
Number Name/Location
195CL Wing To Body Fairing - Left Side
4) Zone 196:
a) Install the non-designated electrical bond fasteners for this access panel [23]:
Number Name/Location
195AR Wing To Body Fairing - Right Side
b) Install the non-designated electrical bond fasteners for this access panel [24]:
Number Name/Location
195BR Wing To Body Fairing - Right Side
c) Install the non-designated electrical bond fasteners for this access panel [25]:
Number Name/Location
195CR Wing To Body Fairings - Right Side
SUBTASK 53-51-21-400-005
(3) Install the bonding fasteners for the applicable panel:
(a) Apply compound, C00528 to the fastener and its hole.
(b) Measure the maximum electrical resistance for each bonding fastener.
1) Refer to this task: Wing-To-Body Fairing Panel Maximum Electrical Resistance
Check, TASK 53-51-21-760-801.
a) Make sure that the maximum resistance for each bonding fastener is not more
than 300,000 ohms for these access panels:
In Zone 192: 192AL, 192AR, 192HL, 192HR
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-51-21
Page 416
D633A101-ILF Oct 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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