BHT-206L4-MM-1
5-00-00
25 FEB 2011 Rev. 13 Page 127
ECCN EAR99
5-44. AFTER FUEL SYSTEM MAINTENANCE AND/OR COMPONENT CHANGE
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
Accomplish immediately after fuel system
maintenance and/or component change/removal, at
an adequate maintenance facility.
Chapter 28 FUEL SYSTEM
Installation and removal of a fuel boost pump
cartridge, fuel quantity probe, or fuel drain valve does
not require this inspection.
If fuel system maintenance and/or component change/removal
is performed at a site remote from an adequate maintenance
facility, accomplish step 1, substep c through substep e, and
step 3, or step 2 and step 3, as applicable, prior to flight. Upon
return to an adequate maintenance facility, but not to exceed 10
flight hours, accomplish entire inspection.
1. When maintenance or component change/removal is
conducted below the top fitting of the aft fuel cell immediately
following fuel system maintenance and/or major component
change/removal (boost pump assembly, manifold, flow
switches, inline filters, ejector pumps, check valves, fuel line or
hoses), ground run helicopter and check for air and fuel leaks
and for proper operation as follows:
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