After Fuel System Maintenance And/Or Component Change - Bell 206L4 Maintenance Manual

5-44.

AFTER FUEL SYSTEM MAINTENANCE AND/OR COMPONENT CHANGE

DATA REFERENCE
Chapter 28
ECCN EAR99
SPECIAL INSPECTIONS
INSPECTION TASK DESCRIPTION
DATE: __________________W.O. _____________________
FACILITY: _________________ _ ________________________
HELICOPTER S/N: __________ _ ________________________
REGISTRY NO.: ____________ _ ________________________
TOTAL TIME:_______________________________________
SIGNATURE:_______________ _ ________________________
Accomplish immediately
maintenance and/or component change/removal, at
an adequate maintenance facility.
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
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:
NOTE
after fuel system
NOTE
pump assembly, manifold,
25 FEB 2011 Rev. 13
BHT-206L4-MM-1
INITIAL
MECH OTHER
flow
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