BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14 Page 145
Export Classification C, ECCN EAR99
5-46. 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.
FUEL SYSTEM
Installation and removal of a fuel boost pump
cartridge, upper or lower 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.
Chapter 28 1. When maintenance or component change/removal is
conducted below top fitting of aft fuel cell immediately following
fuel system maintenance and/or major component change/
removal (boost pump assembly, check valve, fuel line or hoses),
ground run helicopter and check for air and fuel leaks and for
proper operation as follows:
Chapter 12 a. Ensure all fuel has been drained from fuel cell.
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