BHT-206A/B-SERIES-MM-1
5-00-00
Page 96 Rev. 14 30 APR 2013
Export Classification C, ECCN EAR99
Chapter 53 TAILBOOM
ANY CRACK, CORROSION, OR LOOSE OR
SHEARED RIVET IS CAUSE FOR IMMEDIATE
GROUNDING OF THE HELICOPTER UNTIL THE
PROBLEM IS CORRECTED.
3. Remove the access panel on right side of aft fuselage.
Chapter 53 4. Make sure the area is clean and examine the four tailboom
attachment fittings on fuselage aft bulkhead and tailboom
forward bulkhead for cracks. Give special attention to the
tailboom attachment fittings/intercostals and bolts, and to
fasteners between the intercostals. Particular attention must be
given to inspection of the upper left fitting.
5. Make sure the area is clean and visually examine all visible
sections of the upper left longeron between aft fuselage frame
at STA 179.92 and fuselage frame at STA 206.76 for general
condition, corrosion, and cracks.
a. If corrosion or a defect is found, submit details to
Product Support Engineering for evaluation and possible repair.
b. If no defects are found, reinstall the access panel.
5-28. 100-HOUR INSPECTION (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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