BHT-206A/B-SERIES-MM-1
5-00-00
Page 88 Rev. 14 30 APR 2013
Export Classification C, ECCN EAR99
Chapter 53 8. Examine baggage compartment door, seal, and latches for
operation, condition, and security.
Chapter 96 9. Verify operation of the baggage door ajar caution light, if
installed.
FUSELAGE (INTERIOR)
Chapter 53 1. Examine baggage compartment for condition.
2. Gain access to inside of aft fuselage through access
panels in baggage compartment and access panel located on
the aft right side fuselage:
a. Examine access panels and fasteners for condition.
b. Examine under engine pan for fuel, oil, or water leaks.
c. Examine drain lines for condition and security.
d. Examine aft fuselage longerons for cracks, corrosion,
and condition. Pay particular attention to the upper left longeron.
e. Examine interface between longerons and engine pan
structure for cracks, corrosion, distortion, and loose fasteners.
f. Inspect engine mount attachment structure for
condition.
ANY CRACK, CORROSION, OR LOOSE OR
SHEARED RIVET IS CAUSE FOR IMMEDIATE
GROUNDING OF THE HELICOPTER UNTIL THE
PROBLEM IS CORRECTED.
g. 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.
5-26. 300-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 6 (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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