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Textron Bell 212 - Page 103

Textron Bell 212
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BHT-212-MM-1
5-00-00
Page 80 Rev. 14 26 JUN 2013 Export Classification C, ECCN EAR99
FUSELAGE — CABIN
Chapter 53 1. Forward fuselage:
a. Cabin exterior structure for corrosion and damage.
b. Cabin interior structure for corrosion and damage.
c. Ensure all drain holes are open.
d. All compartments for evidence of water entrapment and
corrosion.
2. Underside of fuselage:
a. Fuselage structure for damage, corrosion, and working
rivets.
b. Exterior finish for condition and cleanliness.
c. Evidence of excessive fluid leakage.
d. Structure around landing gear for condition.
e. Forward crosstube support structure for working
fasteners, cracks, corrosion, and excessive wear.
f. Aft crosstube support structure for working fasteners,
cracks, corrosion, and excessive wear.
Chapter 52 3. Doors and windows:
a. Crew and passenger doors structure for corrosion,
damage, distortion, and positive locking mechanisms. Seals for
adherence, tears, separations, and deterioration.
b. Crew doors emergency jettison mechanism for
condition and security. Perform operational check.
5-13. 300 HOURS — PART B (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER

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