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Textron Bell 212 - Page 39

Textron Bell 212
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BHT-212-MM-1
5-00-00
Page 16 Rev. 14 26 JUN 2013
Export Classification C, ECCN EAR99
Chapter 32 LANDING GEAR SYSTEM
1. Visually inspect landing gear as follows:
a. Forward crosstube assembly and retention caps for
condition and security of attachment.
b. Aft crosstube assembly and retention caps for condition
and security of attachment.
c. Skid tubes and skid shoes for condition and security of
attachment. Replace skid shoes that are worn into shoe surface.
Repair weld beads as required.
d. Fuselage supports for wear, damage, and security of
attachment.
e. If installed, landing gear forward crosstube crew step
fittings for corrosion, damage, and security in area of attachment.
f. Emergency float reservoir pressure indicator for proper
charge indication (if installed).
g. Floats for proper stowage and condition (if installed).
2. Visually inspect tail skid for deformation and security of
attachment.
Chapter 52 DOORS, WINDOWS, AND EMERGENCY EXIT
1. Visually inspect nose door for obvious damage, security of
attachment, proper latching, and seal for condition.
2. Visually inspect all windows for damage. Crew door
windows, cargo hinged door window, passenger sliding door
windows, cabin roof windows, cabin lower nose windows and
windshields.
3. Visually inspect crew door emergency release pins for
security.
4. Visually inspect crew and cabin doors for condition, security,
and freedom of operation.
SCHEDULED INSPECTIONS
5-8. DAILY INSPECTION — PART A (CONT)
DATA
REFERENCE
INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER

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