Textron Bell 212, Maintenance Manual

Page: 123 / 269

BHT-212-MM-1
5-00-00
Page 100
Rev. 14 26 JUN 2013 Export Classification C, ECCN EAR99
AFTER COMPLETION OF INSPECTION
1. Reinstall all panels, fairings, and cowlings removed during
inspection.
2. Carry out a ground run and leak check prior to releasing
the helicopter back to service.
FORWARD FUSELAGE
Chapter 53 1. Center and outboard bulkhead, below WL 22.0 at FS 23.0
for cracks, deformation, and corrosion along structure joints.
2. Collective and cyclic control jackshafts support intercostal
for cracks and corrosion.
3. Cyclic support for corrosion and cracks.
4. Collective, cyclic, and anti-torque control system
bellcranks, levers, and support brackets for corrosion, cracks,
and indication of wear at attaching points.
5. Crew seat support beams at BL 14.0 and 30.0 and FS 23.0
and 74.30 for cracks and corrosion.
6. Forward crosstube attach points and support structure at
FS 63.33 and 74.30 for damage, corrosion, and cracks. Aft
crosstube attach points and support structure at FS 155.06 and
166.00 for damage, corrosion, and cracks.
7. Crew and passenger cabin floor FS 23.0 to 155.06 for
corrosion and damage. Seat fasteners and cargo tie-down rings
for condition.
8. Joints and supports in area under floor panel at BL 14.0 left
and right and FS 74.25 to 92.0 for corrosion, cracks, and bottom
skin damage.
9. Joints and supports under floor fuel cell cavities left and
right at FS 102.0 to 145.56 for corrosion, cracks, and bottom
skin damage.
SCHEDULED INSPECTIONS
5-15. 3000 HOURS/ 5 YEARS — PART B (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER