EasyManua.ls Logo

Textron Bell 212 - Page 125

Textron Bell 212
269 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
BHT-212-MM-1
5-00-00
Page 102 Rev. 14 26 JUN 2013
Export Classification C, ECCN EAR99
4. Tailboom access panels and covers for condition and
attachment.
5. Tailboom baggage compartment door for condition,
attachment, and latching.
6. Tailboom baggage compartment interior for damage and
corrosion.
7. Tailboom interior bulkheads and stringers for cracks and
corrosion.
8. Intermediate gearbox mount pad for damage and
corrosion. Tail rotor gearbox mount pad for damage and
corrosion.
9. Tailboom exterior bonded panels adjacent to baggage
compartment for damage, delamination, and corrosion.
Chapter 28 FUEL SYSTEM
1. Inspect fuel cells for condition and serviceability. Verify
self-sealing gum of the lower cell has not been activated.
Repairs to be accomplished at an authorized facility.
Chapter 67
BHT-212-CR&O
BHT-212-SI-4
BHT-212-SI-89
TB 212-87-98
FLIGHT CONTROLS
1. Disassemble pilot and copilot collective sticks (if installed)
to the extent necessary to remove throttle twist grips.
2. Referring to Figure 5-3 visually inspect stick tube for cracks
using a 3X magnifying glass and a bright light. Pay particular
attention to the base of the throttle slots that form the twist grip
stops.
3. If a crack is found, replace stick tube.
4. Reassemble pilot and copilot collective sticks (if installed).
5-15. 3000 HOURS/ 5 YEARS — PART B (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER

Table of Contents

Related product manuals