Textron Bell 206A Series, Руководство по обслуживанию

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BHT-206A/B-SERIES-MM-1
5-00-00
Page 158
Rev. 14 30 APR 2013 Export Classification C, ECCN EAR99
Chapter 32 1. Inspect landing gear skid tubes and crosstubes for damage
and deflection.
BHT-ALL-SPM 2. Remove riveted or clamped crosstube support and
accomplish NDI inspection of forward and aft crosstube.
Chapter 53 3. Inspect crosstube attachment points on fuselage for
damage or distortion.
4. Check all cowling, fairing and doors for proper fit and
alignment. Misaligned cowling, fairing, or doors may indicate a
distorted fuselage, resulting in major stresses and damage to
components.
5. Remove all cowlings and fairings necessary to perform a
complete visual inspection.
Rolls-Royce 250
Series Operation and
Maintenance Manual,
5W2 or 10W2 6. For engine inspection instructions, refer to the Rolls-Royce
250 Series Operation and Maintenance Manual.
Chapter 29 and
Chapter 67 7. Check for leaks in hydraulic system, interference or binding
of hydraulic actuator and controls, and for satisfactory
operation.
Chapter 67 8. Perform complete visual inspection of the flight control
system from pilot controls to main rotor head and check for bent
or damaged tubes, bellcranks, and supports. Particular attention
should be given to pitch link assemblies swaged ends for cracks
and to swashplate pivot sleeve at lever attachment points for
damage.
a. Remove and inspect suspected control tube for
straightness by rolling on a surface plate or with use of a metal
straight edge. On fixed control tubes swaged end must be
concentric to tube within 0.06 inch (1.5 mm) (TIR). Scrap
damaged control tube. If no damage is found, reinstall control
tube.
BHT-206B3-CR&O,
Chapter 62 b. If visual inspection reveals damage to swashplate and
support assembly, accomplish the following:
(1) Overhaul swashplate and support assembly.
CONDITIONAL INSPECTIONS
5-52. HARD LANDING (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER