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BHT-206L4-MM-1
5-25.
300-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 5 (CONT)
DATA REFERENCE
Chapter 96
Chapter 11
5-00-00
Page 72
Rev. 13 25 FEB 2011
PROGRESSIVE INSPECTIONS
INSPECTION TASK DESCRIPTION
2.
Examine the cyclic control stick for condition and security
and minimum friction. Examine copilot cyclic control stick if
installed.
3.
Examine the anti-torque control pedals for condition and
security and minimum friction. Examine copilot anti-torque
control pedals if installed.
ELECTRICAL
1.
Verify operation of cockpit map reading light.
2.
Verify operation of aft cabin reading lights (if installed).
USE EXTREME CARE WHEN IN PROXIMITY OF
PITOT TUBE WITH HEAT APPLIED, TOUCHING
TUBE MAY RESULT IN SERIOUS BURNS.
3.
Verify operation of the pitot tube heating system.
4.
Verify operation of defog blowers.
5.
Verify operation of ENGINE OUT and LOW ROTOR RPM
audio and mute switch (if installed).
6.
Verify illumination of all caution panel annunciator light
segments by depressing test switch, or each individual light
segment, as applicable.
7.
Verify instrument lighting and dimming capabilities.
ZONE 8 — FORWARD FUSELAGE
PLACARDS AND MARKINGS
1.
Examine the placards, decals and markings. Ensure they
are readable, correctly applied and in agreement with the
applicable configuration of your helicopter.
CAUTION
INITIAL
MECH
OTHER
ECCN EAR99
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