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5-55.
ENGINE COMPRESSOR STALL OR SURGE (CONT)
DATA REFERENCE
BHT-206L-CR&O
Chapter 53
Chapter 63
Chapter 65
BHT-206L4-FM-1
Export Classification C, ECCN EAR99
CONDITIONAL INSPECTIONS
INSPECTION TASK DESCRIPTION
TAIL ROTOR GEARBOX
1.
Remove the tail rotor gearbox input pinion.
2.
Inspect the following gear teeth for scoring and other
mechanical damage.
a. Input pinion gear.
b. Spiral bevel gear.
3.
If any damage suspected to be related to the stall or surge
is found, make an entry on the Historical Service Record and
attach a tag on the tail rotor gearbox and write, "THIS
COMPONENT WAS REMOVED FROM SERVICE BECAUSE
OF A COMPRESSOR STALL". Send the tail rotor gearbox to a
Bell Helicopter Textron approved facility for overhaul.
4.
If no defects were detected on the gears, the tail rotor
gearbox is serviceable.
FUSELAGE
1.
Examine the complete tailboom structure for distortion,
buckles, cracks in the skin, and sheared or loose rivets.
2.
Inspect tailboom attachment fittings for cracks.
3.
Inspect the vertical fin for condition and security of
attachment.
GROUND RUN
1.
Perform a ground run for a minimum of 30 minutes with the
helicopter light on its skids. Remove and examine the chip
detectors of the transmission assembly, freewheel assembly,
and tail rotor gearbox.
BHT-206L4-MM-1
INITIAL
MECH OTHER
7 JUN 2013 Rev. 18
5-00-00
Page 173
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