Schweizer S300C 269C - Main Rotor System; Tailboom Left Side

ENGINE - LEFT SIDE (cont) 
 Rear oleo damper extension CHECK
CAU TION
IF CRACKING OF CLUSTER FITTINGS IS
SUSPECTED, A DYE PENETRANT INSPECTION
MUST BE PERFORMED BEFORE FURTHER
FLIGHT OPERATIONS.
 Center frame aft cluster fittings for cracks,
deformation, or damage CHECK
MAIN ROTOR SYS TEM 
 Main rotor transmission and mast CHECK
 Main transmission oil level CHECK
 Blades and rotor head CHECK
 Main rotor dampers CHECK
 Main rotor swashplate, pitch links, upper and
lower bearings CHECK
 Main rotor mixer bellcrank CHECK
 Main rotor control rods CHECK
 Tail rotor shaft, set alignment marks CHECK
TAILBOOM LEFT SIDE 
 Tailboom for damage or dents CHECK
 Tailboom supports and fittings - for cracks,
deformation, damage, looseness and security CHECK
 Beacon light CHECK
 Static port clear of obstructions CHECK
 Tailboom support strut end fitting for cracks,
deformation, or damage CHECK
 Exhaust diffuser installation (if installed) for
cracks, deformation, damage, looseness and
security. CHECK
Normal Procedures
Pilot's Flight Manual
4-6
Reissued: 16 Jan 2019
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
SCHWEIZER
Model 269C Helicopter
FAA Approved
CSP Book 1 CSP-C-1.indd 90 8/4/19 12:45 PM