Schweizer S300C 269C - Page 93

 Fuel tank sump, for water (30 gallon tank) DRAIN
 Fuel strainer, for debris or water DRAIN
 Fuel tank vent NO OBSTRUCTIONS
 Engine driven fuel pump drain line for security
(Service Bulletin B-235) CHECK
 General engine area for loose wires, fittings or
damage 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
 Rear oleo damper extension, strut, and skid CHECK
 Ground handling wheel (if installed) in up
position with quick-release pin installed CHECK
 Ground handling wheel handle (if installed);
quick-release pin installed CHECK
 Tail rotor control cable CHECK
Normal Procedures
Pilot's Flight Manual
Reissued: 16 Jan 2019
4-8.1
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 93 8/4/19 12:45 PM