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Schweizer S300C 269C - Exterior Inspection; Nose Area; Cabin - Left Side

Schweizer S300C 269C
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EX TE RIOR
NOSE AREA
Aircraft tiedowns and covers REMOVED
Aircraft attitude for weak or damaged oleos CHECK
NOTE
: With fuel tank(s) full, ob serve stance of he li -
cop ter. Nor mal stance is slightly nose up.
Canopy for condition and cleanliness CHECK
OAT thermometer sun shield NO OBSTRUCTIONS
Induction System and Fairing NO OBSTRUCTIONS
Pitot tube NO OBSTRUCTIONS
Frame, front crossbeam, drag strut, and skid for
damage CHECK
Tail rotor pedals for condition and security of
retaining pins (both sides if dual controls) CHECK
Landing light, and forward rotating beacon for
damage or security CHECK
NOTE
: Late model he li cop ters equipped with stan dard
height land ing gear have the land ing light mounted on
the aft cross beam. Late model he li cop ters have strobes
(in lieu of ro tat ing bea con) mounted with nav i ga tion
lights.
VHF antenna for damage or security CHECK
CABIN - LEFT SIDE
Cabin for damage or dents CHECK
Door and latching CHECK
Canopy slat for damage or looseness CHECK
Front oleo damper extension CHECK
Skid tube CHECK
Ground handling wheel (if installed) in up
position with quick-release pin installed. CHECK
Normal Procedures
Pilot's Flight Manual
4-4
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 88 8/4/19 12:45 PM

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