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Schweizer S300C 269C - Default Chapter; Table of Contents

Schweizer S300C 269C
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Model 269C Helicopter Pilot's Flight Manual
Reissued: 16 Jan 2019
Fiii
STNET NOC FO ELB AT
Section Title Page
I
II
III
GENERAL
Introduction ................... 1-1
Scope ...................... 1-1
Organization .................. 1-1
Method of Presentation ............ 1-4
Helicopter Description ............. 1-4
Helicopter Certification ............ 1-5
Design and Construction Description ..... 1-6
General Dimensional Data ........... 1-9
Conversion Tables - MPH/K/KmH ...... 1-16
2-1 Rotorcraft Certification ......... 2-1
2-2 Flight Limitations ............ 2-1
2-3 Flight Limitations Placards ....... 2-2
2-4 Multipurpose Utility Operation ..... 2-4
2-5 Airspeed Limitations .......... 2-4
2-6 Rotor Speed Limitations ........ 2-4
2-7 Weight and CG Limitations....... 2-6
2-8 Center of Gravity (CG Envelope) ... 2-6
2-9 Power Plant Limitations (Lycoming
HIO-360-DIA) .............. 2-8
2-10 Fuel System ............... 2-9
2-11 Auxiliary Fuel Tank Calibration .... 2-9
2-12 Aircraft Instruments ........... 2-10
EMERGENCY AND MALFUNCTION
PROCEDURES (FAA APPROVED)
3-1 Engine Failure - Altit
ude Above
450 Feet ................. 3-1
3-2 Engine Failure - Altitude Above 7
Feet and Below 450 Feet ........ 3-1
3-3 Engine Failure - Altitude
Below 7 Feet ............... 3-2
3-4 Ditching - Power Off .......... 3-2
3-5 Ditching - Power On .......... 3-2
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
LIMITATIONS (FAA APPROVED)
CSP Book 1 CSP-C-1.indd 3 8/4/19 12:45 PM

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