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Schweizer 269C-1 - Default Chapter; Table of Contents

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Pilot's Flight Manual
Reissued: 16 Jan 2019 Fiii
TA BLE OF CON TENTS
Section Title Page
I
II
III
GENERAL
Introduction ................... 1-1
Scope ...................... 1-1
Organization .................. 1-1
Method of Presentation ............ 1-3
Helicopter Description ............. 1-4
Helicopter Certification ............ 1-4
Design and Construction Description..... 1-5
General Dimensional Data ........... 1-8
Conversion Tables - KT/MPH/KmH ..... 1-13
2-1 Rotorcraft Certification ......... 2-1
2-2 Flight Limitations ............ 2-1
2-3 Flight Limitations Placards ....... 2-2
2-4 Multipurpose Utility Operation .... 2-3
2-5 Airspeed Limitations .......... 2-3
2-6 Rotor Speed Limitations ........ 2-3
2-7 Weight and CG Limitations ...... 2-5
2-8 Power Plant Limitations
(Lycoming HO-360-C1A)
(Lycoming HIO-360-G1A) ....... 2-6
2-9 Fuel System ............... 2-7
2-10 Instrument Markings .......... 2-8
EMERGENCY AND MALFUNCTION
PROCEDURES (FAA APPROVED)
3-1 Engine Failure - Altitude 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
SCHWEIZER
Model 269C-1 Helicopter
LIMITATIONS (FAA APPROVED)
CSP book 2..indd 3 8/4/19 12:53 PM

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