Model 269C Helicopter
Pilot's Flight Manual
Reissued: 16 Jan 2019
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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 - 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
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
