Schweizer RSG, LLC.
Model
269D
Helicopter
Pilot's Flight Manual
Fiii
Reissued:
16
Jan 2019
TABLE OF CONTENTS
Section
Title
Page
I
II
III
GENERAL
Introduction . . . . . . . . . . . . . . . . . . . . .
1-1
Scope . . . . . . . . . . . . . . . . . . . . . . . .
1-1
Organization . . . . . . . . . . . . . . . . . . . .
1-1
Method of Presentation . . . . . . . . . . . . . .
1-4
Helicopter Description . . . . . . . . . . . . . . .
1-5
Helicopter Certification . . . . . . . . . . . . . .
1-5
Design and Construction
. . . . . . . . . . . . .
1-6
General Dimensional Data . . . . . . . . . . . . .
1-9
Control Rigging. . . . . . . . . . . . . . . . . . .
1-12
LIMITATIONS
(FAA APPROVED)
2-1.
Rotorcraft Certification . . . . . . . . . . .
2-1
2-2.
Flight Limitations . . . . . . . . . . . . . .
2-1
2-3.
Flight Restrictions . . . . . . . . . . . . . .
2-2
2-4.
Multipurpose Utility Operations . . . . . .
2-4
2-5.
Airspeed Limits . . . . . . . . . . . . . . .
2-4
2-6.
Rotor Speed Limits . . . . . . . . . . . . .
2-4
A
2-7.
Weight Limitations . . . . . . . . . . . . .
2-4
A
2-8.
Center of Gravity (CG Envelope) . . . . .
2-6
2-9.
Power Plant Limits -
Rolls Royce Model 250-C20W . . . . .
2-9
2-10.
Fuels . . . . . . . . . . . . . . . . . . . . .
2-11
2-11.
Instrument Markings . . . . . . . . . . . .
2-13
2-12.
Instrument Markings - 250-C20W . . . . .
2-15
2-13.
Limitations Placards, V
NE
(250-C20W) . .
2-16
2-14.
Limitations Placards . . . . . . . . . . . .
2-17
EMERGENCY
AND
MALFUNCTION
PROCEDURES
(FAA APPROVED)
3-1.
Engine Failure . . . . . . . . . . . . . . . .
3-2
3-2.
Engine Failure - Cruising at Altitudes 450
Feet and Above . . . . . . . . . . . . . .
3-3
3-3.
Engine Failure - Altitude Above 8 Feet and
Below 450 Feet . . . . . . . . . . . . . .
3-4
3-4.
Engine Failure - Altitude Below 8 Feet . .
3-4
Book 3.indd 3
8/4/19 1:25 PM
