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Schweizer 269C-1 - User Manual

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PUBLICATION NO. CSP-C1-1
PILOT’S FLIGHT MANUAL
CONTAINING THE
FAA APPROVED ROTOCRAFT FLIGHT MANUAL FOR
SCHWEIZER S300CB™/CBi™
HELICOPTER MODEL 269C-1
d
vio-l
in the
Warning:
This document, or an embodiment of it in any media, discloses information which is proprietary, is the property of
Schweizer RSG, LLC.; is an unpublished work protected under applicable copyright laws, and is delivered on the
express condition that it is not to be used, disclosed, reproduced, in whole or in part (including reproduction as a
erivative work), or used for manufacture for anyone other than Schweizer RSG, LLC. without its written consent,
and that no right is granted to disclose or so use any information contained herein. All rights reserved. Any act in
ation of applicable law may result in civil and criminal penalties.
Export Warning
These commodities, technical data or software are subject to the export control of either the International Traffic in
Arms Regulations (ITAR) or the Export Administration Regulations (EAR) and cannot be exported without the prior
authorization of either the Department of State or the Department of Commerce. The term “Export” includes disclo-
sure and/or provision of access to commodities, technical data or software to or by foreign nationals (whether located
United States or abroad). This requirement applies also applies to foreign national employees of U.S. Compa-
nies and their foreign subsidiaries
Schweizer RSG, LLC. | Fort Worth, TX 76106
CSP book 2..indd 1 8/4/19 12:53 PM

Table of Contents

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Summary

SECTION II LIMITATIONS (FAA APPROVED)

FLIGHT LIMITATIONS

Critical operational restrictions for safe flight.

WEIGHT AND CG LIMITATIONS

Center of gravity and weight constraints for safe operation.

SECTION III EMERGENCY AND MALFUNCTION PROCEDURES (FAA APPROVED)

ENGINE FAILURE - ALTITUDE ABOVE 450 FEET

Steps for handling engine failure at higher altitudes.

DITCHING - POWER OFF

Procedures for ditching the helicopter without engine power.

TAIL ROTOR FAILURE

Corrective actions for loss of tail rotor control.

ELECTRICAL FIRE - IN FLIGHT

Actions to take if an electrical fire occurs during flight.

SECTION IV NORMAL PROCEDURES (FAA APPROVED)

PILOT’S PREFLIGHT INSPECTION

Detailed checklist for pre-flight aircraft checks.

HOVERING AND TAKEOFF

Procedures for initiating hover and takeoff.

SECTION V PERFORMANCE DATA (FAA APPROVED)

SECTION VI WEIGHT AND BALANCE DATA

Schweizer 269C-1 Specifications

General IconGeneral
BrandSchweizer
Model269C-1
CategoryToy
LanguageEnglish

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