Schweizer S300CBi - User Manual

PUBLICATION NO. CSP-C1-1
PILOT’S FLIGHT MANUAL
CONTAINING THE
FAA APPROVED ROTOCRAFT FLIGHT MANUAL FOR
SCHWEIZER S300CB™/CBi™
HELICOPTER MODEL 269C-1
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erivative work), or used for manufacture for anyone other than Schweizer RSG, LLC. without its written consent,
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Schweizer RSG, LLC. | Fort Worth, TX 76106
CSP book 2..indd 1 8/4/19 12:53 PM

Summary

Section II LIMITATIONS (FAA APPROVED)

Rotorcraft Certification

Flight Limitations

Prohibits IFR, specifies night ops, min crew, and max altitudes.

Flight Limitations Placards

Required placards for operating limitations and gross weight.

Airspeed Limitations

Specifies VNE and altitude reduction for airspeed.

Rotor Speed Limitations

Max and min rotor speed limitations.

Weight and CG Limitations

Max gross weight and center of gravity envelopes.

Power Plant Limitations

Engine RPM limits, idle speed, and clutch engagement speeds.

Fuel System

Instrument Markings

Section III EMERGENCY AND MALFUNCTION PROCEDURES (FAA APPROVED)

Engine Failure - Altitude Above 450 Feet

Steps for engine failure at high altitudes, including autorotation.

Engine Failure - Altitude Above 7 Feet and Below 450 Feet

Procedures for engine failure during takeoff.

Engine Failure - Altitude Below 7 Feet

Actions for engine failure at very low altitudes.

Ditching - Power Off

Steps for ditching the helicopter with power off.

Ditching - Power On

Procedures for ditching the helicopter with power on.

Transmission Warning;Caution Indicators

Fuel Low, Caution Indicator

Clutch Warning Light

Tail Rotor Failure

Corrective actions for complete loss of tail rotor thrust.

Section IV NORMAL PROCEDURES

Preflight Requirements

Pilot’s Preflight Inspection

Visual checks of exterior, cabin, and engine components for wear or damage.

Engine Prestart Cockpit Check

Engine Starting Procedure

Step-by-step guide for starting carbureted and fuel-injected engines.

Engine Starting Procedure - Hot;Flooded Conditions

Rotor Engagement

Steps for engaging the rotor system, including collective and throttle control.

Engine Ground Check

Checks performed on the ground before takeoff, including engine RPM and instruments.

Hovering and Takeoff

Procedures for hovering, lifting off, and initial climb.

Cruise

Practice Autorotation

Use of Carburetor Heat

Landing Approach

Running Landing

Engine Cooling Shutdown

Pilot’s Check of Idle Mixture, Idle Speed, and Fuel Boost Pump

Post Flight Requirements

Section V PERFORMANCE DATA

Performance Data

Section VI WEIGHT AND BALANCE DATA

Weight and Balance Characteristics

Maximum gross weight and reference datum for CG calculations.

Load Limits and Balance Criteria

Helicopter designed to specific loading limitations.

Weight and Balance Determination - Passenger Configuration

Calculating longitudinal CG for passenger configurations.

Permissible Lateral Loadings - Passenger Configuration

Determining lateral CG within limits for passenger configurations.

Schweizer S300CBi Specifications

General

Brand	Schweizer
Model	S300CBi
Category	Toy
Language	English