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Eads Eurocopter BO 105 CBS-5 User Manual

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TITLERev. 1
BO 105 CB-5/CBS-5
APPROVED ROTORCRAFT
FLIGHT MANUAL
Valid for Model BO 105 C Variants:
and Model BO 105 S Variants:
CB-5
CBS-5
Registration No.
Serial No.
LBA Type Certificate No. 3025
THIS MANUAL MUST BE CARRIED IN THE HELICOPTER AT ALL TIMES.
IT IS THE OPERATOR’S RESPONSIBILITY TO MAINTAIN THIS MANUAL IN A
CURRENT STATUS IN ACCORDANCE WITH THE LIST OF EFFECTIVE PAGES.
Second Issue - April 10, 1995
Published by:
EUROCOPTER DEUTSCHLAND GmbH
Postfach 13 53
86603 Donauwörth

Table of Contents

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Eads Eurocopter BO 105 CBS-5 Specifications

General IconGeneral
BrandEads
ModelEurocopter BO 105 CBS-5
CategoryToy
LanguageEnglish

Summary

SECTION 1 GENERAL

SECTION 2 LIMITATIONS

Contains operational constraints and limitations for helicopter use.

SECTION 3 EMERGENCY AND MALFUNCTION PROCEDURES

Provides procedures for handling emergencies and malfunctions.

SECTION 5 PERFORMANCE DATA

Presents data for flight planning and performance calculations.

SECTION 6 MASS AND BALANCE

Covers helicopter loading and center of gravity calculations.

LOG OF REVISIONS

LIST OF EFFECTIVE PAGES

SECTION 2 LIMITATIONS

2.6 MASS AND LOAD LIMITATIONS

Covers maximum and minimum gross mass and loading constraints.

2.7 CENTER OF GRAVITY LIMITATIONS

Specifies longitudinal and lateral CG limits for safe operation.

2.8 AIRSPEED LIMITATIONS

Lists airspeed limits for forward, sideward, and rearward flight.

2.12 ENGINE AND TRANSMISSION POWER LIMITATIONS

Details torque, temperature, and RPM limits for engines and transmission.

2.14 FUEL LIMITATIONS

Provides specifications and limitations for authorized fuels and additives.

SECTION 3 EMERGENCY AND MALFUNCTION PROCEDURES

3.2 WARNING AND CAUTION LIGHTS

Explains the meaning and indications of warning and caution lights.

3.3 ENGINE EMERGENCY CONDITIONS

Details procedures for various single and double engine failures.

3.4 FIRE EMERGENCY CONDITIONS

Provides procedures for cabin/cargo compartment and electrical fires.

3.5 TAIL ROTOR FAILURE CONDITIONS

Outlines procedures for tail rotor drive failure and pedal vibrations.

3.6 SYSTEM EMERGENCY/MALFUNCTION CONDITIONS

Covers malfunctions in electrical, trim actuator, fuel pump, and hydraulic systems.

SECTION 4 NORMAL PROCEDURES

4.3 PREFLIGHT CHECK

Details general, exterior, and interior checks before flight.

4.4 STARTING ENGINES

Provides step-by-step procedures for starting the first and second engines.

4.6 PRE-TAKEOFF CHECK

Details checks to be performed on the ground and at hover before takeoff.

SECTION 5 PERFORMANCE DATA

5.2 INFLIGHT POWER CHECKS

Details power assurance and engine trend checks.

5.5 HEIGHT-VELOCITY DIAGRAMS

Illustrates critical altitude/airspeed envelopes for engine failure scenarios.

5.6 HOVER CEILING

Presents charts for maximum hover gross mass at various conditions.

5.7 TAKEOFF PERFORMANCE

Details takeoff procedures and required distances.

5.9 LANDING PERFORMANCE

Covers landing procedures and distances, including OEI scenarios.

SECTION 6 MASS AND BALANCE

6.3 LOADING DATA

Lists item locations for calculating longitudinal CG.

SECTION 8 HANDLING, SERVICING, AND MAINTENANCE

SECTION 11 SPECIAL OPERATIONS SUPPLEMENTS

A.3 EMERGENCY AND MALFUNCTION PROCEDURES

Covers OEI procedures for takeoff and landing.

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