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BRM Aero BRISTELL B23 - User Manual

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Document No.: ADXC-73-001-AFM
Non-approved page
Revision: A2
I
Date of Issue: 15.04.2021
The technical content of this document is approved under the authority of the DOA ref. EASA. 21J.411
BRISTELL B23
AIRCRAFT FLIGHT MANUAL

Table of Contents

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Summary

Contact Data for Occurrences

SECTION 0 TECHNICAL INFORMATION

0.1 Record of revisions

Details of revisions made to the manual, including dates and changes.

0.2 List of Effective Pages

Index of all pages included in the manual and their revision status.

0.3 Table of Contents

List of sections and their corresponding page numbers.

0.4 Symbols, Abbreviations, Terminology

Definitions of symbols, abbreviations, and technical terms used in the manual.

SECTION 1 GENERAL

1.1 Introduction

Overview of the flight manual's purpose and content for pilots and operators.

1.2 Certification basis

Details the aircraft's approval by the European Union Aviation Safety Agency.

1.3 Warnings, cautions and notes

Defines the meaning and application of warning, caution, and note statements.

1.4 Descriptive data

Provides detailed technical specifications and characteristics of the aircraft.

SECTION 2 LIMITATIONS

2.1 Introduction

Overview of operating limitations, instrument markings, and basic placards for safe operation.

2.2 Airspeed

Details critical airspeed limitations including VNE, VNO, VA, and VFE.

2.4 Powerplant

Provides specifications for the engine, coolant, oil, fuel pressure, and exhaust gas temperature.

2.7 Weight

Specifies maximum takeoff, landing, and baggage weights, plus fuel weight.

2.8 Centre of gravity

Defines the operating CG range and provides a graph for CG limits.

2.15 Other limitations

Covers maximum altitude, OAT range, and autopilot engagement prohibitions.

2.16 Placards

Illustrates various placards and their locations on the aircraft.

2.17 Minimum Equipment

Lists required equipment for VFR-Day and VFR-Night operations.

SECTION 3 EMERGENCY PROCEDURES

3.2 Engine failure

Detailed procedures for engine failure during takeoff run, enroute, or during takeoff.

3.3 In-flight engine restart

Step-by-step guide for attempting an engine restart while in flight.

3.4 Smoke and fire

Procedures for dealing with engine fires on ground or in flight, and cockpit fires.

3.6 Emergency landing

Guidance for emergency landings with and without engine power, and specific landing scenarios.

3.7 Recovery from unusual attitudes

Procedures for recovering from loss of spatial orientation and unintentional spins.

3.9 AEPS activation (if installed - optional equipment)

Instructions for activating the optional Airplane Emergency Parachute System.

SECTION 4 NORMAL PROCEDURES

4.1 Introduction

Overview of checklists and procedures for normal operation.

4.2 Daily inspection

Detailed steps for performing the pre-flight daily inspection of the aircraft.

4.3 Pre-flight inspection

Instructions for conducting a thorough pre-flight inspection to ensure safety.

4.4 Normal procedures and check list

Comprehensive list of normal procedures and checklists for aircraft operation.

SECTION 5 PERFORMANCE

5.1.1 ISA Conversion

Diagram for determining ISA offset based on temperature and pressure altitude.

5.2 Approved data

Presents flight test data for airspeed calibration, stall speeds, and performance reference values.

5.2.2 Stall speeds

Provides wing level and turning flight stall speeds with altitude loss data.

5.2.4 Take-off performance

Provides take-off distances and correction factors for various conditions.

5.2.5 Landing distances

Details landing distances and correction factors for varying conditions.

5.2.6 Climb performance

Presents climb performance data in graphs for different density altitudes and conditions.

SECTION 6 WEIGHT AND BALANCE

6.1 Introduction

Information on aircraft empty weight, center of gravity, and operational weight determination.

6.2 Definitions

Defines basic empty weight, center of gravity, and lever arms relative to the datum.

6.3 Airplane weighing procedure

Step-by-step guide for determining the aircraft's empty weight and CG.

6.5 Loaded Aircraft Weight and CG

Method for determining loaded aircraft weight and CG using blank forms and graphs.

6.6 Equipment list

List of all equipment installed in the BRISTELL B23 with masses and locations.

SECTION 7 AEROPLANE AND SYSTEM DESCRIPTION

7.2 Airframe

Describes the main airframe structure: wing, fuselage, and control surfaces.

7.3 Flight controls

Details the operation of aileron, elevator, rudder, and flap controls.

7.4 Instrument panel and glare shield

Overview of the instrument panel layout and controls.

7.10 Fuel system

Details the fuel system, including tanks, selector valve, pumps, and quantity indication.

7.11 Electrical system

Describes the 14V DC electrical system, generators, battery, and bus system.

7.14 Avionics

Overview of the avionics system components, including Garmin and L-3 EFIS units.

SECTION 8 AEROPLANE HANDLING, SERVICING AND MAINTENANCE

8.1 Introduction

Overview of factory-recommended procedures for ground handling and servicing.

8.2 Aeroplane inspection periods

Details required inspection and maintenance based on referenced manuals.

8.3 Aeroplane alterations or repairs

Guidelines for approved alterations and repairs, emphasizing authorized personnel and parts.

8.4 Ground handling

Procedures for towing, parking, and mooring the aircraft.

8.5 Cleaning and care

Instructions for cleaning painted surfaces, propeller, engine, and interior.

SECTION 9 SUPPLEMENTS

9.1 Introduction

Information on supplements for operating optional systems and equipment.

9.2 List of supplements

List of supplements with document numbers, titles, and installation status.

9.3 Supplements inserted

Placeholder for inserted supplement details.

BRM Aero BRISTELL B23 Specifications

General IconGeneral
BrandBRM Aero
ModelBRISTELL B23
CategoryAircrafts
LanguageEnglish