Boeing 757-200/300 RB211 & PW2000 General Familiarisation

The Boeing 757-200/300 RB211 & PW2000 General Familiarization course meets ATA 104 Specification Level I: General Familiarization; a brief overview of the airframe, systems, and powerplant as outlined in the Systems Description Section of the Aircraft Maintenance Manual.

The course complies with EASA’s knowledge LEVEL 1 definition as contained in Regulation EU No. 1321/2014, Part 66, Appendix III Basic Knowledge Requirements. It provides familiarization with the principal elements of the subject, ensuring that:

(a) The applicant should be familiar with the basic elements of the subject.
(b) The applicant should be able to give a simple description of the whole subject, using common words and examples.
(c) The applicant should be able to use typical terms.

This self-study course will take approximately 40 hours. Students must pass a quiz at the end of each ATA chapter before the next chapter is unlocked. Upon successful completion of the course, a certificate will be issued.

Course Objectives: Upon completion of the course, the student will be able to:

Identify safety precautions related to the airframe, systems, and powerplant.
Identify maintenance practices important to the airframe, systems, and powerplant.
Define the general layout of the aircraft’s major systems.
Define the general layout and characteristics of the powerplant.
Identify special tooling and test equipment used with the aircraft.

SYSTEM REQUIREMENTS

The course is compatible with PC, laptop, tablet, Android, and iPhone devices. An internet connection is required.

STUDY TIME

Course completion time varies per individual; however, we estimate approximately 40 hours will be required. You have 6 months to complete the course, with your progress saved so you can stop and restart as needed. Once completed, you have an additional 90 days to review the course.

SUPPORT

Should you need assistance during the course, feel free to contact us during normal working hours for support.

WHY USE OUR GENERAL FAMILIARIZATION COURSES?

Our online Boeing 757-200/300 RB211 & PW2000 General Familiarization course provides an excellent solution for training engineers or company support staff. It offers the required in-depth aircraft type knowledge with the flexibility of distance learning.

WHY TRUST US WITH YOUR TRAINING?

Our Boeing 757-200/300 RB211 & PW2000 General Familiarization course is designed and produced by EASA and UK CAA B1/B2 Engineers, Type Instructors, and Part 147 Training Managers. We ensure that each course covers all relevant ATA chapters.

DETAILED COURSE SYLLABUS

The Boeing 757-200/300 RB211 & PW2000 General Familiarization course begins with an aircraft type introduction, then covers each ATA chapter to approximately Part 66 Level 1:

ATA 00 – AIRCRAFT INTRODUCTION

Aircraft General: General construction and design features of the aircraft.
Aircraft Construction: Structural elements of the fuselage, wings, and empennage.
Fuselage Section: Detailed layout of body stations and sections.
Wing Structure: Overview of primary and secondary wing structures, including fuel tanks and load-bearing elements.
Horizontal and Vertical Stabilizers: Structure and functionality of stabilizers and rudders.
Zone System: Explanation of aircraft zoning and identification of maintenance zones.
Access Panel Zones: Familiarization with service and access panels for inspections and repairs.
Aircraft General Servicing: Routine checks, servicing points, and jacking/leveling procedures.
Levelling and Jacking Points: Axle and fuselage jacking points, procedures, and safety.

ATA 21 – AIR CONDITIONING

Temperature Control: Operation and control of temperature regulation systems.
Distribution Systems: Airflow distribution to cockpit, cabin, and cargo compartments.
Pressurization System: Automatic pressure control, cabin altitude controls, and emergency depressurization systems.
Recirculation Systems: Air recirculation and cooling processes.
Air Conditioning Packs: Operation and maintenance of air conditioning packs and valves.
Component Locations: Layout of air conditioning system components, including ECS bays and control panels.

ATA 22 – AUTOFLIGHT

Automatic Flight Control: Overview of the Autopilot system and components.
Yaw Damper System: Yaw control, stabilization features, and control panel.
Thrust Management: Engine thrust management during various flight phases.
Flight Control Systems: Description of Flight Director modes, control surfaces, and stabilization functions.
Modal Suppression Accelerometer: Understanding yaw damper suppression and stabilizer trim functions.

ATA 23 – COMMUNICATIONS

VHF and HF Systems: Voice and data communications systems and control panels.
SELCAL: Selective calling system functionality and configuration.
ACARS: Aircraft Communication Addressing and Reporting System for data link communication.
Interphone System: Communication between cockpit, cabin, and ground crew.
Voice Recorder System: Functionality and operation of cockpit voice recorders.

ATA 24 – ELECTRICAL SYSTEMS

AC and DC Generation: Overview of power generation and distribution systems.
Battery Systems: Standby power and battery backup systems.
Electrical Load Management: Load shedding, power prioritization, and control mechanisms.
External Power: Procedures for using external power sources during ground operations.
Electrical Control Panels: Operation of electrical power and generation control panels.

ATA 25 – EQUIPMENT AND FURNISHINGS

Passenger Compartment Equipment: Configuration of seats, galleys, lavatories, and emergency equipment.
Cargo Compartments: Layout and handling of cargo areas, including loading systems and securing mechanisms.
Flight Compartment: Overview of flight crew equipment and cockpit layout.

ATA 26 – FIRE DETECTION

Fire Detection: Engine, APU, and cargo fire detection systems, including smoke detectors.
Fire Extinguishing Systems: Operation of fire suppression systems, including engine fire extinguishers and lavatory extinguishing systems.
Fire Warnings: Procedures for fire warning annunciation and cockpit controls.

ATA 27 – FLIGHT CONTROLS

Primary Flight Controls: Operation of ailerons, elevators, and rudders.
Secondary Flight Controls: Functionality of spoilers, speed brakes, slats, and flaps.
Autopilot Interface: Integration of flight control systems with autopilot modes.
Hydraulic Flight Controls: Use of hydraulic systems to power flight control surfaces.

ATA 28 – FUEL SYSTEMS

Fuel Storage: Layout and capacity of fuel tanks, including wing and center tanks.
Fuel Distribution: Fuel transfer, feed, and crossflow operations.
Fuel Quantity Indication: Methods of measuring and indicating fuel quantity and pressure.

ATA 29 – HYDRAULIC POWER

Hydraulic Systems: Redundant hydraulic power systems, including center, left, and right systems.
Power Distribution: Flow control, heat exchangers, and safety measures for hydraulic systems.
Hydraulic Ground Servicing: Procedures for ground maintenance of hydraulic systems.

ATA 30 – ICE AND RAIN PROTECTION

Wing and Engine Anti-Ice: Functionality of thermal anti-ice systems for wings and engine nacelles.
Probe Heating: Heating systems for pitot-static tubes, angle of attack sensors, and TAT probes.
Windshield Anti-Ice: Anti-ice and defogging systems for cockpit windows.
Rain Protection: Wiper systems and drain mast heating mechanisms.

ATA 31 – INDICATING AND RECORDING SYSTEMS

Flight Data Recording: Overview of FDR systems, including data collection, storage, and fault reporting.
EICAS: Engine Indication and Crew Alerting System for monitoring engine performance and aircraft status.
Cockpit Displays: Description of cockpit instrumentation for warning, caution, and advisory alerts.

ATA 32 – LANDING GEAR

Landing Gear Extension and Retraction: Normal and alternate methods for extending and retracting landing gear.
Brake Systems: Brake operation, anti-skid, and autobrake functions.
Steering: Nose wheel steering mechanisms and associated control systems.

ATA 33 – LIGHTS

Interior and Exterior Lighting: Description of cockpit, cabin, and exterior lights, including landing and navigation lights.
Emergency Lighting: Overview of exit and emergency lighting systems for safe evacuation.

ATA 34 – NAVIGATION SYSTEMS

EFIS: Electronic Flight Instrument System operation, including PFD and MFD displays.
TCAS: Traffic Collision Avoidance System operation and functionality.
ILS and GPS: Instrument Landing System and Global Positioning System usage during navigation.
Weather Radar: Operation and use of weather radar for detecting turbulence and precipitation.

ATA 35 – OXYGEN

Crew Oxygen: Emergency oxygen systems for flight crew, including masks and portable units.
Passenger Oxygen: Emergency oxygen deployment systems for passengers.
Portable Oxygen: Overview of portable oxygen systems and refilling procedures.

ATA 36 – PNEUMATICS

Pneumatic Air Supply: Operation of engine and APU bleed air systems.
Temperature Regulation: Control of air temperature and flow in pneumatic systems.
Overheat Protection: Mechanisms for preventing overheating in pneumatic lines.

ATA 38 – WATER WASTE

Potable Water System: Water storage, distribution, and heating for lavatories and galleys.
Vacuum Waste System: Operation of vacuum waste systems, including toilet assemblies and waste tank management.

ATA 49 – AUXILIARY POWER

APU Operation: Auxiliary Power Unit operation, fuel, and cooling systems.
APU Start/Stop: Procedures for starting and stopping the APU, including bleed air operation.
Cooling and Lubrication: Cooling air and lubrication systems for APU operation.

ATA 52 – DOORS

Passenger and Cargo Doors: Operation of entry, emergency exit, and cargo doors, including door warning systems.
Flight Deck Door: Description of the reinforced cockpit door and locking mechanisms.

ATA 71-80 POWERPLANT – PRATT & WHITNEY PW2000 & ROLLS ROYCE RB211

Engine Systems: Overview of powerplant architecture, fuel systems, thrust reversers, and oil systems.
Electronic Engine Control (EEC): Functionality of engine control systems, including fuel flow and temperature monitoring.
Ignition and Starting: Procedures for engine start-up and shutdown, and emergency procedures for engine overspeed and fire.