aircraft maintenance training
CARC Yearly Plan - 2020
Icing/De-Icing /Anti-Icing
Objective:
To familiarize the candidates with Federal Aviation Regulations (FAR) and Joint Aviation Regulation (JAR).
Minimum prerequisites:
None
Duration:
12 Hours
Human Factors For Maintenance Engineers.
Objective:
To improve safety standards, reduce errors and prevent accidents.
Minimum prerequisites:
None
Duration:
12 Hours.
Aircraft Inspection
Objective:
To familiarize the candidates with Federal Aviation Regulations (FAR), Joint Aviation Regulation (JAR) and the inspection of aircraft structure and systems.
Minimum prerequisites
None
Duration:
60 Hours
ETOPS Maintenance
Objective:
To instruct maintenance engineers on ETOPS basics and technical requirements based on operator ETOPS manual.
Minimum prerequisites
None
Duration:
12 Hours.
RVSM Maintenance
Objective:
To instruct maintenance engineers on RVSM basics and technical requirements based on operator maintenance manual.
Minimum prerequisites:
None
Duration:
6 Hours
Safety Management System (SMS) and Quality Control
Objective:
The most important aim of this course is that the trainee must understand the safety management and recognize the four basic elements of the Safety Management System (SMS) and understand the need of quality system and to do his role in which will help achieving a positive safety culture and implanting the quality system,.
Minimum prerequisites
None
Duration:
36 Hours.
Internal Auditing
Objectives:
- Measure the objective evidence of an organization's degree of compliance with regulatory requirements
- Present your assessments in a clear and concise reporting format
- Apply auditing requirements to the aviation industry and aviation authorities
Minimum prerequisites:
None
Duration:
30 Hours
Fuel Tank Safety Level II
Objective:
On successful completion of the course the student will be familiar to the background and history of the theoretical and practical elements of the Fuel Tank Safety (FTS) as required by EASA and FAA, have an overview of Special Federal Aviation Regulations (SFARs) from 14 CFR SFAR 88 of the FAA and of JAA Temporary guidance Leaflet TGL 47, be able to give a detailed description of the concept of ALI, CDCCL and AWL.
Minimum prerequisites
None
Duration:
12 Hours.
Electrical Wiring Interconnection System (EWIS)
Objectives:
After completion of the course, the trainee should show competency of demonstrate the safe handling of airplane electrical systems, Line Replaceable Units (LRU), tooling, troubleshooting procedures, electrical measurement, the construction and navigation of the applicable wiring practices manual.
Minimum prerequisites
None
Duration:
18 Hours
CFM56-5 Engine Run Up
Objectives:
Upon completion of this course the trainee shall be able to:
• Describe the relevant safety precautions
• Identify and use appropriate aircraft documentation
• Perform the normal and abnormal engine start procedures
• Perform procedures, to assess the behavior and performance of the engine
• Perform system, engine and component functional checks and adjustments as specified in the maintenance manual
• Correlate Information for the purpose of making decisions in respect to fault diagnosis and rectification
EASA 147 A318/A319/A320/A321 T1/B1+T2/B2 (CFM56-IAE V2500) (Theoretical & Practical)
Objectives:
Upon completion of the course, the students will be able to:
• Recall the normal function of these systems as applicable; electrical, fuel, auxiliary power unit, power plant, hydraulic power, landing gear, flight controls, pneumatic power, air conditioning, fire protection, oxygen, water and waste, equipment and furnishings, lights, doors, windows, indicating, recording, communication, navigation and auto flight. • Identify the interfaces between all airframe systems.
CFM56-5 Engine Maintenance
Objectives:
Upon completion of this course the student will be able to:
IAE V2500 Engine Maintenance
Objectives:
Upon completion of this course the student will be able to:
• Identify and locate components for each engine part.
• Describe the function of the subsystems and identify its interface.
• Servicing procedures of engine components.
• Be able to safely operate the engine after a major repair and/or replacement of engine Components.
• Identify normal and abnormal start procedures.
A320 (V2500-A5) Engine Run Up
Objectives:
Upon completion of this course the trainee shall be able to:
A320 Vs. A321
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
A320 Initial Type Rating Course
Duration:
A320 Vs. A319
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
A320 Initial Type Rating Course
Duration:
A319/A320/A321 Vs. Enhanced A318/ A319/A320/A321 (B1+B2)
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
A319/A320/A321 Initial Type Rating Course
CFM56-5 Vs. V2500
Objectives:
- To provide the systems differences between the two Engines.
- Describe the function of the systems and identify its interface.
- Identify and explain controls and indications associated with the engine and its components.
- Servicing procedures of aircraft engine and its components.
Minimum prerequisites:
Initial A320 CFM56-5 or A320 V2500-A1/A5 course
Duration:
12 Hours
EASA 147 A330 T1/B1+T2/B2 (PW4000)
Objectives:
EASA 147 A330 T1/B1+T2/B2 (RR RB 211 Trent 700)
Objectives:
EASA 147 A330 T1/B1+T2/B2 (GE CF6)
Objectives:
EASA 147 A330 (RR RB 211 TRENT 700) To A340 (CFM56) Differences T1/B1+T2/B2
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites
EASA 147 A330 (PW4000) To A340 (CFM56) Differences T1/B1+T2/B2
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites
EASA 147 A330 (GE CF6) To A340 (CFM56) Differences T1/B1+T2/B2
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites
EASA 147 A330 (RR RB211 Trent 700) To A330 ( GE CF6 ) Difference
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites
EASA 147 A330 (RR RB211 Trent 700) To A330 ( PW4000 )
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites
EASA 147 A330 (PW4000) To A330 (RR RB211 Trent 700)
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites
EASA 147 A330 (PW4000) To A330 (GE CF6) Difference
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
EASA 147 A330 (GE CF6) To A330 (RR RB211 Trent 700) Difference
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites
EASA 147 A330 (GE CF6) To A330 (PW4000) Difference
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
EASA 147 A340 (CFM56) To A330 (RR RB211 Trent 700 ) Differences T1/B1+T2/B2
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
EASA 147 A340 (CFM56) To A330 (PW 4000) Differences T1/B1+T2/B2
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
EASA 147 A340 (CFM56) To A330 (GE CF6 ) Differences T1/B1+T2/B2
Objectives:
- To provide the systems differences between the two models.
- Identify and locate components of the Aircraft.
- Describe the function of the systems and identify its interface.
- Identify and explain the controls associated with each system including its indications and annunciators associated with it.
- Servicing procedures of aircraft systems and components.
Minimum prerequisites:
EASA 147 A340 (CFM56-5C) T1/B1+T2/B2
Objectives:
Upon completion of the course, the students will be able to:
· Recall the normal function of these systems as applicable; electrical, fuel, auxiliary power unit, power plant, hydraulic power, landing gear, flight controls, pneumatic power, air conditioning, fire protection, oxygen, water and waste, equipment and furnishings, lights, doors, windows, indicating, recording, communication, navigation and auto flight.
EASA 147Embraer ERJ-170/190 (GE CF34) T1/B1+T2/B2
Objectives:
Upon completion of the course, the students will be able to:
GE CF34 Engine Maintenance
Objectives:
Upon completion of this course the student will be able to:
GE CF34 Engine Run Up
Objectives:
Upon completion of this course the trainee shall be able to:
CFM56-7B Engine Run Up
Objectives:
Upon completion of this course the trainee shall be able to: