Initial

Fuel Tank Safety (phase 1)

TRAINING TYPE

Fuel tank safety - video presentation with voice over, online training


TIME REQUIRED

At least 2 hours 27 minutes


CATEGORY

FTS


ABOUT THE COURSE

FTS (phase 1) aviation online training program will include the theoretical background behind the risk of fuel tank safety, concepts to prevent explosions.

The program will includes a short background, showing examples of the FTS accidents and incidents, the description of concept of fuel tank safety and Critical Design Configuration Control Limitations (CDCCL).

The examples of manufacturer's documents showing the CDCCL items, the cases of FTS defects, as well as the examples for maintenance instructions for inspection.


OBJECTIVES

The trainee should, after the completion of the training:

  • Be familiar with the basic elements of the fuel tank safety issues.
  • Be able to give a simple description of the historical background and the elements requiring a safety consideration, using common words and showing examples of non-conformities.
  • Be able to use typical terms.




TARGET GROUP

  • Organization management structure persons,
  • Quality managers
  • Maintenance organization management personnel,
  • Quality auditors,
  • National aviation authority personnel

BENEFITS

  • Flexibility
  • Comfort/Mobility
  • Demo version preview
  • Until course presentation isn't finished - possibility replay training material
  •  No pressure at all
  •  Support
  •  Saving money


METHODS AND CONCEPTION

Everyone can manage the learning pace and learning duration depending on each person possibilities.

You can choose perfect timing and comfortable place with internet access.


NECESSARY CONDITIONS

  • Internet access
  • Fluent technical aviation English language
  • At least 2 hours 30 minutes of learning time

PREREQUISITES

Familiarity with relevant regulations


GROUP SIZE

Unlimited size for online training


EXAMINATION

  • During the FTS (phase 1) online training course, interactive questions are asked, seeking that students better understand course material.
  • No examination will be held.

COMPLETION

Upon successful completion of the FTS (phase 1) aviation online training course (100%), participants will receive online training certificate issued by EASA Part-147 approved Maintenance Training Organization (MTO).

  • Part-147 under approval reference No LT.147.001
  • Part-145 under approval reference LT.145.011
  • Part-CAMO under approval reference No LT.CAMO.0015
  • Part-21 under approval reference EASA.21J.496 and LT.21G.0004
  • ISO 9001:2015 and ISO 14001:2015 

NOTE

  • For private accounts: purchased FTS (phase 1) online training course can be activated within the 6 months past the purchase date. Once the course is activated it must be completed within the period of 2 months.
  • For corporate accounts: purchased FTS (phase 1) online training course can be activated within the 1 year past the purchase date. Once the course is activated it must be completed within the period of 2 months.

CONTENT

  • Introduction
  • The theoretical background behind the risk of fuel tank safety, concepts to prevent explosions
  • The major accidents related to fuel tank systems
  • The requirements of SFAR 88 of the FAA and JAA Interim Policy INT POL 25/12
  • The results of SFAR 88 of the FAA and JAA INT/POL 25/12
  • Airworthiness Limitations and CDCCL in the context of Maintenance Data
  • Examples of defects and the associated repairs as required by the TC / STC holder’s maintenance data

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Fuel Tank Safety (phase 1)

play_circle_outline 66 Chapters
access_time 2 hours 27 minutes
Initial

Syllabus

0
chapter 0
34s

0 Introduction

1
chapter 1
56s

1 General

1.1
chapter 1.1
1min 8s

1.1 Overview

1.2
chapter 1.2
45s

1.2 Objectives of FTS training course

1.3
chapter 1.3
3min 17s

1.3 Personnel involved in FTS training

1.4
chapter 1.4
1min 18s

1.4 Documents forming the legal basis of this training

1.5
Quiz

1.5 Quiz

1.6
Quiz

1.6 Quiz

2.
chapter 2.
7s

2. PART I - The theoretical background behind the risk of fuel tank safety, concepts to prevent explosions

2.1
chapter 2.1
24s

2.1 Overview

2.2
chapter 2.2
1min 50s

2.2 Flash point

2.3
chapter 2.3
36s

2.3 Auto-ignition Temperature

2.4
chapter 2.4
1min 13s

2.4 Jet A1 ID Card

2.5
chapter 2.5
57s

2.5 Russian Jet Fuels

2.6
chapter 2.6
15s

2.6 Gasoline ID Card

2.7
chapter 2.7
52s

2.7 Fire triangle

2.8
chapter 2.8
37s

2.8 Two concepts to prevent explosion

2.9
chapter 2.9
6min 25s

2.9 3 primary phenomena that can result in ignition - electrical arcs and sparks, friction sparks, hot surface ignition or auto-ignition

2.10
chapter 2.10
2min 2s

2.10 Fuel system electrostatics

2.11
chapter 2.11
1min 32s

2.11 Flammability envelope

2.12
chapter 2.12
2min 40s

2.12 Fuel Tank Flammability Exposure

2.13
chapter 2.13
43s

2.13 Stand Alone Approach for Fuel Tank Safety

2.14
chapter 2.14
1min 6s

2.14 Balanced Approaches for Fuel Tank Safety

2.15
chapter 2.15
4min 37s

2.15 Flammability Reduction

2.16
Quiz

2.16 Quiz

2.17
Quiz

2.17 Quiz

2.18
Quiz

2.18 Quiz

3
chapter 3
5s

3 PART II - The major accidents related to fuel tank systems

3.1
chapter 3.1
1min 41s

3.1 Brief History of Accidents

3.1.1
chapter 3.1.1
1min 11s

3.1.1 Brief History of Accidents 1

3.1.2
chapter 3.1.2
3min 32s

3.1.2 Brief History of Accidents 2

3.2
chapter 3.2
2min 15s

3.2 747 TWA 800 Accident on July 17, 1996

3.2.1
chapter 3.2.1
35min 35s

3.2.1 Video of B747 TWA 800 Accident on July 17, 1996

3.2.2
chapter 3.2.2
5min 25s

3.2.2 B747 TWA 800 Accident (continue)

3.3
chapter 3.3
2min 15s

3.3 Bangalore Accident 2006

3.4
Quiz

3.4 Quiz

3.5
Quiz

3.5 Quiz

4
chapter 4
14s

4 PART III - The requirements of SFAR 88 of the FAA and JAA Interim Policy INT POL 25/12

4.1
chapter 4.1
1min 37s

4.1 FAA requirements

4.2
chapter 4.2
33s

4.2 FAA SFAR 88 applicability

4.3
chapter 4.3
2min 2s

4.3 FAA SFAR 88 requirements

4.4
chapter 4.4
7min 15s

4.4 JAA INT/POL 25/12

4.4
Quiz

4.4 Quiz

4.5
Quiz

4.5 Quiz

5
chapter 5
18s

5 PART IV - The results of SFAR 88 of the FAA and JAA INT/POL 25/12

5,1
chapter 5,1
44s

5,1 Results of SFAR-88 & INT/POL 25/12 design review

5,2
chapter 5,2
6min 47s

5,2 Examples of modifications

5.3
chapter 5.3
2min 51s

5.3 Fuel System Airworthiness limitations

5.4
chapter 5.4
3min 48s

5.4 CDCCL

5.5
chapter 5.5
59s

5.5 Airworthiness Limitations Instructions (ALI for Boeing) or Maintenance/Inspection Tasks (for Airbus)

5.6
Quiz

5.6 Quiz

5.7
Quiz

5.7 Quiz

6
chapter 6
12s

6 PART V - Airworthiness Limitations and CDCCL in the context of Maintenance Data

6.1
chapter 6.1
2min 2s

6.1 Manufacturers Documents Showing AWL

6.2
chapter 6.2
2min 35s

6.2 ALI/CDCCL examples from B737NG MPD

6.3
chapter 6.3
1min 51s

6.3 Maintenance/inspection task examples from A318-321 ALS Part 5

6.4
chapter 6.4
1min 42s

6.4 CDCCL examples from A318-321 ALS Part 5

6.5
chapter 6.5
4min 24s

6.5 AWLs in Boeing AMM Procedures

6.6
chapter 6.6
2min 18s

6.6 FAL (CDCCL) in Airbus AMM Procedures

6.7
Quiz

6.7 Quiz

6.8
Quiz

6.8 Quiz

7
chapter 7
12s

7 PART VI - Examples of defects and the associated repairs as required by the TC / STC holders maintenance data

7.1
chapter 7.1
10min 2s

7.1 Examples of Boeing Service Bulletins related with defects and repairs

7.2
chapter 7.2
6min 26s

7.2 Examples of Airbus Service Bulletins related with defects and repairs

7.3
Quiz

7.3 Quiz

8
chapter 8
2min 27s

8 Summary