Air Transport Safety : A school english presentation has been given in 2007. It also talks about the crash of Tuninter Flight 1153 occured in August 2005.
An endeavor to approach or remind some useful terms of Aviation,ideal for starting up Flight Attendants provides just a small idea of a such a unique occupation....
An endeavor to approach or remind some useful terms of Aviation,ideal for starting up Flight Attendants provides just a small idea of a such a unique occupation....
Malaysia airlines flight mh370: what went wrong ?Dominique Touel
This presentation has been given in AeroDAY'14 in Tunis Tunisia in May the 3rd, 2014. It's another point of view about what happened to Malaysian Boeing B777 crashed in the indian ocean in march the 3rd, 2014.
This presentation tells about how the Malaysian Aircraft MH-370 is disappeared and what must have happened to it ..
The conclusion we gave is not a real one.. We have arrived at our own conclusion...
Laporan ini disusun sebagai salah satu tugas besar mata kuliah
AE3140 Sertifikasi Kelaikudaraan
Disusun oleh:
Mohammad Arif Izzuddin - 13617035
Rais Fadillah - 13617058
I Gede Anjastara Bandem - 13617064
Marco Wijaya - 13617066
David Waldo Parlindungan - 13617069
Dosen:
Dr. Ir. Rais Zain M.Eng.
PROGRAM STUDI TEKNIK DIRGANTARA
FAKULTAS TEKNIK MESIN DAN DIRGANTARA
INSTITUT TEKNOLOGI BANDUNG
2019
Malaysia airlines flight mh370: what went wrong ?Dominique Touel
This presentation has been given in AeroDAY'14 in Tunis Tunisia in May the 3rd, 2014. It's another point of view about what happened to Malaysian Boeing B777 crashed in the indian ocean in march the 3rd, 2014.
This presentation tells about how the Malaysian Aircraft MH-370 is disappeared and what must have happened to it ..
The conclusion we gave is not a real one.. We have arrived at our own conclusion...
Laporan ini disusun sebagai salah satu tugas besar mata kuliah
AE3140 Sertifikasi Kelaikudaraan
Disusun oleh:
Mohammad Arif Izzuddin - 13617035
Rais Fadillah - 13617058
I Gede Anjastara Bandem - 13617064
Marco Wijaya - 13617066
David Waldo Parlindungan - 13617069
Dosen:
Dr. Ir. Rais Zain M.Eng.
PROGRAM STUDI TEKNIK DIRGANTARA
FAKULTAS TEKNIK MESIN DAN DIRGANTARA
INSTITUT TEKNOLOGI BANDUNG
2019
Air transport has become an essential economic and social conduit throughout the world. Beyond the benefits of fast and inexpensive transcontinental travel, air ...
Transportation is the movement of products from one node in the distribution channel to another.
Types of transportation are explained in detail in the presentation
Fatigue life estimation of rear fuselage structure of an aircrafteSAT Journals
Abstract Integrity of the airframe structure is achieved through rigorous design calculations, stress analysis and structural testing. Finite element method (FEM) is widely used for stress analysis of structural components. Each component in the airframe becomes critical based on the load distribution, which in-turn depends on the attitude of the aircraft during flight. Fuselage and wing are the two major components in the airframe structure. The current study includes a portion of the fuselage structure. Empennage is the rear portion of the aircraft, which consists of rear fuselage, Horizontal tail and vertical tail. The air loads acting on the HT also get transferred to rear portion of the fuselage. First step in ensuring the safety of the structure is the identification of critical locations for crack initiation. This can be achieved through detailed stress analysis of the airframe In this project one of the major stress concentration areas in the fuselage is considered for the analysis. Rear fuselage portion with a cargo door cutout region will be analysed. The structure considered for the stress analysis consists of skin, bulkheads and longerons, which are connected to each other through rivets. Aerodynamic load acting on the aircraft components is a distributed load. Depending on the mass distribution of the fuselage structure the inertia forces will vary along the length of the fuselage. The inertia force distribution makes the fuselage to bend about wing axis. During upward bending, bottom portion of the fuselage will experience tensile stress. A cutout region in the tensile stress field will experience high stress due to concentration effect. These high stress regions will be probable fatigue crack initiation locations in the current work, fatigue damage calculation will be carried out to estimate the fatigue life of the structure under the fluctuating loads experienced during flight. Miner’s rule will be adopted for fatigue damage calculation. Keywords: Transport aircraft, Rear fuselage, Cargo door, Finite element method, Stress concentration, Fatigue damage, Miner’ rule
CHC Safety & Quality Summit 2016 - Risk Culture in Commercial Air TransportCranfield University
This presentation was given at the 2016 CHC Safety & Quality Summit in Vancouver. The aim was to present an argument to introduce 'Risk Culture' as a new component of 'Safety Culture. This is an academic research which aims to explore what/how operational risk decisions are made by pilots and engineers and if such decisions are also acceptable at different levels including senior management.
Root cause analysis of The Concorde (Air France Flight 4590) crash, that occurred in Paris in 2000. This document will be updated.
Air France Flight 4590 was a Concorde flight operated by Air France which was scheduled to fly from Charles de Gaulle Airport near Paris, to John F. Kennedy International Airport in New York City. On 25 July 2000, it crashed into a hotel in Gonesse, France. All one hundred passengers and nine crew members on board the flight died. On the ground, four people were killed and one critically injured.
Aircraft accident investigation on an accident which happened on 23 Sep, 1999 in Bangkok Airport , Thiland. Operator of plane was Qantas and plane was Boeing 747-400 registered as VH-OJH.
Leonard Favre Speech at Middle East Corporate Aviation Summit (MECAS 2015) - Al Bateen Executive Airport Abu Dhabi (Aeropodium conference - www.aeropodium.com)
On the afternoon of January 15, 2009, Captain Chesley "Sully" Sullenberger and First Officer Jeff Skiles board US Airways Flight 1549 from LaGuardia Airport to Charlotte Douglas International Airport. Three minutes into the flight, at an approximate altitude of 2,800 ft (850 m), the Airbus A320 strikes a flock of birds, damaging both engines. Without much time to think, they judge themselves unable to reach nearby airports (Teterboro Airport being the closest), and Sully ditches the aircraft on the Hudson River. Though with mild injuries, the crew and passengers evacuate without any fatalities. Sully is hailed a hero, but the incident leaves him traumatized. He tries to find himself able to escape the attention from the press, which is not only targeting him but also his family.
Human Factors in Aviation by Omar KuzbariOmar Kuzbari
Case study on Human Factors in Aviation based on the Air Ontario Flight 1363 Fokker F-28 at Dryden from March 10, 1989 (Ontario) prepared by Omar Kuzbari in 2018.
EMAS - Engineered Material Arrestor System (seminar ppt) Chinnu Mohanan
The purpose of an Engineered Material Arresting System (EMAS) is to stop an aircraft overrun with no human injury and minimal aircraft damage. The aircraft is slowed by the loss of energy required to crush the EMAS material. An EMAS is similar in concept to the runaway truck ramp made of gravel or sand. It is intended to stop aircraft that have overshot a runway when there is an insufficient free space for a standard runway safety area (RSA).
EMAS - Engineered Material Arrestor System Chinnu Mohanan
The purpose of an EMAS is to stop an aircraft overrun with no human injury and minimal aircraft damage. The aircraft is slowed by the loss of energy required to crush the EMAS material. An EMAS is similar in concept to the runaway truck ramp made of gravel or sand. It is intended to stop aircraft that have overshot a runway when there is an insufficient free space for a standard runway safety area (RSA).
We have compiled the most important slides from each speaker's presentation. This year’s compilation, available for free, captures the key insights and contributions shared during the DfMAy 2024 conference.
NUMERICAL SIMULATIONS OF HEAT AND MASS TRANSFER IN CONDENSING HEAT EXCHANGERS...ssuser7dcef0
Power plants release a large amount of water vapor into the
atmosphere through the stack. The flue gas can be a potential
source for obtaining much needed cooling water for a power
plant. If a power plant could recover and reuse a portion of this
moisture, it could reduce its total cooling water intake
requirement. One of the most practical way to recover water
from flue gas is to use a condensing heat exchanger. The power
plant could also recover latent heat due to condensation as well
as sensible heat due to lowering the flue gas exit temperature.
Additionally, harmful acids released from the stack can be
reduced in a condensing heat exchanger by acid condensation. reduced in a condensing heat exchanger by acid condensation.
Condensation of vapors in flue gas is a complicated
phenomenon since heat and mass transfer of water vapor and
various acids simultaneously occur in the presence of noncondensable
gases such as nitrogen and oxygen. Design of a
condenser depends on the knowledge and understanding of the
heat and mass transfer processes. A computer program for
numerical simulations of water (H2O) and sulfuric acid (H2SO4)
condensation in a flue gas condensing heat exchanger was
developed using MATLAB. Governing equations based on
mass and energy balances for the system were derived to
predict variables such as flue gas exit temperature, cooling
water outlet temperature, mole fraction and condensation rates
of water and sulfuric acid vapors. The equations were solved
using an iterative solution technique with calculations of heat
and mass transfer coefficients and physical properties.
Final project report on grocery store management system..pdfKamal Acharya
In today’s fast-changing business environment, it’s extremely important to be able to respond to client needs in the most effective and timely manner. If your customers wish to see your business online and have instant access to your products or services.
Online Grocery Store is an e-commerce website, which retails various grocery products. This project allows viewing various products available enables registered users to purchase desired products instantly using Paytm, UPI payment processor (Instant Pay) and also can place order by using Cash on Delivery (Pay Later) option. This project provides an easy access to Administrators and Managers to view orders placed using Pay Later and Instant Pay options.
In order to develop an e-commerce website, a number of Technologies must be studied and understood. These include multi-tiered architecture, server and client-side scripting techniques, implementation technologies, programming language (such as PHP, HTML, CSS, JavaScript) and MySQL relational databases. This is a project with the objective to develop a basic website where a consumer is provided with a shopping cart website and also to know about the technologies used to develop such a website.
This document will discuss each of the underlying technologies to create and implement an e- commerce website.
Hierarchical Digital Twin of a Naval Power SystemKerry Sado
A hierarchical digital twin of a Naval DC power system has been developed and experimentally verified. Similar to other state-of-the-art digital twins, this technology creates a digital replica of the physical system executed in real-time or faster, which can modify hardware controls. However, its advantage stems from distributing computational efforts by utilizing a hierarchical structure composed of lower-level digital twin blocks and a higher-level system digital twin. Each digital twin block is associated with a physical subsystem of the hardware and communicates with a singular system digital twin, which creates a system-level response. By extracting information from each level of the hierarchy, power system controls of the hardware were reconfigured autonomously. This hierarchical digital twin development offers several advantages over other digital twins, particularly in the field of naval power systems. The hierarchical structure allows for greater computational efficiency and scalability while the ability to autonomously reconfigure hardware controls offers increased flexibility and responsiveness. The hierarchical decomposition and models utilized were well aligned with the physical twin, as indicated by the maximum deviations between the developed digital twin hierarchy and the hardware.
Student information management system project report ii.pdfKamal Acharya
Our project explains about the student management. This project mainly explains the various actions related to student details. This project shows some ease in adding, editing and deleting the student details. It also provides a less time consuming process for viewing, adding, editing and deleting the marks of the students.
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Dr.Costas Sachpazis
Terzaghi's soil bearing capacity theory, developed by Karl Terzaghi, is a fundamental principle in geotechnical engineering used to determine the bearing capacity of shallow foundations. This theory provides a method to calculate the ultimate bearing capacity of soil, which is the maximum load per unit area that the soil can support without undergoing shear failure. The Calculation HTML Code included.
An Approach to Detecting Writing Styles Based on Clustering Techniquesambekarshweta25
An Approach to Detecting Writing Styles Based on Clustering Techniques
Authors:
-Devkinandan Jagtap
-Shweta Ambekar
-Harshit Singh
-Nakul Sharma (Assistant Professor)
Institution:
VIIT Pune, India
Abstract:
This paper proposes a system to differentiate between human-generated and AI-generated texts using stylometric analysis. The system analyzes text files and classifies writing styles by employing various clustering algorithms, such as k-means, k-means++, hierarchical, and DBSCAN. The effectiveness of these algorithms is measured using silhouette scores. The system successfully identifies distinct writing styles within documents, demonstrating its potential for plagiarism detection.
Introduction:
Stylometry, the study of linguistic and structural features in texts, is used for tasks like plagiarism detection, genre separation, and author verification. This paper leverages stylometric analysis to identify different writing styles and improve plagiarism detection methods.
Methodology:
The system includes data collection, preprocessing, feature extraction, dimensional reduction, machine learning models for clustering, and performance comparison using silhouette scores. Feature extraction focuses on lexical features, vocabulary richness, and readability scores. The study uses a small dataset of texts from various authors and employs algorithms like k-means, k-means++, hierarchical clustering, and DBSCAN for clustering.
Results:
Experiments show that the system effectively identifies writing styles, with silhouette scores indicating reasonable to strong clustering when k=2. As the number of clusters increases, the silhouette scores decrease, indicating a drop in accuracy. K-means and k-means++ perform similarly, while hierarchical clustering is less optimized.
Conclusion and Future Work:
The system works well for distinguishing writing styles with two clusters but becomes less accurate as the number of clusters increases. Future research could focus on adding more parameters and optimizing the methodology to improve accuracy with higher cluster values. This system can enhance existing plagiarism detection tools, especially in academic settings.
Cosmetic shop management system project report.pdfKamal Acharya
Buying new cosmetic products is difficult. It can even be scary for those who have sensitive skin and are prone to skin trouble. The information needed to alleviate this problem is on the back of each product, but it's thought to interpret those ingredient lists unless you have a background in chemistry.
Instead of buying and hoping for the best, we can use data science to help us predict which products may be good fits for us. It includes various function programs to do the above mentioned tasks.
Data file handling has been effectively used in the program.
The automated cosmetic shop management system should deal with the automation of general workflow and administration process of the shop. The main processes of the system focus on customer's request where the system is able to search the most appropriate products and deliver it to the customers. It should help the employees to quickly identify the list of cosmetic product that have reached the minimum quantity and also keep a track of expired date for each cosmetic product. It should help the employees to find the rack number in which the product is placed.It is also Faster and more efficient way.
Forklift Classes Overview by Intella PartsIntella Parts
Discover the different forklift classes and their specific applications. Learn how to choose the right forklift for your needs to ensure safety, efficiency, and compliance in your operations.
For more technical information, visit our website https://intellaparts.com
Understanding Inductive Bias in Machine LearningSUTEJAS
This presentation explores the concept of inductive bias in machine learning. It explains how algorithms come with built-in assumptions and preferences that guide the learning process. You'll learn about the different types of inductive bias and how they can impact the performance and generalizability of machine learning models.
The presentation also covers the positive and negative aspects of inductive bias, along with strategies for mitigating potential drawbacks. We'll explore examples of how bias manifests in algorithms like neural networks and decision trees.
By understanding inductive bias, you can gain valuable insights into how machine learning models work and make informed decisions when building and deploying them.
4. 4
THE PLAN
1. Why do aircraft accidents happen ?
Human factors
Aircraft reliability
Weather and flight conditions
A. Reasons
B. James Reason’s "Swiss Cheese" Model
Companies
The theory
AIR TRANSPORT SAFETY
5. 5
THE PLAN
2. Example : TUNINTER Flight 1153
Informations about the flight
A. Story Reconstruction
B. Investigation
Design of the low level alarm
Aircraft specifications : ATR-72
Problem of interchangeability
Crew qualification
AIR TRANSPORT SAFETY
6. 6
THE PLAN
3. Other examples in Tunisia
Sekorsky HH-3 helicopter : crash
A. Airforce accidents
C-130 Hercules : take-off missing
F-5 fighters : crashs
B. Civilian air transport accidents
EGYPTAIR : crash of B-737
AIR TRANSPORT SAFETY
7. 7
THE PLAN
4. Recommendations and conclusion
B. Conclusion
A. General recommendations
The importance of air transport
The low rate of accidents
Studying air transport accidents
Developing new systems
Crew training
Maintenance
AIR TRANSPORT SAFETY
8. 8AIR TRANSPORT SAFETY
Introduction
Nowadays, aircraft is the most important mean of
transport :
Faster : higher speed and longer distance
Efficient : hundreds of passengers and
tonnes of freight
Safer : One accident for 1.000.000 flights
Inspite of security mesures and defenses, accidents can take
place because of these following reasons :
1. Why do aircraft accidents happen ?
9. 9AIR TRANSPORT SAFETY
A. Reasons
Human capabilities and limitations can influence
task performance and safety inside the aircraft cockpit
and within the maintenance environment.
A.1 Human factors
Pilots, technicians and air traffic controllers are
often the principal actors of many tragedies because
of :
1. Why do aircraft accidents happen ?
10. 10AIR TRANSPORT SAFETY
A. Reasons
Bad attitude towards work and colleagues
Poor communication skills
Etc …
A.1 Human factors
Physical fatigue, tiredness …
Insufficiency of technical knowledge
Routine: same job, same tasks …
Synchronization (time zone, date/night shifts)
1. Why do aircraft accidents happen ?
11. 11AIR TRANSPORT SAFETY
A. Reasons
Systems failures : avionics, engines …
Etc …
A.2 Aircraft reliability
Problems of fuselage and structure
Aircrafts not in accordance with regulations
Problems of design and conception
1. Why do aircraft accidents happen ?
12. 12AIR TRANSPORT SAFETY
A. Reasons
Problems with maintenance and spare parts
: Charter operators
Etc …
A.3 companies
High workload for pilots and technicians
Incompetence of some directors : bad
decisions taken
1. Why do aircraft accidents happen ?
13. 13AIR TRANSPORT SAFETY
A. Reasons
Precipitation, fog and ice
A.4 Weather and atmospheric conditions
Engineers can never control the weather and
atmospheric parameters :
Wind, wind shear, whirlwind : while take off,
approch or landing
Problem of visibility and runway condition
1. Why do aircraft accidents happen ?
15. 15AIR TRANSPORT SAFETY
B. James Reason’s "Swiss Cheese" Model
A series of Human Factor problems form an error
chain. If any one of the links in this chain had been
broken the incident may have been prevented. It might
be done by building in measures/defenses, which may
not permit an error at one or more of the stages. A
good example is J.Reason’s ‘Swiss Cheese’ Model.
1. Why do aircraft accidents happen ?
B.1 The theory
16. 16AIR TRANSPORT SAFETY
1. Why do aircraft accidents happen ?
B. James Reason’s "Swiss Cheese" Model
B.2 J.Reason’s ‘Swiss Cheese’ Model – fig -
17. 17AIR TRANSPORT SAFETY
A. Story Reconstruction
2. Example : TUNINTER Flight 1153
A.1 Aircraft specifications : ATR-72
Capacity………………….....68
Length…………………27,17m
Wingspan……….…….27,05m
Height…………….……..7,65m
Maximum weight………..21,5t
Freight………………….….7,3t
Flight range…………. 2222km
Maximum speed…….516km/h
18. 18AIR TRANSPORT SAFETY
A. Story Reconstruction
2. Example : TUNINTER Flight 1153
A.2 Informations about the flight
Saturday, 6th of August, near Palermo:
During daily flight from Bari to Djerba, at
15:24 (local time) the crew of the flight 1153
(TUINTER) contacted Palermo for an
emergency landing.
19. 19AIR TRANSPORT SAFETY
A. Story Reconstruction
2. Example : TUNINTER Flight 1153
A.2 Informations about the flight
The aircraft (ATR-72) had lost both engines.
The crew tries to reach the nearest airoport.
But They did not make it to Palermo and ditched
in the sea around 15:40.
20. 20AIR TRANSPORT SAFETY
A. Story Reconstruction
2. Example : TUNINTER Flight 1153
A.3 Cockpit voice recorder CVR
Captain: Please confirm the distance...
Palermo ATC: 20…
Captain: Please confirm the distance..
Palermo ATC: The distance is 20 miles
Captain: I think…we are not able, we
are not able to reach the terrain. We are
4.000ft and we are not able, we lose
both engines. Can you send us
helicopters or something like that?
Quick, quick, quick…
http://www.youtube.com/watch?v=6OnwwE1s1hg
21. 21AIR TRANSPORT SAFETY
A. Story Reconstruction
2. Example : TUNINTER Flight 1153
A.4 Casuality
Crew (total 4)……….victimes: 2
Pax (total 35)……..victimes: 14
Total on bord 39….victimes: 16
Aircraft: during the ditshing, the
fuselage had been broken in several parts.
Only the wings remains on the sea
surface.The rest falls in 12 meter depth.
22. 22AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.1 Friday 5th of august (end of the day)
The crew noted on the LogBook that the FQI (Fuel Quantity
Indicator) had three dispaly-bars misfunctionning.
23. 23AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.2 The maintenance
The technician asked the warehouse for ATR-72 FQI using a
special management software: AMASIS system.
He didn’t find the right FQI but AMASIS system told him that an
ATR-42 FQI can be installed in place of the ATR-72 one
24. 24AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.2 The maintenance
The technician did not check the compatibility of the ATR-42 FQI
in the ATR-72 documentation.
<< AMASIS program
25. 25AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.3 First error : Maintenance error
FQI of ATR72 & ATR 42
ARE NOT INTERCHANGEABLE.
26. 26AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.3 First error : Maintenance error
After replacement of the FQI, the quantity of fuel indicated is
3050 kg, instead of 790 kg.
27. 27AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.4 Second error : Pilot error
During preparion for flight 152F to Bari. An amount of 465 kg fuel
was added for the flight. 3800 Kg is indecated (real quantity is 1255
Kg).
After landing in Bari, the FQI shows 2300 Kg. 1500Kg of fuel had
been consumed in stead of 1050Kg . The crew noticed this but does
not react.
The A/C took off Bari with only 305 kg. 26Km north of Palermo the
fuel tanks are empty ( the indicator shows 1800Kg). The Captain tries
to joint the airport, but the A/C ditched near the coast.
28. 28AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.5 Third error : Design and conception error
On the ATR Family, The Fuel Level Alarm : « LO LVL » is
depending on the FQI.
The quantity of fuel computed by the FQI is erroneus
and the alarm had never been triggered.
TANK
WARNING
29. 29AIR TRANSPORT SAFETY
B. Investigation
2. Example : TUNINTER Flight 1153
B.6 Application of J Reason’s Model
Maintenance
Crew qualification
Design and conception
36. 36AIR TRANSPORT SAFETY
B. Civilian air transport accidents
3. Other examples in Tunisia
EGYPTAIR : crash of B-737
7th of mai 2002, Tunis, while
starting the landing to Tunis
Cathage airport, the B-737
of EGYPTAIR hit the hill of Nahli
park.
The visibility was very bad
and the pilot has forgetten to
adjust his altimeter.
37. 37AIR TRANSPORT SAFETY
B. Civilian air transport accidents
3. Other examples in Tunisia
EGYPTAIR : crash of B-737
14/62 passengers killed
38. 38AIR TRANSPORT SAFETY
A. Recommendations
4. Recommendations and conclusion
Technology and new systems can improve the aircraft performance and
help pilots to take the right decision.
companies should review its maintenace system and procedures.
companies should review its monitoring procedures and training exercises.
Aircraft crashs must be studied and analysed to correct anomalies in order
to avoid any futur accident.
40. 40AIR TRANSPORT SAFETY
B. Conclusion
4. Recommendations and conclusion
Inspite of accidents, the international air traffic is still growing and new
machines: powerful, larger, faster, more modern and sophisticated are under
production to transport passengers safely and smoothly : A-380, B-787
If we believe in a future without accidents, we will be able to make the
air transport more popular, less expensive and more reliable.
Aircraft crashs are not the result of one error but of several errors done
by the different actors of the accident.
41. 41AIR TRANSPORT SAFETY
4. Bibliography
Documentary : « pourquoi les avions tombent? » arte
Internet: www.airdisaster.com
Documentary : FATAL DITCHING T-BRO production :
Part 1 : http://www.youtube.com/watch?v=Xvkdwnr1Anc
Part2 : http://www.youtube.com/watch?v=IIXKDUQHILM
Part3 : http://www.youtube.com/watch?v=aO_-GiJyJys