Syed Ahmed Ali

Aircraft Maintenance / Manufacturing / Stress / Fatigue Engineer

Riyadh, Saudi Arabia, +966*********

TOTAL YEARS OF EXPERIENCE IN AIRCRAFT INDUSTRIES: 20 SUMMARY OF WORK EXPERIENCE:

Twenty years of worked experience as a stress analyst of Aircraft structures, Aero Engine, Aero Engine Tooling, Static Strength Test Schedule preparation, Stress concession – manufacturing supports, Aircraft maintenance, Repair, modifications and Corrosion repair (Aero Engine), Complete product life cycle experience from conceptual design till certification and airworthiness standards. EDUCATION:

B.E– Bachelor degree in Mechanical Engineering, Kuvempu University, Davanagere, India MTech – Master Degree in Aeronautical Engineering, Visvesvaraya Technological University, India TOOLS / CERTIFICATE:

MSC/Nastran, MSC/Patran, Ansys, MATLAB, MathCAD, ISSY Software (Airbus), Catia V4, Hyper Mesh. I have done course on 7X7 Aircraft Structural Repair for Engineers from Boeing. I have certificate from Council of Saudi Engineers.

WORKED ON DIFFERENT PROGRAMS/CUSTOMERS

A400M, Alenia-Bombardier, Airbus A318, PW6000 Engine, Boeing 787, 737, 707, Tejas LCA-Navy, Saras HT-VT, HJT-36, Kaveri engine, A380F, A380, Engine Tooling, AS907 Engine, MPA3 PIAGGIO. SKILL SETS:

• Linear Static Analysis Manufacturing Support

• Buckling Analysis Fatigue Analysis

• Aircraft Maintenance Static Test Report Preparations WORK EXPERIENCE

06/14 – present

Alsalam Aerospace Industries (A joint venture with Boeing, USA) Manufacturing Project Engineer

Riyadh, Saudi Arabia

First Project: Manufacturing support of F-15SR Wing structures Worked involved manufacturing of Wing & Forward Fuselage of defense project (F-15SR), the brief descriptions of work are as follows

• Redline the work instruction on the work order (Job card) and updating planning

• Guiding the technicians

• Solving the QAR (quality assurance report) whenever arises, working with the customer guidelines

• Responsibilities for technical all issues by way of stampings. Second project: Aircraft Maintenance, Repair and modifications Aircraft Engineer

Work involves Aircraft Maintenance, Repair and modifications of Saudi Arabian Military and Business jets on the following programs

• Boeing 707 Tanker

• Boeing 707 AWACS

• Business Jet Boeing 737

• Lockheed Martin C-130

• Business Jet A340, A320

• gulfstream IV

Third project (Current Assignment): Reverse Engineering Lab and Factory Qualification Mechanical Engineer

Setup of Reverse Engineering Lab for aircraft parts by taking PMA (parts Manufacturing Approval) permission from FAA (Federal Aviation Administration), work location is Directorate General of Local Industry development under Ministry of Defense office, Riyadh, Saudi Arabia. 11/12 - 05/14

Piaggio Aerospace Industries, Finale Ligure, Italy Tata-HAL Technologies Limited, Bangalore, India

Technical Manager - Stress Analysis

Project: Conceptual Design, Preliminary Design and Detail Design of Front Fuselage, Rear Fuselage and Vertical Tail of multi-role patrol aircraft MPA3 (PIAGGIO ITALY) 02/12 – 11/12

QuEST Global Engineering Pvt. Ltd.

Bangalore, India

Project Leader - Stress Analysis

First Project: Corrosion repair substantiation of the Outer Fan Duct (OFD) on the AS907 engine The worked involved was corrosion repair substantiation of the Outer Fan Duct (OFD) on the AS907 engine installed on the BD-100 aircraft. The allowable material that can be removed at critical locations of OFD flanges, skin and bolts based on static analysis report and fatigue analysis report. This produced as additional information to Engine Light Maintenance Manual. The allowable reduction in thickness is calculated based on the nominal dimensions for positive margin of safety (>0.01) and allowable fatigue life of 75000 cycles. For components which do not satisfy the above-mentioned criteria the part should be replaced.

Second Project: Fatigue and Damage Tolerance Analysis of Landing gear Hinge Door of A380 A investigation on failure of landing gear Hinge Door of A380 on MSN001 has been carried out, a detail stress and Fatigue & Damage Tolerance Analysis has been carried out. Third Project: A350 Rear Spar Repair and FE Static and Dynamic validation Report In GFEM model of A350 wing the rear spar repair by fine meshing in the area of interest and padding it to give extra strength.

03/07-02/12

CADES Digitech Pvt. Limited

Bangalore, India

Asst. Technical Manager - Stress Analysis

First Project: Hydraulic and Fuel Tube Interface load calculations and stress analysis for Boeing 787.

Different piping circuits are modeled in PATRAN by importing IGES input generated by CATIA V5 and analysis is performed in MSC Nastran. To meet the Initial design criteria, considering simple beam analysis, maximum constrain forces at the clamp locations and ends are determined at different load cases for fuel lines. Incase of hydraulic lines, distributed load is applied to determine the clamp forces.

Second Project: Design and Stress Analysis of Light Combat Aircraft (Indian, Tejas) Detail Stress analysis of Stubwing and Levcon of Light Combat Aircraft (Indian, Tejas), by using fem based software Nastran/Patran and Hand calculations. Third Project: Fatigue and Damage Tolerance analysis of C- 295 0f EADS CASA (Spain) Fourth Project: Sensitivity Analysis of the influence of Temperature gradient on the Over speed and Burst speed margin of a Gas Turbine Disc (HPT) The assessment of the Over Speed and Burst Speed margin of a Gas Turbine Disc which influenced by several factors like Stress, Strain, Temperature, average stress, average temperature, peak stress or peak temperature. One should have to control these parameters other words that yields to failure of Engine, so one has to take care these parameters in designing of a Gas Turbine Disc to ensure the safe operation of the Engine.

Fifth Project: Stress Concession

Working extensively on the Stress Concession for the Light Combat Aircraft (Tejas Aircraft) and the Vertical Tail & Horizontal Tail of the Saras Aircraft Sixth Project: Alenia Rudder and Elevator Design

Detail Design & Stress Analysis of Rudder and Elevator Brackets Seventh Project: GECI A400M

Detail Stress analysis of Pipes and Brackets of Hydraulic System of A400M 07/06-09/06

Bishop GmbH, Hamburg, Germany

Stress Analyst

Stress report writing for Cabin interior parts and Cargo Customization 4/05-07/06

ATENA Engineering GmbH, Munich, Germany/

ATENA India Pvt. Ltd., Bangalore, India

Senior Stress Engineer

First Project: Stress Sizing of Rear Fuselage frame of A380F Work involved Stress Sizing of Rear Fuselage frame of A380F, using ISSY software and also Hand calculations has been carried out.

The sizing has been done by setting the Airbus Germany requirements and optimised the Frame to R.F=1.10

Second Project: Engine tooling

Stress analysis (Hand calculations only) of engine builds tooling for the Trent 1000 Engine for the 787 Boeing Aircraft.

Third Project: Design optimization and stress analysis of Gas Turbine disc of Kaveri Engine 10/03-4/05

Snecma, Toulouse, France

Snecma Aerospace India Pvt. Ltd., Bangalore, India Stress Engineer

Work involved Design, Stress Analysis (composite and metallic), Optimisation and Certification of Thrust Reversal Unit of PW6000 Aircraft A318 Engine, Analysis with Patran, Nastran, Catia V4 and Hand calculations has been carried out.

01/00- 10/03

Aircraft Research and Design Centre, Hindustan Aeronautics Limited, Bangalore, India

Structural Analysis Engineer

Work involved Detailed Stress Analysis and Optimisation of Vertical Tail of HJT-36 (Hindustan Jet Trainer) with two Rudder deflected positions (Load Cases), using Nastran/Patran and as well as Hand Calculations has been carried out.

The Vertical Tail has two parts FIN and RUDDER, Fin is get attached with the Fuselage by means of three fittings, two Shear and one Bending fitting, Rudder is with Fin by means of the three hinges. Idealized in Patran and has been analysed using Nastran. Static, Buckling pre and post and Optimisation analyses has been carried out

ADDITIONAL QUALIFICATION:

1. I have under gone a course on fundamental of finite element analysis at Indian Institute of Science, Bangalore.

2. I have under gone a course on Fatigue and Fracture Mechanics at Indian Institute of Science, Bangalore.

PERSONAL PROFILE:

Born on : Jun 01, 1975

Place of Birth: Raichur (India)

Current Location: Riyadh, Saudi Arabia

Nationality: Indian

Contact Number: +966*********

E-mail: ad4djp@r.postjobfree.com, ad4djp@r.postjobfree.com

AUTHORISED SIGNATORY:

1. I had authorized signatory approval from Centre for Military Airworthiness and Certification

(CEMILAC) for signing on the Stress documents for Military Aircraft. 2. I had authorized signatory approval from Directorate General of Civil Aviation, (DGCA) for signing on the Stress documents for Civil Aircraft as Compliance Verification Engineer

(CVE) & Airworthiness

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