FAHIM RAZA

Communication Address: #**, *th Main

4th A cross, Mobile: +91-998*******

BTM Layout 1st Stage,

Bangalore-560029. Date of birth: 20th Dec 1976, India

India (As recorded in Matriculation)

Nationality: India

Email: acecf0@r.postjobfree.com Driving: Indian

driving license

acecf0@r.postjobfree.com Marital Status: Married.

Education:

B.Tech 1996-2000 B.Tech in Manufacturing Engineering,

University of Ranchi, India. Result obtained: 9.11 CGPA

out of 10.

Intermediate (12th): Passed in 1993 with Aggregate (63.2 %).

Matriculation (10th): Passed in 1991 with Aggregate (76.11 %).

SKILL SET

# Skill Area Experience (in Years) Proficiency

1 CADDS5 1.5 EXPERT

2 CATIA V5(part 4.5 EXPERT

3 design,sheetmetal,GSD,FTA) 2.0 EXPERT

VPM(ENOVIA)

4 PRO-Engineer 1 EXPERT

5 ICAD 1.5 EXPERT

6 AUTOCAD 2002 1.0 EXPERT

7 Wind chill 1.0 EXPERT

8 PRIMES 2.0 1.0 EXPERT

9 SAP 1.0 EXPERT

10 DPDS 1.0 EXPERT

Employment History

Company Position Held From Date To Date

Wipro Technical 12Aug 2011 Till Date

Technologies Consultant 01 Feb 2011 05 Aug 2011

Goodrich Technical Lead 05-Apr-2010 31 Jan 2011

Aerospace Senior

Goodrich Engineer-

Aerospace

Infosys Engineering Lead 01-Oct-2009 31-Mar-2010

Infosys Project Manager 01-Feb-2008 30-Sep-2009

Infosys Sr. Design 01-Aug-2005 31-Jan-2008

Engineer

Infosys Design Engineer 12-Jul-2004 31-Jul-2005

ADA Research Fellow-A 13-Jun-2002 08-Jul-2004

Overall Summary of Experience

. I have 12 years' experience in the field of Aerospace Design and

Development projects and project management.

. Currently holding US B1 visa valid upto 23 Jan 2023.

. Currently handling multiple aerospace projects like CESA, Recaro, P3 and

also non aero project like Rolls Royce Marine and Shell.

. I have nearly 1.5 years onsite experience at Airbus, Filton, UK as a

subcontrator for IFTE (Inner Fixed Trailing Edge) -A380-Freighter -Design

of Skin and stringers.

. Worked on Aerospace projects of Light Combat Aircraft..

. Expertise in Tools like ICAD, CATIA V5, CADDS5, VPM, DMU,&Pro/Engineer

. Worked on Hyde concession of Long Range Aircraft (A330-200/300 and A340-

500/600). Hyde Group is one of the suppliers of Airbus.

. Worked on MRJ 90 Mid Fuselage structure specially Frames, Skin, Stringer,

Floor structure, Splices and Cutouts etc. at onsite MJET Nagoya Japan for

1 year and at offshore Infosys Mysore.

. Worked on C Series (Bombardier)/MRJ Engine Mount at Goodrich Aerospace

Ltd, Bangalore.

. Currently managing the project of Recaro Aircraft Seating,P3,CESA and

Shell DDC Program at Wipro (Engineering Design Services)

Work Experience:

01 Project Re-engineering of S92 MLG Actuator.

Name

Company Wipro Technologies Ltd.(Engineering Design Services)

Client CESA, Spain

Description of the project

This Project involves in the design support activity of S92 MLG

Actuator.The team in Wipro (Engineering Design Services) supports CESA in

Solid modelling, assemble and detailing of Manufacturing Parts. This

project also involve the Solid modelling of Standard parts in Catia V5.

Role : Technical Consultant

Responsibility : 3D Solid modelling and 2D drawings of S 92 MLG Actuator

component.

Review of the project deliverables.

Compliance of CESA Standards

Direct Interaction with customer and weekly and monthly

reporting.

Fully involved in Invoicing and payment process.

Vendor coordination and interaction with global teams.

Leading and developing the team of Engineers.

Project planning, monitoring and reporting.

Implementing Wipro Quality process methodologies

Managing offshore and onsite team

Monitoring and controlling the deliverables to client

Designing to confirm the materials, fastening & assembly

specs.

Engineering design & supporting documentation

Tracking the timeframe for the deliverables

Duration : From: Jun-2013

To: Till date

Hardware : Dell, Unix HP

Software : CATIA V5

01 Project Design support of Recaro Aircraft Seating for different

Name airlines and Standard part Harmonization of Rolls Royce

Marine.

Company Wipro Technologies Ltd.(Engineering Design Services)

Client RECARO and Rolls-Royce

Description of the project

This Project involves in the design support activity of Aircraft Seating.

Recaro team in Wipro (Engineering Design Services) supports RECARO

seating division in Germany, at different stages of the product

development and design.

Role : Project Manager

Responsibility : Tolerance and Interface Analysis of seating component.

Direct Interaction with customer and weekly and Monthly

reporting.

Fully involved in Invoicing and payment process.

Vendor coordination and interaction with global teams.

Leading and developing the team of Engineers.

Project planning, monitoring and reporting.

Implementing Wipro Quality process methodologies

Managing offshore and onsite team

Monitoring and controlling the deliverables to client

Designing to confirm the materials, fastening & assembly

specs.

Engineering design & supporting documentation

Tracking the timeframe for the deliverables

Duration : From: Aug-2011

To: Till date

Hardware : Dell, Unix HP

Software : CATIA V5

01 Project DDC Shell Program.

Name

Company Wipro Technologies Ltd. (Energy and Utility)

Client Shell Houston.

Description of the project

This Project involves in document and data controlling of engineering

drawings.

Role : Project Manager

Responsibility :

Direct Interaction with onsite team and weekly

reporting.

Fully involved in Invoicing and payment process.

Vendor coordination and interaction with global teams.

Leading and ramp up the team of document controllers.

Project planning, monitoring and reporting.

Implementing Wipro Quality process methodologies

Managing offshore and onsite team

Monitoring and controlling the deliverables to client

Contract management.

Program management activity

Duration : From: Sep-2013

To: Till date

Hardware : Dell

02 Project Detail design of Engine Mount for C series

Name (Bombardier)/MRJ using MBD approach

Company Goodrich Aerospace Ltd.

Client Bombardier

Description of the project

This Project involves in the detail design of Engine Mount. Engine Mount

team in Goodrich IDC (India Development Center), supports Goodrich Aero

structure division in USA, at different stages of the product development

and is being developed as a COE.

Role : Technical Lead

Responsibility : Tolerance and Interface definition for the Engine

Mounts.

GD&T development for the different components involved.

Detailed design development in Catia FT&A module - MBD

(Model Based Definition).

Vendor coordination and interaction with global teams.

Leading and developing the team of Engineers.

Project planning, monitoring and reporting.

Implementing Goodrich CI (Continuous Improvement) and

GLPD (GR Lean PD) methodologies

Defining Enovia and Catia Attributes

Concurrent approach to ensure design for manufacture &

assembly

Designing to confirm the materials, fastening & assembly

specs.

Engineering design & supporting documentation

Tracking the timeframe for the deliverables

Fair understanding on aircraft production methods and

processes

Duration : From: APR-2010

To: Aug-2011

Hardware : SUN Microsystem Unix,HP

Software : CATIA V5, VPM (ENOVIA LCA).

03 Project Design of MRJ 90 -Mid Fuselage structure- specially Frames,

Name Skin, Stringer, Floor structure, Splices and cutouts etc

Company Infosys Technologies Ltd.

Client Mitsubishi Aircraft corporation, Japan-Worked at onsite in

Japan for 1year and now working at offshore

Description of the project

This Project involves in the design of Skin, stringers, Frames, splices, cutouts, Floor structure,,intercoastals etc of Mid Fuselage structure

.

Role : Onsite and offshore Design Lead (Engineering Lead)

Responsibility : Design of Sheet metal frames

Design of Machined frames

Design of Edge frames of cutouts

Design of Door Cutout structure

Customer and interface partner Interaction.

Creating Design definition.

Weight reduction activities

Involved in the design and modelling of skin panels RSM

and DDMs

Creating sheet metal model of frame using CATIA V5.

Creating RSM (Relational skeleton Model)s for Frames and

Cutout activities .

Parametric RSM approach linked with Design Table.

Involved in defining Relational Map of RSM (relation

skeleton model) and DDM (detail design model).

CAD 3D modelling, detail design and detailing using

CATIA V5

Used the VPM for data management.

Used DMU for clash checking of interface component.

Defining Enovia and Catia Attributes

Concurrent approach to ensure design for manufacture &

assembly

Designing to confirm the materials, fastening & assembly

specs.

Engineering design & supporting documentation

Tracking the timeframe for the deliverables

Fair understanding on aircraft production methods and

processes

Duration : From: Dec-2008

To: Mar-2010

Hardware : SUN Microsystem UNIX, HP

Software : CATIA V5, VPM(ENOVIA LCA).

04 Project Name : Concession of Long Range Aircrafts (A330-200/300

and A340-500/600)

Company Infosys Technologies Ltd.

Client : Hyde Group, UK (Airbus supplier)

Description of the project

Concession is the written authorization to use or release an item

which does not conform to the specified requirements, i.e. Definition

Dossier (ISO 8402) (Ref 1) or concession is the way by which

nonconforming items may be accepted for use, with or without repair.

Once the manufacturing personnel raise concession, it comes to Design

office, which decides the remedy/answer for the non-conformance. The

decision to accept a nonconforming item, with or without repair, by

concession shall be taken only by the Design Office

The decision is recorded on the concession form, with all supporting

drawings and sketches attached, and the concession classified

according to this decision. Design Office acceptance is given by an

authorized signatory(s), as per the Design Organization Manual.

Role : Design Lead (Senior Design Engineer)

Responsibility : 1. Design Assessment of the non-conformance

occurred in the aircraft component.

2. Review of the concession executed by team

members

3. Controlling the defect tracker.

4. Ensuring a defect free delivery to Hyde group.

5. Consultation with Hyde design signatory and

stress team also.

Duration : From Date: Jun-2006 To Date: Nov-2008

Hardware : Pentium IV and III PCs

Software : SAP, DPDS, AutoCAD

05 Project Name Skin Extension-Inner Fixed Trailing Edge of

A380-Freighter

Design of Stringers Using ICAD.

Company Infosys Technologies Ltd.

Client GEDSitec, UK-Worked onsite at United Kingdom.

Description of the project

This Project involves in the design of Skin, stringers, and

stiffeners of Inner Fixed Trailing Edge -A380 Freighter.

Role : Senior Design Engineer

Responsibilit : ICAD design of stringers

y Design of Fastener Maps

Generation of ICAD scheme drawings.

Customer and interface partner Interaction.

Creating drawing set in the primes and sign off as

Designer.

Involved in the design and modelling of skin Top and

btm toolbody,flat skins, skin thk drawing, skin

profiles, Edge beam, Stiffener beam,Striffener edge

beam, top skin stiffener,Owp Buttstrap,Seal carrier,

Reinforcement Plate,FWD Hinge brkt door etc.

Creating Formed model of the flat skin using ICAD.

Creating loft and Formed Models of stringer using

ICAD.

Configure Management at onsite.

CAD 3D modelling, detail design and detailing using

CADDS5

Used the CAMU tree as the design aid for designing

components

Used DMU for clash checking of interface component.

Concurrent approach to ensure design for manufacture

& assembly

Designing to confirm the materials, fastening &

assembly specs.

Engineering design & supporting documentation

Tracking the timeframe for the deliverables

Fair understanding on aircraft production methods

and processes

Duration : From: Jan-2005

To: Jun-2006

Hardware : SUN Microsystem Unix,HP

Software : ICAD, CADDS 5, CATIA V5, PRIMES 2.0, Wind chill.

06 Project Name ATCHKSTR (WP1 Covers Geometry & WP9 Ribs Geometry

Support)

Company Infosys Technologies Ltd

Client ATKINS, UK

Description of the project

The project involves data collection activities. The data collected

shall be used for static and F&DT Checkstress analysis of the

A380-800 main wingbox covers and spars, and in particular with

regards to skin overhang widths and fwd & aft skin panel widths.

Task 1: Data collection of skin overhangs and skin panel dimensions.

Provision of true length of the skin line (i.e. taking account of

curvature) as follows:

from the spar datum to the skin edge.

from the spar datum to the first skin to spar bolt.

the separation between the aft-most stringer bolts to the fore-most

rear spar bolt.

the separation between the fore-most stringer bolt and the aft-most

front spar bolt.

Task 2: Data collection of Stringer bolting positions.

As part of the static and F&DT Checkstress analysis of the A380-800

covers there is a requirement to identify the location and size of a

large number of bolting positions. We Provide following parameters of

fasteners from CAD model:

Pitch

Edge distance.

Distance from stringer datum.

Panel Thickness.

Runout dimensions (Flange width, Flange Thickness etc.)

Task 3: Check of ICAD & DFM Data

As part of the static and F&DT Checkstress analysis for A380-800,

main wingbox metallic ribs Cabot Design (Cabot) have created a

database of rib geometry data which has been populated with

information from ICAD and DFM sources.

Task is to validate the geometry data within this database against

the CADDS 5 solid model. This will validate the accuracy of both the

initial transfer of CADDS 5 information into ICAD & DFM, and the

transfer of ICAD & DFM data into Cabot's database.

Task 4: Provision of non-ICAD and non-DFM Data

The Cabot database is not complete, as few rib geometry do not have

ICAD and DFM sources. We measure the CAD model and update the

database.

Task 5:Provision of Spar to Rib connection Data

Provision of X and Y distances of bolt centre for outboard and

inboard forward ribs as follows:

Outboard rib connection to front spar.

Outboard rib connection to rear spar.

Inboard fwd rib connection to front spar.

Inboard fwd rib connection to centre spar

Inboard aft rib connection to rear spar

Provision of parameters X, SL, B, L2, and D for inboard aft rib

connection to centre spar.

Role : Module Lead

Responsibilit : Customer Interaction.

y Migration of CADDS 5 solid model to Catia V5.

Measurement and data collection of skin overhang and

skin panel dimensions from Catia V5 model.

Measurement and data collection of covers fastener

map dimensions from Catia V5 model.

Verifying geometry data against the Catia V5 model

of skin.

Review of skin overhang database and Fastener Maps

database.

Duration : From: Aug-2004

To: Dec-2004

Hardware : Pentium IV and III PCs

Software : Catia V5, CADDS5

07 Project Name FERCHCAG3 (Creation of Standard Part Library)

Company Infosys Technologies, Ltd.

Client Airbus Germany

Description of the project

The project included creation of CATIA V5 Standard Part Library. The

process involved Modelling the part, Creating the design table and

linking it to the part, which facilitated in deriving various

configuration of the standard, Resolving the parts and maintaining

the standards.

Role : Design Engineer

Responsibilit : 1.Creation of 3D model drawings for system equipment

y of Aircraft.

2. Review of models received from suppliers to

ensure conformity to Airbus Standards.

Duration : From: Jul-2004

To: Aug-2004

Hardware : Pentium IV and III PCs

Software : Catia V5

PRIOR EXPERIENCE OUTSIDE INFOSYS

Company worked for : AERONAUTICAL DEVELOPMENT AGENCY, BANGALORE

Duration : From Date: 13-Jun-2002 To Date: 08-Jul-2004

Worked As : RESEARCH FELLOW

1 Project Name : Drop Tank of Light Combat Aircraft (LCA)

Client : ADA, Bangalore

Description of the project

An external store, detachable during flight meant to serve as

additional fuel tank in order to enhance the range of flight of the

aircraft. The two Drop tanks are of fuel capacity 800 litres and 1200

litres. Drop Tank is divided into three main parts externally nose

cone, centre section and rear cones and internally into two parts

namely fwd and aft shells. Whole Drop Tank Design is carried out in

Detail Design, ADA. CPDC, Hyderabad carries out the Drop Tank

production. Job involved drafting 2D layouts, subassemblies,

assemblies, part drawings of sealing bulkhead, bottom frame assembly,

rack assembly etc, and corresponding 3D modelling for stress and

weight analysis and to the final assembly of parts.

Role : Research Fellow

Responsibility : 1. Surface & Solid modelling of the Structural

components for

Analysing, weight calculation & checking for

interference.

2. Detail study of parts of aircraft, control

surfaces with their

location in the Aircraft assembly

3. Converting 3D views to suitable 2D views and

drafting detail

Drawing.

4. Creation of 3D and 2D preliminary layouts,

station diagram of

A/C structures, sub-assemblies, assemblies and part

drawings.

Duration : From Date: Jun, 2002 To Date: Jul, 2004

Hardware : Pentium IV and III PCs

Software : Catia V5, Pro-E, AutoCAD

2 Project Name : Air brake of Light Combat Aircraft (Technical

Demonstration -1)

Client : ADA, Bangalore

Description of the project

Airbrake is one of a control surface, which helps in creating a

control Drag during take off, taxing and landing. LCA has twin

airbrakes, one on LH & RH sides mounted on the outer periphery of

fuselage surface in between the fin attachment frames Station #34 and

Station #37. These airbrakes are operated by means of Hydraulic

jacks. Job involved in

modelling of parts such as Stiffeners, Ribs, Beams, Torque box &

assembly of all the parts. Air brake is used for the Manoeuvring of

the Aircraft. It is used as brake while landing the Aircraft.

Role : Research Fellow

Responsibility : 1. Surface & Solid modelling of the Structural

components for

Analysing, weight calculation & checking for

interference.

2. Detail study of parts of aircraft, control

surfaces with their

location in the Aircraft assembly

3. Converting 3D views to suitable 2D views and

drafting detail

Drawing.

4. Creation of 3D and 2D preliminary layouts,

station diagram of

A/C structures, sub-assemblies, assemblies and part

drawings.

Duration : From Date: Jan-2003 To Date: Feb-2003

Hardware : Pentium IV and III PCs

Software : Catia V5, Pro-E, AutoCAD

3 Project Name : Rear Fuselage of Light Combat Aircraft Trainer.

Client : ADA, Bangalore

Description of the project

Trainer is a two-seater aircraft, which is similar to fighter used to

train the pilot. The fighter version of LCA is already completed the

design part .The Design work of front fuselage is carried out in

Detail Design. I was involved in modelling team of Sta #16 Bulkhead,

Inclined shear walls, Central shear wall, Framelets, Side door

assemblies, Skin & Stringer assembly.

Role : Research Fellow

Responsibility : 1. Surface & Solid modelling of the Structural

components for

Analysing, weight calculation & checking for

interference.

2. Detail study of parts of aircraft, control

surfaces with their

location in the Aircraft assembly

3. Converting 3D views to suitable 2D views and

drafting detail

Drawing.

4. Creation of 3D and 2D preliminary layouts,

station diagram of

A/C structures, sub-assemblies, assemblies and part

drawings.

Duration : From Date: Nov-2002 To Date: Dec-2002

Hardware : Pentium IV and III PCs

Software : Catia V5, Pro-E, AutoCAD

DETAILS OF TRAINING UNDERGONE

# Trained On Period (in Days)

1 Undergone intensive training on Advance GD & T at 5 Days

IDC (India Design Center), Goodrich Aerospace

Ltd, Bangalore.

2 Undergone intensive training on Windchill Primes 2 days

2.0 for A380 at Filton Airbus UK.

3 Undergone intensive training on Windchill DMS for 1 day

A380 at Filton Airbus UK.

4 Undergone intensive training on CATIA V5 for 20 days.

solid /surface/wire frame modelling conducted by

EDS Technologies, Bangalore.

5 Undergone intensive training on PRO-E 2001 for 12 days

Solid modelling conducted by Rolta India Pvt Ltd

Bangalore.

6 Undergone intensive training in VPM for Solid/ 6 days.

Surface modelling conducted by CSM Software Ltd,

Bangalore.

7 Undergone intensive training on PRO-E Wildfire 12 days.

for Solid modelling conducted by Rolta India Pvt

Ltd Bangalore for a period of 12 days.

8 Undergone Project Management Certification 6 Days

training within WIPRO LTD

Training Courses:

Computer and IT: MS Office 98', MS Project 98', AutoCAD 2000, . Use

of Word processing, presentation packages, spreadsheets and

analytical tools were endemic in my daily job at Airbus UK

as well as in Infosys, Bangalore.

Skills:

Interpersonal Skills Team working, group meeting and report writing were

common at work experiences, which continuously helped me to

improve my communication skills both verbally and in

writing.

Problem Solving Design activities and calculations at UK and Japan enabled

me to enhance my technical knowledge about Interface

matrix; I was able to develop a Design solution for

Interface related Problem.

Languages Fluent in English, Urdu and Hindi.

Leisure Interests:

Sports: I enjoy playing Cricket, Badminton, Vollyball, and tennis at

non-competitive level.

Permanent Adress: C/O Mohammad Nasim, 3rd Floor Flat -E

Haideri Apartment Block -B Main

Road Ranchi-834001

References:

Mahammad Nayeem Annavaram Mohammad Vasib

Engagement Manager Design Lead,

Unisys Global Services Quest,

IndiaBangalore, India Bangalore, India

Mobile +91 Tel. No. +91 (0-944*******

97829765535917829765535 Email:

Email: acecf0@r.postjobfree.com acecf0@r.postjobfree.com

m

Previous UK Work Permit Details:

PERMIT NUMBER: F030592

WORKER REFERENCE NO. C094265

DATE OF ISSUE: 13OCT 2004

VALID UNTIL : 01OCT 2006

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