1. INDRAJEET SINGH
: +91-9880417920 /:indrajitsinghR@gmail.com
SENIOR TECHNICAL MANAGEMENT PROFESSIONAL
Aeronautical Engineering
Proficient in running successful method-oriented operations and taking initiatives for process improvement
Location Preference: Pune/Bengaluru/Overseas
Industry Preference: Aeronautical/Automobile
PROFILE SUMMARY
• A dynamic professional with more than 8 years of rich experience in Aeronautical Engineering
• Lastly associated with Multi Role Transport Aircraft Ltd. (MTAL) as Project Manager
• Demonstrated abilities in the practical applications of aerospace engineering technology and science including
principle and procedures for the conceptual design, development, Performance & Analysis
• Proficient in performance & validation, IVHM, Standard Parts Qualification of aircraft mechanical systems/Air frame
(Fuel, Hydraulic, Landing Gear, Pneumatic, De-icing, Fuel Innerting), Structural Analysis, Aircraft Integrated Systems
analysis, Aerodynamic performance and Certification process
• Proficient in Weight Reporting Management of aircraft Integrated Mechanical Systems for ATA-21, ATA-28, ATA-
29, ATA-32, ATA-36, ATA-38 and insightful knowledge of ATA-21, ATA-28, ATA-29, ATA-32, ATA-34, ATA-36, ATA-
38 & ATA-47, DO-160, FAR23/25
• Renowned for swiftly completing-up projects with experience in planning, managing and executing project;
streamlining the working Quality Management System for enhancing operational & productive activities
• Experienced in planning, managing & executing project operations like Learning curve, Impact cost on project delay &
point of occurrence etc., streamlining the working standards operating system for enhanced operational activities
• Keen planner with skills in carrying out various Design & development activities for various aircrafts project and
monitoring and checking the deliverable quality
CORE COMPETENCIES
~ Project Management ~ R&D & Analysis ~ Design & Development
~Quality Management System ~ Supply chain Management ~ Team Management
~ Supplier Management ~ Aircraft Structure (Air Frame) ~ Aerodynamics
~ Qualification & Certification ~ Continual Improvement ~ Aircraft Integrated Systems & IVHM
~Weight Reporting Management ~ Aircraft Propulsion & Systems ~ General Administration
ORGANISATIONAL EXPERIENCE
Aug 2014 – Feb 2015 with Multi Role Transport Aircraft Ltd. (MTAL) as Project Manager
Oct 2011 – Aug 2014 with National Aerospace Laboratories (NAL/CSIR) as Consultant – PE
Nov 2008 – Sep 2011 with Altran Technologies India Pvt. Ltd. as Aero-Technical Consultant
Dec 2006 – Nov 2008 with National Aerospace Laboratories (NAL/CSIR) as Project Scientist
Mar 2004 – Oct 2004 with Hindustan Aeronautics Ltd. as Industrial and Management Trainee
KEY RESULT AREAS
Project Management:
• Developed project baselines while monitoring and controlling projects with respect to cost, resource deployment,
time over-runs and quality compliance to ensure its satisfactory execution
• Managed various activities like Cost estimation, Cost negotiation, Project planning, Resource planning, Execution,
Monitoring, Status update, QMS Documentation and Delivery of the entire Multi Role Transport Aircraft (MTAL –

2. INDO-Russian JV- HAL) project
• Collated information, interpreted data and published the results of specific projects in technical report form
• Worked with teams, suppliers, clients and managers to agree budgets, timescales, specifications & enhanced
Continual Improvement
Aeronautical Planning & Design Activities:
• Performed baseline configuration design for various mechanical system layouts/sizing, performance analysis and
weight estimations as per FAR25
• Analysed aircraft health monitoring to identify trends and initiates corrective actions; diagnostic activities that may
include aircraft propulsion, hydraulic, air conditioning, fuel systems, and landing gear to improve flight safety, reduce
costs and reduce man per hour
• Calculated and evaluated flow/pressure loss on the technical requirements of Aircraft Fuel System & Hydraulic
system, heat loss calculation for ECS/air conditioning, etc.
• Ensured development and validation of various mechanical/integrated systems such as Fuel System, Hydraulic
System, Landing Gear, Anti-icing, Water/Waste System & Fuel Inserting System and Engine Performance & analysis
• Weight Reporting Management (Estimation & Reduction) of Integrated Mechanical Systems for Airbus aircraft
• Entrusted with the responsibilities of:
o Design, Developing, Modelling, Simulation, Analysis & Performance testing of aircraft integrated systems
o Assessing design requirements
o Managing Aircraft standard parts qualification to execute mission requirements
o Analysing Engine performance and prepared certification process and road map
Research & Development:
• Underwent research studies on conceptual designing Integrated Systems of National Civil Aircrafts
• Undertook static and dynamic analysis of Aircraft Structures and FSI for Wing; diagnosis and prognosis practice for
aircraft mechanical/Integrated systems
• Undertook aero-elasticity analysis of Aircraft wing flutter to initiate corrective actions
• Underwent research on Integrated Vehicle Health Management (IVHM) of Landing Gear & Fuel Systems
• Undertaking theoretical and practical research
• Researching ways to improve the performance of fuel-efficient parts, such as wings, fuselage and engines
Stakeholder Management:
• Managed relationship with project stakeholders, Kick of meeting, keeping stakeholders informed of progress and
issues in order to manage expectations on all project requirements and deliverables
• Communicated technical and regulatory advice to clients, teams, suppliers and other professionals within the
industry and presented data to groups and individuals
HIGHLIGHTS
• Successfully prepared the technical specifications managed by the requirements with complete analysis of product or
Systems for Regional Transport Aircraft (RTA)
• Successful in reducing the man hour cost rate of Multi Role Transport Aircraft (MTA) by 13% of overall cost
• Structured and implemented programs for engine performance to identify deformities, malfunctions or other
abnormality for P&W turbo-prop
• Independently and successfully executed the Airbus project on Product Development
• Acknowledged for attaining significant reduction in weight by 0.05 % in Integrated Mechanical Systems (Airbus)
product
• Maintenance Cost Reduction for Indigenous Project on Regional Transport Aircraft
• Prognostic & Diagnostics Programme of Aircraft Integrated System to establish the trends of data acquisition system
for Integrated vehicle Health Management
• Steered efforts towards successful establishment of the product validation Test Laboratory & Report along with
development of Hydraulic systems, fuel system & Air conditioning (Airbus) product

3. • Acquired pre-launch approval for Airbus products from the customer, this was significant as it included a large
number of activities including detailed discussions with customers on important topics like technical requirements,
test specification, systems installation drawings, and so on
• Distinguished for completing quality projects within time by taking more than 60% initiatives
• Implemented several measures to identify deformities, malfunctions or other abnormalities such as Highly Resistive
Union (HRU) in parts / components / products for Fuel, Hydraulic Systems & Air Conditioning/ECS (Airbus)
ACADEMIC DETAILS
• MS (Aero) from Jain University, Bangalore with Distinction
• B.Tech.in Aeronautical Engineering (Propulsion) from Aeronautical Society of India, Delhi in 2006 with 61.34%
• Graduate in Automobile Engineering from IAE, Chennai in 2001 with 71.1%
• 12th
from PTPS College, BIEC Board, Patratu in 1994 with 50%
• 10th from PTPS School, BSEB, Patratu in 1992 with 61.33%
Diploma:
• Diploma in QC – 9000 from AIIMS, Chennai in 2000 year with 67%
TECHNICAL SKILLS
~Aircraft Fuel System ~ ECS/Air Conditioning ~ ATA, FAR & FSI ~IVHM Networking
Architecture
~Hydraulic System ~ Aerodynamics analysis ~ Landing Gear ~Std. Parts Qualification
~ Fuel Innerting ~ Engine Performance ~Aeroelasticity(Flutter) ~Water/waste System
~Certification Process ~Pneumatic System ~Weight Estimation &Reduction
IT SKILLS
Designing Software: Flow-Mater, AMESim, Easy5, CATIA V5, Hypermesh, Nastran, Patran, Anys
Operating Systems: Windows 98/2000/XP
Application software: MS Office (Word, Excel and PowerPoint) in context to Project Planning
Airbus Specific Tool: GRAM-CAM, GeRS
Airbus ID: ST-04861
TRAININGS
• Attended:
o Government Advanced Training on HAL-Kanpur & HAL-Lucknow for Aircraft Mechanical/Integrated Systems,
Organized by National Aerospace Laboratories (NAL)-Bangalore for 2 months
o Industrial Training on HAL-ARDC, Bangalore for 3 months
o Graduate Training on NAL/CSIR, Bangalore for 6 months
PAPER PUBLICATIONS
• Publication of:
o Technical Paper on “Detail Design of Aircraft Fuel System” from National Aerospace Laboratories, Bangalore for
NCA (RTA)-90/110 Aircraft
o Technical Paper on “Environmental Control System” from National Aerospace Laboratories, Bangalore for RTA-
70-90 aircraft
o Technical report on “Analysis of Landing Gear networking” and “Analysis of Fuel system networking” from
National Aerospace Laboratories, Bangalore
o International paper based on IVHM (PHM Society) on “A typical approach to aircraft fuel system failure analysis
using Maintenance Aware Design environment software” and got selected
o International paper based on IVHM (IEEE) on “A typical approach to aircraft Landing Gear failure analysis using
Maintenance Aware Design environment software” (Abstract selected)
o Four ‘ABS’ Airbus Standard specification documents (e-Room) for ‘HRU’ (Airbus)
PERSONAL DETAILS
Date of Birth: 24th
February, 1977

4. Languages Known: English, Hindi, Tamil and German (Beginner)
Passport: L 5760311
Marital Status: Unmarried
Nationality: Indian
Visa: NA
Address: # 352/2, Ground floor, Ist Cross, Behind salvage road, Anna Sandra Palya,
Vimanapura, HAL, Bangalore - 560017
Driving License: KA01 20100006457
Please refer the Annexure for Paper Publications and Project Details
ANNEXURE
PROJECT DETAILS
Project Title: Prognostic & Diagnostics Programme of Aircraft Integrated System
• Integrated Vehicle Health Management (IVHM) and Design & analysis the Fuel System (ATA28)
& Fuel Innerting System (ATA47) and Landing Gear
• Structural Aero-elasticity analysis of UAV Fuselage, Fluid Structure Interaction (FSI)
Period: Oct’ 11 – Sep’14
Organisation: National Aerospace Laboratories (NAL/CSIR), Bangalore
Software Used: LMS-AMESim, MADe, Easy5, Flow master, CatiaV5, Hypermesh, Nastran, Anys, Fluent and MS
office
Description: The project was undertaken in order to focus on development of Mechanical Integrated Systems
(technical study, capture of needs, development plan) and for analysing the more sensitive zones
to prevent from castrophic failure of components and LRUs thereby reducing the cost and
weight
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Project Title: Systems Installation Technical Referential (SITR), AIRBUS SAS
Period: Jul’10 – Sep’11
Organisation: Airbus SAS behalf of Altran Technologies
Software Used: MS-Office, Airbus tool, CatiaV5
Description: The project was undertaken in order to focus on development of mechanical standard parts
(technical support, technical study, capture of needs, development, standardization,
manufacturing process definition, program reporting and development plan) and generating the
SITR for ATA21, ATA28, ATA29, ATA34, ATA35, ATA36, and ATA38 for Airbus (XX Aircraft)
taking the reference of SA (A319, A320 & A321), LR (A330, A340) and WB (A340-500)
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Project Title: Mechanical Standard Parts Qualification (Onsite with work permit- Germany)
Period: Jun’09 –Jun’11
Organisation: Airbus GmbH SAS behalf of Altran GmbH, Bremen, Germany
Software Used: MS-Office, GRAMS-CAM, GeRS
Description: The project was undertaken in order to focus on development of mechanical standard parts
(technical support, technical study, capture of needs, supplier consultation, development,
standardization, manufacturing process definition, program reporting, development plan,
qualification status, maturity review). These standard parts are included in the following
families: Tubes; Flexible Hoses Assembly; Fittings; Couplings (rigid and flexible); Air
Conditioning Flexible Hoses, Sleeve and Bellow; Seals; Insulation; Clamps; HRU fittings and
accessories for Hydraulic System, Aircraft Fuel System, Pneumatic System & water/waste
System
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Project Title: Weight Reporting Management, AIRBUS GmbH (Onsite-Germany)
Period: Nov’08 – Jun’09
Organisation: Airbus GmbH behalf of Altran GmbH, Hamburg, Germany
Software Used: MS-Office, CatiaV5 (DMU) & Airbus Tool
Description: The project was undertaken in order to understand the new techniques of Airbus tool for

5. studying the complete Airbus (XX Aircraft) configuration including overall weight estimation
and reduction of the aircraft mechanical systems such as ATA21, ATA28, ATA29, ATA36 and
ATA38
Project Title: Design and Architecture of Aircraft Fuel System and Hydraulic Power Generation System
for NCA-90/110seater Aircraft
Period: Dec’06 – Nov’08
Organisation: National Aerospace Laboratories/CSIR, Bangalore
Software Used: MS-Office, Flow-Master, CatiaV5, Hypermesh and Nastran
Description: The project was undertaken in order to analyse Airworthiness rule & regulations, LRU’s layout,
Component weight and to calculate total load of ECS in conjunction with Honeywell
-------------------------------------------------------------------------------------------------------------------------------------------------------
Project Title: Maintenance Cost Reduction for Indigenous Project on Regional Transport Aircraft (RTA-
70)
Period: Jul’ 2007 – Dec’2007
Organisation: National Aerospace Laboratories/CSIR, Bangalore
Software Used: MS-Office
Description: The project was undertaken in order to find the measures of improvement in the maintenance
program of existing NCA (ATR-72) through Structural Health Monitoring system and Integrated
Avionics. Processed technical data through Case study of Maintenance Ideology of Airbus-380
and Boeing 787 to be used in further developments of project
-------------------------------------------------------------------------------------------------------------------------------------------------------
Project Title: To assist in the re-design and development of double slotted flap of a LTA (SARAS)
aircraft
Period: Jun’ 2007 – Jan’2008
Organisation: National Aerospace Laboratories/CSIR, Bangalore
Software Used: Gambit and Fluent & CatiaV5, Hypermesh and Nastran
. -------------------------------------------------------------------------------------------------------------------------------------------------------
Project Title: Light Combat Aircraft (LCA) Fuel System development programme and Industrial
Management Training
Period: Mar’04 – Oct’04
Organisation: Hindustan Aeronautic Limited (HAL), Bangalore
Software Used: CATIA, AutoCAD, MS-office
Description: The project was undertaken in order to make extensive literature survey and technical analysis
for the similar systems, to design & develop the suitable architecture, hand calculation, mission
analysis and performance analysis using MS-Excel, study the FAR and ATA standard for
designing
-------------------------------------------------------------------------------------------------------------------------------------------------------
REFERENCES:
Will be provided upon request
Date:
Place: Bangalore (Indrajeet Singh)

6. studying the complete Airbus (XX Aircraft) configuration including overall weight estimation
and reduction of the aircraft mechanical systems such as ATA21, ATA28, ATA29, ATA36 and
ATA38
Project Title: Design and Architecture of Aircraft Fuel System and Hydraulic Power Generation System
for NCA-90/110seater Aircraft
Period: Dec’06 – Nov’08
Organisation: National Aerospace Laboratories/CSIR, Bangalore
Software Used: MS-Office, Flow-Master, CatiaV5, Hypermesh and Nastran
Description: The project was undertaken in order to analyse Airworthiness rule & regulations, LRU’s layout,
Component weight and to calculate total load of ECS in conjunction with Honeywell
-------------------------------------------------------------------------------------------------------------------------------------------------------
Project Title: Maintenance Cost Reduction for Indigenous Project on Regional Transport Aircraft (RTA-
70)
Period: Jul’ 2007 – Dec’2007
Organisation: National Aerospace Laboratories/CSIR, Bangalore
Software Used: MS-Office
Description: The project was undertaken in order to find the measures of improvement in the maintenance
program of existing NCA (ATR-72) through Structural Health Monitoring system and Integrated
Avionics. Processed technical data through Case study of Maintenance Ideology of Airbus-380
and Boeing 787 to be used in further developments of project
-------------------------------------------------------------------------------------------------------------------------------------------------------
Project Title: To assist in the re-design and development of double slotted flap of a LTA (SARAS)
aircraft
Period: Jun’ 2007 – Jan’2008
Organisation: National Aerospace Laboratories/CSIR, Bangalore
Software Used: Gambit and Fluent & CatiaV5, Hypermesh and Nastran
. -------------------------------------------------------------------------------------------------------------------------------------------------------
Project Title: Light Combat Aircraft (LCA) Fuel System development programme and Industrial
Management Training
Period: Mar’04 – Oct’04
Organisation: Hindustan Aeronautic Limited (HAL), Bangalore
Software Used: CATIA, AutoCAD, MS-office
Description: The project was undertaken in order to make extensive literature survey and technical analysis
for the similar systems, to design & develop the suitable architecture, hand calculation, mission
analysis and performance analysis using MS-Excel, study the FAR and ATA standard for
designing
-------------------------------------------------------------------------------------------------------------------------------------------------------
REFERENCES:
Will be provided upon request
Date:
Place: Bangalore (Indrajeet Singh)