This resume is for Md Nishar, an IT professional with over 4.9 years of experience in software testing. He has extensive experience testing safety critical avionics systems according to DO-178B standards. Some of his skills and experiences include unit testing, software integration testing, model based testing, debugging, requirements and configuration management tools. He has worked on projects for companies like Rockwell Collins, Goodrich, and Gulfstream testing components like head up displays, electric brake controls, and touch screen controllers. His education includes a Bachelor's degree in electronics engineering.

1. RESUME
Md Nishar
Email : nishar.md@gmail.com
Phone: +91-814712176
Objective
 Intend to build a career with leading corporate of Hi-tech environment with committed &
dedicated people, which will help me to explore myself fully and realize my potential.
Summary
 Overall 4.9 years of IT Experience which include experience in the field of RBT in HSIT
(Hardware software integration testing), SWI (Software integration testing), UT (Unit
testing) Experienced in the Software Verification activities for safety critical systems in
compliance with DO-178B standards
 Well skilled in the area of Software Testing and Debugging for safety critical systems.
 Well skilled in the area of Model Based Testing like SCADE Models and MATLAB
Models.
 Good Understanding of DO-178B guidelines.
 Good in programming with C language.
 Good understanding in UML, MATLAB, SCADE Module testing.
 Strong Debugging and problem solving skills.
 Have good experience in Software Integration Testing, Unit Testing and System Testing.
 Good experience in Traceability and requirement management tools and Configuration
Management Tool.
Professional Experience:
 Working in client place at Rockwell Collins in Hyderabad as a contractor and permanent
employee of L&T Technology services, as a Senior Software Engineer in Bangalore.
Education:
 Bachelor of Engineering in Electronic & Communication engineering from B.I.T Sindri
Engineering College, Dhanbad affiliated to VBU, in the year 2006 – 2009 with aggregate
of 72.76%.
 DIPLOMA. Electrical Engineering with 80.25%from Jharkhand University.
Technical Skills:
Domain Knowledge : Avionics / Embedded Systems
Testing tools : TESSY, LDRA,TIU TATS, TIU Client, TIU Server, EASE
Simulation, Escape Tool, SC Tool, UDC+,Vector Cast,ALM
Languages : C, VB script, Perlscript, C script
Guideline : DO-178B
Protocols : ARINC 429, CAN, AFDX
Configuration Tool : SVN, PVCS (Serena Dimensions), Jira issue tool,
Rational CLEAR CASE and Clear Quest
Requirement Tool :DOORS

2. PROJECTS
1. Project Name: HUD (Head Up Display) on B737 Max
Client Rockwell Collins
Role Low Level Testing
Software
Criticality
Level –A
Project duration Jan 2015 to Till now
Environment
(With skill
versions)
Software &
Tools
Target system, SVN ,DOORS,Understand C, Jira
tools,ALM
Project Description:
HUD is a display device which provides the primary interface between the crew and the aircraft
systems. HUD have total 5 LRU which will provide the display of runway information like how
to take land off how much angle is required to landing it will display the altitude latitude At the
top of head.
Contribution:
As a Senior Software Engineer, was responsible for,
 Development of test case and test procedures for low level requirements to comply DO-
178B guidelines.
 Execution of test procedures and verifying on Target and host system.
 Confirms that test procedures adequately verify the requirements such that the test meets
design standard and the results are correct.
 Interaction with Client through WebEx.
 Delivery responsibility of artifacts to the customer.
2. Project Name: EBAC (Electric Brake actuator control) on E787
Client Goodrich
Role High Level Testing
Software
Criticality
Level –A
Project duration July 2014 to Jan 2015
Environment
(With skill
versions)
Software &
Tools
Actual system, SVN , Polarion ,DOORS
Project Description:
EBAC is a LRU which provide the Brake in Aircraft. EBAC is directly interface with EBPSU,
RDC and BSCU by CAN Protocol. There are total four EBAC used in one aircraft and four
Brake assembly two are in Left side and two are Right side .In Left side two brake assembly are

3. left out board and left in board In Right side two brake assembly are right out board and right in
board. Aircraft have total 8 wheel and each 2 wheel are belong to each brake assemble brake
assemble are control by one EBAC .Each EBAC have 8EBA then totally 32 EBA in one aircraft
Contribution:
As a Senior Software Engineer, was responsible for,
 Development of test case and test procedures for high level requirements to comply DO-
178B guidelines.
 Execution of test procedures and verifying on Actual system.
 Confirms that test procedures adequately verify the requirements such that the test meets
design standard and the results are correct.
 Analyze and report the bugs and Manage test results.
 Coordination of team with for technical problem.
 Interaction with Client through WebEx.
 Delivery responsibility of artifacts to the customer.
3. Project Name: TSC(Touch screen controller) on G650
Client Gulf stream
Role High Level Testing
Software
Criticality
Level –A
Project duration April 2013 to June 2014
Environment
(With skill
versions)
Software &
Tools
C, VBscript, TIU TATS, TIU Client, TIU Server, EASE
Simulation Tool, PVCS, Jira Tool, EscapTool, SC Tool.
Project Description:
TSC is a LRU that provides primary interface between the crew and the aircraft systems. SC will
interface to system that are federated using individual interface busses or to system that are
integrated using an interface to MAU (Modular Avionics Unit) .TSC provides a flexible
interactive space that uses the LCD display to provide a configuration of interactive elements to
meet needs of flight crew. TSC replaces MCDU and SMC (Controller Functionality) and crew
audio interface is moved on TSC. There are 5 TSC on PV-10 flight deck. 2 outboard, 2 pedestals,
1 in the observer station. Each TSC is connected to the two onside AGM-300 via point to point
Ethernet connections. TSC 2, 3 & 5 also support A429 direct connect functions.
Contribution:
As a Software Engineer, was responsible for,
 Development of test plan and test procedures for single level requirements to comply
DO-178B guidelines.
 Execution of test procedures and verifying on simulation tool.
 Confirms that test procedures adequately verify the requirements such that the test meets
design standard and the results are correct.
 Analyze and report the bugs and Manage test results.
 Coordination of team with technical problem.
 Interaction with Client through WebEx.

4.  Delivery responsibility of artifacts to the customer.
4. Project Name: Flight Control System(FCS) for Russian Regional Jet
(RRJ)
Client Liebherr-Aerospace Lindenberg GmbH
Role Unit Integration Testing
Software
Criticality
Level –A for Monitor channel, Level –B for control channel and Level –
C for Motor control channel pertaining to DO-178B guidelines.
Project duration Jan 2012 to April 2013
Environment
(With skill
versions)
Software &
Tools
C, UDC+, Tessy Testing Tool, Clear Quest.
Project Description:
RRJ flight control system (FCS) is a digital fly-by-wire (FbW) FCS with no mechanical backup.
The FCS consists of cockpit controls, two Rate Sensor Units (RSU), three types of flight control
computers (primary flight control units (PFCU), actuator control electronics (ACE) and motor
actuator control electronics (MACE)), as well as control surface actuation elements, Cockpit
controls and RSU inputs are transmitted to the ACEs and MACEs, and further to the PFCUs. On
the ACEs, MACEs and PFCUs these inputs and inputs from other aircraft systems are processed
by flight control law algorithms and computed control surface commands are transmitted to the
actuators. All flight control computers are designed in control and monitor channel architecture.
All functionalities are implemented by software.
Contribution:
As a Software Engineer, was responsible for,
 Identify the all test inputs software requirements, software architecture,
traceability, source code and executable object code as per SVP (Software
verification plan).
 Analyze the requirements whether it is verifiable or not
 Define Software Verification Cases and Procedures (SVCP) which includes all test
cases and test scripts and instructions for how to execute these test scripts.
 Execute Functional and performance tests on target computer to ensure
compliance to the software requirements
 Perform requirement coverage analysis to check for which requirement test cases
are missed out
 Perform code coverage by using TESSY TOOL to check for which code structure
test cases are missed out.
 Perform analysis of the test results and update Software Verification Report
 Peer Review and group coordinator in Code Reviews.
5. Project Name: FLAP CONTROL SYSTEM for Learjet (LJ200)
Client Liebherr-Aerospace Lindenberg GmbH
Role Unit Integration Testing

5. Software
Criticality
Level –A for Monitor channel, Level –B for control channel and Level –
C for Motor control channel pertaining to DO-178B guidelines.
Project duration Dec 2010 to Jan 2012
Environment
(With skill
versions)
Software &
Tools
C, UDC+, Tessy Testing Tool, Clear Quest.
Project Description
The project is to realize a campaign of unit-integration testing in on the host machine.
The requirements are given as a Design Description Document for testing. The
functional test cases are created by understating the requirements. As the process of
integration is complicated, the tool performs the action of identifying the global
variables from the source code. From the tool, truth table is prepared in CTE
(Classification tree editor). Empty test cases are created by the tool. In TDE (Test data
editor) test cases are edited and perform testing with a debugger window enabled.
Contribution
As a Software Engineer, was responsible for,
 Identify the all test inputs software requirements, software architecture,
traceability, source code and executable object code as per SVP (Software
verification plan).
 Analyze the requirements whether it is verifiable or not
 Define Software Verification Cases and Procedures (SVCP) which includes all test
cases and test scripts and instructions for how to execute these test scripts.
 Execute Functional and performance tests on target computer to ensure
compliance to the software requirements
 Perform requirement coverage analysis to check for which requirement test cases
are missed out
 Perform code coverage by using TESSY TOOL to check for which code structure
test cases are missed out.
 Perform analysis of the test results and update Software Verification Report
 Peer Review and group coordinator in Code Reviews.
Major Achievements in the company
 Got five times the Pat on back (POB) reward for on time delivery and quality product.
 Got Associate of the Month reward for integrating different builds within short span of
time.
Personal Profile:
Languages known – English ,Hindi
Nationality - Indian
Passport No. - H4100908
Validity - Till 06-MAY-2019

6. Declaration:
I hereby declare that the particulars given herein are true to the best of my knowledge and belief.
Md Nishar