Santhosh Kumar R
Self Employed at Electrical Engineer
10 Year(s) 0 Month(s) | Bangalore/Bengaluru | INR 11.70 Lac(s)
8073764126
santhoshrnaidu@gmail.com
10+ years work experience in Avionics Embedded System (Hardware and Software), Networking and Teaching Engineering Students.
WORK SUMMARY
Role: My Role and Responsibility is on multiple works on Development and testing life cycle of
Software and Hardware, Technical Support for Vendors and Other internal & external Teams, Test
facilities improvements, LRU System Integration with existing System. Defect investigation.

1. Design and Development of 7 Avionics Real time Simulation Models Windows VC++ (6.0, 2008) and VxWorks (TORNADO, ZINC ).
2. Employee review committee Accredited as Best Employee.
3. Rig are Enhanced as actual A/C Requirements for resolving the Aircraft Hardware Defect
4. Design and Development of Miniature Test Rig.
5. Leading Internal and External team for simulation software and Hardware enhancement for Test facilities.
6. Technical Support to Out Sourced Projects for Vendors on New Hardware and Software Developments.
8. Software Enhancement, Testing, Certification and Deployment of existing LRU Simulation Models.
9. Hardware Enhancement, Testing, Certification and Deployment of Actual RT integration
Aviation
Engineering - Software & QA
Technical Lead
WORK EXPERIENCE
Self Employed Jun 2016 - Till Date
Electrical Engineer
Electrical wiring works and fault findings and solutions.
Project Engineer -2 Jun 2011 - Jun 2016
Aeronautical Development Agency ADA, Min of Defense, Bangalore
Design Life Cycle for Simulation Software and Hardware with Hardware Defect Investigation and solutions. Design and Development of Miniature Test Rig. SDLC of NEW LRU models with Certification and Deployment on Test facilities. Hardware Defect Investigation in Aircraft. Leading Internal and External team for simulation software and Hardware enhancement for Test facilities. Technical Support to Out Sourced Projects for Vendors on New Hardware and Software Developments. Software Enhancement, Testing, Certification and Deployment of existing LRU Simulation Models. Hardware Enhancement, Testing, Certification and Deployment of Actual RT integration. Integration of technologies for Test Rig Facilities improvement with Certification.
Sr RF-H Aug 2007 - Jun 2011
Aeronautical Development Agency ADA, Min of Defense, Bangalore
Independent Verification And Validation of : Avionics Mission critical Software Life Cycle and Recommend for Airworthiness Certification. 1. Verification and Validation of Software and its artifacts SDLC Requirements, Analysis, Design, Development, Testing. 2. Generation of Observation Documents for IVV process validated Software. 3 Generation of Recommendation Documents for IVV process validated Software for Airworthiness Certification . 4. Testing and Clearing 3 HSI of Rigs .
Electronics Lecturer Mar 2007 - Aug 2007
MS Engineering College Bangalore.
Teaching engineering subjects
Electronics Lecturer Sep 2006 - Mar 2007
SVCE Bangalore
Teaching engineering subjects
Project trainee Sep 2005 - Mar 2006
Project trainee
Ic design IP Devp of ADPLL with Multiplier
PROJECT DETAILS
STANAG 3350 B to VGA converter and 1553B Device data acquisition unit
Jan 2016 to Feb 2016
DATA-SOL
7
Full Time
1. Technical Support for Vendors to interface and Test the Product with Existing Test Facilities. 2. Providing the interface for New Actual LRU/RT with the existing systems.
3
Wiring Changes/modification of Hardware is analyzed for test rig Enhancement, Problems in the facilities are debugged and modified, Actual RT/Support.
Project Details:
STANAG3350 VGA converter is integrated with existing test facilities, necessary wiring modification to interface Video, Controls and development environment are Analyzed modified and provided. Each modification Certification process is processed to get certification for Rollout the test facilities. The Video is STNAG-3350B problem is identified, debugged and informed to the team for the circuit electrical and connector modifications from single end to differential end signal type. DDA: Device data acquisition unit is the interface used to record the BUS Data. This is integrated with existing test facilities, necessary wiring modification to interface BUS, Read Write Controls and Data retrieving. DDA is under development, DDA are problems are Analyzed (timings issues with data read and write on BUS) observation is given to the Vendors and provided.
MSA RADAR
Oct 2015 to Jan 2016
LRDE
7
Full Time
Technical Support for Out Source/ Vendors/Other Teams to support the project
3
Hardware, Technical Support and Analysis of Display Video Signals electrical problem
Project Details:
MSAR is integrated with existing test facilities, necessary wiring modification to interface Video, Controls and development environment are Analyzed modified and provided. Each modification Certification process is processed to get certification for Rollout the test facilities. The MSAR Video is STNAG-3350B problem is identified, debugged and informed to the team for the circuit electrical modifications.
STANAG 3350B to VGA converter
Sep 2015 to Feb 2016
VIDEOTRONIXS
7
Full Time
1. Technical Support for Vendors to interface and Test the Product with Existing Test Facilities. 2. Providing the interface for New Actual LRU/RT with the existing systems.
4
Changes/modification of Hardware is analyzed for test rig Enhancement, Problems in the facilities are debugged and modified, Actual RT/Support equipments Integrated.
Project Details:
STANAG3350 VGA converter is integrated with existing test facilities, necessary wiring modification to interface Video, Controls and development environment are Analyzed modified and provided. Each modification Certification process is processed to get certification for Rollout the test facilities. The Video is STNAG-3350B problem is identified, debugged and informed to the team for the circuit electrical voltage level modifications and connector modifications from differential end signal type. For each modification are Tested with internal team and Certification agency. Each modification Certification process is processed to get certification for Roll out the test facilities.
Develpmet Life Cycle of Mission Critical MIN Modeler Test Rig
Sep 2015 to Jan 2016
ADA
7
Full Time
Design and Development life cycle, Resolving problems, technical support, testing and Certification of MIN Modeler Test Rig as per DO-2167A STD with Artifacts.
3
c, c++, MFC
Project Details:
New Avionics Test facility is designed and developed for regular Mission critical software testing activities. This facility designed in modular type. Test facility Specification, Requirement, Analysis, Design, Development, Testing, Certification and Deployment with Artifacts are completed by In-house my team of 3 members with regular activities. This facility is developed at Very low cost and Less Space with full fledged functionalities with Partial Dynamic. This Rig is designed to reduce the Space, Cost, Power with Full functionality for the user. this rig uses 2 Desktop PC for all functionality instead of 35 PC used by other old facilities by providing new features like Dynamics DATA updates . Both Hardware and Software are designed, developed, tested, artifacts generated and Deployed for the user. this rig can be spared and reconnected with in 30 min. this can be connected on floor/ table also. this is use full for carry the Rig fro one place to another place.
Multifunction Display unit is the interface to display the Displays Data and recitals.
Feb 2013 to Sep 2013
MILL COTS
3
Full Time
1. Technical Support for Vendors to interface and Test the Product with Existing Test Facilities. 2. Providing the interface for New Actual LRU/RT with the existing systems.
2
Technical Support
Project Details:
Multifunction Display unit is the interface to display the Displays Data and recitals. This is integrated with existing test facilities, necessary wiring modification to interface RS422 Data and RGB video, RS422 Controls. This is support for the commercial MFD is under development, MFD are problems are Analyzed (color, Protocols, timings issues with data in RS422 on BUS) observation is given to the Vendors and provided.
DP557
Jan 2012 to May 2014
DATA PATTERNS
7
Full Time
Changes/modification of Hardware is analyzed for test rig, Enhancement, Problems in the facilities are debugged and modified, Actual RT/Support equipment's Integrated, for each modification are Tested with internal team and Certification agency
1
Providing the interface for New Actual LRU/RT with the existing systems
Project Details:
DP557 PCI based card are used in the RT/LRU simulation Model Development. DP557 is the interface used to connect PC and 1553B BUS to Read and Write Data. DP557 are problems are Analyzed (Diver issues with data read and write on BUS) observation is given to the Vendors.
Design and Development of New LRU Models
Jan 2012 to Feb 2016
ADA
7
Full Time
DOD2167A with SDLC - Waterfall Model, STLC, Certification and placed on Rig Providing requirements for Design and Development of new LRU Models. Resolving the Problems/Bugs and directing the team to move smoothly ahead in project.
2
C, C++, MFC, VC++,
Project Details:
Developed New Seven LRU Simulation Models, certified, integrated and maintained in Test facilities. Requirement is captured, analyzed, Design is provided for internal development team for implementation. Functionalities of model are tested with internal and certifying team for Certification. Certified models are deployed and maintained in the Test facility
Radar Interface
Oct 2011 to Jan 2012
ADA
9
Full Time
High Level Requirements Capture, Use Case, Test Case. ADA95 Coding. CSC, CSU and CSCI (DO178B Level B/C).
1
ADA95 implementation by ADA multi 4.5., Apex ADA, RTRT, Knowledge DOORS.
Project Details:
System Integration of Multi Mode Radar (MMR) RT functionalities and display with existing Avionics System through 1553B protocol. Interface requirements are captured by the provided MMR specification documents and display requirements given by User (Pilot) for display are analyzed implemented as per development life cycle(DOD 2167A STD) with waterfall process and Tested with artifacts. Updated source code builds are given to the testing team for testing and certification process.  Language : ADA95.  OS And IDE : Windows Apex ADA.  Development and Process: DOD2167A, Water Fall.
Technical support for vendors
Jul 2011 to Jun 2016
ACL Hyderabad
8
Full Time
SDLC - Waterfall Model , STLC, certifiication, integrated and maintained in Test facilities, Test facilities used for testing and certifying the developed Airworthy Software for its Real Time functionalities".
3
C, C++, Vc++MFC
Project Details:
For existing 34 LRU Simulation Models New change request/Bugs/model functionalities improvements requirements are analyzed and capture, design changes are provided to Internal /External(Out sourced) team for enhancement of models. Updated model are Tested with internal and certifying team for clearance and Certification. Certified models are deployed and maintained in the Test facility.
Technical support for vendors on Hardware.
Aug 2007 to Feb 2016
COMAVIA , SLN Technologies,Pinaka Areospace LTD
7
Full Time
System interfaces, Hardware and software Defects investigation and solutions for the system interface in ADA Avionics Missions Management Systems test facilities.
12
DO 2157A STD.
Project Details:
Wiring Changes/modification of Hardware is analyzed for test rig Enhancement, Problems in the facilities are debugged and modified, Actual RT/Support equipments Integrated, for each modification are Tested with internal team and Certification agency. Each modification Certification process is processed to get certification for Rollout the test facilities.
Software testing in Independent Verification and Validation Team carried out on Application software
Aug 2007 to Jun 2011
ADA
11
Full Time
Software testing in Independent Verification and Validation Team carried out on Application software test faculties Simulation Software. CIU and ECFM Simulation Software for test facilities for testing Airworthy Application Software
1
ADA 95, Apex, ADA Muilt.
Project Details:
Verification and Analysis:  System/Segment Specification document  Software Requirements document  Software design document  Code analysis  Software Test description document  Software Test Report document  Tractability Matrix All above are comply then Validation process for the Software build will be started. Validation: Software build tested with test cases provided by the developer and manual test ceases are generated as per the requirements for verification. Documents:  Observations Report are raised on each level if it fails comply for given requirements.  If all the Verification, Analysis and Validation process complies for the specification and requirements, then Recommendations report is given to certification agency for certifying the Software build for Airworthy use.
EDUCATION DETAILS
P.G.
M.Tech (Electronics/Telecommunication) 2006
NMAMIT
U.G.
B.Tech/B.E. (Electronics/Telecommunication) 2002
Visveswaraiah Technological University (VTU)
IT SKILLS
Skill Name Version Last Used Experience
ADA 95 2012 4 Year(s) 6 Month(s)
VxWorks 5.4.2 2016 4 Year(s) 6 Month(s)
ZINC 6.0 2016 4 Year(s)
Design Life Cycle Software and Hardware 2167A, 2016 8 Year(s) 6 Month(s)
COMMINICATION 1553B 2016 8 Year(s) 6 Month(s)
C, C++, VC++ MFC VC++6.0 2016 4 Year(s) 6 Month(s)
knowledge on STD Not worked DO - 178B 2016
knowledge on STD Not worked IEEE12207 2011 6 Month(s)
DESIRED JOB DETAILS
Permanent / Temporary
Full Time, Part Time
Need H1 Visa
Bangalore/Bengaluru
PERSONAL DETAILS
Santhosh Kumar R
Male
Married
19 Mar 1978
S/O RAJANNA.M, SANTHOSH NILAYA,NEAR BAY PASS CIRCL BASAVANAMUTT ROAD,NELAMANGALA, Bengaluru-562123
8073764126(M) , 91 80 27723236(R)
santhoshrnaidu@gmail.com
CANDIDATE TEXT RESUME
RESUME





10+ years work experience in Avionics Embedded System (Hardware and Software), Networking
and Engineering Teaching.

1. Aeronautical Development Agency (ADA) Year: August 2007 � June 2016.
a. Independent Verification and Validation Year: August 2007 � June 2011.
b. Project Engineer-2(Test Facility Manager) Year: June 2011 � June 2016.
2. Teaching in Engineering collage Year: Sep 2006 � August 2007.
3. Networking and System Service in Infinity InfoTech Year: Nov 2002 � Dec 2003.

8 years 7 months of experience in Aeronautical Development Agency (ADA), Ministry of Defense,
Bangalore. Year: Aug 2007 � June 2016.

1. Project Engineer-2 as an Avionics Test Facility Manager: Year: June 2011 � June 2016.
�Multiple Role and Responsibilities carried out on both Hardware and Software of Lane
Replacement Unit(LRU) and Test Facilities on Development life cycle (Requirements capture
Design and Development or Enhancements, Testing), Certification, Deployment, Maintenance and
Technical Support for Vendors, Other Internal & External Teams. LRU System Integration and
Defect investigation onsite and insight�

? Software (SDLC) Development Life cycle, Certification, Deployment and Maintenance with
Avionics DOD-2167A-STD.

? Hardware Development Life cycle, Certification, Deployment and Maintenance with Avionics
DOD-2167A-STD.

? Experience in Design and Development of Avionics Test Facilities to facilitates for testing the
real time functionalities of developed Airworthy software.

? Experience in Defect investigations and Analysis on both Hardware and Software of Lane
Replacement Unit(LRU) and Test Facilities.


Email: santhoshrnaidu@gmail.com Contact No: 8073764126/9448324803

RESUME
? Exposure in drafting and implementing different processes and have actively involved in
DO2167A and IEEE 12207 certifications for both Hardware Multiple Test facilities and
Software.

? Handling and supporting the Vendor's team for outsourced projects, with all the stages of
Hardware and Software including Designing, Developing, Enhancement, Integration, Testing,
Certification and Roll out of Products for LCA Avionics Test Facilities.

Projects Handled: Dated: - Feb 2012 - June 2016.

Role and Responsibilities: �RT/LRU Simulation Models are developed, certified, integrated and
maintained in Test facilities, Test facilities used for testing and certifying the developed Airworthy
Software for its Real Time functionalities�.

? Leading the Software Teams:

Sl. No Team Members LRU Simulation Software Models
1. Internal 3 Requirements, Debug, Analysis, Design,
Vendor ACL, Development, Enhancement, Testing, Integration,
2. 3
Hyderabad Certification, Deployment & Maintenance.

Project 1 Test Facilities Software:

A. SDLC on New 7 LRU Simulation Models, certified, integrated and maintained in Test facilities.
Requirement capture, analyze, design is provided for internal development team for
implementation of model functionalities, model functionalities are tested with internal and
certification certifying team certified models are deployed and maintained in the Test facility.

B. For existing 34 LRU Simulation Models New Change Request/ Identified Bugs which effects on
model functionalities improvements requirements are analyzing, requirements capture and design
changes are provided to Internal /External(Outsourced) team for enhancement of models. Updated
model are Tested with internal testing team and for Clearance and Certification by IVV and
Certifying Agency teams. Certified models are deployed and maintained in the Test facility.

C. Major Modification in Test Facility by 1553B Multiple RT technology is implemented using DDC PCI
based Hardware for development of new Test facility. Specification, Requirement, Analysis,
Design, Development, Coding (C and C++ with Multi thread concepts) and Testing of 24 LRU
Models functionalities are emulated Real Time Concepts.

D. By test criteria technically support provided for Vendors to Develop or Modify the existing system
functionalities as per the real time requirements for project. While integrating the systems its defect
is identified and solution are provided LRU application Software modification.

a) Language : C, C++, MFC.

Email: santhoshrnaidu@gmail.com Contact No: 8073764126/9448324803

RESUME
b) OS and IDE : Windows VC++ (6.0, 2008) and VxWorks (TORNADO,
ZINC for GUI).
c) Development STD and Process: DOD2167A, Iterative/Incremental
Model.
? Design Pattern Layer Type is used for Design and Development.
? GUI developed by using VC++ MFC used for display receives and transmit the
data.
? Data Intercommunication between the layers by predefined structures,
memory allocation, internal timers, threads and semaphores used for receive
and transmit the data and data conversion. (Note No process are used)
I don�t get opportunity to work on device driver�s development work.

E. Defects are identified by data analysis, suggestion is provided (Modification of System timing,
Communication, Interface Issues etc...) for Vendors and internal team for the Systems under test.

Project 2 Test Facilities Hardware:

Role and Responsibilities on Avionics Mission Software Test Facilities Hardware:
�Avionics Mission Software Test Facilities Are Developed, Certified, Integrated and Maintained.
Test facilities used for testing and certifying the developed Airworthy Software for its Real Time
functionalities�.

? Leading the out sourced Hardware for Maintenance Teams:

? Technical Support for Vendors to Enhance, Test and Certification of 3 Test Facilities.

? Requirement, Analysis, Design, Development/Enhancement, Testing, Certification, Deployment
and Maintenance of Existing Test Facilities for Avionics Mission Software testing.

Sl. No Company Team Avionics Mission Software Test Facilities
1. COMAVIA 3 Wiring Changes/Modification of Hardware is analyzed for test rig
Year: 2011-2016 Enhancement, Problems in the facilities are debugged and modified,
2. PINAKA 2 Actual RT/Support equipment�s are Integrated and each modification
AEROSPACE is Tested with internal team and Certification agency. Each /multiple
LTD modification processed to get certification and Rollout the test facilities
Year: 2011-2013 for software testing team for testing there developed software.

? Technical Support for Out Source/ Vendors/Other Teams to support the project:

? Technical Support for Vendors to interface and Test the Product with Existing Test Facilities.

? Providing the interface for New Actual LRU/RT with the existing systems.

Email: santhoshrnaidu@gmail.com Contact No: 8073764126/9448324803

RESUME

Sl. No Company Project Responsibility
1. LRDE MSA MSAR is integrated with existing test facilities, necessary wiring
RADAR modification to interface Video, Controls and development
environment are Analyzed modified and provided.
Each modification Certification process is processed to get
certification for Rollout the test facilities.
The MSAR Video is STANAG-3350B problem is identified,
debugged and informed to the team for the circuit electrical
modifications.
2. DATA-SOL STANAG STANAG-3350B VGA converter is integrated with existing test
3350 B to facilities, necessary wiring modification to interface Video, Controls
VGA and development environment are Analyzed modified and
converter provided.
Each modification Certification process is processed to get
certification for Rollout the test facilities.
The Video is STANAG-3350B problem is identified, debugged and
informed to the team for the circuit electrical and connector
modifications from single end to differential end signal type.
3. DATA-SOL DDA Device data acquisition unit is the interface used to record the BUS
Data. This is integrated with existing test facilities, necessary wiring
modification to interface BUS, Read Write Controls and Data
retrieving. DDA is under development, DDA are problems are
Analyzed (timings issues with data read and write on BUS)
observation is given to the Vendors and provided.
4. VIDEOTRONIXS STANAG- STANAG-3350B VGA converter is integrated with existing test
3350B to facilities, necessary wiring modification to interface Video, Controls
VGA and development environment are Analyzed modified and
converter provided.
Each modification Certification process is processed to get
certification for Rollout the test facilities.
The Video is STANAG-3350B problem is identified, debugged and
informed to the team for the circuit electrical voltage level
modifications and connector modifications from differential end
signal type.
5. MIL COTS MFD Multifunction Display unit is the interface to display the Displays
Data and recitals. This is integrated with existing test facilities,
necessary wiring modification to interface RS422 Data and RGB
video, RS422 Controls. This is support for the commercial MFD is
under development, MFD are problems are Analyzed (color,
Protocols, timings issues with data in RS422 on BUS) observation
is given to the Vendors and provided.
6. DATA DP-557 DP-557 PCI based card are used in the RT/LRU simulation Model
PATTERNS Card Development. DP557 is the interface used to connect PC and
1553B BUS to Read and Write Data.

Email: santhoshrnaidu@gmail.com Contact No: 8073764126/9448324803

RESUME
DP557 are problems are Analyzed (Diver issues with data read
and write on BUS) observation is given to the Vendors.





Project 3:
Role and Responsibilities Software Developer in the same department for a year:
Dated: - June-2011- Feb 2012
a) Language : ADA95.
b) OS And IDE : Windows Apex ADA.
c) Development and Process : DOD2167A, Iterative/Incremental
Model
System Integration of Multi Mode Radar (MMR) RT functionalities and display with existing
Avionics System through 1553B protocol. Interface requirements are captured by the
provided MMR specification documents and display requirements given by User (Pilot) for
display are analyzed implemented as per development life cycle(DOD 2167A STD) with
waterfall process and Tested with artifacts. Updated source code builds are given to the
testing team for testing and certification process.

Achievements:

? Invention of New Avionics Test facility is designed and developed for regular Mission critical
software testing activities. This facility designed in modular type by reducing 35 PC to 3 PC which
reduced Power consumption, Cost, Space, Manpower etc....
? Test facility Specification, Requirement, Analysis, Design, Development, Testing, Certification and
Deployment with Artifacts are completed by In-house my team of 3 members with regular activities.
This facility is developed at Very low cost and Less Space with full fledge functionalities with Partial
Dynamic.
? Modification of existing 3 Test facilities for ergonomics conditions and providing functionalities
improvements for current technologies for the fast process.
? Technical Support and Problem resolving for Vendors.

2. Independent Verification and Validation as Senior Research Fellow � H:
Dated: - Aug 2007 � June 2011
Role and Responsibilities: Software testing in Independent Verification and Validation Team
carried out on Application software test faculties Simulation Software.
? Language : ADA95 Airworthy Application software,
C, C++ Simulation Models of Test Facilities
? OS : Windows and VxWorks.
? IDE and Tools : Geeen Hils ADA, Apex ADA, Understand ADA and VC++ 6.0
? Development and Process : DOD2167A, Iterative/Incremental Model.
Email: santhoshrnaidu@gmail.com Contact No: 8073764126/9448324803

RESUME
? Company : L&T (SPECTRUM INFOTECH)
? Projects : ECFM SOP-III Test Facilities.
CIU Test Facilities.
RT/ LRU CIU and ECFM Airworthy CIU and ECFM Simulation Software for
Role & Application Software test facilities for testing Airworthy
Responsibilities Application Software
Language ADA95 C, C++
? System/Segment Specification document
? Software Requirements document
? Software design document
Verification and ? Code analysis
Analysis ? Software Test description document
? Software Test Report document
? Tractability Matrix
All above are comply then Validation process for the Software build will be started
Software build tested with test cases provided by the developer and manual test cases
Validation
are generated as per the requirements for verification.
? Observations Report are raised on each level if it fails comply for
given requirements.
Documents ? If all the Verification, Analysis and Validation process complies for the
specification and requirements, then Recommendations report is given to
certification agency for certifying the Software build for Airworthy use.
? IVV process on Heuristic tool with reference to LDRA Functionalities.
Other
? Supporting to project IVV process on other system on emergency.

3. 1 year of experience teaching Engineering Students in Engineering collage.
Role: Lecturer
Subject: Telecom and Switching, Satellite communication, VHDL, Basic of computers
LAB: VHDL, Digital Electronics, Logic Design.

4. 1 year of experience on LAN Networking and System Service in Infinity InfoTech,
Bangalore.
Role and responsibility: LAN networking problem resolving, Servicing of PC till Board level
Technical Skills:

? Programming Languages : C, C++, MFC and ADA95.
? Operating Systems : Windows.
Email: santhoshrnaidu@gmail.com Contact No: 8073764126/9448324803

RESUME
? Tools & Technologies : Understand, VC++.
? Coding Standards : Avionics DO-2167A, IEEE 12207.
? Communications : 1553B, RS232, RS422, Ethernet.
? Technical Support : Vendors team and Internal Other Dept. team.
? Knowledge : HDL (VHDL, Verilog). ARINC 429.

Education Details:
Sl. No Course Specialization Institute Year of completion
1. M-Tech Microelectronics & Control Systems NMAMIT VTU 2004-2006
2. BE Electronics & Communication APSRCE VTU 1998-2002



Personal Details:

1. NAME : Santhosh Kumar R
2. DOB : 19.03.1978
3. Address : Santhosh Nilaya, Basavannamutta Road,
Near Bypass Circle, Nelamangala, Bangalore Rural,
Karnataka .562123.
4. Contact No : 8073764126
5. Notice Period : 8 days
6. Pervious CTC : 11 LAP
7. Expected CTC : As per company norms,
8. Present Employment : Self-employed.
9. Email ID : santhoshrnaidu@gmail.com




Email: santhoshrnaidu@gmail.com Contact No: 8073764126/9448324803