1. PIYUSH KANT SINGH
Mobile: 08197074284(Bangalore)/8897195275(Hyderabad) E-Mail: piyushkantmech@gmail.com
Seeking Reliability Engineer assignments with an organisation of repute
3.4+ years of experience as Reliability Engineer in Aerospace industry.
Excellent abilities in analyzing complex problems to develop corrective action alternatives; skills in
preparing comprehensive, clear and concise reports.
Tr
Growth Path
Jun’ 2010-Jul’2010: Industrial trainee Gas Turbine Research Establishment (DRDO), Bangalore
Jan' 2013- Oct’ 2013: Trainee engineer for Bharat Electronics, Bangalore
Oct' 2013- July 2015: Reliability & System Safety Engineer in Aeronautical Development Agency,
Bangalore (DRDO)
Aug’2015- Till date: CYIENT (UTAS), Bangalore
 Working on RIO tool (Reliability input to on track)
 Functional Hazards Analysis (FHA) as part of System Safety Analysis for MK-II Light
Combat Aircraft (LCA).
 Reliability Allocation of Hydraulics System for LCA MK-II Fighter Aircraft.
 Analysed system level Failure Modes, Effects & Criticality analysis (FMECA) for hydraulics
system of Light Combat Aircraft (LCA)
 Carried out FMEA of BASOV (Bleed Air Shut Off Valve) of Environmental Control System
(ECS) of Naval Variant of LCA for ski- jump from SBTF (Shore-Based Take-Off Facility).
 Constructed Reliability Block Diagram (RBD) and Prediction for aircraft Hydraulics
(HYD) System.
 Carried out Reliability Prediction for important Line replaceable units (LRU) like non
return valve, quick disconnect coupling, filters, hydraulic release valve, feed line filter
assembly etc of Light Combat Aircraft (LCA).
 Sound knowledge of Propulsion And Fuel System (PFS)
 Carried out the Fault Tree Analysis (FTA) for Brake Parachute System (BPS) for MK-II.
 Zonal Safety Analysis (ZSA) for all LRUs of Prototype Variant of LCA.
 Qualification and Acceptance testing of the LRU
 working knowledge of Life data analysis, FRACAS
 Understood Basics of fighter aircraft gas turbine engine
CAREER PRÉCIS
CAREER CONTOUR
RELIABILITY ENGINEERING PROFICIENCY
INDUSTRIAL TRAINING

2.  engine testing at GTRE
Reliasoft BlockSim 6.5, Item Toolkit 8.0, Relex 6.2, Weibull++.
I. Project: RIO (Reliability input on track)
 Commercial aircrafts
Project Summary: As various LRUs is being manufactured by UTAS and delivered to various
commercial airlines across the world, whenever some failure occurs (Scheduled/unscheduled)
they give description of those LRUs further we have to validate the data using RED BOOK and
ACAS and then analyze those failure description as part Root Cause Analysis (RCA).
II. Project: Functional Hazards Analysis (FHA) of :
 LCA MK-II Aircraft
Project Summary: As a part of System Safety Analysis, FHA for has been carried out using Mil-
STD-882D. Various hazards were identified and their respective Severity levels and Probability
of occurrence was recognized. Further, mishap/Hazard Risk Index (HRI) with suitable
acceptance criteria was established.
III. Project: LRU Level Reliability Allocation of hydraulic system for MK II Fighter Aircraft.
Tool Used: Microsoft Excel
Project Summary: Reliability apportionment is a technique used to allocate the LRU level
reliability requirement in order to meet the system level reliability goal using KARMIOL
METHOD. In this method, subsystem allocation reliability is computed as a function of numerical
factors of system complexity, state of the art, duty cycle, and environmental conditions.
IV. Project: Reliability Prediction of
 LRU level
Tool Used: Relex, Mechrel
Project Summary: The LRU Level reliability is predicted using Parts Stress method. It includes
LRUs of different systems mainly PFS and HYD.
V. Project: Reliability Prediction of
 Hydraulics system
Tool Used: Relex, Mechrel
Project Summary: The system level Reliability is predicted for Mission and Safe Return is
carried out with the help of BlockSim tool and using Mil-Std-756B. The Reliability analysis
enables to identify the measures required to enhance the performance Reliability of the system.
VI. Failure Mode Effect Analysis (FMECA)
 Hydraulic System (MK-I & MK-II)
Project Summary: FMECA is performed to identify basic faults at component level and
determine their effects at system level and finally on aircraft level. By tracing the effects of an
individual item, failures up to the system level are analyzed and thus how this failure affects the
overall aircraft level performance. Failure mode effect analysis is aimed at evaluating adequacy
of warnings/other safety provisions available for detection by pilot and ground crew in the
event of failure within the guidelines of MIL-STD-1629A.
VII. Project: Risk Assessment For LCA MK-I
Tools Used: Item Toolkit 8.0
MAJOR ASSIGNMENTS HANDLED
PROFICIENCY IN FOLLOWING TOOLS

3. Project Summary: The safety analysis for LCA MK-I aircraft system involves consideration of
many complex situations taken from aircraft level FHA. The various complex situations arising out
of the non-availability of essential functions and also due to inadvertent triggering of undesirable
events are meticulously identified. A probability of loss of function for all the identified complex
situations had been estimated using Fault Tree Analysis (FTA). From the estimated probability
and the assessed severity of the hazard of these complex situations, Hazard Risk Index Number has
been derived as per the MIL-STD-882D guidelines. Based on the risk index number, the decision
criterion is arrived.
VIII. Project: Life Cycle Management of SDR (Software Defined Radio)
Tools Used: NPRD-95, Pro-E, CATIA-V5, AutoCAD 2-D
Project summary: Responsible for quality, reliability & safety of Audio Adaptor Unit (AAU) and 50W
Power Amplifier during product Life Cycle management for LRUs. Modeling and drafting of LRUs of
SDR. Conducted Qualification testing viz. vibration, shock, thermal, gun fire, salt fog, bench handling,
bump & acceleration.
 B.TECH in Mechanical Engineering (2007- 2011)
Noida Institute of Engg & Tech. Greater Noida (Affiliated to UPTU, Lucknow)
 M.TECH in Quality Management (2015-2017) (On going)
BITS (WILP), PILANI
Date of Birth: 16th August 1989
Marital Status: Unmarried
Passport no: L8178788
REFERENCE
Shri Vijay Negi Shri N. Ramalingaiah
Scientist/Engineer ‘C’ Scientist/Engineer 'F'
Aeronautical Development Agency Aeronautical Development Agency
Bangalore - 560017 Bangalore - 560017
Work No: 9901021164 Work No: 08025087174
DECLARATION
I hereby declare that all the statements made above are true to the best of my knowledge and belief.
Piyush Kant Singh
PERSONAL DOSSIER
EDUCATIONAL DETAILS