Qualification
Year
School/Institute
Board/University
B. Tech
(Aeronautical
Engineering)
2017
Feroze Gandhi
Institute of
Engineering
&Technology,
Raebareli
Dr. A.P.J Abdul
Kalam Technical
University(U.P)
Diploma
(Electrical
Engineering)
I.T.I.
(Electrician)
2014
2012
Prasad
Polytechnic,
Lucknow
RMS ITI,
Varanasi
Board of Technical
Education (U.P)
State Council for
Vocational Training
(U.P)
High School
2007
DAV Public
School
Dudhichua
CBSE Board
NARENDRA KUMAR
Contact details -
adjbzl@r.postjobfree.com
Singrauli, (M.P)
Address -
B-764
Sector -B Colony
Dudhichua
Singrauli, (M.P)
486888
Personal profile -
Date of birth – 20-July-1991
Gender – Male
Blood group - B+
Nationality – Indian
Marital status – Unmarried
Objective -
To obtain a responsible, challenging, and awarding position in an aviation development organization with an established track record where my skills and technical abilities can be utilized.
Specialization -
Aeronautical Engineering
Academic Insight -
Summer Training -
Industrial Summer training at Hindustan Aeronautics Limited, Lucknow (U.P)
Description –
Studied hydraulic & pneumatic landing gear system
Studied about various aircraft accessories
Details about fuel system of SUKHOI SU-30 MKI
No. of fuel tank – 6 (1, 2, 3RT, 3LT, 4, 5)
tank no. 2 (service tank)
Fuel capacity - 1200 kg
Capacitance probes used – DT41-4, DT41-5, DT41-6,
DT41-7, DT41-8
Fuel Quantity unit – BT3-4 (warning signal)
Graduate Apprentice Training –
(01-05-2018 to 30-04-2019)
Languages –
English
Hindi
Line and base experience -
One year Graduate Apprenticeship Training from Hindustan Aeronautics Limited, TAD Kanpur (U.P)
Worked in DO 228 structural assemblies (fuselage, wing, spar, ribs and stringers and sheet metal skin).
(DO228NG) Glass cockpit -
–– Four 8.9 inch liquid crystal HD displays
–– Primary Flight Display (PFD) with multiple display setting
–– Navigation display with TAWS overlay
–– Multi-sensors FMS
–– Emergency ESIS with navigation capability
(DO228NG) Engine and Propeller -
Improved performance by new 5-bladed propeller in
combination with the fuel-efficient TPE331-10 engine. Engine specifications -
Dimensions - 1080 – 518 – 676 (mm)
(length – width – height)
Weight - 385 lb
Pressure ratio - 10.55
Power - 940 shp
ESFC - 0.534 lb/hp-h
Commercial operation min 800 h/yr
Utility software –
MS Office
Area of Interest -
Aircraft Propulsion
Aircraft maintenance
Aircraft Quality Inspection
Hands on experience in assembly & disassembly of Dornier
(DO-228) and AVRO (HS-748) overhaul system.
Aircraft hydraulic LRU’s (Line Replaceable Unit) as – Power packs, accumulators, brake assembly, etc.
Overhauling & maintenance of propeller blades
(Dismantle, NDT process, rectification of item, removal of dents, balancing, etc.)
Gear box repair & overhaul
(Fits, shafting, gearing, cases & housing, assy. & run test, etc.) Strength –
Quick learner
Hardworking
Adaptive to any
environment
Engine Benefits -
–– Very high ram pressure recovery
–– Low frontal area reducing drag to a minimum
–– Simple Engine Anti-Ice System
–– Low Maintenance Cost
–– Time between overhaul up to 7,000 hours
5-bladed Propeller -
–– Lighter propeller: Reduced stress on the engine and electrical system during start up.
–– Smaller propeller diameter: Reduce noise and increased ground clearance.
Industrial exposure –
Assuring the machined parts, detail components & fastener used in aircraft as per the quality standard
Analyzing the technical drawings and ensuring the team follows the assembly manufacturing process
Possess the administrative skill
Effective team management
Key skill & Proficiency –
Can work effectively in team as well as individually Good communication skills
Ability to work under pressure & consistently meet deadlines. Declaration –
I hereby declare that above information is correct to the best of my knowledge and belief.
Date -
Place – Singrauli (M.P) Narendra Kumar
Hobbies –
Walk, yoga
Travelling
Internet surfing