S Anasuri Resume *

SRIKANTH ANASURI

accklq@r.postjobfree.com - Cellular: 316-***-****

PROFESSIONAL PROFILE

Total experience as Stress Engineer: Nine (9.0+) years

Airframe commodity experience: Fuselage, Wing Leading Edge and Trailing Edge Devices, and

Empennage

Stress skills:

Metals and Composites – Detail Part Sizing – Using Classical Hand Calculations, Static Strength and

Fatigue Strength Analysis (Durability), Linear FEM

Damage Tolerance Analysis (Residual Strength and Crack Growth Analysis)

Fleet Support Engineering – Structural Repairs

Formal Documentation

Design skills:

Catia V5 (familiar), Materials Selection and Corrosion Protection, and Load Path Development

Stress Engineer with extensive experience with various airframes such as Boeing 737, 767, 777 and Airbus projects.

Familiar with FAA/EASA Part 25 structures rules and regulations.

PROFESSIONAL EXPERIENCE

THE B OEING C OMPANY, E VERETT, WA 98204

STRESS ENGINEER ( CONTRACTING T HRU V OLT LLC) AUGUST 2007 –

TECHNICAL R ESOURCES

OCTOBER 2013

Position Profile:

Sustaining Engineering (in-service aircraft support) Groups: 767 Fuselage Stress (duration: 4.0+ years); 777 Wing

Control Surfaces and Empennage (duration: 2.0+ years).

Performed stress analysis of primary and secondary metallic and composite aircraft structures.

Performed stress analysis using Boeing Books 1, 2, 3 and 4, Boeing design manuals and also using Bruhn,

Roark, Niu, Peterson’s etc. reference books. Stress analysis included classical hand calculations, Boeing specific

computer programs and using Finite Element Analysis (FEA) tools.

Addressed several structural service related problems (SRP’s) in the fleet, and contributed into safety

investigation by preparing continued operational safety program (COSP) reports, providing product design

improvements and repairs.

Provided AOG support.

Developed, analyzed and documented structural repairs that were added into the SRM/CMM/SB’s.

Developed structural inspection plans using damage tolerance analysis in compliance with the FAA/EASA

regulatory requirements as in 14 CFR Part 25.571 and 14 CFR Part 26.43 (Aging airplanes - Repairs)

requirements.

Provided telex support by writing technical accomplishment instructions for repairs and modifications (addressing

SB’s, AD’s and AMOC’s as and when required) to Operators .

Created strength check notes in support of compliance finding of repairs for FAA approval with FAA 8100-9 form.

Very well familiar with the entire fuselage configuration, wing control surfaces (flaps, ailerons, flapperons, spoilers,

slats etc.) and empennage construction.

S Anasuri Resume 2

S Anasuri Resume 3

SPIRIT A EROSYSTEMS, WICHITA, KS 67218

(CONTRACTING THRU INFOSYS ) FEBRUARY 2006 –

STRESS ENGINEER

A UGUST 2007

Position Profile:

Group: Boeing 737 NG Sustaining

FAA/JAA Formal Documentation: as part of 737-900ER and 737-800FPB (FPB – aft Flat Pressure Bulkhead)

fuselage stress team, performed residual strength and crack growth analyses and prepared Formal Documents

for FAA/JAA certification purposes.

Worked on converting an existing Mid Exit Door of 737-900ER fuselage to a Plug for retrofit purposes. My primary

duties are validating the newly designed structural parts of the plug for static and fatigue strengths and helping the

designers in their drawing releases.

Got recognized for timely completion of documentation for the certification of 737-900ER airplane.

INFOSYS TECHNOLOGIES LTD, BANGALORE, INDIA 560 100

STRESS ENGINEER J ULY 2004 –

FEBRUARY 2006

Position Profile:

Group: Fatigue and Damage Tolerance team for Airbus A380 aircraft

Performed A380 (Passenger and Freighter aircraft) wing box skins and ribs crack growth analysis and prepared

documentation for the aircraft certification (at off-shore, Infosys Technologies Ltd, Bangalore, India).

Tools used: Structural Integrity Manuals (SIM’s), FESPS, Airbus suite of programs (DAMTOL etc.), and PATRAN

etc.

EDUCATION

M.E. (Master of Engineering in Mechanical Engineering), 2004

University: Birla Institute of Technology and Science – Pilani, India 333 031

B.Tech. (Bachelor of technology in Mechanical Engineering), 2002

University: Kakatiya Institute of Technology and Science – Warangal, India 506 015

TECHNICAL COMPETENCIES

FEA/Engineering Tools:

ABAQUS CAE, PATRAN, NASTRAN (familiar), CATIA V5 (familiar)

Also familiar with various OEM (especially Boeing) specific analysis tools like IAS, SA+, JOLT, THKAL, IDTAS,

MAGIC, CSW, CASTLE etc.

Software Skills: FORTRAN, C, Visual Basic, UNIX and MS-Office suite of programs, etc.

TRAINING

Linear FEA and ABAQUS CAE (Structural Analysis), Catia V5 for designers, ENOVIA for Analysis, Catia V5 for

Structural Analysis, Durability and Damage Tolerance Analyses – Methods, Non Destructive Testing Methods for

aircraft repairs

Open Systems (UNIX, C, Visual Basic)

PROFESSIONAL REFERENCES

References will be provided when needed.

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