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MOCH MUSTOFA CITEPUS I RT.02 RW.05 NO.20 PAJAJARAN BANDUNG INDONESIA 40173 Contact Tel: 62-22 6020649 Email tofa@plasa.com PERSONAL PROFILE: Date of birth : KEBUMEN, 24 JULY 1971 Nationality : INDONESIAN Marrital Status : MARRIED Education : GRADUATED FROM MECHANICAL ENGINEERING GADJAH MADA UNIVERSITY Qualification : STRESS ENGINEER Current Employer : INDONESIAN AEROSPACE (IAe) Years of Experience : Over 5 Years Language : INDONESIAN; ENGLISH SUMMARY OF WORK EXPERIENCE: Stress analyst, aerospace industry, over 5 years. Performed in stress and strength analysis of aircraft structures both primary and secondary structures especially on fuselage and wing. Use both conventional (hand calculation) and computer methods of analysis. Familiar with PC. Experienced with Nastran, Patran, Una, Femap, MS Word, Excel. Having knowledge of MATLAB and MathCAD. Responsible in disposition of production drawings, rejection tags problem solving, liaison between manufacturing and engineering, in-service of the aircraft have been delivered, preparing the test plan of aircraft structure parts and then analyze the test result, sizing the aircraft structure parts, stress and strength analysis of aircraft structure and write the analysis result on a document then submit the document to the authority for their approval. DETAIL OF WORK EXPERIENCE: I). January 2002 - Present 1. Stress and strength analysis of static line bracket and fitting of CN235-220 aircraft. MELTEM PROGRAM: 1. Stress and Strength Analysis of Wing due to Torpedo and Depth Charge Installation on the Outer Wing. 2. Cut-outs and reinforcement analysis on fuselage. 3. Skin, stringer, ribs and frame stress and strength analysis. 4.Search Light Installation On Wing Stress And strength Analysis 5.Torpedo Installation on Wing Stress And Strength Analysis II). January 2001 - December 2001 1.CN235-220M Bracket for Port Door on Upper Former Frame-43 Stress and Strength Analysis. 2.CN235-220M Tow Plate Provision on Frame 28-Frame 30 Stress and Strength Analysis. 3.Certified Document CN235-220M Internal Equipment Stress and Strength Analysis. 4.Certified Document CN 235-220M Bridge for Ramp Door Stress and Strength Analysis. Finishing this document with FEMAP for modelling and then solved it with UNA. III). January 2000 – December 2000 1.Certified document, Wind Deflector for Ramp Door Stress and Strength Analysis. This wind deflector is made from composite material. 2.Certified Document, CN235-220M Rear Fuselage Modification due to Chaff and Flare Installation Stress and Strength Analysis. Two holes (cut-outs) are made on the rearfuselage for this installation. 3.CN 235-220M Flap Door Lock Mechanism Strength Analysis. 4.CN235-220M Rear Spar Fitting and Lug Analysis. IV). January 1999 - December 1999 1.Certified document, CN235-220M Cargo Ramp Telescopic Rod Stress and Strength Analysis. 2.Certified document, Side Safety Bar and Ramp recovery Bar for CN235- 220M Aircraft Stress and Strength Analysis. 3.Certified document, Test Plan of Cargo Ramp Telescopic Rod Test. V). April1997 - December 1998 1.Certified Document, CN235-220 Airscoop for NRM1 Rain Making Powder Version System Stress and Strength Analysis. This documentcontain the analysis of center fuselage modification due to Rain Maker configuration. 2.Rotary Fairing Spring for CN235 Aircraft Analysis. 3.CN235-220 Artificial Ice Shape and Attachments Analysis. 4.CN235 Elevator Rib Fatigue and Damage ToleranceAnalysis. 5.CN235-220 Structure Analysis for Natural Icing Test . 6.Structure Limitation of CN235-220(N020) to flight with Artificial Ice Shape. 7.CN235-220 False Spar Defect Analysis.