AGING AIRCRAFT 2007

2007 ASIP PROCEEDINGS
TUESDAY, DECEMBER 4, 2007
Welcome
8:00 AM - 8:10 AM	Welcome and Administrative Remarks Dr Lawrence Butkus, USAF AFRL/Materials & Manufacturing Directorate
8:15 AM - 8:20 AM	Presentation of the ASIP Manager of the Year Award Dr Joseph Gallagher, USAF (Ret)
8:20 AM - 8:55 AM	Presentation by the John W. Lincoln Award Recipient “Determining Reinspection Intervals” Dr Alan Berens, University of Dayton Research Institute
8:55 AM - 9:00 AM	Presentation of the Lincoln Award Dr Joseph Gallagher, USAF (Ret)
STRUCTURAL INTEGRITY OVERVIEWS Chair: Mr John Bowlus, USAF
9:15 AM - 9:45 AM	ASIP on the U-2: Tailoring of an Aircraft Structural Integrity Program for High Demand, Low Density Pre-ASIP Aircraft Mr Gregory Birdsall, Lockheed Martin Co and Mr Scott Mangrum, USAF 560 ACSG
9:45 AM - 10:15 AM	Integration of Ground and Flight Testing on F-35 Lightning II Program Mr Joseph Yates, Lockheed Martin
10:15 AM - 10:45 AM	C-130 Center Wing Fatigue Cracking Lessons Learned: Application to ASIP Force Management Execution Mr Peter Christiansen, USAF
STRUCTURAL INTEGRITY OVERVIEWS (Continued) Chair: Mr John Bowlus, USAF
11:00 AM - 11:30 AM	T-38 Fuselage Structural Life Assessment Mr Zachary Whitman, Southwest Research Institute (Proceedings Paper)
11:30 AM - 12:00 PM	F-15 Service Usage Data Collection Overview and Lessons Learned Mr Kent Ruffing, The Boeing Company
12:00 PM - 1:30 PM	GROUP LUNCHEON Aircraft Structural Integrity and the F-22video Brig Gen Clyde Moore II, 478th Aeronautical Systems Wing
STRUCTURAL MODELING Chair: Dr Mark Thomsen, USAF
1:30 PM - 2:00 PM	Finite Element Analysis on the F-35 Lightning II Program Mr David McSwiggen, Lockheed Martin Company
2:00 PM - 2:30 PM	The Effects of Residual Tensile Stresses Induced by Cold-Working a Fastener Hole Mr Abraham Brot, Israel Aerospace Industries (Proceedings Paper)
2:30 PM - 3:00 PM	The Effect of Stress Intensity Factor Models on Inspection Intervals Lt Col Scott Fawaz, USAF Academy (Proceedings Paper)
USAGE CHARACTERIZATION FOR MAINTENANCE DECISION-MAKING Chair: Mr Archie Woods, USAF
3:30 PM - 4:00 PM	Using Predictive Maintenance Concepts for Structure Integrity in the IAF LtC Rotem Halevi, Israeli Air Force
4:00 PM - 4:30 PM	Operational Service Life Evaluation for the United States Forest Service P-3 Aircraft Mr James Burd, Avenger Aircraft & Services
4:30 PM - 5:00 PM	Structural Fatigue Life Tracking of USN T-45 Jet Aviator Training System Mr Michael Pawlik, The Boeing Company
5:00 PM - 5:30 PM	Requirements for Life Cycle Management of U.S. Army Helicopter Structural Integrity Mr David White, Avion Inc
WEDNESDAY, DECEMBER 5, 2007
REPAIR & REPLACEMENT CONCEPTS Chair: Dr John Bakuckas, FAA
8:00 AM - 8:30 AM	Improving Structural Durability and Aircraft Availability Through Innovative Tracking, Analysis and Repair Technology Mr Bryce Harris, USAF
8:30 AM - 9:00 AM	C-130 Center Wing Rainbow Fitting Spare Redesign Mr Frank McElwain, Lockheed Martin Company
9:00 AM - 9:30 AM	Advanced Hybrid Structural Concepts for Care-Free Structures: Experimental Validation and Path Forward Dr Markus Heinimann, Alcoa Technical Center
ADDRESSING INSPECTION RELIABILITY Chair: Mr Dave Campbell, USAF
10:00 AM - 10:30 AM	USAF NDI Reliability Improvement: Lessons Learned Mr Karl Kraft, USAF
10:30 AM - 11:00 AM	Canadian Air Force Automated Bolt Hole Eddy Current (ABHEC) Probability of Detection (PoD) Study Capt DJ Butcher, Canadian Department of National Defence
11:00 AM - 11:30 AM	F-22A NDI Development: Challenges, Successes and a Path to the Future Mr Robert Bair, USAF
11:30 AM - 12:00 PM	Development of a Nondestructive Inspection (NDI) Approach Based on Bolt Hole Ultrasonic Testing (BHUT) for Complex, Multi-Layered Aircraft Structures Mr Bartolo Drennen, Integrated Technologies Inc
12:00 PM - 1:30 PM	GROUP LUNCHEON “Application of the Holistic Structural Integrity Process to Canadian Forces Challenges” Mr Jerzy Komorowski, National Research Council Canada
Panels
1:30 PM - 3:15 PM	Composite and Hybrid Structures Certification Issues Chair: Mr Richard Reams, USAF Panelists: Dr Larry Ilcewicz, FAA Mr Jens Hinrichsen, Alcoa Technical Center Col Robert Fredell, USAF Mr Mike Woodward, Lockheed Martin Mr Phil Larson, Advanced Composites Office Mr. Benson Black, The Boeing Company
3:45 PM - 5:30 PM	Applying CBM+ Tenets to Aircraft Structural Integrity – Sustainment Related Data Needs Chair: Mr Russell Howard, USAF Panelists: Mr John McDonald, USAF Dr James Larsen, USAF Dr Paul Hoffman, US Navy Mr Tim Fallon, US Navy
THURSDAY, DECEMBER 6, 2007
RESIDUAL STRESS EFFECTS Chair: Dr Michael Shepard, USAF
8:00 AM - 8:30 AM	Cold-working Validation and Structural Health Monitoring Using DMI SR-2 Technology Dr William Ranson, Direct Measurements Inc (Proceedings Paper)
8:30 AM - 9:00 AM	Mitigation of Fatigue and Pre-Cracking Damage in Aircraft Structures Through Low Plasticity Burnishing (LPB) Dr Narayanan Jayaraman, Lambda Technologies
9:00 AM - 9:30 AM	Test Demonstrated Damage Tolerance of F-22 Wing-Attach Lugs with ForceMate Bushings Dr Jeffrey Bunch, The Boeing Company (Proceedings Paper)
RISK BASED FORCE MANAGEMENT DECISIONS Chair: Dr Paul Hoffman, US Navy
10:00 AM - 10:30 AM	Risk Analysis to Review a Request to Over-fly an IAT-Based F-22 Structural Inspection Requirement Dr Thomas Brussat, Lockheed Martin Company
10:30 AM - 11:00 AM	Establishing Reliability of Inspection Intervals for Structures Subjected to Fatigue Loads Maj Alberto Mello, Institute of Aeronautics & Space - IAE
11:00 AM - 11:30 AM	B-1 Maintenance Schedule Impact Based on Risk Assessment Results Dr Tony Torng, The Boeing Company
11:30 AM - 12:00 PM	A Computer Simulation of the Life of the Structures of a Fleet of Aircraft Mr Arnold Anderjaska, Technical Data Analysis Inc (Proceedings Paper)
STRUCTURAL HEALTH MONITORING Chair: Maj Jess Vickers, USAF
2:00 PM - 2:30 PM	Health Monitoring for Structural "Hot Spots": A Systems Approach Mr Eric Haugse, The Boeing Company
2:30 PM - 3:00 PM	Structural Sensors for C-130 Condition Based Maintenance and Prognostics Dr Kenneth Taylor, Mercer Engineering Research Center
DEVELOPING/STORING MEANINGFUL DAMAGE INFORMATION Chair: Mr Russell Alford, USAF
3:30 PM - 4:00 PM	F/A-18E/F Full Scale Structural Fatigue Test Results Mr Timothy Callihan, The Boeing Company (Proceedings Paper)
4:00 PM - 4:30 PM	Improved Risk Analysis through Data Management – Development and Implementation of the Structural Maintenance Information Management System (SMIMS) Mr James Suzel, S&K Technologies Inc and Mr Tim Allred, Aging Aircraft Analysis Group
4:30 PM - 5:00 PM	T-37B Wing and Carry-Through Structure Teardown Analysis Program Dr Gregory Shoales, HQ USAFA/DFEM and Mr John Pendleton, USAF 506 ACSS/CC
5:00 PM - 5:30 PM	USAF F-16 ASIP Data Collection Dr Kimberli Jones, SAIC

Posters
	Kyriakos Kourousis, Hellenic Air Force & National Technical University of Athens “Cyclic Elastoplastic Response of Aluminum Alloy 7050 to Low-Cycle Fatigue”
	Yushi Sun, Innovative Materials Testing Technologies, Inc. (IMTT) “Inspection of Fastener Hole Cracks Using Motorized Remote Field Eddy Current Probe ”