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×	520. Self Improvement, Independent Action and Participation	$20.00	520. Self Improvement, Independent Action and Participation quantity	$20.00
×	524. Wing Pivot Weight Estimation Method	$20.00	524. Wing Pivot Weight Estimation Method quantity	$20.00
×	505. An Approach to an Automated System for Determination of Mass Moments of Inertia	$20.00	505. An Approach to an Automated System for Determination of Mass Moments of Inertia quantity	$20.00
×	550. A Simplified Technique for Precision Measurement of Three Axis Center of Gravity	$20.00	550. A Simplified Technique for Precision Measurement of Three Axis Center of Gravity quantity	$20.00
×	521. Weight Growth and the Principle of Minimum Contingency	$20.00	521. Weight Growth and the Principle of Minimum Contingency quantity	$20.00
×	2258. Using Microsoft Excel and Word as Weight Control Tools	$20.00	2258. Using Microsoft Excel and Word as Weight Control Tools quantity	$20.00
×	2193. Accuracy in Weighing Aircraft: Second and Third Order Effects and Techniques for Their Corrections	$20.00	2193. Accuracy in Weighing Aircraft: Second and Third Order Effects and Techniques for Their Corrections quantity	$20.00
×	2266. Affordable Thermoplastic Tailboom Structures	$20.00	2266. Affordable Thermoplastic Tailboom Structures quantity	$20.00
×	2207. Oracle Relational Database as a Mass Properties Control Tool	$20.00	2207. Oracle Relational Database as a Mass Properties Control Tool quantity	$20.00
×	2263. Army Aviation and the Mass Properties Engineer	$20.00	2263. Army Aviation and the Mass Properties Engineer quantity	$20.00
×	2228. Aircraft Cost Estimation Methodology and Value of a Pound Derivation for Preliminary Design Development Applications	$20.00	2228. Aircraft Cost Estimation Methodology and Value of a Pound Derivation for Preliminary Design Development Applications quantity	$20.00
×	2191. The Rock and Roll Telescope (Using a Gravitational Pendulum to Determine Moment of Inertia)	$20.00	2191. The Rock and Roll Telescope (Using a Gravitational Pendulum to Determine Moment of Inertia) quantity	$20.00
×	2190. Design of Fixtures for Mass Properties Measurement	$20.00	2190. Design of Fixtures for Mass Properties Measurement quantity	$20.00
×	2267. Weight Reduction Obtained by Process Improvements in Aircraft & Component Painting	$20.00	2267. Weight Reduction Obtained by Process Improvements in Aircraft & Component Painting quantity	$20.00
×	2189. Mass Properties Process Improvement	$20.00	2189. Mass Properties Process Improvement quantity	$20.00
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