3.2.8.2.8

MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures

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3.7.3.1.8(a) Rothweiler, C. E., and Maynard, P. S., "Evaluation of 7049-T73 Aluminum Alloy for RA-5C Wing Inner Panel Fold Rib," CMES Contract N00256-71-C-0064, Task No. NAR-18 (P046-10), Report No. NR72H-278, North American Rockwell, Columbus, Ohio (July 14, 1972) (MIL-HDBK-5 Source M-170).
3.7.3.1.8(b) Anon., "Boeing Test Data on X7049-T73," Submitted to Battelle to provide input data for Item 68-24 (1969) (MCIC 78639).
3.7.3.1.8(c) Mixon, W., and Turley, R. V., "Evaluation of Aluminum Alloys 7049-T73 and 7175-T736 Die Forging," Engineering Technical Report No. ETR-MDC-J0692, McDonnell Douglas (April 7, 1970) (MCIC 110111).
3.7.3.1.8(d) VanOrden, J. M., "Evaluation of 7049-T73 Aluminum Alloy Hand-Forged Billet," Lockheed California Company, Report No. LR 23447 (February 1970) (MIL-HDBK-5 Source M-43).
3.7.3.1.8(e) "Effect of Manufacturing Processes on Structural Allowables—Phase I," Battelle, Columbus, Ohio, AFWAL-TR-85-4128 (January 1986).
3.7.4.2.8(a) Guthorn, P. S., "Design Properties and Processing Limits for Improved Aluminum Alloys," McDonnell Douglas Corporation, MDC-J1912 (December 1983) (MIL-HDBK-5 Source M-629).
3.7.4.2.8(b) Garland, K., "Evaluation of X7050-T736 Die Forgings," McDonnell Aircraft Company, McDonnell Douglas Corporation, Report No. 514-131.10 (February 1973) (MCIC 85880).
3.7.4.2.8(c) Deel, O. L., Ruff, P. E., and Mindlin, H., "Engineering Data on New Aerospace Structural Materials," AFML-TR-114 (June 1973) (MIL-HDBK-5 Source M-467).

MIL-HDBK-5J

MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures

Last Updated 29 Oct 2026

Hover any section to copy its link or text, ask Copilot about it, or bookmark it.

3.7.3.1.8(a) Rothweiler, C. E., and Maynard, P. S., "Evaluation of 7049-T73 Aluminum Alloy for RA-5C Wing Inner Panel Fold Rib," CMES Contract N00256-71-C-0064, Task No. NAR-18 (P046-10), Report No. NR72H-278, North American Rockwell, Columbus, Ohio (July 14, 1972) (MIL-HDBK-5 Source M-170).
3.7.3.1.8(b) Anon., "Boeing Test Data on X7049-T73," Submitted to Battelle to provide input data for Item 68-24 (1969) (MCIC 78639).
3.7.3.1.8(c) Mixon, W., and Turley, R. V., "Evaluation of Aluminum Alloys 7049-T73 and 7175-T736 Die Forging," Engineering Technical Report No. ETR-MDC-J0692, McDonnell Douglas (April 7, 1970) (MCIC 110111).
3.7.3.1.8(d) VanOrden, J. M., "Evaluation of 7049-T73 Aluminum Alloy Hand-Forged Billet," Lockheed California Company, Report No. LR 23447 (February 1970) (MIL-HDBK-5 Source M-43).
3.7.3.1.8(e) "Effect of Manufacturing Processes on Structural Allowables—Phase I," Battelle, Columbus, Ohio, AFWAL-TR-85-4128 (January 1986).
3.7.4.2.8(a) Guthorn, P. S., "Design Properties and Processing Limits for Improved Aluminum Alloys," McDonnell Douglas Corporation, MDC-J1912 (December 1983) (MIL-HDBK-5 Source M-629).
3.7.4.2.8(b) Garland, K., "Evaluation of X7050-T736 Die Forgings," McDonnell Aircraft Company, McDonnell Douglas Corporation, Report No. 514-131.10 (February 1973) (MCIC 85880).
3.7.4.2.8(c) Deel, O. L., Ruff, P. E., and Mindlin, H., "Engineering Data on New Aerospace Structural Materials," AFML-TR-114 (June 1973) (MIL-HDBK-5 Source M-467).