APPENDIX II
REFERENCES USED TO DEVELOP
THE TRAMAN
NOTE: Although the following references were current when this TRAMAN
was published, their continued currency cannot be assured. Therefore, you need to
be sure that you are studying the latest revision.
Chapter 1
Adhesive Bonded Aerospace Structure Repair, MIL-HDBK-337, Department of
Defense, Washington D.C., 1982.
Aerospace Metals–General Data and Usage Factors, NAVAIR 01-1A-9, Naval Air
Systems Command Headquarters, Washington, D.C., 22 November 1967,
Change 19, 1 September 1989.
Aircraft Radomes and Antenna Covers, NAVAIR 01-1A-22, Naval Air Systems
Command Headquarters, Washington, D.C., 1 January 1990.
Airman, NAVEDTRA 12000, Naval Education and Training Program Management
Support Activity, Pensacola, Fla., 1990.
Composite Repair, A1-F18AA-SRM-400, Naval Air Systems Command
Headquarters, Washington, D.C., 1982.
Fabrication, Maintenance and Repair of Transparent Plastics, NAVAIR 01-1A-12,
Naval Air Systems Command Headquarters, Washington, D.C., 1 July 1982.
General Aircraft Information Navy Model F-14A Aircraft, N A V A IR
01-F14AAA-2-1, Commander, Naval Air Systems Command, Washington,
D.C., 1981.
General Information F-18 Aircraft, A1-F18AC-SRM-200, Commander, Naval Air
Systems Command, Washington, D.C., 1 November 1992.
General Manual for Structural Repair, NAVAIR 01-1A-1, Commander, Naval Air
Systems Command, Washington, D.C., 1 September 1991.
Landing Gear Systems F-14, NAVAIR 01-F-14AAA-2-2-1, Naval Air Systems
Command, Washington, D.C., 1975.
Navy Training Plan Advanced Composite Material Repair Program,
NTP-A-50-8084/A, Chief of Naval Operations, Washington D.C., January
1987.
Plastics for Aerospace Vehicles, Parts I and II, MIL-HDBK-17A, Department of
Defense, Washington D.C., June 1977.
Structural Sandwich Composites, MIL-HDBK-23A, Department of Defense,
Washington D.C., June 1974,
Typical Repair, A1-F18AA-SRM-250, Naval Air Systems Command Headquarters,
Washington, D.C., 1 August 1992.
AII-1
