707-320 aluminum structure
Both aircraft are militarized 707-320 family ships: riveted fail-safe fuselage, 2024 skins, 7075 stringers, 20-inch frames, tear straps.
Direct shop-floor orientation for metallic structure work on militarized 707-320 derivatives — not a glossy brochure.
People supporting E-3 Sentry and E-6 Mercury metallic structure — depot fab, manufacturing technology, planning, and hands-on repair.
Both aircraft are militarized 707-320 family ships: riveted fail-safe fuselage, 2024 skins, 7075 stringers, 20-inch frames, tear straps.
~30 ft dome, roughly 11 ft above the fuselage, hydraulic systems near 5000 psi, and EMP hardening baked into the design.
No rotodome. Dual VLF trailing wires, wingtip pods, extra aft structure. SLEP drove heavy wing fastener cold-work (~15,000 fasteners) and life extension ~27k → 45k hours.
Work the six steps in order. Videos and formal courses come after you know the airframe and the shop flow.
E-3 vs E-6 differences that drive metallic work today.
2Alloys, tempers, product forms, Alclad rules.
3Blank → form → heat treat → chem mill → machine → holes → peen → finish → NDI. Each machine card embeds a process demo.
4Process tooling groups and common hand-tool sizes.
5Curated public videos by process — structures through CNC.
6Two-week checklist plus formal course links.
Four starters. Public content teaches machines and methods — not Boeing production jigs.
Flush rivet process walkthrough — dimple, countersink, and set.
How stretch presses pull skins over form blocks.
Why airframe shops use high-pressure rubber-pad hydroform.
Split-sleeve cold expansion fundamentals used heavily on wing life-extension work.
Public video ≠ production jig drawings
These videos teach principles and common machines. Ship-specific fixtures, drill templates, and approved tooling live in the SRM, AMM, and controlled tooling packages — not on YouTube. Do not treat any clip as official E-3 or E-6 training.