AS9100 & DFARS 252.225-7009 Technical Receiving Guide

6061-T6 & 7075-T651 Aluminum MTR Checklist: Why Aluminum is Exempt from DFARS 252.225-7009 Specialty Metals + Conductivity/Temper Checks

Editorial & Regulatory Scope Notice: This technical guide is published as an administrative quality-control reference for AS9100 Rev D and ISO 9001 precision machine shops inspecting wrought aluminum bar, plate, sheet, and extrusions (UNS A96061 / UNS A97075). Statutory citations reference public US federal law (10 U.S.C. § 4863, DFARS 252.225-7009, DFARS 252.225-7001, DFARS 252.225-7021). No copyrighted SAE/AMS or ASTM specification tables are reproduced; inspectors must verify actual values against their facility's licensed specification revision, Purchase Order (PO) flow-downs, and the requirement rows printed on the mill certificate. Final material release rests solely with authorized human QA personnel.

Every week in aerospace and defense CNC job shops, one of two costly aluminum receiving mistakes happens on the loading dock:

  1. The False Quarantine Mistake: A receiving inspector quarantines a perfectly conforming bundle of 6061-T651 or 7075-T651 plate—halting spindle production for days—because the MTR shows melt/cast origin in South Africa, Bahrain, Austria, or South Korea and the PO boilerplate includes DFARS 252.225-7009 (Specialty Metals).
  2. The Real Origin / Temper Mistake: Conversely, a shop assumes "aluminum never has origin restrictions," ignoring DFARS 252.225-7001 (Buy American), DFARS 252.225-7021 (Trade Agreements Act), or U.S. sanctions/tariff origin flow-downs—or accepts non-stress-relieved T6 in place of stretched T651 / T7351 aerospace plate without checking Eddy-Current Electrical Conductivity (% IACS)!

Here is the exact regulatory truth and 10-point MTR verification checklist for 6061 and 7075 aluminum.


Quick Check: Run the Deterministic Alloy & DFARS Validator Free


1. Why 6061 & 7075 Aluminum Are EXEMPT from DFARS 252.225-7009 Specialty Metals

Look directly at the federal statutory definition codified in 10 U.S.C. § 4863(l)(1) and implemented verbatim in DFARS 252.225-7009(a):

Under US law, "Specialty Metal" covers only four specific metallurgical categories:

  1. Steel (exceeding specified alloy limits, including >0.25% Aluminum as an alloying element inside steel—NOT aluminum-base alloys!);
  2. Base metal alloys of Nickel, Iron-Nickel, and Cobalt (containing >10% other alloying metals except iron);
  3. Titanium and Titanium Alloys; and
  4. Zirconium and Zirconium Base Alloys.

What This Means at Receiving Inspection


2. The Temper Suffix Trap: T6 vs. T651 vs. T6511 vs. T7351

On aluminum MTRs, missing two digits at the end of the temper callout leads directly to warped thin-wall housings or stress-corrosion cracking rejections:

Temper DesignationExact Metallurgical / Mechanical MeaningWhy Drawings Forbid Unapproved Substitution
-T6Solution heat-treated and artificially aged (not mechanically stress-relieved by stretching).High residual quench stresses! Thin-wall hog-outs machined from plain -T6 plate bow and twist dramatically as skin stresses are milled away.
-T651 (Plate / Rolled or Cold-Finished Bar)Solution heat-treated, stress-relieved by controlled stretching (1.5%–3% permanent set on plate/bar per spec), and artificially aged; receives no straightening after stretching.Standard callout for precision CNC aerospace plate/bar hog-outs to ensure dimensional stability.
-T6510 vs. -T6511 (Extruded Bar/Rod/Shapes)Solution heat-treated, stress-relieved by stretching, and aged. -T6510 permits no minor straightening after stretching; -T6511 permits minor straightening after stretching to meet straightness tolerances.Extruded 6061-T6511 bar is widely stocked by distributors—check your print/spec before substituting Extruded (-T6511 / ASTM B221 / AMS-QQ-A-200/8) when Cold-Finished/Rolled Bar (ASTM B211 / AMS-QQ-A-225/8) or Plate (AMS 4027 / ASTM B209) was specified! Grain flow and transverse properties differ!
-T73 / -T7351 / -T7651 (Common on 7075)Solution heat-treated, stress-relieved (when -T7X51), and intentionally over-aged to achieve superior resistance to Stress-Corrosion Cracking (SCC) and exfoliation corrosion (at a modest trade-off in peak tensile strength vs. -T651).Supplying peak-aged 7075-T651 on a 7075-T7351 airframe fitting creates catastrophic in-service SCC fracture risk!

3. Eddy-Current Electrical Conductivity (% IACS) & Lot Acceptance Checks on 7075

When inspecting 7000-series aerospace aluminum (7075-T73, 7075-T7351, 7075-T7651, 7050-T7451) MTRs, tensile strength and hardness alone cannot prove proper over-aging!

Because an under-aged lot and an over-aged lot of 7075 can exhibit identical Rockwell B / Brinell hardness on either side of the aging curve peak, aerospace specifications require Lot Acceptance Testing for Stress-Corrosion Resistance combining:

  1. Mechanical Yield / Tensile Strength Verification (checking both minimum AND, on over-aged tempers, maximum yield strength ceilings or yield-to-conductivity relationships); AND
  2. Electrical Conductivity (% IACS — International Annealed Copper Standard, per AMS 2658 / eddy-current testing): As 7075 over-ages from -T6 into -T73, precipitates coarsen out of solid solution and electrical conductivity rises (for example, 7075-T73XX requires significantly higher % IACS conductivity than 7075-T6XX).

Inspector Rule: On every 7075-T73XX or 7075-T76XX aerospace MTR, verify both % IACS electrical conductivity AND tensile/yield values against the printed specification limits on the cert!


4. Thickness-Dependent Mechanical Limits & Clad vs. Bare Sheet Traps

Two additional pitfalls catch receiving inspectors on aluminum EN 10204 3.1 / mill certs:

  1. Thickness-Bracketed Minimum Properties: A 0.500" thick 7075-T651 plate and a 3.500" thick 7075-T651 plate made to the exact same specification have different minimum UTS, Yield, and Elongation requirements due to quench-rate mass effects through thick sections (and frequently shift from longitudinal L to long-transverse LT / short-transverse ST test orientations). Always check that the MTR's printed min/max row corresponds to the exact ordered thickness bracket.
  2. Alclad vs. Bare Sheet/Plate (Alclad 2024 / Alclad 7075 vs. Bare): Aerospace sheet and thin plate come in both Bare and Alclad (metallurgically bonded pure-aluminum corrosion-protective surface cladding, which has slightly lower composite tensile/yield minimums and looks shinier/softer on outer faces). Mixing Bare and Alclad fails anodize appearance, conductivity, and AS9102 FAI verification immediately.

5. 10-Point AS9100 Receiving Checklist for 6061 & 7075 Aluminum


Stop Second-Guessing DFARS Exemptions & MTR Math at the Receiving Dock

Whether your inspector is checking if 6061-T651 needs a DFARS melt waiver, converting metric MPa plate certs from European rolling mills into ksi, or verifying % IACS conductivity on 7075-T7351 airframe hog-outs, manual paperwork slows spindles down.

ProvaTrace gives AS9100 and ISO 9001 machine shops instant receiving clarity:

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Disclaimer: ProvaTrace provides administrative document-extraction and deterministic comparison software requiring authorized human QA inspector verification. Never upload ITAR (22 CFR 120–130) or DoD CUI technical blueprints.