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:
- The False Quarantine Mistake: A receiving inspector quarantines a perfectly conforming bundle of
6061-T651or7075-T651plate—halting spindle production for days—because the MTR shows melt/cast origin in South Africa, Bahrain, Austria, or South Korea and the PO boilerplate includesDFARS 252.225-7009 (Specialty Metals). - 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-relievedT6in place of stretchedT651/T7351aerospace 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
- Launch the ProvaTrace DFARS 252.225-7009 & MTR Bounding-Box Validator →Select
Aluminum Alloys (6061 / 7075 / 2024)in the free validator to generate a documented statutory10 U.S.C. § 4863Specialty Metals Exemption memo—plus automatic alerts for Buy American / TAA PO flow-downs and MTR chemistry/mechanical bounding-box verification.
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:
- Steel (exceeding specified alloy limits, including
>0.25%Aluminum as an alloying element inside steel—NOT aluminum-base alloys!); - Base metal alloys of Nickel, Iron-Nickel, and Cobalt (containing
>10%other alloying metals except iron); - Titanium and Titanium Alloys; and
- Zirconium and Zirconium Base Alloys.
What This Means at Receiving Inspection
- Aluminum and Aluminum Base Alloys (
6061,7075,2024,5052,5083,MIC-6, etc.) are NOT Specialty Metals under10 U.S.C. § 4863/DFARS 252.225-7009. - Why do defense prime POs stamped "DFARS 252.225-7009 Applies" land on aluminum orders anyway? Because ERP procurement systems at primes and Tier-1 contractors automatically attach standard defense terms & conditions to every line item on a military contract, relying on the clause's self-limiting text ("...any specialty metal...").
- Wait—Before Releasing Foreign Aluminum, Check These 3 Actual Origin Clauses!Just because
DFARS 252.225-7009does not apply to aluminum does NOT mean country of origin never matters on your PO:- Buy American Act / Balance of Payments (
FAR 52.225-1/DFARS 252.225-7001) & Trade Agreements Act (DFARS 252.225-7021): Govern end-item manufacture and domestic/qualifying/designated-country component thresholds when your shop delivers finished defense/federal end items. - Russian / Sanctioned Aluminum Prohibitions & Section 232 / Customs Rules: Federal sanctions and prime-contractor compliance declarations strictly prohibit or require tracing primary aluminum smelted or cast in Russia (even if rolled into plate in a third country!). Always check Country of Smelt / Cast as well as rolling country when sanctions compliance clauses appear on the PO.
- Prime Customer "Domestic / Approved Mill Only" Engineering Notes: Structural airframe plate (
7075-T7351,7050-T7451,2024-T351) frequently invokes prime-specific Approved Mill Source Lists (e.g., Kaiser, Constellium, Arconic, AMAG, Hulamin—depending on the prime's qualified plate schedule). Always check PO quality notes!
- Buy American Act / Balance of Payments (
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 Designation | Exact Metallurgical / Mechanical Meaning | Why Drawings Forbid Unapproved Substitution |
|---|---|---|
-T6 | Solution 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:
- Mechanical Yield / Tensile Strength Verification (checking both minimum AND, on over-aged tempers, maximum yield strength ceilings or yield-to-conductivity relationships); AND
- Electrical Conductivity (
% IACS— International Annealed Copper Standard, perAMS 2658/ eddy-current testing): As7075over-ages from-T6into-T73, precipitates coarsen out of solid solution and electrical conductivity rises (for example,7075-T73XXrequires significantly higher% IACSconductivity than7075-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:
- Thickness-Bracketed Minimum Properties: A
0.500"thick7075-T651plate and a3.500"thick7075-T651plate 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 longitudinalLto long-transverseLT/ short-transverseSTtest orientations). Always check that the MTR's printed min/max row corresponds to the exact ordered thickness bracket. - Alclad vs. Bare Sheet/Plate (
Alclad 2024/Alclad 7075vs. 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:
- Deterministic
10 U.S.C. § 4863Statutory Engine: Automatically identifies non-specialty metals like6061and7075aluminum (generating an audit-ready statutory citation note for your receiving file) while flagging Buy American / TAA and specialty-metal melt rules accurately. - Side-by-Side Bounding-Box MTR Verification: Highlights chemistry (
Others Each / Total), thickness-specific tensile/yield (MPa <-> ksi), and% IACSconductivity cells right on the PDF for 10-second human QA sign-off. - 1-Click AS9102 Form 2 & Customer Cert Turnover Packs: Build clean customer material cert binders and FAI tables in seconds.
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