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| Guideline for Etching Time, Etchant Class, and Material Time - Table 1 |
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| All Titanium Alloys except Titanium Aluminide Alloys
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| Carbon and Low Alloy Steels (4340, 9310, etc.)
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| Maraging Steels (Marage 250, etc.)
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| Low Expansion Alloys (Incoloy 903, 907, 909, Thermospan, etc.)
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| All Stainless Steels (300s, 400s, PH, etc.)
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| Iron Superalloys (A286, V57, etc.)
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| Turbine Airfoil Nickel Superalloys (Inconel 738, Rene 77, 80, 125, 142, N5, etc.)
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| Non-Turbine Airfoil Nickel Superalloys - Chromium content less than 20% (Inconel 600, 718, Rene 41, 88DT, 95, 104, UDIMET 500, 700, etc.) See Note 3.
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| Non-Turbine Airfoil Nickel Superalloys - Chromium content 20% and above (Hastelloy X, Inconel 601, 625, 939, MA754, etc.) See Note 3.
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| Cobalt Superalloys (HS188, L605, MarM 509, X40, etc.) See Note 3.
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| Copper-Cobalt-Beryllium Alloy (B11H49 or B11H68) - Solution Heat Treated. See Note 5.
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| Copper-Cobalt-Beryllium Alloy (B11G25, B11H49, or B11H68) or Copper-Nickel-Silicon-Chromium Alloy (B11G48) - Age Hardened. See Note 6.
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| Gamma Titanium Aluminide Alloys
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| NOTE: |
| (HES)For Waspaloy, use Class C etchant. GEnx Combustion Case (72-41-01) is a Non-Turbine Nickel Superalloys - Chromium content less than 20%, therefore you use 4-5 min. Refer to Case #01997402. |
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| NOTE: |
| (HES)For RENE220, use Class C etchant. Refer to Case #02006908. |
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| NOTE: |
| (HES) Seal support outer flange faces material (GTD222 Alloy) is IN783 of PN 2303M26G01 /2303M26G013/2303M26G04 HPT forward outer seal support. IN783 is a low expansion alloy, therefore it should fall under this category with 2.5-3 min. These alloys have no chromium or only low amount of chromium (like Thermospan and IN783), so they are less corrosion resistant and they need shorter etching time. Refer to Case #02044366. |
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| NOTE: |
| (HES) Use Class B etchant for alpha-beta titanium aluminide alloys (titanium aluminide alloy 6-2-4-2/6Al-2Sn-4Zr-2Mo etc.). Refer to Case #02068521. |
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| NOTE: |
| (HES) Refer to Maraging Steels in SPM 70-24-01, Table 1 for etching time and etchant class for GE1014.. Refer to Case #02078974. |
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| NOTE: |
| 1. The materials listed in parentheses are examples only. The lists are not intended to be all inclusive. |
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| NOTE: |
| 2. When etching surfaces containing two different alloys with different etching times specified in Table 1, use the shortest etching time specified. |
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| NOTE: |
| 3. A clean and active surface (a surface containing no oxides and no scale) is required for effective etching of cobalt and nickel superalloys. Light abrasion is recommended to activate the surface prior to etching. Refer to paragraph 3.A.(1), Subtask 70-24-01-110-342 for abrasive products. |
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| NOTE: |
| 4. Class D is cancelled. Class D is superseded by Class C. |
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| NOTE: |
| 5. When etching solution heat-treated Copper-Cobalt-Beryllium Alloys, etching should be done using a pair of two cotton swabs with approximately 0.02 to 0.04 grams of cotton on each swab. |
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| NOTE: |
| 6. When etching cast or age hardened Copper-Cobalt-Beryllium or Copper-Nickel-Silicon-Chromium Alloys, etching should be done using one cotton swab with approximately 0.02 to 0.04 grams of cotton on the swab. |
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