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GuidePublished 14 Aug 202615 min readBy Kevin JoginManufacturingSurface EngineeringMetal Surface TreatmentConversion Coatings and Plating

Engineering · Manufacturing · Surface Engineering

Metal Surface Treatment, Conversion Coatings and Plating: Magnesium Anodic Treatment

Engineering handbook for metal surface treatment, conversion coatings and plating, covering magnesium anodic treatment — mil-m-45202c, tin-lead — mil-p-81728a,...

Executive summary

This handbook section converts the supplied engineering material into a practical, source-controlled reference. It concentrates on the following learning outcomes.

Magnesium Anodic Treatment — MIL-M-45202C
Tin-Lead — MIL-P-81728A
Hard Facing: When the Surface Must Be Harder Than the Part
Hard-Facing Material Comparison
Detailed NiCr Properties (Rod vs. Electrode)
Flame Spraying: Building Surfaces from Molten Particles

Magnesium Anodic Treatment — MIL-M-45202C

The HAE anodic finish is probably the hardest coating currently available for magnesium. It exhibits stability at high temperatures, good dielectric strength, and serves as an excellent paint base. Requires resin seal or paint for maximum corrosion protection.

Type/Class Typical Thickness Description
Type I, Class A 0.2 mil Tan coating (HAE); Grade 1: without post-treatment (dyed); Grade 2: with bifluoride-dichromate post-treatment
Type I, Class C 0.3 mil Light green coating (Dow #17)
Type II, Class A 1.5 mil Hard brown coating (HAE); Grade 1: without post-treatment; Grade 3: with bifluoride-dichromate post-treatment; Grade 4: with post-treatment + moist heat aging; Grade 5: double application + moist heat aging
Type II, Class D 1.2 mil Dark green coating (Dow #17)


Tin-Lead — MIL-P-81728A

Excellent solderability. Matte or bright luster acceptable. For electronics components, only matte or flow-brightened finish.

  • Brightened electronics components: maximum thickness 0.0003 in.
  • Tin 50–70% by weight, lead remainder: 0.0003–0.0005 in.


Hard Facing: When the Surface Must Be Harder Than the Part

the practitioner's breakthrough came when a senior metallurgist showed her a set of agricultural crusher jaws that had been hard-faced with cobalt-chromium alloy. The jaws had survived three seasons of crushing rock — while uncoated jaws lasted one.

Hard facing is a method of adding a coating, edge, or point of a metal or alloy capable of resisting abrasion, corrosion, heat, or impact to a metal component. It can be applied equally well to new parts or worn parts.

Application methods:

  • Oxyacetylene gas welding
  • Shielded-metal arc welding (SMAW)
  • Submerged arc welding
  • Plasma arc welding
  • Inert-gas-shielded arc welding (consumable and nonconsumable electrode)
  • Spraying process (wire or powder)

Selection principle: The first consideration is always the type of service the part will undergo. Other factors include machinability, cost, porosity, appearance, and ease of application. Generally, the greater the hardness, the greater the resistance to abrasion and impact wear.


Hard-Facing Material Comparison

Material Designation Hardness (As-Welded) Max Service Temp Impact Resistance Corrosion Resistance Machinability Best For
High-Speed Steel RFe5 / EFe5 55–60 Rc 1100°F Medium (improved when tempered) Atmospheric only Must anneal first Cutting tools, shear blades, forming dies, broaches
Austenitic Manganese Steel EFeMn 170–230 Bhn (work-hardens to 450–550 Bhn) 500–600°F max Very high Similar to carbon steel Very difficult; usually ground Rock crushers, railway frogs/crossings
Austenitic High-Chromium Iron RFeCr-A / EFeCr-A 51–62 Rc 1800°F (oxidation resistant) Light only — avoid > 60,000 psi dynamic compression Not very resistant to liquids; rusts in moist air Commercially unmachinable; grinding only Agricultural machinery, coke chutes, steel mill guides, sandblasting equipment
Cobalt-Base Alloy (Stellite) RCoCr / ECoCr CoCr-A: 38–47 Rc; CoCr-B: 45–49 Rc; CoCr-C: 48–58 Rc 1200°F+ (return to original hardness on cooling) Moderate Resistant to air, food, certain acids Difficult; increases with carbon; CoCr-C by grinding only Exhaust valves, valve trim, pump shafts, corrosion/erosion environments
Copper-Base Alloy RCuAl / ECuAl series CuAl-A2: 130–190 Bhn; CuAl-D/E: 230–390 Bhn < 400°F (hardness drops above this) CuAl-A2 highest; decreases with Al content CuAl: atmospheric, acids, mild alkalies, salt water All deposits machinable Bearing surfaces, gears, cams, wear plates, dies
Nickel-Chromium-Boron RNiCr / ENiCr NiCr-A: 35–40 Rc; NiCr-B: 45–50 Rc; NiCr-C: 56–62 Rc 1750°F (oxidation resistant to 1800°F) Light Completely resistant to atmosphere, steam, salt water, salt spray, mild acids Tungsten carbide tools: slow speed, light feeds Seal rings, cement pump screws, valves, screw conveyors, cams

Detailed NiCr Properties (Rod vs. Electrode)

The hardness difference between rod and electrode deposits matters in specification:

Alloy Rod Deposit (Rc) Electrode Deposit (Rc)
NiCr-A 35–40 24–35
NiCr-B 45–50 30–45
NiCr-C 56–62 35–56

Lower hardness values and greater ranges in electrode deposits are attributed to dilution of deposit and base metals.

Hot hardness — NiCr-C electrode deposits: Range from Rc 49 (instantaneous) to Rc 31 (3-minute loading) over 600–1000°F. Rod deposits: Rc 55 to Rc 40 under the same conditions.

Compression properties (all NiCr alloys):

  • Elastic limit: 42,000 lb/in²
  • Yield strength at 0.01% offset: 92,000 lb/in²
  • Yield strength at 0.10% offset: 150,000 lb/in²
  • Yield strength at 0.20% offset: 210,000 lb/in²


Flame Spraying: Building Surfaces from Molten Particles

The flame spraying process deposits metals, alloys, ceramics, and cermets on metallic or other surfaces. Applications include:

  • Building up worn or undersize parts
  • Providing wear-resisting or corrosion-resisting surfaces
  • Correcting defective castings

Three primary equipment types:


. Wire-Fed Combustion Spray

Wire is fed automatically through the spray gun nozzle. A combustible gas (usually acetylene), oxygen, and compressed air melt and atomize the wire, blowing it against the surface.

Key capability: Any desired thickness can be deposited. Materials include steels (low to high carbon), brass and bronze compositions, babbitt metal, tin, zinc, lead, nickel, copper, and aluminum.

Production applications: Automotive exhaust valves, transfer ink rollers, truck clutch plates, glass meter box windows, aluminum-on-cloth for electrolytic condenser plates, zinc/copper on ceramic insulators.


. Powder-Fed Combustion Spray

Uses metal, refractory, and ceramic powder instead of wire. Employs two gases: oxygen and a fuel gas (usually acetylene; sometimes hydrogen).

Four basic coating powder types:

  1. Ceramics
  2. Oxidation-resistant metals and alloys
  3. Self-bonding alloys
  4. Alloys for fused coatings

These produce wear-resistant, corrosion-resistant, heat-resistant, and electrically conductive coatings.


. Plasma Flame Spraying

Uses plasma to raise material vapors to a higher energy level than ordinary gases. This raises the temperature ceiling and provides a controlled atmosphere using inert or chemically inactive gas, controlling oxidation during heating and application.



Plasma Arc Surface Coating

A transferred arc (between electrode and workpiece) applies coatings to the workpiece surface. Key parameters:

  • Arc temperatures: 25,000–50,000°F (14,000–28,000°C)
  • Deposition rates: Up to 15 lb/h (powder) or 28 lb/h (wire)
  • Base metal dilution: Can be held below 5% if required

The nontransferred arc process (arc between electrode and nozzle, not touching the work) is used for metal spraying — building surfaces for hard facing and applying anticorrosion/barrier layers. Over 500 different powder combinations are available, with deposition rates up to 100 lb/h.



Laser Surface Treatment: Precision Without Distortion

This was the practitioner's "aha" moment. When she learned that a defocused CO₂ laser impinging on room-temperature steel has over 90% of its power reflected (about 93% for steels), she understood why laser heat treatment requires a completely different approach than conventional heating.


The Reflectivity Problem

Laser heat treatment operates at power densities below 10⁴ W/cm² — insufficient to overcome reflectivity effects. The surface must be prepared to enhance absorption by one of several methods:

  • Surface roughening — creates tiny craters that trap beam energy long enough to raise surface temperature to where more energy is absorbed
  • Surface coating — black enamel paint is common; the laser vaporizes the enamel, leaving a clean surface beneath

Once absorbed, the laser energy (converted to heat) raises the temperature in the beam pattern. Dwell time controls the depth of heat treatment and is extremely effective for case depth control in hardening.


Materials Applicability

Category Examples Hardenability
Good candidates Medium/high-carbon steels, tool steels, low-alloy steels, cast irons, steels with fine-carbide dispersion Fully hardenable
Marginally hardenable Annealed carbon steels, spheroidized carbon steels, mild-carbon steels (0.2% C), ferritic nodular cast irons Limited case depth
Not hardenable Low-carbon steels (< 0.1% C), austenitic stainless steels, nonferrous alloys and metals No hardenability

Microstructure effect on case depth:

Microstructure Carbon Diffusion Distance Resulting Case Depth
Graphite + tempered martensite (cast iron) Low Deep
Tempered martensite or bainite (steel) Low Deep
Graphite + ferrite (cast iron) Large Very shallow or none
Fe₃C + ferrite (spheroidized iron) Large Very shallow or none

Typical hardening rate: 130 cm²/min (20 in²/min) for a 1 mm (0.039 in.) case depth in 4140 steel.

Compared to conventional techniques: Laser hardening is typically slower than induction heating. However, by limiting the area to be hardened, the laser eliminates residual heat effects that cause part distortion — making it cost-effective for precision components.


Laser Cladding

In laser cladding, a shaped or defocused beam heats preplaced or gravity-fed powdered alloys. The cladding alloy melts, flows across the substrate surface, and rapidly solidifies when laser power is removed.

Compatible alloys include: Stellites, Colmonoys, alloys containing carbides, Inconel, Triballoy, Fe-Cr-C-X alloys, tungsten and titanium carbides.

The key advantage — minimal dilution:

Process Dilution Level
Laser cladding < 2%
Plasma arc cladding 5–15%
Stick electrode cladding 20–25%

The laser process produces a dense, homogeneous, nonporous clad layer that is metallurgically bonded to the substrate — in contrast to the mechanically bonded, more porous layer produced by other methods.



Laser Marking: Permanent Identification Without Contact

Two groups of laser marking technology:


Mask Marking

A CO₂ laser beam is projected through a reflective mask, reimaged by optics onto the material's surface. The absorbed heat changes the molecular structure to produce a visible mark.

  • Line speeds: Up to 20,000 marks/h
  • Energy densities: 1–20 J/cm²
  • Minimum line width: 0.1 mm (0.004 in.)
  • Applications: Clouding PVC or acrylics, changing colored surfaces by adjusting pigment proportions, ablating surface layers to expose sublayers of different color

Scanned-Beam Marking

A pulsed YAG or CO₂ laser beam is directed onto the surface by controlled mirror oscillation in a preprogrammed pattern. Provides virtually unlimited choice of patterns.

  • Heat-type marks: Up to 2500 mm/s (100 in/s)
  • Engraved marks: 500–800 mm/s (20–30 in/s)
  • Typical writing field: 100 × 100 mm (4 × 4 in.)

For highly reflective metals like aluminum, better results come from pretreating the surface (e.g., anodizing). Not all scanned-beam applications remove base metal — some remove only a coating or produce a heat discoloration.



Act IV: The Etching Workshop — Chemical Surface Artistry


Etching Fluids for Different Metals

The final piece of the practitioner's surface treatment education came from the company's in-house toolroom, where master toolmakers still used acid etching for precision scale graduation and identification marking.

Standard etching method for steel: Apply a thin, even coating of beeswax or similar acid-resistant substance (the "resist"), scribe lines through the wax to expose the steel, then apply acid.

Resist composition (for fine graduation work): Approximately 50% asphaltum, 25% beeswax, plus small percentages of Burgundy pitch, black pitch, and turpentine. For some work, melted paraffin is poured over the surface at elevated temperature to form a thin protective coating.

Etching fluid reference:

Material Solution
Carbon steel Nitric acid : water = 1:4 (adjust water ratio based on carbon content and hardness)
Hard steel Nitric acid : acetic acid = 2:1
High-speed steel, nickel, brass Nitro-hydrochloric acid (nitric 1 : hydrochloric 4) — may add more nitric for HSS
Bronze Nitric acid : muriatic acid = 100:5
Brass Nitric acid 16 : water 160; separately dissolve potassium chlorate 6 in water 100; mix solutions
Aluminum Alcohol 4 oz : acetic acid 6 oz : antimony chloride 4 oz : water 40 oz
General purpose (frost or deep etch) Copper sulfate 1 oz, alum ¼ oz, salt ½ tsp, vinegar 1 gill, nitric acid 20 drops


Act V: The Heat-Affected Zone — Understanding What Heat Treatment Does to Surfaces

the practitioner's final lesson came from the EDM shop, where wire-cut parts showed surface damage that was invisible to the naked eye but devastating in service.


The Recast Layer and HAZ in EDM

When EDM sparks strike the workpiece, the dielectric oil breaks down into hydrocarbons, tars, and resins. The molten metal draws out carbon atoms and traps them in the resolidified metal, forming a very thin, hard, brittle recast layer covering the heat-affected zone (HAZ).

Recast layer characteristics:

  • Appearance: White
  • Composition: Particles melted by sparks, enriched with carbon, drawn back to surface
  • Hardness: Harder than parent metal — can be as hard as glass
  • Required action: Must be reduced or removed by vapor blasting with glass beads, polishing, electrochemical or abrasive flow machining — or risk cracking and flaking in service

HAZ characteristics (in steel):

  • Consists of martensite hardened by heating/cooling sequences
  • Expansion and contraction rates differ from parent metal
  • Under thermal cycling, the differential stresses may cause surface cracks
  • HAZ depth depends on amperage and on-time: increases to about 0.012–0.015 in. deep
  • Residual stress can reach 650 N/mm²

Best practice: Program successive cuts so that each cut removes most of the HAZ from the previous cut. Reduce cut depth gradually until finishing cuts produce HAZ thickness < 0.0001 in.



Heat Treatment of Steel Castings

Steel castings can be heat treated to achieve:

  • Diffusion of carbon or alloying elements
  • Softening or hardening
  • Stress relieving
  • Toughening
  • Improved machinability
  • Increased wear resistance
  • Removal of hydrogen entrapped at the casting surface

Heat treatment of steel castings follows closely that of wrought steel of similar composition.

Mechanical properties achievable by heat treatment:

Tensile Strength (psi) Yield Point (psi) Elongation (%) Brinell Hardness Heat Treatment Application
60,000 30,000 32 120 Annealed Low resistivity, magnetic properties, carburizing/case hardening, weldability
65,000 35,000 30 130 Normalized Good weldability, medium strength, high ductility
80,000 45,000 26 160 Normalized & tempered High strength, good machinability, toughness, fatigue resistance
100,000 70,000 20 200 Quenched & tempered Wear resistance, hardness
150,000 125,000 12 300 Quenched & tempered Deep hardening, high strength, wear/fatigue resistance
200,000 170,000 5 400 Quenched & tempered Maximum strength and hardness, wear resistance


The Decision Framework: Choosing the Right Surface Treatment

the practitioner built this framework after months of investigation, testing, and failure analysis. It became the standard reference in her plant.


Surface Treatment Selection Matrix

Primary Requirement Recommended Treatments Key Considerations
Corrosion protection (mild) Black oxide + oil/wax, phosphate coating, passivation Lowest cost; limited protection; dimensional stability
Corrosion protection (moderate) Zinc plating, cadmium plating, chemical films Hydrogen embrittlement risk on high-strength steels
Corrosion protection (severe) Anodizing (Al), chrome plating, electroless nickel, nickel plating Higher cost; excellent long-term performance
Wear resistance Hard chrome, hard anodize, hard facing (cobalt/NiCr), laser cladding Match hardness to service conditions
Fatigue-critical parts Thin anodize (Type I/IB), shot peening + thin coating Avoid thick coatings that initiate cracks
Lubricity / anti-galling Manganese phosphate + oil, solid film lubricant, silver plating Critical for sliding interfaces
Electrical conductivity Gold plating, silver plating, tin plating Specify minimum thickness for contact resistance
Solderability Tin plating, gold plating (thin), electroless nickel (AMS 2433B) Consider shelf life of solderability
Paint adhesion Zinc/iron phosphate, chromate conversion, anodize + seal Surface roughness profile matters
High temperature (> 1000°F) Cobalt-base hard facing, NiCr alloys, chrome plating Verify hot hardness at service temperature
Dimensional restoration Flame spraying, chrome plating (heavy), electroless nickel Specify final dimension after coating
Decorative finish Coloring (copper alloys), black oxide, anodize + dye Specify post-treatment for longevity

The Hydrogen Embrittlement Decision Tree

This is the issue that catches engineers off guard and causes catastrophic failures:

Is the steel ≥ Rc 33 (or ≥ 1000 MPa tensile)?
├── YES → Hydrogen embrittlement risk exists
│   ├── Can you avoid electroplating entirely?
│   │   ├── YES → Use vacuum cadmium, mechanical plating, or conversion coatings
│   │   └── NO → Proceed with extreme caution:
│   │       ├── Stress relieve BEFORE plating (375°F, 3+ hours)
│   │       ├── Bake AFTER plating (375°F, 3–24 hours depending on process)
│   │       ├── Bake within 4 hours of plating completion
│   │       └── Do NOT flex springs or flexure parts before baking
│   └── Is the steel ≥ Rc 40 (or ≥ 1700 MPa tensile)?
│       ├── YES → Some processes are PROHIBITED
│       │   ├── Zinc plating: SHALL NOT be applied > 1700 MPa
│       │   ├── Nickel plating: Requires specific agency approval > 220,000 psi
│       │   └── Vacuum cadmium: Recommended alternative for ≥ 220,000 psi
│       └── Extended bake times required (8–12+ hours for chrome)
└── NO → Standard plating procedures apply


Engineering takeaway

the practitioner's six-month journey from catastrophic die failure to surface treatment expertise taught her a principle that every engineer, machinist, and manufacturing professional should internalize:

The surface is not separate from the part. It IS the part — at the one place where the part meets the world.

Every coating, plating, conversion treatment, and surface engineering process described in this guide exists because someone, somewhere, learned the hard way that naked metal isn't enough. Corrosion doesn't care about your alloy selection if the surface isn't protected. Wear doesn't care about your heat treatment if the contact interface isn't engineered. Fatigue doesn't care about your design margins if the surface finish initiates cracks.

The specifications in this guide — the MIL-SPECs, the ASTM standards, the AMS requirements — aren't bureaucratic red tape. They're the accumulated wisdom of millions of failures, distilled into precise instructions for preventing the next one.



Your Next Step

Look at the last part that failed in your shop, your plant, or your client's facility. Ask yourself:

Was the failure at the surface?

If the answer is yes — and statistically, it probably is — then the right surface treatment could have prevented it. Go back through this guide with that specific failure in mind. Match the failure mode to the treatment category. Check the specification requirements against what was actually applied.

The answer is almost always in the surface.



Quick Reference: Military and Industry Specifications Covered

Specification Treatment Material
MIL-A-8625F Anodize (chromic, sulfuric, hard coat) Aluminum alloys
MIL-C-14538C Black chrome Steels
MIL-C-13924C Black oxide coating Ferrous metals
QQ-P-416F Cadmium plating Various
MIL-C-8837B Vacuum cadmium High-strength steels
MIL-C-5541E Chemical films Aluminum alloys
MIL-F-495E Chemical finish (black) Copper
QQ-C-320B Chrome plating Various
MIL-C-14550B Copper plating Various
AMS 2404C/2405B/2433B Electroless nickel Various
MIL-G-45204C Gold plating Various
MIL-L-46010D Solid film lubrication Multiple metals
MIL-M-3171C Magnesium process Magnesium alloys
MIL-M-45202C Magnesium anodic treatment Magnesium alloys
QQ-N-290A Nickel plating Various
MIL-P-45209B Palladium plating Various
QQ-P-35C Passivation Stainless steels
TT-C-490D Phosphate coating (light) Ferrous metals
DOD-P-16232-F Phosphate coating (heavy) Low/medium alloy steels
MIL-R-46085B Rhodium plating Various
QQ-S-365D Silver plating Various
MIL-T-10727C Tin plating Various
MIL-P-81728A Tin-lead plating Electronics
ASTM B633 Zinc plating Iron and steel

This guide covers conversion coatings, electroplating, electroless plating, anodizing, hard facing, flame spraying, plasma arc coating, laser heat treatment, laser cladding, laser marking, etching, coloring, passivation, and all associated military and industry specifications. Bookmark it. You'll be back.

Engineering use and verification

Choose and control a process from the required function, material, geometry, tolerance, surface condition, volume, safety and inspection plan. Confirm the process window with representative trials, identify the variables that move quality, and connect each critical characteristic to an observable control and reaction plan. Do not convert a successful source example into a universal limit; validate capability using the actual machine, tooling, material batch and operating conditions.

  • Confirm scope, assumptions, interfaces and required outcome.
  • Use one controlled unit system and show every conversion.
  • Identify current project, customer and regulatory requirements.
  • Separate source examples from mandatory acceptance criteria.
  • Check calculations, tables and selections by an independent method.
  • Verify safety, maintainability and credible failure modes.
  • Record evidence, revisions, approvals and unresolved limitations.
  • Validate the result under representative operating conditions.

Continue learning

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