Aerospace Industry

Electropolishing for Aerospace Applications

Flight-critical starts at the surface.

From engine hot sections and landing gear to rotor systems, hydraulic manifolds, and airframe fasteners, electropolishing extends the fatigue life and corrosion resistance that demanding cycle-life specifications require.

70+
Years Experience
30×
Better vs. Passivation
24/5
Production
#1
Largest EP Specialist
Able Is Trusted By

Every flight-critical part carries a cycle-life number — and machining, stamping, grinding, and EDM leave behind exactly the surface anomalies that cut it short. Microburrs, embedded contaminants, tool marks, and recast layers become the initiation sites where fatigue cracks start and corrosion takes hold.

Able Electropolishing has spent decades finishing components for commercial and military aircraft manufacturers, rotorcraft OEMs, engine builders, landing gear suppliers, hydraulic and fuel system OEMs, and aerospace fastener producers. Our AS9100:2016-certified process removes a microscopically controlled surface layer, eliminating the defects that mechanical finishing leaves behind — while improving Ra up to 50% in a single step.

The result: measurably longer fatigue life, superior corrosion resistance, reliable penetrant inspection, and reduced friction on the parts where cycle-life specifications are non-negotiable.

Precision aerospace component surface before and after electropolishing

Machining and EDM leave surface defects that electropolishing removes with microscopic precision

Prove it on your own part. Send us a sample and we’ll electropolish it free — processed on production equipment, returned with Ra data in 24–48 hours.

Applicable Standards
AS9100:2016 ISO 9001:2015 ITAR Registered ASTM B912 AMS 2700 ASTM A967 ASTM F86 ASTM E1417 100% US-Based
Why Electropolishing

Nine Ways Electropolishing Extends Aerospace Part Life

Thousands of pressurization cycles, extreme temperature swings, and decades of service between overhauls — aerospace hardware fails at the surface first. Here’s what electropolishing does about it.

01 / Fatigue

Fatigue life for cycle-limited parts

Fatigue cracks initiate at surface stress risers — tool marks, microcracks, burr roots. Removing them electrochemically measurably extends cycle life on rotating and pressurized hardware.

Engine Hardware · Rotor Systems · Landing Gear
02 / EDM

EDM recast layer removal

Wire and sinker EDM leave a brittle, microcracked recast layer on cooling holes, injector features, and intricate geometries. Electropolishing strips it uniformly, controlled to ±.0002″.

Cooling Holes · Fuel Nozzles · Blisks
03 / FPI

Reliable penetrant inspection

Machining smear seals surface-breaking defects away from FPI penetrant. Removing .0002″–.0005″ per surface restores true indication visibility on fracture-critical parts.

FPI · DPI · Fracture-Critical Hardware
04 / Corrosion

Corrosion resistance at altitude & on the ramp

Condensation cycling, de-icing fluid, and coastal operations attack contaminated surfaces. A chromium-enriched passive layer delivers up to 30× the corrosion resistance of passivation alone.

Airframe Hardware · Fasteners · Fittings
05 / Hydraulics

Deburring for hydraulic & fuel systems

A single detached microburr becomes contamination in a 3,000-psi hydraulic system. Electropolishing dissolves burrs at the root on manifolds, spools, and fittings — no mechanical contact, no new debris.

Manifolds · Servo Valves · Fuel Fittings
06 / Titanium

Alpha case & titanium surface recovery

Heat treatment leaves an oxygen-enriched alpha case that embrittles titanium surfaces. Electropolishing removes it uniformly, restoring the fatigue performance the alloy was specified for.

Ti 6Al-4V · Airframe · Engine Mounts
07 / H₂

No hydrogen embrittlement

Acid pickling and plating drive hydrogen into high-strength steels. Electropolishing is anodic — oxygen evolves at the part surface — making it safe for 300M, 4340, and PH-grade hardware without bake-out.

Landing Gear · 300M · PH Stainless
08 / Fasteners

Bulk electropolishing for fasteners

Thread burrs scatter preload and invite galling. Able’s automation-enhanced bulk EP finishes high-volume aerospace fasteners with consistent thread-root quality, lot after lot.

A286 · Inconel · Ti Fasteners
09 / High Temp

Superalloy & exhaust hardware

Inconel, Hastelloy, and Haynes components in hot sections and exhaust paths benefit from contamination-free, oxide-free surfaces that resist high-temperature corrosion and thermal fatigue.

Inconel 718 · Exhaust · Bellows
Service Environments

Engineered for the Conditions Aircraft Actually Fly In

Surface preparation for the environments that define aerospace duty cycles.

🔄

Pressurization Cycles

Tens of thousands of ground-air-ground cycles loading every structural surface.

🌡

Thermal Extremes

−60°F at altitude to 1,800°F+ in the hot section — every flight.

🧪

Fluids & De-Icing

Skydrol, jet fuel, de-icing glycol, and runway salts attacking exposed hardware.

🛠

Decades Between Overhauls

Parts must inspect clean and perform to spec across 20–30 year service lives.

AS9100:2016Aerospace quality management system — certified, with full lot traceability.
ASTM B912Electropolishing of stainless steels — the spec most commonly called out on prints.
AMS 2700 / ASTM A967Nitric and citric passivation, all types and classes.
ITAR RegisteredControlled handling for military aircraft programs and technical data.
Specifying the Finish

AMS 2700 Passivation vs. Electropolishing + Passivation

When a print calls for passivation, you’re choosing between nitric, citric, or electropolishing followed by passivation. All three are available in-house at Able. For fatigue-rated aerospace hardware, EP + passivation is the strongest specification — it removes the defects passivation can only clean around.

Nitric

AMS 2700 Method 1 · ASTM A967
  • Proven on the widest range of aerospace stainless
  • Strong free-iron removal on heavily handled parts
  • Economical at volume
  • No change to surface finish or Ra
  • Burrs, microcracks, and tool marks remain
  • Flash attack risk on lower Cr-Ni grades

Citric

AMS 2700 Method 2 · ASTM A967
  • Gentler chemistry — safer for sensitive alloys
  • Environmentally preferred handling
  • Effective passive layer formation
  • No Ra improvement or defect removal
  • Slower cycle than nitric
  • Less aggressive on heavy contamination
Strongest Spec

EP + Passivate

ASTM B912 + AMS 2700 / A967
  • Removes the defect layer, then passivates — corrosion resistance up to 30× passivation alone
  • Ra improvement up to 50% in the same operation
  • Deburrs and removes microcracks — direct fatigue-life benefit
  • No flash attack risk
  • Fully compatible with FPI and downstream NDT
  • One purchase order, one supplier, one cert package
In ASTM B-117 salt spray testing, electropolished coupons in 304, 410, 420, and Trinamet ran 888 hours without rusting; passivation-only coupons showed corrosion onset within the first 24–72 hours.

Zooming Out: Electropolishing vs. Pickling vs. Passivation

Pickling still shows up in aerospace — titanium descaling after heat treatment, exhaust and duct weldments, and mill-prepped stock. Here’s how the three process classes compare on flight-critical criteria, including the hydrogen embrittlement risk pickling carries on landing gear steels like 4340 and 300M and on PH grades.

CriterionPicklingPassivationElectropolishing
Removes base materialAggressive / uneven etchNoMicroscopically precise (±.0001″–.0005″)
Removes burrs & microcracksPartialNoYes
Surface roughness (Ra)Roughens & etchesNo changeImproves up to 50%
Weld heat tint & oxide scaleYes — but uncontrolledNoYes — down to clean base metal
Improves fatigue lifeNoNoYes
Corrosion resistanceCan pit if uncontrolledImprovesUp to 30× vs. passivation alone
Hydrogen embrittlement riskYes — high-strength & high-carbon steelsLowNone — anodic process
Leaves part passivatedNoYesYes
Process consistencyBath weakens with ageGoodControlled & repeatable
Alloy compatibilityToo corrosive for many alloysLimited — flash attack risk on low Cr-Ni grades35+ alloy families

Full details in our technical guide: Passivation, Pickling or Electropolishing — Which Metal Finishing Process Is Right for Your Parts? Available from our Learning Center.

Technical Resources

Aerospace Guides & Whitepapers

Deep-dive references written for aerospace engineers specifying surface finishing.

Technical Guide

Electropolishing for the Aerospace Industry

Improving part lifecycle for commercial and military aircraft — fatigue life, cycle specifications, alloy guidance, and application examples.

Download Guide
Whitepaper

Electropolishing for Penetrant Testing

Why electropolishing is the ideal pre-cleaning step for penetrant inspection of fracture-critical aerospace parts — and what smear does to indication reliability.

Download Whitepaper
Whitepaper

Advantages of Electropolishing for Deburring

How microscopically precise material removal outperforms mechanical deburring on precision parts — with consistent, repeatable results.

Download Whitepaper
Possible Components for Electropolishing

The Hardware That Keeps Aircraft Flying

From the hot section to the wheel well, we finish the components that carry cycle-life requirements. Send us a print ›

// 01

Engine Components

Fuel nozzles, cooling-hole hardware, combustor parts, blisks, seals, and EDM’d features.

// 02

Landing Gear

Struts, pins, bushings, torque links, and high-strength steel hardware — no H₂ embrittlement risk.

// 03

Hydraulic Systems

Manifolds, servo valve components, spools, actuator internals, and fittings.

// 04

Fuel Systems

Injector components, fuel controls, filters housings, and contamination-sensitive fittings.

// 05

Rotorcraft & Rotor Systems

Pitch links, swashplate components, rotor hub hardware, blade retention pins, and transmission gears — the highest-cycle fatigue parts on any aircraft.

// 06

Airframe Structural

Machined fittings, brackets, lugs, and titanium structural components.

// 07

Fasteners

Bolts, screws, pins, and collars in A286, Inconel, and titanium — bulk EP capability.

// 08

Actuation & Flight Controls

Ball screws, gears, linkage hardware, and precision motion components.

// 09

Exhaust & Ducting

Bellows, ducting, heat shields, and superalloy exhaust-path hardware.

// 10

Avionics & Enclosures

Housings, chassis, connectors, and EMI-sensitive precision hardware.

// 11

MRO & Overhaul

Refurbished components requiring restored surface condition and re-passivation.

// 12

UAS & Unmanned Systems

Propulsion, fuel system, and precision-machined components for unmanned aircraft programs.

Penetrant Inspection Prep

Before FPI Can Find the Crack, the Surface Has to Show It

Fracture-critical aerospace parts live and die by penetrant inspection — but machining and grinding smear metal across the very defects FPI is looking for. Electropolishing dissolves that smeared layer so the penetrant reaches real indications, not a false-clean surface.

As-Machined — Indications Suppressed

What smear does to inspection

  • Cutting, grinding, and EDM plastically deform the surface, folding metal over defect openings
  • Crack mouths, laps, and porosity get partially or fully sealed
  • Penetrant can’t wick into what it can’t reach — indications never develop
  • Parts pass inspection while carrying detectable defects into service
After Electropolishing — True Surface Exposed

What a clean surface shows

  • Uniform removal of .0002″–.0005″ per surface dissolves the smeared layer
  • Real crack mouths and porosity open to the penetrant
  • Bright, oxide-free surface wets consistently — fewer false calls
  • Inspection reliability holds lot after lot, part after part
ASTM E1417Penetrant inspection practice requires defects be open to the surface — smeared metal is a recognized cause of missed indications.
Fracture-Critical PartsRotating engine hardware and primary structure carry mandatory NDT — surface prep quality directly drives detection probability.
Whitepaper AvailableElectropolishing for Penetrant Testing — the complete technical case.
Pre-Penetrant Surface Prep

Chemical Etch vs. Electropolishing Before Penetrant Inspection

AMS 2649 chemical etch is the traditional pre-FPI prep in aerospace NDT — but etching attacks grain boundaries, can drive hydrogen into high-strength alloys, and drifts with bath age. Electropolishing removes the same smeared layer with none of those liabilities.

FactorChemical Etch (AMS 2649)Electropolishing (ASTM B912)
Smear removalEffective on work-hardened smearUniform dissolution of smear and surface peaks
Defect exposureOpens crack mouths, but attacks base metal tooOpens crack mouths with no base-metal damage
Material removal controlUneven, difficult to predictControlled to ±.0001″ per surface
Hydrogen embrittlementRisk on PH grades, 4340, 300M — bake-out may be requiredNone — anodic process, no bake-out
Intergranular attackRisk on sensitized materialNone — dissolution uniform across grain structure
Post-prep surfaceMatte, roughened — can trap penetrant and create false callsRa improved up to 50% — cleaner backgrounds, fewer false calls
Titanium alpha casePartial, uneven removalComplete, uniform removal
RepeatabilitySensitive to bath age and temperatureCurrent, time, and chemistry controlled — lot after lot
Best fitLow-cost prep where dimensions and alloy allowFracture-critical and fatigue-rated hardware
For fracture-critical aerospace parts: a prep process that can introduce hydrogen, intergranular attack, or a rougher surface works against the inspection it’s preparing for. Electropolishing exposes true indications without adding new metallurgical risk — and improves the part while doing it.
EDM Recast Removal

EDM Builds the Feature. Electropolishing Makes It Flightworthy.

EDM is everywhere in modern aerospace manufacturing — cooling holes, fuel nozzle orifices, blisk features, seal slots. But the spark that cuts the feature also re-deposits molten metal as a recast layer: amorphous, brittle, and laced with microcracks that propagate under thermal and mechanical cycling.

Electropolishing dissolves the recast layer uniformly — material removal controlled to ±.0002″ — exposing sound base metal while preserving the tight tolerances the feature was cut to. On fatigue-rated hardware, that’s the difference between the recast layer’s crack initiation life and the base alloy’s.

Read: Eliminating EDM Recast Layer with Electropolishing ›
Problem
Brittle recast layer with microcracks on EDM’d features
Risk
Fatigue crack initiation, FPI false-negatives, contamination
Removal
Typically .0001″–.001″, matched to recast depth
Control
±.0002″ — critical dimensions preserved
Standards & Certifications

Certified for Aerospace Supply Chains

Certificates of compliance ship with every order; process documentation supports first-article and PPAP-style submissions.

Aerospace QMS

AS9100 : 2016

Internationally recognized aerospace quality management certification — the credential your supplier quality team looks for first.

Quality Management

ISO 9001 : 2015

Foundation quality system certification underpinning every process at our Chicago facility.

Export Control

ITAR Registered

DDTC registration for military aircraft programs — controlled handling of defense articles and technical data.

Electropolishing

ASTM B912

Standard specification for passivation of stainless steels using electropolishing.

Passivation

AMS 2700 / ASTM A967

Aerospace passivation of corrosion-resistant steels — nitric and citric, all types and classes.

Sourcing

100% US-Based

All processing at our Chicago, IL facility — nothing subcontracted offshore.

Alloys & Materials

Alloys We Electropolish for Aerospace

Search or filter the alloys behind airframes, engines, landing gear, and flight systems.

AlloyCategoryFinishTypical Aerospace PartsWhy It’s SpecifiedEP BenefitRa Before → After

Able processes 35+ alloy families with proprietary recipes. Full alloy library at ableelectropolishing.com/alloys-electropolished.

Our Process

Our Electropolishing Process

1

Print & Spec Review

Drawings reviewed against AMS, ASTM, and customer process specifications before any part is processed.

2

Cleaning & Prep

Machining oils, oxides, and handling contamination removed ahead of processing.

3

Electropolishing

Alloy-specific recipe dissolves surface peaks, burrs, smear, and recast with controlled removal.

4

Passivation

Where specified, nitric or citric passivation per AMS 2700 / ASTM A967 follows.

5

QC & Delivery

Ra verification, C of C, and lot traceability documentation with every shipment.

FAQ

Frequently Asked Questions

Is Able AS9100 certified?+

Yes — Able holds AS9100:2016 certification, the internationally recognized quality management standard for aerospace organizations, alongside ISO 9001:2015 and ISO 13485:2016. Our current certificate is available for download on our certifications page.

How does electropolishing improve fatigue life?+

Fatigue cracks initiate at surface defects — tool marks, microburrs, microcracks, and inclusions act as stress concentrators. Electropolishing removes the defective surface layer electrochemically, without introducing new mechanical stress, leaving a smooth surface with dramatically fewer initiation sites. For cycle-limited aerospace hardware — rotor system components above all, where vibratory loads accumulate millions of cycles between overhauls — that translates directly into extended service life.

Can you process titanium and remove alpha case?+

Yes. Able electropolishes titanium alloys including 6Al-4V (Grade 5) and CP grades. Electropolishing uniformly removes the oxygen-enriched alpha case layer left by heat treatment, restoring the surface fatigue properties of the base alloy. We also passivate titanium per ASTM F86.

Does electropolishing cause hydrogen embrittlement on high-strength steels?+

No — this is one of electropolishing’s key advantages for landing gear and other ultra-high-strength steel hardware. Electropolishing is an anodic process: oxygen, not hydrogen, evolves at the part surface. Unlike acid pickling or plating, there is no hydrogen uptake and no bake-out requirement for 4340, 300M, or PH-grade parts.

What are your maximum part sizes?+

Electropolishing:

  • 300 & 400 series stainless steel: 108″ L × 41″ W × 42″ H
  • Copper, brass, aluminum, steel, and nickel alloys: 72″ L × 14″ W × 17″ H
  • Titanium, Nitinol, tungsten, niobium: 26″ L × 8-3/4″ W × 9-3/4″ H

Email a print to sales@ableelectropolishing.com for review of anything near these limits.

What’s the standard lead time?+

Standard delivery is 3 to 5 working days after receipt of order. Next-day and same-day expedite services are available for AOG situations — contact sales for options.

Do you also serve defense and space programs?+

Yes. Able is ITAR registered and supports military aircraft, defense, and space programs from the same AS9100-certified facility. See our dedicated Space & Satellites page — and our Defense industry page — for program-specific details.

Get Started

Try Electropolishing on Your Aerospace Component — Free

Send us your actual production parts. We process them on production equipment — not bench tests — and return them with Ra measurements and documentation you can put in a qualification package. Turnaround is 24–48 hours.

Facility2001 S. Kilbourn Ave. · Chicago, IL 60623 · USA

Request a Quote or Free Sample

Tell us about your aerospace component and we’ll follow up within one business day.

Your information is confidential. ITAR-controlled inquiries welcome.

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Complete Alloy Library

124+ alloys with finish documentation — stainless, titanium, superalloys, aluminum, and specialty steels.

Read more ›

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Passivation: Improve the Corrosion Resistance of Stainless Steel Parts

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