Aerospace machining brings difficult materials, thin-wall geometry, tight tolerances and documentation requirements into one program. We machine structural components, fittings, housings and hardware with traceability, inspection planning and special-process coordination aligned to your drawing and flow-down requirements.
Every aerospace component carries the same implicit requirement: it cannot fail. That shapes material selection, distortion control, tolerance planning, inspection, special processes and documentation.
We support aerospace OEMs, tier suppliers and MRO programs with structural brackets and fittings, actuation and hydraulic components, avionics housings, engine-adjacent hardware, cabin hardware and legacy replacement parts.
Flow-down clauses, material sourcing rules, special-process requirements, export-control instructions and required records must be supplied with the RFQ so compliance can be confirmed before quotation.
Aerospace components are planned around strength, weight, distortion risk, material traceability, finish requirements and documented release.
Wing, fuselage and equipment attachment components machined from plate, billet or forgings with weight-optimized geometry.
Cylinder bodies, valve manifolds, pistons and fittings where sealing surfaces and bore geometry influence system performance.
EMI-aware housings, heat-sink chassis and connector panels with precise hole patterns and mounting datums.
Non-rotating mounts, brackets and ducting hardware in titanium or nickel alloys where thermal cycling and vibration matter.
Bushings, pins, shafts and linkages in high-strength steels with heat treatment and grinding when specified.
Seat components, latch mechanisms and galley hardware where weight, finish and documentation intersect.
Non-standard sizes, proprietary threads and low-volume hardware that catalog suppliers do not carry.
Drawing-controlled or sample-assisted replacements for aging fleets, with acceptance requirements agreed before release.
Aerospace parts punish unplanned machining routes through distortion, tool wear, special-process failures and incomplete release records.
The manufacturing route is reviewed around material condition, wall geometry, datum structure, flow-down clauses and the documentation package required at delivery.
Stress-relieved stock, symmetric roughing, controlled fixturing and verification after unclamping help manage thin webs, pockets and large structural parts.
Titanium, Inconel and hardened steels require rigid setups, appropriate tooling, coolant strategy and honest cycle-time planning.
AS9102-style FAI, material certificates, finish records and special-process documentation are planned as part of the job.
Material sourcing, supplier qualification, counterfeit prevention and special-process records are reviewed against supplied quality clauses.
Hydraulic, actuation and control components require bore geometry, sealing surfaces and critical diameters to be protected through machining and finishing.
Replacement parts require careful drawing review, sample correlation, material confirmation and documented acceptance criteria before release.
Our aerospace machining routes use mill-turn machining, Swiss machining, CNC turning and CNC milling, including 3-axis and 5-axis milling. Process selection follows the part geometry, material, datum structure and inspection requirements.
Combine turned diameters, bores and threads with flats, cross-holes and milled features on aerospace fittings, valve components and actuator shafts. Y-axis tooling and rear-side operations reduce transfers between machines and help maintain feature relationships.
Machine small-diameter pins, slender shafts, miniature fittings and custom fasteners from bar stock. Guide-bushing support, driven tools and back-working operations control deflection and support fine threads and concentric features.
Produce aerospace bushings, sleeves, shafts and flanged components with drawing-defined diameters, bores, threads and sealing surfaces. Tooling and cutting parameters are selected for the specified alloy and material condition, including titanium and nickel alloys where applicable.
Use 3-axis and 5-axis milling for structural brackets, housings, pockets, compound angles and multi-face features. Select fixtures, tool access and machining sequences around functional datums, wall stiffness and the properties of the specified aerospace alloy.
The sequence covers drawing and flow-down review, material sourcing confirmation, process planning, first article inspection, production machining, special processes, final inspection and complete release documentation.
Provide the STEP model and dimensioned drawing with the current revision, material grade, quantity, surface finish, required delivery date and inspection requirements. Where required, an NDA is signed before drawings and models are exchanged.
Review geometry, dimensional and geometric tolerances, stock condition, tool access, workholding and measurement access. Identify features that affect machining feasibility, dimensional stability or inspection, and resolve proposed drawing changes with your engineering team.
Confirm the drawing revision, material specification, datum scheme, critical dimensions, surface finish and inspection requirements. Resolve drawing queries and document approved changes. Prepare the quotation from the confirmed part requirements, quantity and delivery schedule.
Define the operation sequence, machining datums, fixtures, cutting tools and cutting parameters. Prepare the NC program and inspection plan, review toolpaths through machine simulation, and establish the setup instructions for the first-article machining trial.
Specified material grades and stock forms are purchased exclusively from approved or qualified suppliers, matched to the requirements of your drawing and purchase order.
Check stock identification, dimensions, surface condition and material certificates against the specified grade, condition and purchase order. Record the heat or batch number and link the accepted material to the production work order.
Machine the first article using the planned NC program, fixtures and tools. Inspect drawing characteristics with the specified measurement methods, record the results and correct setup or program deviations before batch production begins.
Run the approved Aerospace CNC machining program with the documented fixture setup, tooling and cutting parameters. Maintain the specified datums and machining sequence, and record approved changes to programs, tool offsets or setup instructions.
Measure critical dimensions and geometric characteristics at the intervals defined in the inspection plan. Monitor tool wear and dimensional trends, adjust offsets where appropriate, and recheck affected features after adjustment.
Check the completed machining operations against the drawing and review the in-process inspection results. Record dimensional conformity and segregate nonconforming parts before the batch proceeds to finishing or other subsequent operations.
Complete the specified deburring, grinding, polishing, surface treatment or heat treatment. Check treatment records and reinspect features affected by material removal, coating thickness or heat-treatment distortion.
Inspect finished parts against the drawing and final inspection plan, including dimensions, surface condition and finish requirements. Compile the required material certificates and inspection reports, verify quantity and identification, then pack parts to prevent damage during shipment.
Material grade, temper, source and certification requirements are confirmed before procurement. DFARS-compliant or domestic sourcing can be reviewed when specified with the RFQ.
Showing 4 Materials: Aluminum.
A primary structural alloy with high strength at low weight, commonly used for brackets, fittings and structural components.
Airframe brackets, fittings and loaded structural parts
A thick-section plate alloy selected where toughness and stress-corrosion resistance are important.
Large structural plates and thick-section components
A general-purpose aerospace alloy for housings, interior hardware and non-primary structures.
Housings, interior hardware and general aircraft components
A fatigue-resistant airframe alloy for cyclic loading applications where specified.
Fuselage, wing and fatigue-sensitive components
High strength, low density and corrosion resistance make Grade 5 titanium a common aerospace choice, with machining heat carefully controlled.
High-strength brackets, mounts and engine-adjacent hardware
Precipitation-hardening stainless for high-strength fittings and actuation hardware with corrosion resistance.
Fittings, shafts and structural hardware
A strengthened stainless option with improved toughness for highly stressed components where specified.
Highly stressed fittings and structural components
Ultra-high-strength steel for landing gear and highly loaded structural applications, machined with rigid setups and careful finishing.
Landing gear and critical loaded hardware
Heat-treatable high-strength steel for shafts, pins and airframe hardware.
Pins, shafts and structural components
A nickel superalloy that retains strength at high temperature and work-hardens aggressively under the tool.
Engine-adjacent and high-temperature components
A corrosion-resistant nickel alloy used where weldability and environmental resistance are prioritized.
Ducting, exhaust-adjacent and corrosion-resistant hardware
An iron-nickel superalloy used for fasteners and elevated-temperature hardware.
Fasteners and high-temperature components
Very light structural metals for weight-sensitive housings and interiors, quoted with chip and fire-safety controls considered.
Housings and interior components where weight is critical
Aerospace finishing is managed to the supplied specification. Masking, thickness, conductivity, fatigue effects and process certifications are reviewed before release.
Natural or custom color per applicable specification
Sulfuric acid Type II anodizing supports corrosion protection and paint adhesion on aluminum. Clear natural or a custom dyed color is selected with the drawing requirements, masking and acceptance sample.
Aluminum structures, brackets and housings
Type III for wear surfaces
A dense oxide layer improves wear resistance where sliding or repeated contact is expected.
Actuation components, guides and bushings
MIL-DTL-5541 when specified
Conversion coating can provide corrosion protection with electrical conductivity on aluminum surfaces.
Bonding surfaces, under-paint surfaces and conductive interfaces
Qualified supplier certification required
Cadmium plating may be specified for steel aerospace hardware where corrosion protection and lubricity are required.
Steel fasteners and selected hardware
Controlled thickness per drawing
Uniform plating can support corrosion and wear resistance across complex steel or aluminum geometry.
Functional steel and aluminum components
AMS 2700 when specified
Passivation restores stainless corrosion resistance after machining.
Stainless fittings and hardware
Aerospace quality assurance includes dimensional verification, material traceability, special-process records and delivery documentation that can be audited long after shipment.
Customer-specific clauses, AS9100 alignment expectations, ITAR or export-control handling and special records must be supplied with the RFQ for confirmation.
New part numbers can be released with AS9102-style FAI packages, ballooned drawings and complete characteristic accountability when specified.
Mill heat lot, material certificates, work order and finished batch identity are linked to the agreed documentation scope.
Programmed CMM inspection supports geometric tolerances such as true position, profile, flatness and runout with reports delivered as required.
Anodize, plating, heat treatment, coating, NDT and related outside processes are coordinated through qualified suppliers with certifications collected for release.
DFARS, counterfeit prevention, customer-specific quality clauses and export-control instructions are reviewed before quotation and reflected in the release plan when accepted.
Difficult materials, 5-axis structural geometry, documentation, low-volume economics and supplier coordination are handled as one manufacturing problem.
Inconel, titanium, 300M and PH stainless are quoted with the tooling, rigidity and cycle time they actually require.
Thin-wall pockets, compound angles and weight-optimized geometry are planned with distortion control built into the route.
FAI, material certificates and special-process records are assembled during the job rather than reconstructed after shipment.
Prototype, spare and recurring low-volume production work can remain on one controlled manufacturing route.
Qualified finishing, heat treatment, coating and NDT suppliers are coordinated under the agreed purchase-order scope.
Complete RFQs receive an initial engineering response within one working day. Formal quotations follow review of materials, flow-down requirements, inspection scope and delivery timing.
Practical answers about aerospace materials, AS9102 reporting, DFARS sourcing, thin-wall machining, special processes and MRO support.
Aluminum 7075, 7050, 6061 and 2024; titanium Ti-6Al-4V; 17-4 PH and 15-5 PH stainless; 300M and 4340 steels; Inconel 718, Inconel 625 and A286.
Yes, AS9102-style FAI packages with ballooned drawings can be provided when specified with the RFQ and purchase order.
Yes, DFARS or domestic sourcing can be reviewed when specified in the RFQ, with country-of-origin documentation requirements confirmed during quotation.
Thin-wall feasibility is reviewed drawing by drawing. Stress-relieved material, symmetric roughing, controlled fixturing and post-machining verification are used where appropriate.
Yes, special processes can be coordinated through qualified suppliers with certifications delivered as part of the agreed documentation package.
Yes, subject to review. Send the component, drawing or available documentation so material, dimensions and acceptance criteria can be agreed before release.
Single development articles, MRO spares and recurring low- to mid-volume production can be quoted.
NDAs are available before file exchange. Export-control requirements must be identified at RFQ so handling can be confirmed.
