Product Category
AUV — 001 to 013
Aerospace &
UAV High-
Precision Parts
13 product lines covering the full spectrum of aerospace and unmanned aerial vehicle structural parts — from TC4 titanium lightweight brackets and aerodynamic surface structures to UAV motor mounts, gimbal housings, arm connectors, and flight controller frames. Every gram matters. Every dimension is held.
TC4 Ti-6Al-4V
950 MPa
ASTM B265 · 40% lighter than steel · Aerospace standard
Wall Thickness
0.8 mm min
Lightweight pocketed structures in Ti and Al7075
Dimensional Tolerance
±0.005 mm
Critical bores, bearing seats, and alignment features
Flatness
±0.005 mm
Mounting faces, datum surfaces, instrument bases
Surface Profile (Aero)
±0.01 mm
Aerodynamic profile surfaces from 3D CAD model
13
Product Lines
TC4 / Al7075
Aerospace Grade
±0.005mm
Key Tolerance
5-Axis
Simultaneous CNC
24hr
Quote Turnaround
Aerospace Lightweight Brackets ✦
Complex Lightweighted Structures ✦
Engine Peripheral Mounts ✦
Aerospace Connectors ✦
Instrument Mounting Seats ✦
Flight Controller Structures ✦
UAV Motor Mounts ✦
Gimbal Housings ✦
Arm Connector Seats ✦
Landing Gear Connectors ✦
TC4 Lightweight Parts ✦
Aerodynamic Surface Structures ✦
High-Strength Skeleton Frames ✦
Aerospace Lightweight Brackets ✦
Complex Lightweighted Structures ✦
Engine Peripheral Mounts ✦
Aerospace Connectors ✦
Instrument Mounting Seats ✦
Flight Controller Structures ✦
UAV Motor Mounts ✦
Gimbal Housings ✦
Arm Connector Seats ✦
Landing Gear Connectors ✦
TC4 Lightweight Parts ✦
Aerodynamic Surface Structures ✦
High-Strength Skeleton Frames ✦
Full Product Range
13 Aerospace & UAV
High-Precision Product Lines
Select a category tab · All parts machined to drawing · MOQ 1 piece · CMM inspection standard
Product Categories
Aerospace-grade lightweight structural brackets, engine peripheral mounting components, structural connectors, instrument mounting seats, and flight control system frames. All parts machined from AMS-grade aluminium alloys (Al7075-T651, Al7050) or titanium (TC4 / Ti-6Al-4V ASTM B265). Full material traceability. CMM dimensional report standard. AS9100-aligned documentation available.
AUV-001
AEROSPACE STRUCTURAL / 001 — FEATURED
Aerospace Lightweight Brackets
Structural mounting brackets and support frames for airframe, avionics bay, and engine nacelle applications. FEA-optimised pocket geometry removes maximum mass while maintaining stiffness along load paths. Machined from Al7075-T651 stress-relieved plate — no post-machining distortion. Flatness ±0.005 mm on mounting faces. All fastener hole patterns position-toleranced to ±0.008 mm. Hard anodize Type III for surface protection. Full material certificate and CMM report with every order.
Al7075-T651 · Al6061-T651 · TC4 Ti
Get Quote
AUV-002
AEROSPACE STRUCTURAL / 002
Engine Peripheral Mount Parts
Accessory mounting flanges, sensor bosses, and support brackets surrounding aircraft engines and UAV powerplants. High-temperature alloys where required. Vibration-tolerant fastener patterns. Engine case conformity clearance verified.
Al7075 · TC4 · Inconel · SSGet Quote
AUV-003
AEROSPACE STRUCTURAL / 003
Aerospace Structural Connectors
Spar connectors, rib attachment brackets, and panel structural node connectors. Multi-face geometry machined in one 5-axis setup. Load-path alignment within ±0.01 mm. Shear lug and bolt-bore features to tight positional tolerance.
Al7075 · Al7050 · TC4 · SS17-4PHGet Quote
AUV-004
AEROSPACE STRUCTURAL / 004
Instrument Mounting Seats
Avionics bay instrument mounting frames, sensor brackets, and gyroscope isolation mounts. Hole-pattern position ±0.008 mm. Vibration-isolation surface geometry machined per isolator datasheet dimensions. Invar option for thermal stability.
Al6061 · Al7075 · Invar36Get Quote
AUV-005
AEROSPACE STRUCTURAL / 005
Flight Controller Structural Parts
Flight computer mounting plates, autopilot baseframes, and IMU isolation structures. High-flatness datum face ±0.003 mm for IMU alignment. Non-magnetic materials where magnetic compass interference must be avoided.
Al6061 · TC4 · PEEK · BrassGet Quote
UAV motor mounts, gimbal housings, arm connector seats, and landing gear attachment parts — machined from Al7075 and TC4 titanium for maximum stiffness-to-weight. Motor mount perpendicularity directly affects rotor thrust vectoring and hover stability. Arm connectors require tight coaxiality and rotational stop accuracy. All UAV parts supplied with mass verification — weight deviation >3% from design triggers DFM review before delivery.
AUV-006
UAV & DRONE / 006 — FEATURED
UAV Motor Mounts
Brushless motor mounting seats for multirotor and fixed-wing UAV propulsion systems. Motor face perpendicularity to arm axis ≤0.01 mm — directly determines rotor thrust vector alignment and hover efficiency. Motor bolt-pattern position ±0.005 mm. Integral ESC cable management channel and heat-dissipation fin geometry machined from Al7075-T6 billet. Vibration-damping thread insert pattern available. Mass verified — target weight within ±3% of design model. Hard anodize Type III standard for all motor mounts.
Al7075-T6 · Al6061 · TC4 TiGet Quote
AUV-007
UAV & DRONE / 007
Gimbal Housings
2-axis and 3-axis camera gimbal yoke and shell bodies. Motor seat coaxiality ≤0.005 mm for smooth gimbal axis rotation. Thin-wall pocketed design — typically 1.2 mm wall in Al7075. Balance-optimised geometry to minimise gimbal inertia.
Al7075 · TC4 · CF InsertGet Quote
AUV-008
UAV & DRONE / 008
UAV Arm Connector Seats
Central hub arm socket bodies for quick-fold and fixed-arm UAV frames. Arm bore perpendicularity to hub plane ≤0.01 mm. Rotational locking geometry and alignment detent machined integral. Clamp force calculated for specified arm preload.
Al7075 · Al6061 · TC4Get Quote
AUV-009
UAV & DRONE / 009
Landing Gear Connector Parts
Landing leg attachment hinge bodies, skid clamp brackets, and retractable gear pivot housings. Pivot bore H7; hinge axis parallelism ≤0.01 mm. Impact-load tested geometry — stress concentration eliminated by full-radius fillet machining at all transition points.
Al7075 · TC4 · Al6061Get Quote
TC4 (Ti-6Al-4V, ASTM B265 Grade 5) is the aerospace standard titanium alloy — 950 MPa tensile strength at 4.43 g/cm³, 40% lighter than an equivalent steel part of the same stiffness. Complex lightweighted pocketed TC4 structures and integral high-strength skeleton frames where aluminium alloys lack sufficient specific strength. 5-axis simultaneous machining from solid billet — no casting porosity, no weld stress, full material property throughout. ASTM B265 mill certificate standard.
AUV-010
TC4 LIGHTWEIGHT / 010 — FEATURED
TC4 Lightweight Structural Parts
FEA-topology-optimised TC4 Ti-6Al-4V structural components where mass reduction is the primary design driver — fuselage frames, spar lug fittings, and high-load attachment brackets that must be as light as possible while meeting flight load requirements. Pocketed geometry with wall thickness from 0.8 mm; internal radius ≥R1.0 mm to maintain titanium machinability and prevent stress concentration. Mass verified at ±3% of design target. Machined from ASTM B265 Grade 5 billet with full mill certificate. 5-axis continuous toolpath on all pocket interior surfaces to achieve Ra ≤0.8 μm without secondary finishing.
TC4 Ti-6Al-4V (ASTM B265 Grade 5)Get Quote
AUV-011
TC4 LIGHTWEIGHT / 011
Complex Lightweighted Structural Parts
Organic-geometry TC4 lightweight structures where every non-load-bearing gram has been removed — rib-and-web architectures, variable-wall-thickness flanges, and lattice-style structural cores machined from solid billet. 5-axis access to all interior pocket features.
TC4 Ti-6Al-4V · Ti Grade 2Get Quote
AUV-013
TC4 LIGHTWEIGHT / 013
High-Strength Skeleton Frame Parts
Integral one-piece TC4 skeleton frames replacing welded or riveted multi-part assemblies. No joint fatigue failures. Continuous load path through monolithic structure. Complex 3D geometry requiring 5-axis machining throughout. CMM full 3D inspection.
TC4 Ti-6Al-4V · Al7075Get Quote
Curved aerodynamic surface structural parts and high-strength one-piece skeleton frame components — the two most geometrically demanding product types in aerospace CNC machining. Aerodynamic profiles machined from 3D model with surface deviation ≤0.015 mm from nominal CAD surface. Skeleton frames designed as monolithic replacements for multi-part riveted or welded assemblies, eliminating joint fatigue failures and reducing assembly count.
AUV-012
AERO PROFILES / 012 — FEATURED
Curved Aerodynamic Surface Structures
Airfoil-contoured structural parts, fairings, nacelle panels, and aerodynamic surface sections where the outer surface geometry is functionally critical to drag and lift performance. Surface profile deviation from CAD nominal ≤0.015 mm, verified by CMM scan vs CAD surface. Continuous 5-axis toolpath maintains constant tool-to-surface orientation across compound curvature — no faceted step-over marks from 3+2 repositioning. Scallop height controlled to ≤0.005 mm for smooth aerodynamic surface. Leading-edge radius machined to R0.5 mm without manually polished blend. Deviation colour map report included.
Al7075 · Al2024 · TC4 Ti · Carbon InsertGet Quote
AUV-013
AERO PROFILES / 013
High-Strength Aerospace Skeleton Frames
One-piece integral skeleton body frames replacing multi-part riveted assemblies. Continuous load path from single material. No joint fatigue initiation sites. Complex 3D geometry requiring 5-axis machining. Weight controlled to ±3% of design target. CMM full 3D GD&T report.
Al7075 · Al2024 · TC4 TiGet Quote
Manufacturing Capability
What Aerospace & UAV Parts
Demand from a Machining Partner
⚙
5-Axis Simultaneous — All Faces from One Datum
Aerospace structural parts with features on 4–6 faces require 5-axis simultaneous machining from a single datum to maintain inter-feature positional accuracy ±0.008–0.01 mm. Re-fixturing to a second setup compounds error across all subsequent features.
5-Axis simultaneousSingle datum±0.008mm inter-feat.
📐
FEA-Guided Pocket Geometry & Mass Verification
Lightweight structures are machined to customer FEA topology output or to our DFM-suggested lightweighting geometry. Every part weighed against the design mass target — deviation >3% triggers DFM review. We don't guess on aerospace parts.
FEA topology-guidedMass ±3% verifiedDFM review trigger
◆
TC4 Titanium Machining — Dedicated Protocol
Titanium requires reduced cutting speed, high feed rate, and continuous coolant flood — very different from aluminium. We have dedicated TC4 machining protocols: premium TiAlN-coated carbide, minimum chip recutting, and temperature-monitored operations to prevent surface work-hardening.
TiAlN carbideFlood coolantNo recutting
🔬
CMM Full GD&T Report + Deviation Map
Every aerospace part inspected with full GD&T CMM report per AS9102 FAI requirements. Aerodynamic surface parts additionally receive a surface deviation colour map comparing measured surface to CAD nominal — max, min, and RMS deviation reported.
AS9102 FAI formatGD&T all calloutsDeviation colour map
📋
Material Traceability — Mill Cert to Part
AMS-grade material certificates (chemical composition, mechanical properties, heat number) received and logged before first cut. Process traveller links material lot to every machined part. Traceability supports AS9100 supplier audit requirements and incident investigation.
AMS grade certsHeat number logAS9100 ready
💨
Aerodynamic Surface Machining — Controlled Scallop
Aerodynamic surfaces machined with controlled scallop height ≤0.005 mm — specified at CAM programming, not as a post-machining hope. 5-axis continuous toolpath maintains tool normal to surface throughout to ensure uniform scallop height across compound curvature transitions.
Scallop ≤0.005mmNormal to surfaceNo transition steps
Precision Specifications
Tolerances & Standards — Aerospace & UAV Parts
📐
Achievable Tolerances by Feature
General Bore / OD
±0.005 mm
Hole Pattern Pos.
±0.008 mm
Mount Face Flatness
±0.005 mm
Motor Perp. (UAV)
≤0.01 mm
Aero Surface Dev.
≤0.015 mm
Scallop Height
≤0.005 mm
Min Wall (Ti)
0.8 mm
Mass Tolerance
±3% target
🔬
Material & Compliance Standards
Titanium Grade
ASTM B265 Gr5
TC4 Ti-6Al-4V. Full mill cert + chemical composition with every lot.
Aluminium Standard
AMS 2770
Al7075-T651 and Al6061-T651. Stress-relieved plate stock standard.
Quality System
AS9100
AS9100-aligned documentation. FAI per AS9102 available on request.
Inspection Standard
AS9102
First Article Inspection format on all aerospace part numbers.
Surface Treatment
MIL-A-8625
Hard anodize Type III per MIL-A-8625. Chromate conversion available.
CMM Report
GD&T / ISO 1101
Full GD&T report. Deviation colour map for aerodynamic surfaces.
Material Selection
Key Materials for Aerospace & UAV Applications
Scroll to browse all aerospace-grade materials stocked and machined in-house.
MAT / 01
TC4 Ti-6Al-4V
ASTM B265 Grade 5 · 950 MPa · 4.43 g/cm³
Aerospace standard titanium. 40% lighter than equivalent steel structure. Highest specific strength for structural aerospace parts where Al lacks strength. Anodize, passivation, and PEO coating available.
MAT / 02
Al7075-T651
AMS 2770 · 503 MPa · 2.81 g/cm³ · Stress-Relieved
Highest-strength aluminium — standard for aerospace brackets, drone frames, and lightweighted structures. T651 stress-relieved plate eliminates post-machining distortion. Hard anodize T3 standard.
MAT / 03
Al2024-T351
AMS 2770 · 470 MPa · Fatigue-Resistant
Superior fatigue resistance vs 7075 — preferred for parts subjected to cyclic loading (wing attach fittings, landing gear structural parts). Clad or anodized for corrosion protection.
MAT / 04
SS17-4PH H900
1,100 MPa · AMS 5643 · Corrosion Resistant
High-strength stainless for aerospace connectors and fittings exposed to moisture, jet fuel, and hydraulic fluid. Best combination of strength and corrosion resistance in stainless steels.
MAT / 05
Invar 36
CTE 1.2 ppm/K · Thermally Stable
Ultra-low CTE for instrument mounting seats and avionics reference frames where dimensional stability across −55°C to +85°C temperature range is critical for sensor alignment accuracy.
MAT / 06
Inconel 718
AMS 5662 · 1,380 MPa · Up to 700°C
Nickel superalloy for engine peripheral mounts, hot-section brackets, and exhaust-adjacent structural parts. Retains full mechanical properties at elevated temperature where aluminium and standard steel would fail.
Production Workflow
From Drawing to AS9100 Documented Part
01
DFM Review
Geometry, mass target, material grade, and traceability requirements confirmed. 24h response.
02
Material Receipt
AMS/ASTM mill cert received, heat number logged to process traveller before first cut.
03
5-Axis Machining
All features machined in single setup where possible. TC4 dedicated protocol for titanium operations.
04
Mass Verification
Every part weighed vs design target. Deviation >3% triggers DFM review — not silently shipped.
05
CMM Inspection
Full GD&T CMM report per AS9102 FAI. Deviation colour map for aero surface parts.
06
Documentation
CMM FAI, mill cert, surface treatment cert, mass record, and process traveller — full AS9100 pack.
Our Advantage
Why Aerospace Engineers Specify Our Parts
TC4
TC4 Titanium Expertise — Dedicated Protocol
Dedicated TC4 machining protocol: TiAlN carbide, flood coolant, no chip recutting, temperature-monitored operations. Not adapted from aluminium settings — a purpose-built process that prevents surface work-hardening and achieves design-specification surface finish without rework.
±3%
Mass Verified — Every Part, Every Time
Every aerospace and UAV part weighed against the design mass target. Deviation >3% triggers DFM review — not delivered and left for the customer to discover at integration. Mass control is the discipline that separates aerospace machining from general precision machining.
FAI
AS9102 First Article Inspection — Every New Part Number
Full GD&T CMM report formatted to AS9102 FAI requirements on every new aerospace part number. Traceability from material mill cert through process traveller to CMM report. Documentation ready for your AS9100 supplier audit — no reformatting required.
0.005
Aero Surface Scallop Controlled — Not Assumed
Scallop height on aerodynamic surfaces specified at CAM programming stage and verified by CMM scan vs CAD nominal. Deviation colour map included with delivery — showing exactly where the surface is relative to design intent, not just whether a set of coordinate measurements pass.
Get a Quote
Send Your Drawing.
Get a Quote.
Every enquiry includes a DFM review — tolerance feasibility, material confirmation, and process approach confirmed before production starts. MOQ 1 piece.
24hr
Quote Response
MOQ 1
Prototypes OK
ISO
9001:2015
📐
DFM Review on Every Enquiry
Tolerance feasibility, fixturing strategy, and material confirmation. Specific, actionable feedback — not generic pushback.
🎯
First Article Inspection — Standard
FAI report on every new run. Material certs and surface treatment certs included with every shipment.
🔄
Same Process: Prototype to Production
Process plan from your prototype applies to production batches. No re-qualification when you scale.
⚙
3 / 4 / 5-Axis CNC + Turning
Complex structural parts, shafts, housings, and transmission components. Metals and engineering plastics.
ISO 9001:2015
3/4/5-Axis Milling
CNC Turning
CMM Inspection
Global Delivery