Structural floor track (transport aircraft)
Deep I- or T-section tracks that act as floor members, with a slotted crown on top. Produced to the airframe maker's drawing in 7075, 7050 or 7150 over-aged tempers, or titanium in wet zones.
An aircraft seat track is a high-strength aluminium extrusion with a slotted crown, set into the cabin floor so that seats, galleys and cargo fittings can be locked at any 1-inch position. It is both a mounting rail and part of the floor structure, and must hold seats in place under crash loads. Metline supplies seat-track extrusions and machined tracks in 7075, 7050, 7150 and 6061, plus airline-style L-track for vehicles, to customers worldwide.

A seat track looks simple: a rail with a row of circular openings joined by a narrow slot. Seat legs carry stud fittings that drop through the openings, slide half a pitch and lock under the lips of the crown. Because the openings repeat every inch, an operator can change seat pitch or cabin layout without drilling the floor.
In transport aircraft the tracks are much more than rails. They run fore and aft across the floor beams, carry the floor panels at their edges, and transfer seat loads in turbulence and emergency landings into the fuselage. Certification rules require seats and their attachments to withstand high static and dynamic crash loads, so the track crown, its lips and its attachment to the beams are all sized for those cases.
The same track profile, in lighter alloys, is widely used outside aviation as "airline-style" or L-track for securing cargo in vans, trailers, rail cars and race transporters, and for wheelchair tie-downs in buses. Metline supplies both the aerospace and the commercial versions; the material and certification requirements are very different, so it is important to say which you need.
Deep I- or T-section tracks that act as floor members, with a slotted crown on top. Produced to the airframe maker's drawing in 7075, 7050 or 7150 over-aged tempers, or titanium in wet zones.
Lower-profile track bolted on top of a floor or structure, used in business jets, helicopters, light aircraft and modifications.
Adjustable pilot and passenger seat rails with pin holes or slots, often in 6061-T6 or 2024-T3511.
Flush or surface-mounted track for cargo nets, tie-down rings and pallets in freighter and combi cabins.
Surface or flush-mount track for vans, trailers, trucks and buses; usually 6061-T6 or 6005A-T6, mill finish or anodised.
Commercial track with sloped edges so that wheeled loads roll over it without catching.
Aerospace seat tracks are drawn to the airframe maker's or customer's drawing, but most share a common crown pattern so that standard seat fittings can be used.
Dimensions are typical. Always check track geometry against the seat or fitting maker's drawing; small differences in crown depth or lip width can prevent fittings from locking.
Openings can be machined in the extrusion, or the extrusion can be supplied plain for the customer to machine. Machining after extrusion and heat treatment is normal, followed by deburring and corrosion protection of the cut edges.
| Alloy-temper | Typical use | Why |
|---|---|---|
| 7075-T73511 | Aircraft seat and floor tracks | High strength with good stress-corrosion resistance |
| 7075-T6511 | Surface-mounted and light-aircraft tracks | Peak strength where stress-corrosion risk is low |
| 7050-T76511 / T74511 | Floor tracks on modern airframes | Good strength, toughness and corrosion resistance |
| 7150-T77511 | Highly loaded floor tracks and beams | High strength with improved exfoliation resistance |
| 2024-T3511 | Light-aircraft seat rails, legacy tracks | Good fatigue properties |
| 6061-T6 / T6511 | Commercial L-track, cargo track, light aircraft | Economical, corrosion resistant, anodises well |
| 6005A-T6 / 6351-T6 | Commercial vehicle and bus tracks | Good extrudability with moderate strength |
An earlier version of this page also listed 5083 and 6063. These are not suitable for load-rated seat track: 5083 is not normally extruded into such complex hard shapes, and 6063 is too weak for crash loads. Titanium is preferred in the wettest floor zones of some airliners because aluminium tracks there are prone to corrosion.
| Area | Document | What it governs |
|---|---|---|
| Material | AMS-QQ-A-200/11 (7075), AMS 4340-series (7050), AMS 4345 (7150), ASTM B221 | Chemistry, temper, mechanical properties of the extrusion |
| Tolerances | ANSI H35.2, customer drawing | Cross-section, straightness, twist |
| Fittings interface | MS33601 / AS33601 | Stud-fitting pattern that the track must accept |
| Seat strength | 14 CFR 25.561 and 25.562; SAE AS8049; FAA TSO-C127 | Static and dynamic crash loads that seats and attachments must survive |
| Anodising | MIL-A-8625 Type II (sulphuric) or Type I (chromic) | Corrosion protection and wear surface |
| Quality | AS9100 supply chain where the buyer requires it; EN 10204 3.1 certificates | Traceability from cast to finished track |
For installation on a certificated aircraft, the track must also be an approved part for that aircraft, through the type design, a supplemental type certificate, a parts manufacturer approval or a field approval. Raw extrusion supplied to a material specification is not in itself an approved aircraft part.
CNC machining of openings, fastener holes and end features to the drawing pattern, with pitch checked over the full length.
Square, deburred ends; jig holes and alignment features on request.
Clear or black sulphuric anodising for commercial track; chromic or boric-sulphuric anodising for aerospace parts through qualified processors.
Corrosion-inhibiting primer and sealant on machined edges for tracks in wet zones.
Dimensional, pitch, straightness and conductivity checks; first article inspection for new part numbers.
Part, alloy, temper and lot identification for traceability.
Seat tracks sit at the lowest point of the cabin floor, so spilled drinks, cleaning fluids and condensation collect around them. The areas next to galleys, lavatories and doors are the most common sites of seat-track corrosion found during heavy maintenance checks.
1.000 in (25.4 mm) between opening centres, which lets seats and fittings be positioned in 1-inch steps.
High-strength 7xxx alloys in over-aged tempers, such as 7075-T73511, 7050-T76511 or 7150-T77511. Some aircraft use titanium tracks in wet areas.
Yes. Airline-style L-track in 6061-T6 or 6005A-T6 is common for cargo securing. Choose fittings and fasteners rated for the loads you need to restrain.
Not by itself. Material certified to a specification must still be made into a part approved for the specific aircraft through its type design, an STC, PMA or field approval.
Fluids collect around them near galleys, lavatories and doors. Over-aged tempers, sealing, drainage and track covers reduce the risk.
Yes. Openings, fastener holes and end features can be CNC machined to your drawing, or plain extrusion can be supplied for your own machining.
Tell us whether it is for aircraft or vehicle use, with the profile, alloy, length and finish. We will confirm supply and certification.