Steel Structure
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You do not need a construction crew living on your airfield for a year to build a steel aircraft hangar. You need a prefabricated building that shows up ready to bolt together.
Our prefab hangar kits are manufactured complete in-factory — steel frame, cladding, doors and fasteners — then container-shipped to your port. Because every beam is pre-cut and every hole is pre-drilled, a local crew can stand the primary structure in weeks rather than months. No field welding on the primary frame, no surprise material delays, no weather hold-ups. The result is a clear-span structure with zero interior columns, so every square metre of floor is usable.
The modular design works for private aircraft storage, helicopter operations, multi-bay FBO hangars and rapid-deployment shelters. And if you outgrow the first bay, the end walls are engineered for expansion — add a bay later without touching the original structure.
This page covers the prefab kit route: 20–60 m clear span, container-shipped, bolted on site. For heavy spans of 60–180 m carrying wide-body aircraft and overhead cranes, see our large-span aircraft hangar. For a single light aircraft at 12–30 m, the small airplane hangar is the cheaper answer.

Most hangar enquiries we receive cannot be priced, because one of these six is missing. If you send all six, you get a budget figure and a structural concept in about two working days — and a much more useful conversation than a generic price list.
If you only have two or three of these, send what you have. We will tell you what is still missing rather than guess.
We build several hangar types and they are not interchangeable. Most buyers who arrive on this page are looking for one of four things, and the differences are structural, not cosmetic.
| If this is your situation | What you need | Why |
|---|---|---|
| One to four light aircraft — piston, light turboprop, light helicopter — stored by the owner | Small airplane hangar (12–30 m) | A 20 m clear span is wasted money on a single Cessna. Smaller spans also mean a lighter foundation and a smaller door. |
| A kit that ships in containers and is bolted together by a local crew, at 20–60 m span | This page — prefab hangar kit | Pre-drilled, numbered, trial-fitted members. The kit format is what makes a non-specialist crew viable. |
| Aircraft are parked and nothing else happens inside | Aircraft storage hangar | Storage is a loading problem, not a services problem. You should not be paying for MRO infrastructure. |
| Wide-body aircraft, D-check, engine removal, overhead cranes across the full floor | Aircraft hangar (60–180 m) or maintenance hangar | Above roughly 60 m the roof stops behaving like a beam. A rigid portal frame alone becomes uneconomic — you need a truss or space-grid roof, and a different procurement conversation. |
If you are not sure which of these applies, our hangar sizing and local code guide walks through scenario layouts and the wind, snow and corrosion requirements that change by region.

A prefab hangar kit is only “prefab” up to a clearly defined line. Knowing where that line falls is what prevents a scope dispute three months later.
Included, manufactured and inspected before shipment:
Not included — and not hidden in the price:

Sizing a hangar is three decisions, and only the first one is about the aircraft you own today.
Span — set by wingspan plus maneuvering room. As a working starting point: single-engine piston aircraft need 12–18 m; twin turboprops such as a King Air or PC-12 need 18–25 m; corporate jets need 25–40 m; helicopters need the main rotor diameter plus 2–3 m of operating clearance. Our prefab kit range covers 20–60 m (66–197 ft) clear span without interior columns. Plan for the aircraft you expect to own in five years — resizing later is far more expensive than allowing for it now.
Eave height — set by the tallest tail, not by the fuselage. Our standard range is 4–15 m (13–49 ft). A tail-dragger parked nose-down, or a helicopter with the rotor head up, is often taller than buyers expect. The cost difference between 7 m and 9 m of eave height is small at design stage and large as a variation.
Door — the component most likely to be specified wrong. Sliding doors are the economical choice and suit openings up to about 30 m wide, hung from the top or rolling on a bottom track. Bi-fold doors give a full-height opening with no ground track across the apron, which matters for tail clearance and for sites that get snow. Stacking doors handle very wide openings with minimal load on the frame. Vertical-lift doors suit smaller helicopters and general aviation. All four are engineered to the same wind and sealing requirement as the building envelope — a door that leaks wind is a structural load path, not just a draught.

Every prefab hangar is built on a rigid portal frame of welded H-beam columns and rafters, engineered for the specific span, height and load case of your site.
| Component | Options |
|---|---|
| Roof panels | Corrugated steel, standing seam, or insulated sandwich panels |
| Wall panels | Single-skin corrugated steel, EPS sandwich panels, or rock wool fire-rated panels |
| Insulation | Fiberglass batts, rigid board, or insulated panel systems (R-19 to R-30+) |
| Doors | Sliding, bi-fold hydraulic, stacking, or vertical lift — custom sized |
Hangar columns are anchored to reinforced concrete foundations through embedded base plates and high-strength anchor bolts. Because a steel frame weighs far less than a concrete equivalent, the foundation carries less — on comparable projects this reduces foundation cost by roughly 30–50% against conventional construction. We supply the anchor bolt layout and the reaction loads; the design of the footing itself belongs to your local engineer, who knows the soil.
This is the section most suppliers leave out.
None of these disqualify the building. They disqualify the timing or the page — and it is cheaper to find that out before fabrication than after delivery.
The same kit is specified differently depending on where it lands. Two markets we now ship to in volume illustrate how much the local conditions matter.
Aircraft hangars in the US are reviewed under rules that do not exist in most other markets. 14 CFR Part 77 governs the imaginary surfaces around an airport, which sets the maximum height of the structure and can drive the whole design. Height and location may require a notice filing with the FAA on Form 7460-1 before construction — that is your airport’s or your consultant’s filing, but the building height comes from it. Structurally we design to IBC with ASCE 7 wind, snow and seismic loading, and where the hangar falls under NFPA 409 the fire-area classification determines the suppression requirement and what the structure has to be built to.
Practical consequences: ground snow load drives purlin spacing and rafter depth more than wind in the northern states, and a project that is straightforward in Arizona can be a different structure in Michigan. We issue the structural calculation package for a US-licensed engineer to review and stamp, and we ship to the port you nominate rather than the country.
Saudi Arabia’s National Aviation Strategy targets 330 million passengers a year by 2030 — roughly triple the pre-pandemic figure — together with more than 250 international destinations, air cargo capacity of 4.5 million tonnes, and local MRO covering 80% of the national fleet. That programme produces hangar demand in places where the design brief is nothing like a European one.
The building has to answer three local conditions:
We design to the loading requirements of the Saudi Building Code and supply documentation suitable for review by the General Authority of Civil Aviation and your local engineer.
We have shipped to more than 100 countries and can tell you what we have seen approved in a given market — but the local authority always makes the final call. Treat our answer as a starting point for your engineer, not a substitute for one.

The deliverable is not “a container of steel”. It is a documented package that a local crew and a local authority can both work from.
Fabrication typically runs 6–12 weeks from frozen drawings. On-site assembly of the frame and cladding runs 2–6 weeks depending on hangar size and crew proficiency — pre-cut and pre-drilled members are bolt-connected, with only minimal field welding for adjustments. Phased shipping can overlap the two if the programme is tight. Certificates and test reports are listed on our certificates page, and factory and workshop detail is on the production workshop page.
Width is wingspan plus maneuvering clearance, and it is worth planning for the aircraft you expect to own rather than only the one you own now. Working guidelines: single-engine piston aircraft (Cessna 172, Piper Cherokee) need 12–18 m; twin turboprops (King Air, PC-12) need 18–25 m; corporate jets (Citation, Learjet, Gulfstream) need 25–40 m; helicopters need the main rotor diameter plus 2–3 m. Our kits cover 20–60 m clear span. Resizing during initial design is inexpensive; resizing a fabricated frame is not.
A prefab hangar is a kit building sold on span, door and enclosure — it shelters aircraft. A maintenance hangar is sold on floor loading, crane coverage, ventilation and fire classification, because the work happening inside it drives the structure. If your aircraft are parked and inspected between flights, this page is the right product. If they are stripped down, jacked, or engines come off, go to the maintenance hangar page — the structure is genuinely different, not just more expensive.
Four systems, and the choice is driven by opening width, apron space and climate. Sliding doors are the most economical and suit openings to about 30 m wide. Bi-fold doors open full height with no ground track, which matters for tail clearance and for snow-covered aprons. Stacking doors handle very wide openings with low load on the frame. Vertical-lift doors suit smaller helicopters and general aviation aircraft. Decide the door before fabrication — changing it afterwards is the most expensive variation on the project.
Engineering and fabrication typically require 6–12 weeks from frozen drawings. On-site assembly of the frame and cladding takes 2–6 weeks depending on size and crew proficiency. Components arrive pre-cut, pre-drilled and trial-fitted; assembly is predominantly bolted, with minimal on-site welding for adjustments. The 2–6 weeks is on-site work only — it is not the total programme. For urgent projects, phased shipping can overlap fabrication and site work.
Yes, and it is most of what we do. We ship complete kits in sea-worthy containers to the port you nominate — send us the nearest port rather than just the country, because the overland leg frequently exceeds the ocean freight and long spans can become out-of-gauge loads that will not travel certain routes. We provide full export documentation and remote or on-site assembly guidance, and we design to your local code including IBC and ASCE 7 (USA), Eurocode (Europe), and the national standards of Asia, Africa, the Middle East and Latin America. Permit approval remains the responsibility of locally licensed engineers and municipal authorities.
Yes. Helicopter designs have to account for main rotor diameter, tail rotor overhang and vertical clearance, and eave heights of 6–15 m accommodate most civil rotorcraft. The column-free interior allows 360-degree maneuvering without obstructions. Two things to raise at enquiry stage: whether the rotor head height exceeds a standard eave, and whether you want a vertical-lift door for a narrow opening or a full-width opening for ground handling.
Yes, but it must be specified at design stage. End walls can be engineered as expandable, allowing additional bays or length to be added later without disturbing the existing structure. This costs very little to allow for at the outset and a great deal to retrofit — if fleet growth is even a possibility, say so before drawings are frozen.
Cost is driven by four variables, in roughly this order: clear span, eave height, door system, and site wind and snow loads. Those four move the price far more than the choice of cladding supplier. Send us the six numbers listed at the top of this page and we will return a budget figure with the scope of supply stated explicitly, so you are comparing the same package. Company background is on our about us page.
A prefab hangar is not just a building — it is the ground infrastructure that protects your aviation assets. From private aircraft storage and helicopter hangars to multi-bay FBO facilities, Canglong Group delivers steel hangar kits engineered to your local code, manufactured complete in-factory and shipped in containers to your port.
With 20–60 m column-free clear span, pre-drilled and trial-fitted members, and export engineering across more than 100 countries, you get the structural confidence your aircraft deserve — with the engineering, the drawings and the delivery schedule you are actually going to be held to.
See all our steel hangar types, or contact Canglong Group with your six numbers for a budget figure and a structural concept on your prefab aircraft hangar project.
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Canglong projects cover more than 120 countries and regions around the world, providing one-stop steel structure building solutions from design to installation.