A structured digital collection of original factory documentation for the Aermacchi / Macchi MB-308 — the iconic post-WWII Italian light touring and training aircraft. This collection brings together the essential technical and operational manuals in a single, organized download.
Definitive Collection with Free Lifetime Updates
This is a living collection that we continuously expand and refine. As we acquire additional MB-308 documentation, technical bulletins, or variant-specific materials, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.
Historical Note
The Macchi M.B.308 — affectionately nicknamed Macchino — is a post-WWII Italian light touring and training aircraft designed by Ermanno Bazzocchi. Its development was pivotal in the revitalization of the Italian civil aviation industry following the war. The first flight occurred on January 19, 1947, and the type quickly gained recognition for its sleek lines, all-wood construction (in early models), and cantilever high-wing design.
Powered initially by a 60 HP CNA engine, production variants later adopted the Continental C85 and C90 air-cooled flat-four engines, giving the aircraft a maximum speed of 197 km/h and a range of 760 km. The MB-308 served Italian flying clubs extensively, with a seaplane floatplane variant (MB.308 Idro) also produced. A later variant, the MB.308G, was produced and exported to Argentina, where some examples were further modified with Fairchild M.62 wings and alternative powerplants.
The type is remembered as a responsive yet forgiving trainer, well-suited to smaller airfields, and a participant in European touring races of the era. Surviving examples continue to fly today, preserved by enthusiasts across Italy and South America.
Manuals Included in This Collection
- Aermacchi MB-308 Aircraft Illustrated Parts Catalog — Manuale Nomenclatore (Italian Language) — 1949
- Aermacchi MB-308 Aircraft Flight Manual — Descrizione Norme Di Pilotaggio (Italian Language) — C.A. 721 — 1940
This collection covers the core operational and maintenance documentation for the MB-308, spanning the aircraft's initial production and early service period from 1940 to 1949.
Engineering Norms and Standards
The MB-308 was designed and produced under Italian civil aviation regulations of the post-war era, with engineering practices reflecting Aermacchi's (Aeronautica Macchi) established tradition of efficient, aerodynamically clean light aircraft design. Key engineering characteristics include:
- Cantilever single-spar high-wing structure, primarily wood construction
- Continental C85 air-cooled flat-four engine (85 HP), later C90 variants
- Fixed-pitch propeller optimized for touring performance
- Fuel capacity: approximately 80 litres (21 US gal)
- Wingspan: 10.00 m | Length: 6.53 m | Wing Area: 13.72 m²
- Empty Weight: ~410 kg | Gross Weight: ~650 kg
- Maximum Speed: 197 km/h | Cruise Speed: 164 km/h at 70% power
- Service Ceiling: 4,500 m | Range: 760 km
- Crew: 2 (side-by-side seating)
Format and Delivery
Instant digital download. All documents are provided as high-resolution PDFs, optimized for screen reading and printing. Compatible with all standard PDF readers on desktop, tablet, and mobile devices.
Disclaimer
These documents are provided for historical reference and research purposes only. For any airworthiness, maintenance, or operational decisions on currently flying aircraft, always consult the current Type Certificate holder and applicable regulatory authority. Trade names and designations are the property of their respective owners. This digital compilation, structure, indexing and presentation are © Sicuro Publishing.