The Macchi M.416 Manuals Collection brings together four official Italian Air Force technical publications covering the M.416 primary trainer — a license-built version of the Dutch Fokker S.11 Instructor produced by Aeronautica Macchi between 1951 and 1958. This structured digital archive provides the primary reference documentation for historians, restorers, and aviation researchers working with this aircraft.
Definitive Collection with Free Lifetime Updates: This is a living collection that we continuously expand and refine. As we acquire additional Macchi M.416 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.416 was a license-built version of the Dutch Fokker S.11 Instructor, produced by Aeronautica Macchi between 1951 and 1958 for the Italian Air Force (Aeronautica Militare) as a primary trainer. Approximately 180 units were produced, serving in military flying schools until 1960 before being transferred to Italian aero clubs. The aircraft was powered by a single Avco Lycoming O-435A F6 six-cylinder air-cooled engine producing 190 hp, and was known for its docile handling characteristics and side-by-side seating arrangement for student and instructor. Its low-wing monoplane configuration with fixed tricycle undercarriage and mixed construction — welded steel tube fuselage with fabric skin and all-metal two-spar wing — made it an ideal platform for primary military flight training in the postwar era.
Manuals Included in This Collection
- Macchi M.416 Aircraft Illustrated Parts Catalog — Catalogo Nomenclatore (Italian Language), CA-774, 1952
- Macchi M.416 Aircraft Flight Manual — Descrizione e Norme di Pilotaggio (Italian Language), CA-773, 1953
- Macchi M.416 Aircraft Erection and Maintenance Manual — Istruzioni per il Montaggio e la Regolazione (Italian Language), CA-772, 1952
- Macchi M.416 Aircraft Erection and Maintenance Manual — Istruzioni per il Montaggio e la Regolazione (Italian Language), CA-807, 1954
This collection spans the core production and service period of the M.416 (1952–1954), covering assembly, regulation, piloting procedures, and parts identification across both the initial and revised maintenance editions.
Engineering Norms and Standards
The M.416 was produced under Italian military airworthiness standards of the early 1950s, inheriting the structural and aerodynamic engineering norms of the Fokker S.11 design. The aircraft's longitudinal stability is ensured by a conventional tail unit with a cantilever horizontal stabilizer. The Lycoming O-435A engine was operated to military specifications for high-altitude training capability. Many surviving M.416 airframes were subject to structural modifications in the late 1950s and early 1960s to address fatigue from intensive training regimes prior to their transfer to civilian aero clubs. The official documentation includes specialized handling instructions for the aircraft's directional rear tailwheel configuration.
Technical Specifications
- Engine: 1× Avco Lycoming O-435A F6, 6-cylinder air-cooled, 190 hp (142 kW) @ 2,500 RPM
- Propeller: Fixed-pitch two-blade wood propeller
- Maximum Speed: 206–207 km/h (111–112 knots)
- Cruising Speed: 164 km/h
- Stalling Speed: 86 km/h (46 knots)
- Range: 515–537 km
- Service Ceiling: 3,800 m
- Climb Rate: 1,000 m in 6 minutes
- Empty Weight: 850 kg | MTOW: 1,135 kg
- Dimensions: Length 8.18 m | Wingspan 10.97 m | Height 2.44 m
Format and Delivery
Instant digital download. All documents are provided as high-resolution PDF files, optimized for screen reading and printing. Files are organized in a clearly labeled folder structure by document type and reference number. Compatible with all standard PDF readers on desktop, tablet, and mobile devices.
Disclaimer
These documents are provided for historical reference and research purposes only. They do not constitute current airworthiness documentation. For any operational or maintenance use on airworthy aircraft, consult current regulatory authorities and qualified aviation professionals. Trade names and designations are used for identification purposes only. This digital compilation, structure, indexing and presentation are © Sicuro Publishing.