Historical Turbomeca Marboré engine documentation

A specialist digital reference collection for the Turbomeca Marboré family, the French single-spool centrifugal-flow turbojet that powered generations of post-war jet trainers and liaison aircraft.

The Marboré entered service in the early 1950s after its first bench run in December 1950 and maiden flight on 16 June 1951 aboard the Fouga Gémeaux. It evolved from the Turbomeca Piméné and Palas and was produced in France by Société Turbomeca, with licensed derivatives including the Teledyne CAE J69 in the United States, the ENMASA Marboré M21 in Spain, and the Chinese WP11.

What this collection covers

• Marboré II and Marboré VI engine maintenance, overhaul and revision material
• Variants C, F and J, with additional Marboré VI variant references shown in the supplied pages
• Storage, conditioning and packing procedures
• Maintenance rectifications, inspection methods and workshop operations
• Illustrated composition and component information for the Marboré VI J1
• French-language original technical pages, with representative title and sample pages supplied where available

Documents represented in the supplied pages

• Manuel de Révision Générale Marboré VI, variantes C-F-J-N, Partie Texte, edition July 1984
• Manuel de Maintenance, Fascicule Entretien-Retouches, GTR Marboré II et Marboré VI, variantes C-F-J, identification 224 09 931
• Maintenance Manual, Storage Conditioning and Packing, Marboré II and Marboré VI, C-F-J variants, identification 224 09 934, issue December 1978
• Maintenance Manual, Maintenance Rectifications, Marboré II and Marboré VI, alternatives C-F-J, identification 224 09 933
• Marboré VI J1 Turbo-Réacteur, Tableau de Composition Illustré, identification 224 09 935
• Additional supplied technical pages identified by the references 16264, KM 226-00446 and ERF 7731

Engine profile

• Turbojet, single-spool centrifugal-flow design
• Marboré II: approximately 882 lbf / 3.9 kN thrust
• Marboré VI: approximately 1,058 lbf / 4.7 kN thrust
• Approximate weight range: 293-358 lb / 133-162 kg, depending on variant and accessories
• Typical fuel: aviation kerosene, including Jet A-1, JP-4 and JP-5
• Principal applications included the Fouga CM.170 Magister, Fouga CM.175 Zéphyr, Hispano Aviación HA-200 Saeta, Morane-Saulnier MS.760 Paris, Cessna T-37 through its J69 derivative, and Nord Aviation CT-20 target drones

Important reference notice

This is a historical aviation-document collection for research, restoration, preservation and reference. It is not current approved airworthiness data, an approved maintenance programme, or a substitute for instructions from the current type-certificate holder or aviation authority. Confirm applicability, revisions, rights and provenance before using any document for work on an engine or aircraft.

Format: Digital document collection. No physical item will be shipped.