152. "Negrești" presidential plane, used for the official flights of President Ion Iliescu, 1989
Početna cijena
EUR 25.000
Prodano
EUR 165.000
Sesija
Čet., 27 svibnja 2021 18:30
Opis
engine: two Rolls-Royce Spey Mk 512-14DW dual-flow turbofans capable of a thrust of 6,000 kgf, maximum weight: 47,400 kgf, top speed with 119 passengers: 870 km/h, range: 3,500 km Main construction materials are duralumin and special steels. The all-metal structure of the aircraft is processed through aluminium alloys with trade names (old and new) L72 / 2014 and L73 / 2024, delivered in the form of sheet metal, plates and bars. Metal sheets have been processed mainly to become shells by stretching, specific to the ruled areas of the fuselage (front and rear) or by precision rolling specific to the unruled areas (central fuselage). Also, duralumin sheets are made for the upper / lower side wing and left / right covers of the flight control surfaces (flaps, ailerons, aerodynamic brakes, stabilizer, depth rudder, drift, steering), door covers and landing gear hatches. Duralumin plates become integrated shells (built-in strips) upper / lower side wings, by milling and structural parts of assembly and completion. Duralumin bars become frames of the central fuselage, by forming and stretching, followed by relief / contour milling on CNC machines.
DODATNE INFORMACIJE
Za pojašnjenja u vezi s postupkom licitiranja, troškovima kupnje, uvjetima jamstva, plaćanja i preuzimanja osvojenog lota preporučujemo da pažljivo pročitate/ponovno pročitate Pravilnik o licitiranju.
Za dodatne informacije o lotu i aukciji kontaktirajte Odjel umjetničkih savjetnika.
Detalii
DODATNE INFORMACIJE
Za pojašnjenja u vezi s postupkom licitiranja, troškovima kupnje, uvjetima jamstva, plaćanja i preuzimanja osvojenog lota preporučujemo da pažljivo pročitate/ponovno pročitate Pravilnik o licitiranju.
Za dodatne informacije o lotu i aukciji kontaktirajte Odjel umjetničkih savjetnika.
Opis
engine: two Rolls-Royce Spey Mk 512-14DW dual-flow turbofans capable of a thrust of 6,000 kgf, maximum weight: 47,400 kgf, top speed with 119 passengers: 870 km/h, range: 3,500 km Main construction materials are duralumin and special steels. The all-metal structure of the aircraft is processed through aluminium alloys with trade names (old and new) L72 / 2014 and L73 / 2024, delivered in the form of sheet metal, plates and bars. Metal sheets have been processed mainly to become shells by stretching, specific to the ruled areas of the fuselage (front and rear) or by precision rolling specific to the unruled areas (central fuselage). Also, duralumin sheets are made for the upper / lower side wing and left / right covers of the flight control surfaces (flaps, ailerons, aerodynamic brakes, stabilizer, depth rudder, drift, steering), door covers and landing gear hatches. Duralumin plates become integrated shells (built-in strips) upper / lower side wings, by milling and structural parts of assembly and completion. Duralumin bars become frames of the central fuselage, by forming and stretching, followed by relief / contour milling on CNC machines.