IAF Tzukit 25 A/C FOR SALE

Specifications Dimensions Performance Structure Length: 32.97ft (10.05m) Width: 39.90ft (12.16m) Height: 9.09ft (2.77m) Performance Max Speed: 444mph (714kmh; 386kts) Max Range: 575miles (925km) Rate of Climb: 3,345ft/min (1,020m/min) Service Ceiling: 36,079ft(10,997m ; 6.8miles) Structure Accommodation: 2 Hardpoints: 2 Empty Weight: 4,740lbs (2,150kg) MTOW: 7,048lbs (3,197kg)

History in the IAF IAF Modification of the 1960’s Fouga Magister Decision to improve in order to extend life Improvements designed by IAF engineers Engine improvements performed by Bet Shemesh Engines Structural and systems changes by Israel Areospace Industries (IAI) Tzukit – Training aircraft at the IAF Academy

Major Improvements from the Fouga Magister Turbomeca Marbore II engine replaced with Marbore VI-P New automatic/computerized ignition Less flight cancellation Less engine removals Higher credibility Structural Improvments – longer life Maintenance Improvements Lower person/plane ratio Less frequent maintenance Faster dismantling and assembly

More Improvements from the Fouga Magister Gas oxygen replace with liquid Air conditioning system improvements Acoustic isolation installed New instruments and gauges installed Internal illumination installed Comfort improvements to seats Wing improvements (anti-corrosion treatments) Landing gear and fuel tank panels strengthened New approach/access openings added Cockpit improvements and canopy strengthening Fuel system improvements (new pump, filter, valves, faucets, pipes) Smoke systems installed Braking system improvements (sensitivity, reliability) Landing gear improvements Steering control improvements Hydraulic systems improved (pump, emergency pump, pressure filters)

Tzukit as Training Aircraft in IAF Academy

For More Information Sales and Marketing Department Israel Air Force air6165@idf.gov.il +972 (0) 3-606-2817