L 59 “Super Albatros”

February 11, 2014 Jiří — No Comments

L-59 is a single engine, all metal, low wing jet trainer with tandem-seating, designed as an advanced weapon system trainer with enhanced ground attack capability. L-59 combines design features and experience from the extremely successful L-39 aircraft family with new, more powerful engine, advanced avionics and improvements in the airframe and other aircraft systems.

Main Features

Excellent handling characteristics within flight envelope
Updated avionics with HUD and advanced weapon delivery and navigation system
Operation capability on semi-prepared airstrips
Excellent visibility from both cockpits
Zero-zero ejection seats
Complete training system, inc. TL-59 Flight Simulator, Ejection Seat Simulator and full set of ground training aids
Low operational cost
High reliability
Cost Effective training

Technical Data

Note: All performance data are valid for clean A/C T/O weight, 2 pilots. Power Plant.

Type: DV-2 Turbofan

Basic characteristics:

Maximum static thrust: 21,58 kN (4,850 lb)
Bypass ratio: 1,5
Specific fuel consumption: 60 kg / kN.hr

We Offer

Logistic Support
Spare Parts and Systems Supply
Technical Assistance at site,
Full Mission Simulators
Airframe & Engine and its components Repairs & Overhauls, Technology Supplies
Training of Pilots and Ground Personnel
Upgrades

Dimensions:
Wing span	9,542 m	31 ft 4 in
Length	12,203 m	40 ft
Weight empty	4,770 m	15 ft 8 in
Weights and Loadings:
Basic empty weight	4,030 kg	8,884 lb
Clean A/C ramp weight	5,390 kg	11,883 lb
Clean A/C take-off weight	5,300 kg	11,684 lb
Maximum ramp weight	7,000 kg	15,432 lb
Internal fuel capacity	1,200 kg	2,646 lb
Total fuel capacity	2,288 kg	5,044 lb
(Internal and 4350 I drop tanks)
Basic Performance Data:
Maximum level speed	870 km/hr	470 KTAS
Never-exceed speed (sea level)	920 km/hr	497 KTAS
Max rate of climb	25 m/s	4,921 ft/min
Service ceiling	12,200 m	40,000 ft
Maximum range (internal fuel. 10% fuel reserve)	1,570 km	850 nm
Maximum endurance (internal fuel. 10% fuel reserve)	2 hr 55 min
Take-off run (sea level)	590 m	1,935 ft
Landing run (sea level, 50% fuel)	640 m	2,100 ft
Stalling speed (landing flaps, 50% fuel)	172 km/hr	93 KTAS
Max Structural limit	+8g; -4g