Aircraft Components Manufacturing

PRODUCTION
2,600 km
RANGE
1,100 m
FIELD LENGTH
740 km/h
MAX CRUISE
12,500 m
CEILING

Manufacturing of aircraft and aircraft components under approved aviation production standards — including the KEZA-600, a light business jet designed and built in Tbilisi for airfields other jets cannot use.

At a glance
  • Take-off and landing performance comparable to a turboprop, from a balanced field length of 1,100 m
  • Un-improved runway capability, with a maximum take-off and landing altitude of 8,500 ft
  • Access to up to 25% more airports than the best jet competitor, and to more airports than its main turboprop competitor
  • Loaded with six persons — two crew and four passengers — the range is 2,600 km
  • At a full payload of 972 kg the range still exceeds 1,800 km
  • Among the slowest approach speeds of any light jet, which is what opens those shorter runways
  • More flexibility at difficult airports and better mission performance, with a climb rate of 20 m/s at maximum take-off weight

KEZA-TAM

TBILISI AIRCRAFT MANUFACTURING, GEORGIA
The KEZA-600 in KEZA-TAM livery
THE KEZA-600 IN KEZA-TAM LIVERY
01

The KEZA-600 light business jet

A light business jet designed and built in Tbilisi for the airfields other jets cannot use. Its take-off and landing performance is comparable to a turboprop, and its approach speeds are among the slowest of any light jet — which is exactly what opens shorter runways.

  • Un-improved runway capability, with a maximum take-off and landing altitude of 8,500 ft
  • Access to up to 25% more airports than the best jet competitor, and to more airports than its main turboprop competitor
  • A balanced field length of 1,100 m and a landing distance of 900 m
  • More flexibility at difficult airports, and better mission performance
Airfield access compared with other light jets
AIRFIELD ACCESS COMPARED WITH OTHER LIGHT JETS
Three-view general arrangement and key operating data
THREE-VIEW GENERAL ARRANGEMENT AND KEY OPERATING DATA
02

Performance and payload

Loaded with six persons — two crew and four passengers — the range is 2,600 km. At a full payload of 972 kg it still exceeds 1,800 km.

Range and payload envelope
RANGE AND PAYLOAD ENVELOPE

Key operating data

DESIGN ESTIMATES, SUBJECT TO FINAL CONFIRMATION

SPECIFICATIONVALUE
Max operating Mach number (MMO)0.72
Max cruise740 km/h
Stalling speed (MLW, forward CG, landing configuration)140 km/h
Rate of climb, all engines operative (ISA, sea level, MTOW)20 m/s
Rate of climb, one engine inoperative5 m/s
Time to FL370 (MTOW)14 min
Balanced field length1,100 m
Landing distance from 15 m (ISA, SL, flaps 40°, MLW)900 m
Maximum range (2 crew + 4 passengers)2,600 km
Maximum operating altitude12,500 m
03

Payload and range envelope

Configurations

CONFIGURATIONPAYLOADIFR RANGE
Four passengers + two crew, max fuel1,440 lb / 648 kg1,400 nm / 2,600 km
Passenger seats full (8 pax + 1 crew, available fuel)2,140 lb / 972 kg1,000 nm / 1,800 km
MANUFACTURING

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