Embraer/FMA CBA-123 Vector

Embraer/FMA

Embraer/FMA CBA-123 Vector aircraft
Embraer/FMAEmbraer/FMA CBA-123 Vector
Photo: Photograph by Mike Peel ( www.mikepeel.net ). · CC BY-SA 4.0 · Modified

About

The Embraer/FMA CBA-123 Vector was a twin-turboprop regional airliner jointly developed by Embraer of Brazil and FMA (Fábrica Militar de Aviones) of Argentina. First flown in 1990, the CBA-123 represented an ambitious collaboration between the two South American aerospace manufacturers. The aircraft was designed to seat 19 passengers and compete in the commuter aircraft market. Notable for its modern design featuring a low-wing configuration and twin Garrett TPE331 turboprop engines with five-blade propellers, the CBA-123 incorporated advanced composite materials and aerodynamic features for its time. The program was part of broader Brazil-Argentina cooperation agreements in aerospace and defense. Despite promising technical characteristics and successful test flights, the CBA-123 program faced financial challenges and market uncertainty in the early 1990s. Only one prototype (PT-ZYA) was built and flown before the joint venture was dissolved and the program was officially cancelled in 1993-1994. The cancellation reflected both companies' strategic decisions to focus on other programs - Embraer on the ERJ-145 regional jet family and FMA on military projects. The CBA-123 remains a notable example of international cooperation in regional aircraft development, even though it never entered production.

Weightscompared to Airbus A318

MTOW (Maximum Takeoff Weight)

13,500kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

12,700kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

12,000kg
0
25k
53k

Empty Weight

7,850kg
0
25k
40k

Capacitycompared to Airbus A318

Passenger Capacity

19passengers
0
100
132

14% of A318 maximum capacity

Crew

Total
3
Cockpit
2
Cabin
1

Dimensions

Length

19.9m

Wingspan

19.4m

Height

6.5m

Wing Area

39.9m²

Cabin Width

2.13m

Cabin Height

1.85m

Engine Specifications

Engine Count

2×

Engine Model

Garrett TPE331-10

Fuel & Cargo

Fuel Capacity

3,400 L

Cargo Volume

5.2 m³

Production & History

Total Produced

1

Production Status

Cancelled

Manufacturing Period

1987–1993

First Flight

July 18, 1990

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