Collects data from various sensors within the aircraft system, converts it into the required format, and transmits it to the mission computer or flight control computer. Converts control commands received from the mission computer or flight control computer and relays them to sensors and other peripheral devices. Supports system control functions, monitors the status of key systems, and provides feedback. Achieves 70% cost competitiveness compared to equivalent-performance products. - x2 MIL-STD-1553B - x2 UART (RS-422/485) - x24 Analog input interfaces - x8 Analog output interfaces - x64 Discrete input interfaces - x40 Discrete output interfaces - Size : 270 x 270 x 62.2mm - Weight : 2.5Kg - Power : MIL-STD-704F (28VDC, 10W) - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G

APA-110 is designed to eliminate CO2 emissions with its unique technical characteristics. It can perform the complete service of aircraft at remote parking places with diesel engine and it is also capable to operate from the 50/60Hz, 400V, 3 phase main power supply grid as any electrical GPU, without fuel consumption and with zero operating emissions. The range of different APA configurations with no emissions allow for safer, cleaner and more practical operational conditions for operators and personnel at the location.

Original compact design and long-term production know-how. System reliability and overall competitiveness.

Thermostatic Temperature switches

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Communication Antenna for Data and Voice Transmission

A VGA (640×480) LWIR (8–12 µm) uncooled micro-bolometer module with 12 µm pixel pitch and NETD ≤ 50 mK, paired with an F1.0, 10.7 mm EFL lens delivering H42° / V31.5° / D52.5° FOV. It streams at 30 Hz in either UVC (USB-C, 5 V) or GMSL1 (FAKRA, 12 V), with power consumption < 1.9 W. The compact, lightweight housing (30×30×58.9 mm for UVC; 30×30×70.9 mm with FAKRA for GMSL1; IP65; −40 °C to 85 °C) makes it well-suited for autonomous vehicles, UAVs, and security systems, providing reliable day/night thermal perception of pedestrians, animals, and objects in adverse weather.

PTO SHAFT, Proven Performance, Realized in Reality CTLA's Power Transmission Shaft (PTO-shaft) is a key component of the aircraft secondary powertrain, transmitting the high-speed rotational power generated by the aircraft engine drive unit (EMAD) to the gearbox (AMAD). By applying high-strength, lightweight titanium material for the first time in the world, we have achieved both weight reduction and durability, while implementing outstanding stability and reliability through our proprietary electron beam welding technology optimized for high-speed rotation and high-speed precision balancing technology. In particular, this product, which is currently being mass-produced and delivered to the KF-21 fighter jet, has demonstrated excellent power transmission performance while minimizing vibration even in extreme environments. CTLA is leading technological innovation in the field of high-speed rotational machinery, spearheading the self-reliance of domestic aircraft components and advancing into the global market.