Monitors abnormal engine operation based on digital and analog signals from the aircraft engine.
It calculates engine life indices and detects engine malfunctions for generate a Pilot Fault List (PFL), which will stored in memory.
When an engine failure is detected, it provides warning for display on the Central Maintenance Panel (CMP).
Developed as a replacement for obsolete, achieving 60% cost competitiveness compared to equivalent products.

- x1 MIL-STD-1553B
- x16 Discrete Inout
- x14 Discrete Output
- x3 Analog Input
- x1 RS-232
- Size: 283 x 265 x 89 (mm)
- Weight : 4.1Kg
- Environment : MIL-STD-810G
- EMI/EMC : MIL-STD-461G
- Power : MIL-STD-704F (28VDC, 25W)

Receives vibration signals from an accelerometer installed on the aircraft engine and monitors engine vibration.
Processes real-time vibration signals and converts them into IPS AVG units for output.
Developed for localization, achieving 50% cost competitiveness compared to equivalent products.

- x1 MIL-STD-1553B
- x2 UART(RS-422/485)
- x2 Accelerometer sensor
- Sample rate : Up to 5,000Hz
- Size : 220 x 206 x 52 (mm)
- Weight : 1.75Kg
- Environment : MIL-STD-810G
- EMI/EMC : MIL-STD-461G
- Power : MIL-STD-704F (28VDC, 10W)

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

Generates 2D electronic map images using a terrain database and transmits them to the mission computer via the ARINC-818 standard.
Using Collins Aerospace's TERPROM software, enabling automatic terrain-following flight and terrain collision avoidance functions.

- x2 Gigabit Ethernet
- x1 MIL-STD-15583B
- x4 Discrete Input
- x2 Discrete Output
- x4 ARINC-818 Transmit
- 512GB Solid-State Disk (Digital Moving Map)
- 64GB Solid-State Disk (TERPROM)
- Size : 135.1x339.0x225.4 mm
- Weight : 4.25Kg
- Power : MIL-STD-704F (28VDC, 60W)
- Environment: MIL-STD-810G
- EMI/EMC: MIL-STD-461G

Consists of a Data Transmission and Recording Unit (DTRU) for data transmission and collection, and a Removable Mass Memory (RMM) for data storage.
Stores pre-planned flight mission data in the RMM on the ground and transmits it to the aircraft via the DTRU.
Collects various mission data (flight data, monitoring data, video data, and audio data) during flight, stores it in the RMM, and transmits it to the ground for mission analysis.

- x5 ARINC-818 Recording as H.264
- x2 Analog audio recording
- x7 MIL-STD-1553B Bus Monitoring
- x2 Gigabit Ethernet Monitoring
- 512GB Solid-State Disk (up to 2TB)
- Size : 160.1x146.0x232.4 mm
- Weight : 4.25Kg
- Power : MIL-STD-704F (28VDC, 58W)
- Environment: MIL-STD-810G
- EMI/EMC: MIL-STD-461G