Part #: D51615-202

Model: Fortress DAFR

Curtiss Wright
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Fortress-DAFR 

FEATURES

  • Fortress DAFR provides a complete aircraft recording solution supporting the recording of mandatory parametric flight data as well as additional data from different interfaces
  • Combined voice, data, datalink and image recording (stand-alone options available)
  • DAFR attaches directly to an airframe to eliminate the need for heavy mounts and equipment racks/trays
  • Enhanced data acquisition support including direct interface to a tri-axial accelerometer
  • The Fortress DAFR is supported by dedicated recorder independent power supply (RIPS), cockpit area microphone (CAM), cockpit area camera (CAC) and cockpit control unit (CCU)
  • Supporting dual recorder installations, the CCU enables data and image distribution to two installed Fortress DAFR recorders through an integrated Ethernet switch.
  • ED-112A compliant
  • Designed to meet all current and possible future regulations
  • Ultra compact and lightweight 8.1 lb (3.7 kg)
  • Webserver for fast and free data download
  • Approval to ETSO-C123c, C124c, C176a, C177a
  • 90 day Ultrasonic Locator Beacon to TSO-C121b
  • Crash protected recording
  • Data acquisition and storage for +FOQA/FDM/FDAP +Aircraft performance monitoring +Engine condition trend monitoringFortress
  • DAFR also has four channels of cockpit voice recording, CPDLC recording (via ARINC 429 or ARINC 664) for up to 25 hours record capacity and image recording for two hours capacity.
  • Supports parametric data acquisition from either an ARINC 717, up to 4 ARINC 429 or dual input ARINC 664 interface
  • High speed (<45 seconds) and license free flight data download at the gate via a Gigabit Ethernet link
  • Enhanced EMC/Lightning protection for high reliability – especially on composite aircraft
  • Receives GMT/UTC via ARINC 429
  • Comprehensive BIT including individual discrete output for each recording function
  • OMS via ARINC 429
  • Tri-axial accelerometer input
  • Rotor tacho input
  • Gigabit Ethernet maintenance port

Optional Equipment:

  • Cockpit Control Unit (CCU) 
  • Recorder Independent Power Supply (RIPS)
  • Cockpit Area Camera (CAC
  • Cockpit Area Microphone (CAM)
  • Flight Recorder System Accelerometer
  • Ground Replay Support
SPECIFICATION
Power: 28Vdc, 13W max, Dual power input underwater Locator beacon: Beacon to TSO-C121b, battery and bracket included
FIRE INTENSITY: High: 1100°C for 60 minutes, Low: 260°C for 10 hours AIRBORNE IMAGE RECORDING: 2 hours, up to 16 fps, 100BASE-T Ethernet
Environmental: RTCA-DO160G,E1ABB(R(C,C1),U2(F,F1))EWFSFTAZ(XX), AZCWXRRMA3J3L3XXAC Operating temperature: -55°C to +70°C
NONE OPERATING temperature: -55°C to +85°C Altitude: -1000ft to +55,000ft
COCKPIT VOICE RECORDER CVR: 4 channels, 30 minutes to 25 hours duration +3 crew channels +1 cockpit area microphone channel (amplified or unamplified
+Summed Audio Monitor output
PENETRATION RESISTANCE: 500 lb from 10 ft ¼ inch contact point
IMPACK SHOCK: 3,400 G for 6.5 ms DATALINK RECORDER (CPDLC): 2 to 25 hours, ARINC 429 or ARINC 664
STATIC CRUSH: 5,000 lb for 5 mins per axis SHEAR/TENSILE STRENGTH: 6,000 lb for 1 minute each axis
fLIGHT DATA RECORDER: ARINC 717 format 64 – 4096 wps › ARINC 717 FDR monitor output › 4 ch ARINC 429 data at 12.5 or 100 KHz › 2 channels of ARINC 664 data FLUID IMMERSION: Immersion in aircraft fluids for 24 hr
hydrostatic pressure: Equivalent to depth of 20,000 ft mass: 8.1 lb (3.7 kg) including underwater locator beacon
WATER IMMERSION: 30 day sea water    

 

 

 

 

D51615-202
- Data Acquisition Flight Recorder
Price Condition Status
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