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Image of 503-16MM, CPI/ADELT with Memory Module

CPI with Memory Module

Key Features

  • Beacon automatically deploys from aircraft.
  • Transmits the Cospas-Sarsat 406 MHz distress message and GPS coordinates.
  • Memory module storing a back-up of FDR/CVR data 
  • Certified Automatically Deployable Emergency Locator Transmitter (ADELT) 

The Challenges

The ditching of an aircraft in the ocean creates two time sensitive scenarios. Firstly, and most importantly, the crew must be located and rescued. Secondly, the flight data must be recovered to determine the cause of the incident. The Crash Position Indicator with Memory Module (CPI-MM) addresses both scenarios. 

On impact the beacon automatically activates and deploys from the aircraft. Floating on the ocean, it transmits the Cospas-Sarsat 406 MHz distress message, including GPS coordinates to the SAR authorities to coordinate a rescue effort. 

Prior to deployment the state-of-the-art recorder interface unit (RIU) takes a continuous feed of data from the on-board FDR/CVR and transfers directly to the Memory Module housed within the deployable beacon. In the event of a crash, the rescue teams can locate the buoyant beacon and recover the flight data back-up, even if the aircraft has sunk. This allows air crash investigators quicker access to the evidence they require to establish a cause and prevent future accidents.

Leonardo Helicopters – AW169 Guardia Di Finanza

Transmitter Signal

Frequency:

121.5MHz/243MHz (optional)/406MHz

Peak Effective:

75mW at 121.5MHz

Radiated Power :

5.0W at 406MHz

Frequency Stability:

2 x 10-9 per min

Transmission Duration:

24Hrs min, 5W PERP at -40°C

48Hrs min, 75mW PERP at -40°C

Repetition Rate:

520ms (±1%) every 50 secs (±5%)

Memory Module

CVR audio storage: 

min 2 hours

FDR data storage: 

min 25 hours

5.0W at 406MHz

Optional RIPS (Recorder Independent Power Supply) to ensure that data continues to be recorded for up to 2 hours post aircraft power loss, providing vital further insight into the development of an incident.

Activation

Offering five methods of deployment:

  1. Manual – Pilot activation via a cockpit control panel.
  2. G Switch – The SIU detects considerable changes in pre-programmed parameters and deploys the CPI beacon.
  3. Water switch – In the case of water ingress, the switch detects this and will deploy the beacon. This is the final trigger for deployment.
  4. Frangible (Crush) Switch – Impact of an external switch on the aircraft will deploy the CPI Beacon.
  5. Hold Off Loop – In the event of the tail boom breaking off from the aircraft, the BDC will detect a break in the circuit loop and automatically deploy the CPI beacon.

Compliance

Cospas-Sarsat specification C/ST.001

EUROCAE ED-62/RTCA DO-204/RTCA DO-183

EUROCAE ED-14C/RTCA DO-160C

CAA Specification No16, Issue 2

Approvals

TSO C91a, JTSO-2C91a, TSO C126 and JTSO-2C126

CAA WR01029

Cospas/Sarsat Approval 244

TCCA

CPI Beacon

Part No.:

503-16-MM

Dimensions:

305mm x 92mm (12 ins x 3.62 ins)

Battery Storage Life:

5 years

Beacon Release Unit

Part No.:

503-21-MM

Dimensions:

140mm x 70mm x 67mm (5.5ins x 2.76ins x 2.64ins)

Recorder Interface Unit

Part No.:

503-57-A

Dimensions:

187mm x 165mm x 68.9mm (7.4ins x 6.5ins x 2.7ins)

Part No.:

503-57-A503-57-B

Dimensions:

187mm x 165mm x 100mm (7.4ins x 6.5ins x 3.9ins)

System Interface Unit

Part No.:

503-24 Series

503-42 Series

Dimensions:

217mm x 120mm x 82mm (8.5ins x 4.7ins x 3.2ins)

Water Activated Switch

Part No.:

503-23-2

Dimensions:

140mm x 59mm x 31mm (5.5ins x 2.6ins x 1.2ins)

Water Activated Switch

Part No.:

503-23-2

Dimensions:

140mm x 59mm x 31mm (5.5ins x 2.6ins x 1.2ins)

Beacon Deployment Control

Part No.:

503-41

Dimensions:

140mm x 55mm x 89mm (5.5ins x 2.17ins x 3.5ins)

Aircraft Ident Config. Unit

Part No.:

503-40

Dimensions:

150mm x 66mm x 40mm (5.9ins x 2.6ins x 1.57ins)

CPI on Centrifuge
CPI / ADELT in Anechoic Chamber
CPI in Anechoic Chamber