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503-16 CPI / ADELT Beacon

Crash Position Indicator

Key Features

  • Beacon automatically deploys from aircraft. 
  • Beacon housed in an impact resistant, buoyant, and flame proof casing.
  • Transmits the Cospas-Sarsat 406 MHz distress message and GPS coordinates.
  • Certified Automatically Deployable Emergency Locator Transmitter (ADELT).
  • Widely adopted by leading helicopter manufacturers and offshore operators worldwide.

About This Beacon

The need to swiftly and accurately locate downed offshore aircraft has long been a critical challenge faced by search and rescue (SAR) teams. The Techtest deployable Crash Position Indicator (CPI) overcomes this challenge. The CPI is a certified Automatically Deployable Emergency Locator Transmitter (ADELT) operating with the Cospas-Sarsat satellite system to transmit the 406 MHz distress frequency and GPS coordinates of downed aircraft. This ensures rapid and precise identification of accident sites by the authorities, reducing recovery time. 

The 503-16 CPI stands out for its comprehensive deployment options, encompassing manual activation, automatic G-sensor activation and automatic water switch deployment. Additionally, in the event of tail boom break, Beacon Deploy Control (BDC) units provide further redundancy, providing maximum scenario coverage.

The global adoption of the Techtest 503-16 by leading helicopter manufacturers and operators is a testament to its exceptional value and the unwavering trust placed in the beacon. It gives SAR teams the tools they need to locate downed aircraft with utmost precision and efficiency, safeguarding lives and upholding the highest standards of safety.

Transmitter Signal

Dimensions

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%)

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 Series

Dimensions: 

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

Battery Storage Life:

5 years

Cockpit Control Panel

Part No.:

503-22 Series

Dimensions:

146.2mm x 38mm x 66mm (5.75ins x 1.5ins x 2.6ins)

Beacon Release Unit

Part No.:

503-21 Series

Dimensions:

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

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)

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 – In Spray Booth
CPI – Pressure Test