ADSE 744

Pitot-Static tester / AoA tester
AoA testing has never been so easy
The ADSE 744 is the newest of our broad range of pitot and static testers.
This Air Data Test Set was specifically designed for the new-generation pitot tubes that integrate sensing probes, pressure sensors and powerful air data computer processing to provide all critical air data parameters including pitot and static pressure, airspeed, altitude, and angle of attack. This pitot static tester is designed primarily for flight line use to cover the testing of all barometric and manometric pressure instrument systems.

The AoA (Angle of Attack) channel behaves as a second Ps channel, in order to create a differential pressure between the 2 Ps channel, allowing it to perform simulations of different angles of attack. The large touch screen display, with on-screen help, enables all checks to be carried out easily on the flight deck or in the cockpit, by a single operator. The ADSE 744 is robust and housed in a mobile weatherproof case. An attached bag contains the pressure hoses and electrical cables.
Wide choice of pneumatic connectors available upon request.


air data test set ADSE744

  Built-in pressure and vacuum pumps
  Liquid crystal color display with touch
  sensitive screen for operator instructions/help
  Remote control unit based on Windows
  CE tablet PC
  Complete self check of set before use
•  High accuracy, high resolution
•  RVSM compliant

  Programmable leak test
•  Programmable flight envelope to protect
  equipment under test
  All four primary flight parameters displayed
  Programmable (password write protected)
  test schedules
  Select pressure units: hPa; mb; in Hg; mmHg;
  ft; m; kts; km/h, ft/min; hm/min, Mach number

Our pitot-static testers are mainly used with a wired color touchpad, except the ADSE 744 which works in WIFI, thus giving greater freedom to the operator. The HMI has been designed to be as simple and efficient as possible, which is confirmed by users.

Different functions such as flight areas, slope monitoring, balancing, etc. enable flight instrument tests to be carried out safely without accidentally damaging them. It is possible to work in manual or automatic mode by programming test sequences (ideal for testing altimeters in the workshop).

Leak Test
The leak test is a function that measures the leakage rate of the circuits Ps, Pt for and is intended to calculate the leak rate per minute. The test time is set to 1 minute by default, but can be adjusted.

Tester Packaging
Our pitot-static testers are available for the laboratory in 19 “rack version (with or without integrated pumps) or in a rolling suitcase for the hangar and tarmac. We also strive to reduce the size and weight of our testers so that they are easier to transport and use (ex ADSE 744).

For large airplanes with several airspeed circuits, our ADSEs can be equipped with up to 4 Ps, Pt and AoA channels. The operator can then select and isolate the various circuits without leaving the cockpit.

Some devices have a default battery (ADSE 744), and can be added as an option to others.

It is possible to add other options on our Pitot-static testers, such as the AoA (angle of attack), as well as low-speed sensors for helicopters, gliders and drones, high-speed sensors for fighter planes, control alti-coders, etc …



Function Range Accuracy
Altitude -2,300 to 60,000 ft (-700 to 18,000 m)

± 3 ft at 0 ft (± 1 m at 0 m)

± 8 ft at 30,000 ft (± 3 m at 10,000 m)

± 32 ft at 60,000 ft (± 10 m at 18,000 m)

Altitude rate 100 to 6,000 ft/min (30 to 1,800 m/min) ± 10 ft or ± 1 % (±3 m or ± 1 %)
Airspeed (1) 0 to 800 kts (0 to 1,480 km/h)

± 0.5 kt at 50 kts (± 0.92 km/h at 100 km/h)

± 0.14 kt at 500 kts (± 0.26 km/h at 900 km/h)

± 0.07 kt at 800 kts (± 0.13 km/h at 1,480 km/h)

Airspeed Mach 0 to 4.0 Mach ± 0.0006 M at 0.8 M at 25,000 ft

± 0.0003 M at 1.7 M at 30,000 ft

Angle of Attack (2) ± 100 DhPa ± 0.20 DhPa
Static sensor (3) 72 to 1,100 hPa ± 0.13 hPa
Pitot sensor (3) 0 to 1,455 DhPa ± 0.30 DhPa
AoA sensor (3) 72 to 1,200 hPa ± 0.13 hPa

(1) Accuracy after Autozero function
(2) AoA options: ± 1,000 DhPa (± 0.35 DhPa) or ± 2,000 DhPa (± 0.40 DhPa)
(3) Different range & rate of sensors available on request or options

Measurement specifications in standard conditions
  On-going developments may cause a change in specifications without notice.
  Special developments may be considered on a case by case basis.


  Range on Pt: 350 kts
  Range on AoA: ± 1,000 or ± 2,000 DhPa
  EPR (Engine Pressure Ratio)
  Cabin Pressure
  Outflow Valve


•  Wifi Remote control in standard ( Std Remote control availble in the TDS )
•  Two nipples Staubli-M / AN-4 M
•  10 m Ps and Pt flexible hoses with connector AN-4 female /Staubli-M
•  5m AC cable
•  Color Tactile inteface V03
•  Plastic water-restant suitcase
•  Special bag for tubes and cables


Temperature Operating Operating -5°C to 50°C (23°F to 122°F)
Storage -20°C to +60°C (–4°F to 140°F)
(Extanded Range on-demand)
Power supply 90/240V AC from 50 to 400Hz
Housing Completely weatherproof, meets EMC requirements MIL STD 462D
Dimensions 540 x 220 x 470 mm (21 x 9 x 18.5 inch)
18kg (40 lbs)
Calibration Recommended period 12 months
Ease of use Wi-Fi remote control 8” color LCD touch screen
Integrated bag for cables and hoses
Ease of maintenance Maintenance limited to calibration, regular external cleaning