The ADSE 650 is designed for all aircraft types and electrical power supplies.
It can be used for testing high performance civil and military aircraft, fix and rotary wings. This Pitot Static Tester is designed primarily for flight line use to cover the testing of all barometric and manometric pressure instrument systems.
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 Test Set is robust and housed in a mobile weatherproof case. An attached bag contains the pressure hoses and electrical cables.
Accessories for specific applications are available.
ADSE650 : FEATURES
- 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 simultaneously
- 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 650 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).
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.
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 650).
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 650), 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 …
|Altitude||-2,300 to 60,000ft||±1.5ft at 0ft|
|Altitude rate||Up to± 6,000ft/min||± 1%|
|Indicated airspeed||10 to 650 kts||± 1kt at 50kts
(± 0.5kts at 50kts optional)
|Mach N°||0.1 to 4.0 Mach
(0.1 to 10 Mach optional)
|± 0.001M at 0,8M/25,000ft
±0.002M at 1,7M/30,000ft
|Static sensor||71 to 1150 mbar||0.01% FS|
|Pitot sensor||30 to 3000 mbar||0.01% FS|
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.
|Temperature range||Operating -10° to 50°C (14° to 122°F)
Storage -20° to +60°C (-4° to 140°F)
|Power supply||90/240V, 50 to 400Hz AC, 150VA|
|Case||Completely weatherproof, meets EMC requirements MIL STD 462D|
|Physical||339 x 295 x 152mm (13.3 x 11.6 x 5.9 inch) – 6kg (13.22 lbs)|
|Calibration||Recommended period 12 months|
|Ease of use||Remote touch screen Integrated bag for cables and hoses|
|Ease of maintenance||Maintenance limited to calibration, regular external cleaning and exchange of filters (with the calibration)|
Remote Control Software for PC (Windows CE)
Low range Pt sensor: 350 kts max for better accuracy
ADSE650 : FACTSHEETS
Detailed information about the ADSE650 including features, specifications, etc.