mise en page 1...+— 0. 4 kta 65 s machn 0.1to4.0mach +—0.001mat0,8m/25,000ft...
TRANSCRIPT
→ Pitot/Static/AoA testers and adaptators
→ Bonding testers
→ Loop Resistance Tester
→ Battery testers
→ Leak testers
TESTS INSTRUMENTSPRODUCT RANGE
OURPRODUCTSIn order to assist aviation manufacturing and maintenance, ATEQ has developed a wideand complete range of products:→ Automated Pitot/Static testers for indoor use (laboratory & workshop) or outdoor use
(hangar & tarmac). ADSE can control all pressure dependant on-board equipment:altimeters, anemometers, variometers, pressure sensors, air data calculators, etc.Our instruments are extremely accurate, user friendly, reliable, and canbeeasily customized.All our ADSE (except ADSE 712 and 543) are RVSM Compliant, with an accuracy upto 0.007% of the Scale, well above the standard requirements for RVSM compliance.
→ Pitot/Static adaptors for all aircrafts (PSAT)→ Leak detector for indoor or outdoor uses with nitrogen and 5% hydrogen (H 6000)→ Battery tester with a large range of powers according to battery CMMs (EEST)→ Bonding & Loop Resistance Tester for electrical continuity on standard and composite
aircrafts (AX 6000, LRT 6000).
OURCUSTOMERSATEQ already has well-known customers such as:→ Airbus → French air force → French navy → Air France→ Eurocopter → EADS → Thales → Dassault→ Air China → Aeroflot → ATR → Air Canadaand so many others...
OURSERVICESThanks to its worldwide network, ATEQ is providing unrivaled services to customer:→ customized instrument solutions adapted to all requirements→ equipment calibration→ fast after-sales maintenance and repairs
1 ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
hangar/ tarmacADSE 712 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2ADSE 543 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3ADSE 643 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4ADSE 650 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5ADSE 743 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6ADSE 744 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7ADSE 745 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8ADSE 746 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9PSAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
labCDP 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12ePlane PC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13CV 250 - 400 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14ADSE 740 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15ADSE 741 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16ADSE 715 RS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17H 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
electrical testsEEST 50-60 rack edition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20EEST 50-60 workshop edition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21AX 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23Accessories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24LRT 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25Accessories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26
all the specifications in this brochure can be modified
2ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
ADSE 712
ADSE712 ALTITUDECONTROLLERLEAKTESTER
→ MANO-CONTACT TESTING→ ALTITUDE SIMULATION→ LEAK TESTER
The ADSE 712 is a single channel generator thatsimulates an altitude to test different pneumaticequipments for aerospaceapplicationsor equipmentreacting to barometric constraints.
It can test leaks in pneumatic circuits, functions linkedto the depressurization of the aircraft cabin, etc.
The ADSE 712 is presented as a small light-weightcase containing all vacuumandpressure generation,measurement and regulation functions.
All operator interface, management and reportfunctions are displayed on the front panel of theequipment.
The ADSE 712 is controlled with a single button, tolaunch a test program predefined in our workshop.
Main Features• Only one generation channel for pressure or vacuum
• Integrated pumps
• Regulation managed by micro controller
• System operation with a single button
• Leak rate measurement
• Secured for use by occasional users
Options• Choice of altitudes to simulate of leak measurement time
• Serial link for driving the system with a computer
• Pressure generation to test Pitot probes
3 ATEQ - Test instruments for all aircraftsADSE 543
PITOTORSTATICTESTER ADSE543ALIGHTANDRELIABLEPITOTSTATICTESTER
→ ALTIMETER TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING
The ADSE 543 pitot static tester, housed in a plasticcarrying case, is a portable, self contained fieldtester designed to test aircraft pilot ans staticsystems for leaks as well as the operation andcalibration of airspeed, altimeter, engine pressureratio, manifold pressure indicators, and othervacuum or low pressure units.
The tester consists of a hand-operated vacuumpump, a hand-operated pressure pump vacuumand pressure gauges, 5 control valves, an alitmeterand an airspeed indicator. The package accessoriesinclude two 25-foot hoses, a pitot mast adapter,and a static port adapter kit which enable the userto connect the aricraft pitot and static lines.
Main Features• Ps Pt
General detailsTemperature range Operating -10° to 50°C (14° to 122°F)
Storage -20° to +60°C (-4° to 140°F)
Case Water resistantCE and MIL STD462D marking
Physical 515 x 380 x 270 mm (20.3 x 15 x10.6 inch)
Weight 12kg (26.5 lbs)
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -1,000 to -60,000ft +— 1.5ft at 0ft
Rate of climb Up to +— 6,000ft/min +— 1%
Indicated airspeed Up to 650 kts ++— 2kt at 50kts
- Continuing development sometimes necessitates specification changes without notice.- Special options can be analyzed and developped on request
HANGAR
/TARMAC
4ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
ADSE643 PITOT/STATICTESTERTHEMOSTVERSATILEPITOT&STATICONTHEMARKET
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ LEAK TESTER
The ADSE 643 caters fully for all aircraft types andthe different electrical power supplies.It can be used for testing high performance civiland military aircraft, fixed and rotary wing.This Pitot Static tester is designed primarily forflightline use to cover the testing of all barometricand manometric pressure instrument systems.The ease of use and portability enables all checksto be carried out easily on the flight deck or in thecockpit, by a single operator.The test set is housed in an anodized metal andrugged case. An attached case contains the pressurehoses and electrical cables.Accessories to suit specific applications may besupplied.
Main Features• Manual pressure and vacuum generation (automatic as option)
• Simple and easy to use software interface that makes operation quicker and safier
• 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 easily accessible
• Programmable (password write protected) test schedules
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature 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, 24V DC
Case Completely weatherproof, meets EMC requirementsMIL STD 462D
Physical 200 x 240 x 210 mm (7.87 x 9.44 x 8.26 inch) - 12 kg (26.45lbs)
Calibration Recommended period 12 months
Ease of Use Manual pressure and vacuum pump
Ease of maintenance Maintenance limited to calibration, regular external cleaningand exchange of filters (with the calibration)
OptionalPressure and vacuum pumps for automatic generation
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 50,000ft +— 3ft at 0ft+— 7ft at 30,000ft+— 18ft at 50,000ft
Altitude rate Up to +— 6,000ft/min +— 2%
Indicated 10 to 650kts ++— 1kt at 50kts
airspeed +— 0.2kt at 500kts+— 0.04kt at 650kts
Mach N° 0.1 to 3.0 Mach +— 0.001M at 0,8M/25,000ft+— 0.002M at 1,7M/30,000ft
Static sensor 30 to 1100 mbar (absolute) 0,01% FS
Pitot sensor 0 to 1000 mbar (differential) 0,01% FS
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
SPVU 600:pressure and vacuum unit
RVSM COMPLIANT
ADSE 643
5 ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
ADSE 650
PITOT/STATICTESTER ADSE650THEBESTPITOT-STATICTESTERONTHEMARKET
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ LEAK TESTER
The ADSE 650 caters fully for all aircraft types andthe different electrical power supplies.It can be used for testing high performance civil,fixed and rotary wings.This Pitot Static tester is designed primarily forflightline use to cover the testing of all barometricand manometric pressure instrument systems.The large wireless touchscreen display, withon-screen help, enables all checks to be carried outeasily on the flight deck or in the cockpit, by a sin-gle operator.The test set is robust and housed in a mobileweatherproof case. An attached bag contains thepressure hoses and electrical cables.Accessories to suit specific applications may besupplied.
Main Features• Built-in pressure and vacuum pumps
• Liquid crystal colour 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
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature 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 requirementsMIL STD 462D
Physical 339x295x152mm (13.3 x 11,6 x 5.9 inch) - 6kg (13,22 lbs)
Calibration Recommended period 12 months
Ease of Use Remote touch screenIntegrated bag for cables and hoses
Ease of maintenance Maintenance limited to calibration, regular external cleaningand exchange of filters (with the calibration)
OptionalRemote Control Software for PC (Windows CE)
Low range Pt sensor: 350 kts max for better accuracy
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 60,000ft +— 1.5ft at 0ft
Altitude rate +— 0 to 6,000ft/min +— 1%Indicated 10 to 650 kts ++— 1kt at 50ktsairspeed (++— 0.5kts at 50kts optional)
Mach N° 0.1 to 4.0 Mach +— 0.001M at 0,8M/25,000ft
(0.1 to 10 Mach optional) +— 0.002M at 1,7M/30,000ft
Static sensor 30 to 1200 mbar 0,01% FS
Pitot sensor 30 to 3000 mbar 0,01% FS
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
Typical screen display
RVSM COMPLIANT
6ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
ADSE 743
ADSE743 PITOT/STATICTESTERTHEBESTPITOT-STATICTESTERONTHEMARKET
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ LEAK TESTER
The ADSE 743 caters fully for all aircraft types andthe different electrical power supplies.It can be used for testing high performance civiland military aircraft, fix and rotary wing.This Pitot Static tester is designed primarily forflightline use to cover the testing of all barometricand manometric pressure instrument systems.The large touch screen display, with on-screen help,enables all checks to be carried out easily on theflight deck or in the cockpit, by a single operator.The test set is robust and housed in a mobileweatherproof case. An attached bag contains thepressure hoses and electrical cables.Accessories to suit specific applications may besupplied.
Main Features• Built-in pressure and vacuum pumps
• Liquid crystal colour 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
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature 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 requirementsMIL STD 462D
Physical 515x380x270mm (20.3 x 15 x 10.6 inch) - 17kg (38 lbs)
Calibration Recommended period 12 months
Ease of Use Remote touch screenIntegrated bag for cables and hoses
Ease of maintenance Maintenance limited to calibration, regular external cleaningand exchange of filters (with the calibration)
OptionalDC Power supply: 17 to 32V DC
Remote Control Software for PC (Windows CE)
Bigger Pumps: 80,000ft - 15,000ft/min (up to 100,000ft - 60,000ft/min (Volume dependant))
Low range Pt sensor: 350 kts max for better accuracy
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 60,000ft +— 1.5ft at 0ft
(up to -4,000ft to 100,000ft optional) +— 4ft at 30,000ft+— 16ft at 60,000ft
Altitude rate +— 0 to 6,000ft/min +— 1%(up to ++— 60,000ft/min optional) ++— 1%
Indicated 10 to 800 kts ++— 1kt at 50kts (++— 0.5kts at 50kts optional)
airspeed (up to 1000 kts optional) +— 0.2kt at 350kts (++— 0.1kts at 350kts opt.)+— 0.04kt at 650kts
Mach N° 0.1 to 4.0 Mach +— 0.001M at 0,8M/25,000ft
(0.1 to 10 Mach optional) +— 0.002M at 1,7M/30,000ft
Static sensor 30 to 1200 mbar 0,01% FS
Pitot sensor 30 to 3000 mbar 0,01% FS
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
Typical screen display
RVSM COMPLIANT
7 ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
ADSE 744
PITOT/STATIC/AoATESTER ADSE744AoATESTINGHASNEVERBEENMADESOEASY
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ AoA TESTING FOR SPECIFIC PROBES→ LEAK TESTER
Main Features• Built-in pressure and vacuum pumps
• Liquid crystal colour 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
• Selectable pressure units : hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature 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 requirementsMIL STD 462D
Physical 515x380x270mm (20.3 x 15 x 10.6 inch) - 17kg (38 lbs)
Calibration Recommended period 12 months
Ease of Use Remote touch screenIntegrated bag for cables and hoses
Ease of maintenance Maintenance limited to calibration, regular external cleaningand exchange of filters (with the calibration)
OptionalDC Power supply: 17 to 32V DC
Low range Pt sensor: 350 kts max for better accuracy
Remote Control Software for PC (Windows CE)
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 60,000ft +— 1.5ft at 0ft
(up to -4,000ft to 80,000ft optional) +— 4ft at 30,000ft+— 16ft at 60,000ft
Altitude rate +— 0 to 6,000ft/min +— 1%Indicated 10 to 800kts ++— 1kt at 50kts (++— 0.5kts at 50kts optional)
airspeed (up to 1000 kts optional) +— 0.2kt at 350kts (++— 0.1kts at 350kts opt.)+— 0.04kt at 650kts
Mach N° 0.1 to 4.0 Mach +— 0.001M at 0,8M/25,000ft
Static sensor 30 to 1200 mbar 0,01% FS
Pitot sensor 30 to 3000 mbar 0,01% FS
AoA sensor 30 to 1200 mbar 0,01% FS
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
Typical screen display
RVSM COMPLIANT
The ADSE 744 is the new comer of our broad rangeof pitot and static testers. This tester was specificallydesigned for the new-generation pitot tubes thatintegrate sensing probes, pressure sensors andpowerful air data computer processing to provide allcritical air data parameters including Pitot and staticpressure, airspeed, altitude, and angle of attack.This Pitot Static tester is designed primarily forflightline use to cover the testing of all barometricand manometric pressure instrument systems.The AoA Channel behaves as a second Ps channel,in order to create a differential pressure betweenthe 2 Ps Channel, allowing to perform simulationsof different Angles of Attack. The large touch screendisplay, with on-screen help, enables all checks tobe carried out easily on the flight deck or in thecockpit, by a single operator. The ADSE 744 isrobust and housed in a mobile weatherproof case.An attached bag contains the pressure hoses andelectrical cables. Wide choice of pneumaticconnectors can be supplied on demand.
8ATEQ - Test instruments for all aircrafts ADSE 745
HANGAR
/TARMAC
ADSE745 PITOT/STATICTESTERMULTICHANNELPITOTSTATICTESTERFORALLAIRCRAFTS
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ LEAK TESTER→ ANGLE OF ATTACK TESTING OPTION
The ADSE 745 caters fully for all aircraft types andthe different electrical power supplies.It can be used for testing high performance civiland military aircraft, fixed and rotary wing.The multi-pressure outlets option can suit themore complex pilot-static-systems.This Pitot Static tester is designed primarily forflightline use to cover the testing of all barometricand manometric pressure instrument systems.The large touch screen display, with on-screen help,enables all checks to be carried out easily on theflight deck or in the cockpit, by a single operator.The test set is robust and housed in a mobileweatherproof case fitted with rugged tyre wheels.An attached bag contains the pressure hoses andelectrical cables.Accessories to suit specific applications may besupplied.
Main Features• Built-in pressure and vacuum pumps
• Liquid crystal colour 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 – 24 programmes available
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature 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 requirementsMIL STD 462D
Physical 435x310x680mm (17.1 x 12.2 x 26.7 inch) 32 kg (71 lbs)
Calibration Recommended period 12 months
Ease of Use Remote touch screenWheeled case for manoeuvrabilityIntegrated bag for cables and hoses
Ease of maintenance Maintenance limited to calibration, regular external cleaningand exchange of filters (with the calibration)
OptionalMulti-pressure outlet (2 Ps & 2 Pt) variant
DC Power supply: 17 to 32V DC
Rechargeable 24V battery pack (2h)
Bigger Pumps: 80,000ft - 15,000ft/min (up to 100,000ft - 60,000ft/min (Volume dependant)
Low range Pt sensor: 350 kts max for better accuracy
Remote Control Software for PC (Windows CE)
AoA option
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 60,000ft +— 1.5ft at 0ft
(up to -4,000ft to 100,000ft optional) +— 4ft at 30,000ft+— 16ft at 60,000ft
Altitude rate +— 0 to 6,000ft/min +— 1%(up to ++— 60,000ft/min optional) ++— 1%
Indicated 10 to 800 kts ++— 1kt at 50kts (++— 0.5kts at 50kts optional)
airspeed (up to 1000 kts optional) +— 0.2kt at 350kts (++— 0.1kts at 350kts opt.)+— 0.04kt at 650kts
Mach N° 0.1 to 4.0 Mach +— 0.001M at 0,8M/25,000ft
(0.1 to 10 Mach optional) +— 0.002M at 1,7M/30,000ft
Static sensor 30 to 1200 mbar 0,01% FS
Pitot sensor 30 to 3000 mbar 0,01% FS
- On-going developments may causea change in specifications withoutnotice.
- Special developments may beconsidered on a case by case basis.
Typical screen display
RVSM COMPLIANT
9 ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
ADSE 746
PITOT/STATICTESTER ADSE746OURTOPRANGEPITOT-STATICTESTER
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ AOA TESTING FOR SPECIFIC PROBES→ LEAK TESTER
The ADSE 746 caters fully for all aircraft types andthe different electrical power supplies. It can be usedfor testing high performance civil and militaryaircraft, fixed and rotary wing. The multi-pressureoutlets option can suit themore complex pilot-static-systems.This Pitot Static tester is designed primarily forflightline use to cover the testing of all barometricand manometric pressure instrument systems.The large touch screen display, with on-screen help,enables all checks to be carried out easily on theflight deck or in the cockpit, by a single operator.The test set is robust and housed in a mobileweatherproof case fitted with tire wheels.An attached bag contains the pressure hosesand electrical cables. Accessories to suit specificapplications may be supplied.
Main Features• Built-in pressure and vacuum pumps
• Liquid crystal colour 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 - 24 programmes available
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature 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 requirementsMIL STD 462D
Physical 520x380x835 mm (20.4 x 14.9 x 32.8 inch) 32 kg (71 lbs)
Calibration Recommended period 12 months
Ease of Use Remote touch screenWheeled case for manoeuvrabilityIntegrated bag for cables and hoses
Ease of maintenance Maintenance limited to calibration, regular external cleaningand exchange of filters (with the calibration)
OptionalMulti-pressure outlet (4 Ps, 4 Pt & 4 AoA) variant
Rechargeable 24V battery pack (2h)
DC Power supply: 17 to 32V DC
Bigger Pumps: 80,000ft - 15,000ft/min (up to 100,000ft - 60,000ft/min (Volume dependant))
Low range Pt sensor: 350 kts max for better accuracy
Remote Control Software for PC (Windows CE)
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 60,000ft +— 1.5ft at 0ft
(up to -4,000ft to 100,000ft optional) +— 4ft at 30,000ft+— 16ft at 60,000ft
Altitude rate +— 0 to 6,000ft/min +— 1%(up to ++— 60,000ft/min optional) ++— 1%
Indicated 10 to 800 kts ++— 1kt at 50kts (++— 0.5kts at 50kts optional)
airspeed (up to 1000 kts optional) +— 0.2kt at 350kts (++— 0.1kts at 350kts opt.)+— 0.04kt at 650kts
Mach N° 0.1 to 4.0 Mach +— 0.001M at 0,8M/25,000ft
(0.1 to 10 Mach optional) +— 0.002M at 1,7M/30,000ft
Static sensor 30 to 1200 mbar 0,01% FS
Pitot sensor 30 to 3000 mbar 0,01% FS
AoA sensor 30 to 1200 mbar 0,01% FS
EPR Test 0,1 to 10 0,005
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
RVSM COMPLIANT
10ATEQ - Test instruments for all aircrafts
HANGAR
/TARMAC
PSAT
PSAT PS/PTADAPTORKITSTATICPORTUNIVERSALADAPTER
→ KITS AND PARTS→ EASY TO USE→ CASE WITH ROLLING SYSTEM→ COLORED ADAPTORS & TUBES→ CUSTOM DEVELOPMENT ON REQUEST
PSAT UNIVERSAL PsPSAT UNIVERSAL Ps is a static adaptor for virtuallyANY KIND OF AIRCRAFT.PSATUNIVERSALPs is very easy to use on the plane:→ power ON the Succion Unit→ place the Universal adapter on the aircraft and
adjust the Ps port→ release the Security Valve (blue): You are ready
to test your static port !Pneumatic insulation is made with rubber tube.PSATUNIVERSAL Ps is fittedwith a quick connector,which allows to use the adaptor as a cap for specialtests.
PSAT UNIVERSAL PtThe Universal Pitot Tube Adapter is a revolutionaryproduct that will let you test virtually any kind ofdynamic port (Pt) on your aircraft.PSAT UNIVERSAL Pt is very easy to use:→ place it around your pitot tube and tighten the ring→ you are ready to test your dynamic (Pt) port !PSATUNIVERSAL Pt is fittedwith a quick connector,which allows to use the adaptor as a cap for specialtests.
Main Features• Ps Single port adaptor
• Ps Double port adaptor
• Pt Adaptor and its tube holes clamp
• Ps and Pt connection cross
• Ps Tubes (1m, 3m, 5m and 10m)
Adaptator kit available for these aircrafts:
• A318/319/320/321• A330/340 (sauf A340-500)• A340-500• A380• A300/310• A350• A400M• Embraer phenom 100• Embraer phenom 300• Embraer Legacy 650• Embraer Legacy 500• Embraer Lineage 1000• Boeing 737• Dassault Falcon50/900/2000
• Dassault Falcon 7X• Gulfstream G450• Gulfstream G550• Gulfstream G650• Bombardier Challenger605/800
• Bombardier CRJ612• Cessna Grand caravan• Cessna Citation Sovreign• Cessna Citation X• Predator• Learjet 60
• Learjet 25-35-45• Beechcraft king Air• Casa• NH90• Lynx• Harfang• Puma• Alouette• Fennec• Cougar• Tigre• Transall• ATR42-72• Piper• Mitsubishi Solitaire /Marquise / Mu2M
• Cessna 550• MD80• Sabreliner 40• Cessna 150• Piper Aztec• Cessna citation Mustang• Viking Air 400• Cessna citation excel• Cessna citation CJ4• Hawker 400 XP• Hawker 4000
11 ATEQ - Test instruments for all aircrafts
LAB
hangar/ tarmacADSE 712 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2ADSE 543 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3ADSE 643 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4ADSE 650 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5ADSE 743 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6ADSE 744 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7ADSE 745 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8ADSE 746 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9PSAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
labCDP 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12ePlane PC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13CV 250 - 400 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14ADSE 740 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15ADSE 741 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16ADSE 715 RS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17H 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
electrical testsEEST 50-60 rack edition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20EEST 50-60 workshop edition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21AX 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23Accessories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24LRT 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25Accessories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26
all the specifications in this brochure can be modified
12ATEQ - Test instruments for all aircrafts
CDP6000 PITOT/STATICREADERFORLABORATORYANDWORKSHOP
→ ALTIMETERS READING→ AIRSPEED INDICATORS READING→ VERTICAL SPEED INDICATORS READING→ AIR DATA COMPUTERS READING→ PRESSURE SENSORS READING
The CDP 6000 is a complete high performancemulti pressure Ps, Pt and stand-alone static indica-tor specially designed to be used in the workshopor in the laboratory to test and calibrate all air dataequipment (altimeters, vertical speed indicators,anemometer,MACH-meterandair datacomputers ...)and sensors.
The high precision embedded sensors enable theCDP 6000 to be used as a pressure standard.
The CDP 6000 works with a USB cable for PCconnection.
Main Features• High accuracy, high resolution
• RVSM compliant
• Programmable leak test
• All four primary flight parameters displayed simultaneously
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature range Operating 10° to 40°C (50° to 104°F)
Storage -20° to +60°C (–4° to 140°F)
Power supply Lithium polymer Battery
Case Robust aluminiumEMC requirements - MIL STD 462D
Physical 240x120x210 mm (9.4x4.7x8.2) inch - 2.8kg (6.17 lbs)
Calibration Recommended period 12 months
Measurement specifications in standard conditions
FS = Full scale* Specifications in option (adjusted in our metrology laboratory with agreement)
Typical screen display
RVSM COMPLIANT
Pressurerange
AccuracyNo linearity+ Hysteresis
+ Repeatability(extanded uncertainty)
Maximumpressure
Long timedrift(1 year)
T° drift(ref 25°C)
Low pressuresensor
++— 1000 Pa 0,05% FS (Typ)0,25% FS (Max) 2500 Pa 0,5% FS -25 to 85°C
1% FS
Standardpressuresensor
2 bar absolute
5 bar absolute
20 bar absolute
0,04% FS
2 x FS
4 x FS
4 x FS
0,05% FS(Typical)
0,1% FS(Max)
-10 to 50°C0,5% FS
High pressuresensor
1,5 bar absolute
3,5 bar absolute
0,01% FSDrift time included
2 x FS
2 x FS0,01% FS -10 to 50°C
0% (integrated)
LAB
CDP 6000
13 ATEQ - Test instruments for all aircraftsePlane PC
LAB
AIRCRAFTSIMULATOR ePlanePCFORLABORATORYANDWORKSHOP
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ PRESSURE SENSORS TESTING→ AoA TESTING FOR SPECIFIC PROBES
The ePlane is a complete high performance multipressure Ps, Pt and AoA. It’s used for pitot statictesters demonstration and training without anyrisk to on board equipment.
The ePlane is composed of a casing in aluminium,a cable and three pneumatic plugs (Ps, Pt and AoA).
Main Features• Pneumatic connections Ps, Pt and AoA (option)
• High accuracy, high resolution
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min;and Mach number and needle equipment visualisation
• Software executable under Windows 2000 and XP
• USB cable for PC connection
General detailsTemperature range Operating 10° to 40°C (50° to 104°F)
Power supply Through USB
Case Robust aluminiumEMC requirements
Physical 126x107x57mm (5 x 4.2 x 2.2 inch) - 300g (0,66 lbs)
Calibration Recommended period 12 months
OptionalAoA sensor
Measurement specifications in standard conditions
Function Range Accuracy(1)
Static sensor 35 to 1355 mbar 0,1% FS
Pitot sensor 35 to 2700 mbar 0,1% FS
AoA sensor 35 to 1355 mbar 0,1% FS
(1) linearity + repeatability + hysteresis at ambiant +10° to +40°Cx 0,5 for +— 2°C lab use
Typical screen display for Ps / Pt
14ATEQ - Test instruments for all aircrafts
LAB
CV250-400 VACUUMCHAMBERSFORLABORATORYANDWORKSHOP
CV250 - 400
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ MANO-CONTACT TESTING→ PRESSURE SENSORS TESTING→ ALLNONPRESSURISEDEQUIPMENTTESTING
The CV 250 and CV 400 are vacuum chambersfor altitude flight simulation for avionics instrumentssuch as altimeters, rate of climb indicators and allnon pressurised equipment.
They are fitted with pneumatic and electricconnectors and a quick locking door.
The CV 250 and CV 400 have an optional vibratingtable.
Main Features• Only one generation channel for pressure or vacuum
• 370 mm (14.5 inch) internal diameter (CV 400)
• 230 mm (9 inch) internal diameter (CV 250)
• Max. dimensions of the instruments fitting in the chamber:- CV 400: 265x150x280 mm (10.4 x 5,9 x 11 inch)- CV 250: 145x110x280 mm (5.7 x 4.3 x 11 inch)
• Transparent door and case
• Overpressure secured at 1200 hPa
• Quick locking door
• Possible incline up to 20°
• Option: Vibrating table
15 ATEQ - Test instruments for all aircrafts
LAB
ADSE 740
PITOT/STATICTESTER ADSE740FORLABORATORYANDWORKSHOP
The ADSE 740 is a complete high performancedual pressure Ps and Pt standalone test benchspecially designed to be used in the workshopor in the laboratory to test and calibrate all airdata equipment such as altimeters, vertical speedindicators, air speed indicators, MACH-meter, airdata computers ...) and sensors.
The high precision embedded sensors enable theADSE 740 to be used as a pressure standard.
The user interface is programmed underWindows®
and Labview®, with a data base managed in aspreadsheet for easy evaluation, management,statistics and presentation.
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING
Main Features• 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 - 24 programs available
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature range Operating 15° to 40°C (60° to 104°F)
Storage -20° to +60°C (–4° to 140°F)
Power supply 90/240V, 50 to 400Hz AC, 150VA
Case 19” x 4 U x 524 mm (20.6 inch), 14kg (31 lbs)
Screen 17” LCD colour 2,5kg (5,5 lbs)
Calibration Recommended period 12 months
Ease of Use Windows human/machine interfaceProgram scriptEasy programming of test reports
Ease of maintenance Modular design permitting ease of accessibility tomechanical assemblies and electronic components
OptionalInternal pump: 60.000 ft - 6.000 ft/min (Volume dependant)
IEEE488 digital interface
Ps & Pt outlet at the back of the bench
Vertical housing
Specific Pt sensor for improved accuracy at low speed
Pneumatic connectors JIC 37 (AN4) or Staubli
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 60,000ft +— 1.5ft at 0ft
(up to -4,000ft to 100,000ft optional) +— 4ft at 30,000ft+— 16ft at 60,000ft
Altitude rate +— 0 to 6,000ft/min +— 1%(up to ++— 60,000ft/min optional) ++— 1%
Indicated 10 to 800 kts ++— 1kt at 50kts (++— 0.5kts at 50kts optional)
airspeed (up to 1000 kts optional) +— 0.2kt at 350kts (++— 0.1kts at 350kts opt.)+— 0.04kt at 650kts
Mach N° 0.1 to 4.0 Mach +— 0.001M at 0,8M/25,000ft
(0.1 to 10 Mach optional) +— 0.002M at 1,7M/30,000ft
Static sensor 30 to 1200 mbar 0,01% FS
Pitot sensor 30 to 3000 mbar 0,01% FS
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
RVSM COMPLIANT
SPVU 700:pressure and vacuum unit
16ATEQ - Test instruments for all aircrafts
LAB
ADSE741 PITOT/STATICTESTERFORLABORATORYANDWORKSHOPAll in one high performance Pitot Static Tester
ADSE 741
TheADSE 741 is a complete high performance threechannel Ps, Pt and AoA stand-alone test benchspecially designed to be used in the workshop orin the laboratory to test and calibrate all air dataequipment such as altimeters, vertical speedindicators, air speed indicators, pneumatic AoA(Angle of Attack) indicators, MACH-meter, air datacomputers, specific probes and sensors.
The high precision embedded sensors enable theADSE 741 to be used as a pressure standard.
The user interface is programmed underWindows®
and Labview®, with a data base managed in aspreadsheet for easy evaluation, management,statistics and presentation.
→ ALTIMETERS TESTING→ AIRSPEED INDICATORS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ AoA TESTING FOR SPECIFIC PROBES
Main Features• 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 - 24 programs available
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature range Operating 15° to 40°C (60° to 104°F)
Storage -20° to +60°C (–4° to 140°F)
Power supply 90/240V, 50 to 400Hz AC, 150VA
Case 19” x 4 U x 524 mm (20.6 inch), 14kg (31 lbs)
Screen 17” LCD colour 2,5kg (5,5 lbs)
Calibration Recommended period 12 months
Ease of Use Windows human/machine interfaceProgram scriptEasy programming of test reports
Ease of maintenance Modular design permitting ease of accessibility tomechanical assemblies and electronic components
OptionalIEEE488 digital interface
Ps & Pt outlet at the back of the bench
Vertical housing
Low range Pt sensor: 350 kts max for better accuracy
Pneumatic connectors JIC 37 (AN4) or Staubli
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 60,000ft +— 1.5ft at 0ft
(up to -4,000ft to 100,000ft optional) +— 4ft at 30,000ft+— 16ft at 60,000ft
Altitude rate +— 0 to 6,000ft/min +— 1%(up to ++— 60,000ft/min optional) ++— 1%
Indicated 10 to 800 kts ++— 1kt at 50kts (++— 0.5kts at 50kts optional)
airspeed (up to 1000 kts optional) +— 0.2kt at 350kts (++— 0.1kts at 350kts opt.)+— 0.04kt at 650kts
Mach N° 0.1 to 4.0 Mach +— 0.001M at 0,8M/25,000ft
(0.1 to 10 Mach optional) +— 0.002M at 1,7M/30,000ft
Static sensor 30 to 1200 mbar 0,01% FS
Pitot sensor 30 to 3000 mbar 0,01% FS
AoA sensor 30 to 3000 mbar 0,01% FS
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
SPVU 700:pressure and vacuum unit
17 ATEQ - Test instruments for all aircrafts
LAB
ADSE 715 RS
STATICTESTER ADSE715RSFORLABORATORYANDWORKSHOP
It can test virtually all altimeters
The ADSE 715 is a complete high performancesingle pressure Ps stand-alone test bench speciallydesigned to be used in the workshop or in thelaboratory to test and calibrate all air dataequipment such as altimeters, vertical speedindicators, air data computers ...) and sensors.
The high precision embedded sensors enable theADSE 715 to be used as a pressure standard.
The user interface running on a PC connectedthrough USB link is programmed under Windows®
and Labview®, with a data base managed in aspreadsheet for easy evaluation, management,statistics and presentation.
→ ALTIMETERS TESTING→ VERTICAL SPEED INDICATORS TESTING→ AIR DATA COMPUTERS TESTING→ PRESSURE SENSORS TESTING→ ALTIMETER’S WATCH TESTING
Main Features• Complete self check of set before use
• High accuracy, high resolution
• RVSM compliant
• Programmable leak test
• Programmable flight envelope to protect equipment under test
• Programmable (password write protected) test schedules - 24 programs available
• Selectable pressure units: hPa; mb; in Hg; mmHg; ft; m; kts; km/h, ft/min; hm/min, Mach number
Additionnal featuresTemperature 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 370x320x250 mm (14.6 x 12.6 x 9.8 inch), 7kg (15 lbs)
Calibration Recommended period 12 months
Ease of Use Windows human/machine interfaceProgram scriptEasy programming of test reports
Ease of maintenance Modular design permitting ease of accessibility tomechanical assemblies and electronic components
OptionalInternal Pump: 60.000 ft - 6.000 ft/min (Volume dependant)
Bigger Pumps: Altitude 100.000ft
19” 4U housing
Alticoder sensor
Measurement specifications in standard conditions
Function Range Accuracy
Altitude -2,300 to 15,000ft +— 1.5ft at 0ft
(up to -4,000ft to 80,000ft optional) +— 3ft at 15,000ft+— 12ft at 50,000ft
Altitude rate Up to +— 6,000ft/min +— 1%
Static sensor 30 to 1200 mbar 0,01% FS
- On-going developments may cause a change in specifications without notice.- Special developments may be considered on a case by case basis.
Typical screen display
RVSM COMPLIANT
18ATEQ - Test instruments for all aircrafts H 6000
LAB
H6000 HYDROGENPORTABLELEAKTESTERFORFINELEAKDETECTION
→ COST EFFECTIVE SOLUTION→ VOLATILE GAS WITH LOW VISCOSITY→ INDEPENDENT OF TEST VOLUMEAND TEMPERATURE
→ LEAK LOCALIZATION
The H 6000, a new comer in the ATEQ range ofleak detectors, is one of the finest gas tracer andhydrogen leak detectors on the market today.This gas is less expensive than Helium gas.Furthermore, it’s a volatile, non-toxic and non-poisonous gas without any environmental impact.
The H 6000 is equipped with all features for easyintegration in industrial processes and laboratories.
Main Features• Detection of leaking gas traces
• Range: 1.10-4 mbar l/s to 2.10-2 mbar l/s
• Generated Suction Flow control
• 128 programs
• IP 54 protection
• Internal memory: 2 Go
• Visual (red/green leds) and audible signal for results
• USB port
• Battery: 12VDC 4400 mA/h - Lithium Polymer technologyEasy removable battery pack - Autonomy 8 hours
• Bag for H 6000
Measurement principleThe part is filled with hydrogen gas 5% in Nitrogen gas.
For localization, the leaking gas is attracted in a suction probe to the sensor.
Applications• HVAC, Refrigeration and Automotive Leak Detection
• Automotive: leak localization, cooling systems, alloy wheel, …
• Domestic Appliances: compressor, …
• Oxygen cabin supply system for cabin pressurization, kerosene tanks testingCDH 6000 calibrator(option)
19 ATEQ - Test instruments for all aircrafts
ELECTRIC
AL
TESTS
hangar/ tarmacADSE 712 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2ADSE 543 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3ADSE 643 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4ADSE 650 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5ADSE 743 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6ADSE 744 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7ADSE 745 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8ADSE 746 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9PSAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
labCDP 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12ePlane PC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13CV 250 - 400 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14ADSE 740 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15ADSE 741 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16ADSE 715 RS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17H 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
electrical testsEEST 50-60 rack edition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20EEST 50-60 workshop edition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21AX 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23Accessories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24LRT 6000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25Accessories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26
all the specifications in this brochure can be modified
20ATEQ - Test instruments for all aircrafts EEST 50-60 rack edition
ELECTRIC
AL
TESTS
EEST50-60 BATTERYTESTERSERIESRACKEDITION
→ AUTOMATIC TEST BENCH FOR BATTERY MAINTENANCE→ ELECTRONIC MANAGEMENT SYSTEM→ 1 CHANNEL AUTOMATIC CYCLING BENCH→ ALL BATTERY TYPES→ SWITCHED MODE POWER SUPPLY
Mains Characteristics• 1 channel of charge/discharge 50V / 60A
Main powers available are indicative ones(Voltage and intensity in charge and discharge on each channel can be adapted upon request)
• Immediate or delayed test start.
• The Bench can can store 7 sequences of 20 stages
• Charge at I or U constant
• Discharge at I constant
• Stand by phase
• At constant intensity→ stop on voltage limit Min, Max and time of charge and discharge
• Charge at constant voltage→ Charging stop at I min or time or ΔI• Stop on limits – Delta V on charge at I Cst
• Alarms for check level of electrolyte and end of test
• Messages display or alarm when a stage is stopped
• Stage and test display
• Test time display
• U battery and I display and temperature display in in option
• U Max, min display and elements average in option
• Supplied or absorbed capacity display
• Internal temperature of power module display
Options• Individual element voltage measurement
• Cells deep discharge tool
• Battery temperature monitoring
Benches available on request
21 ATEQ - Test instruments for all aircrafts
ELECTRIC
AL
TESTS
BATTERYTESTERSERIES EEST50-60WORKSHOPEDITION/STANDALONEUNIT
EEST 50-60 workshop edition
→ COMPUTERIZED TEST BENCH FOR BATTERY MAINTENANCE→ ALL BATTERY TYPES→ WORKSHOP EDITION→ SWITCHED MODE POWER SUPPLY
Software interfaceMains Characteristics• 1 channel of charge/discharge 50V / 60A
Main powers available are indicative ones(Voltage and intensity in charge and discharge on each channel can be adapted upon request)
• Immediate or delayed test start.
• Control of voltages under 16 bits.
• Temperature Measurement with type K thermocouples.
• Alarm for electrolyte level.
• Shut down at predefined voltages Min, Max or delta V.
• Shut down as a function of time - Protection against temperature defect.
• Set up of multiple cycles and / or sequences
• Functioning in “local” mode, electronic management, if computer fails.
• Possibility of controlling the EEST from a remote location.
• Printing and automatic filing of data at the end of the test.
• Data protection and results saving and backup in case of power shutdown.
• Test result storage and research by user defined criteria.
• Curves drawing per phase.
Option• Connection systems for battery elements voltage, measurement or deep discharge
Typical screen display
22ATEQ - Test instruments for all aircrafts
ELECTRIC
AL
TESTS
EEST 50-60 workshop edition
EEST50-60BATTERYTESTERSERIESWORKSHOPEDITION
1 to 12 independent measurement channelsFUNCTION Characteristics : Standard : Option
Channel selection Selection of one channel available even if others are in use
Charging phase Constant or variable Intensity/Voltage
Adjustable from PC, profile, EXCEL file
On I constant, or variable, limit U max, -ΔV, time,temperature min and max, ΔT°/Δt
On U constant, or variable, limit I min, times ΔI (%),temperature min and max, ΔT°/Δt
Temperature protection probe type K, adjustable
Elements voltage measurementsand stop or stand by on elements voltage
Discharging phase Constant or variable Intensity
Adjustable from PC, profile, EXCEL file
U min limit, time, temperature min and max, ΔT°/Δt
Temperature protection probe type K, adjustable
Elements voltage measurementsand stop or stand by on elements voltage
Automatic deep discharge
Stand by phase Stand by period adjustable from PC
Cycle Choice of phases totally adjustable from PC
In chronological order or according to conditions
Repeat cycles
Sequence of cycles with different phases
Status of channels Permanent display of battery status, colour code
Status of test Permanent display of data regarding current phase
Errors message Error message display
and observations Automatic storage of all errors during test
Send by email: errors, observations, message
Blank play Check up of all contacts before test lanch
Pause, Stop Possibility to pause/stop during the test
Delayed or Select time and date for test startimmediate start
Results Data on test performed and tested battery
Plan voltage, intensity, temperature
Restored or absorbed capacity (% and Ah)
Voltage, Intesity and temperature at the beginningand at the end of phase
Events happened during the selected phase
Voltage of each battery elements
Average, Min and Max of element voltage
FUNCTION Characteristics : Standard : Option
Phase filing Automatic filing at the end of each phase(all data, history → traceability)
Save current data if error encountered
Archives in network
Consultation of archives between different benches
Print Automatic print of results at the end of test
Print on demand of the result of one battery for one phase(modification of axes available)
Possibility to print voltage acquisitions
Display Display of I, U, T° for each channel in test
Display zoom on curves
Display of each channel in test results
Display of elements tension
Intermittent printing Choice of step between prints in automatic mode
Inverter Protection and saving of all data during power cut
Alarm Buzzer for check-up level of electrolyte, temperature defect
Custom-designed Software of piloting and acquisitions(reception, statistics, curves upon request)
CMM programming
Power adjustable on request
Element voltage Individual measurement of each battery element voltage
Re-balancing Deep discharge or re-balancing test
Isolation Automatic isolation measurement
Export data To EXCEL
23 ATEQ - Test instruments for all aircrafts
ELECTRIC
AL
TESTS
AX 6000
PORTABLEMILLIOHMMETERAX6000FORALLAIRCRAFTS
AX6000: The right solution for bonding resistancemeasurement according to all current aircraftspecifications on plane, helicopter, rocket, armyvehicles for both production and maintenance.It is a very easy-to-use and versatile instrument,for applications requiring up to 10 A current mea-surements.
Its ergonomics allow the user to use it either placedon the ground or across one’s shoulder or chest.A wide back-lit LCD display combined with an intui-tive keyboard ensures simple and easy operation.
Technical characteristicsPresentation 240x120x210 mm (9.4 x 4.7 x 8.3 inch) - < 2kg (6lbs)
International Standards Complies with: CE: 61010-1 ; CEM: 61326-1 and 55011
Temperature Operating: 0° to +50°C (25° to 122°F)
Storage: -20° to +60°C (-4° to 140°F)
Relative humidity < 90% none condensing
Use Portable instrument which can be used on the groundor across one’s shoulder or chest.
Accessories• Transport case
• Bag for AX6000
• Kelvin tips
• Additional battery
• Additional battery charger
• Extension cable
• See accessories for full detailed list
Measurement rangeManual Mode Automatic mode
Range Current Range Current
6 mΩ (2 mΩ) 1A - 10A (3A) 1 μΩ - 600 mΩ 10A
60 mΩ (20 mΩ) 0,1A - 1A - 10A (3A) 10 μΩ - 6 Ω 1A / 0,1A
600 mΩ (200 mΩ) 0,1A - 1A - 10A (3A)
6 Ω 0,1A - 1A
Range Measurement current Accuracy Resolution
6 mΩ 1A +— (0,1% MV + 6 μΩ) 10 μΩ10A 1 μΩ
60 mΩ 0,1A +— (0,1% MV + 60 μΩ) 100 μΩ1A - 10A 10 μΩ
600 mΩ 0,1A - 1A - 10A +— (0,1% MV + 0,6 mΩ) 100 μΩ6 Ω 0,1A - 1A +— (0,1% MV + 6 mΩ) 1 mΩ
MV = Measured ValueThe 3A option is in replacement of the 10A current.
Range Measurement current Accuracy Resolution
2 mΩ +— (0,1% MV + 6 μΩ) 10 μΩ20 mΩ 3A +— (0,1% MV + 60 μΩ) 10 μΩ200 mΩ +— (0,1% MV + 0,6 mΩ) 100 μΩ
→ MANUAL OR AUTO RANGE→ FROM 1 μΩ TO 6 Ω→ 4 WIRE MEASUREMENT→ MEMORY OF 2000 READINGS→ COMPACT AND LIGHT WEIGHT (< 2 Kg)
24ATEQ - Test instruments for all aircrafts
ELECTRIC
AL
TESTS
AX 6000
AX6000Accessories
Plastic safety caseThe AX plastic yellowcase can carry allwhat the operator needs to work with:→ AX 6000 with its bag→ Battery pack→ Probes→ Clips→ Manual
The yellow case is weatherproofand shock resistant430x530x230 mm (16.9 x 20.9 x 9.1 inch)MB-0151: Yellow case
Front-BagThe AX front bag frees your hands,making it so easy to take measurements.The large LCD screen is at the rightdistance to be read easily.
EG-0459 (50 x 13)EG-0460 (100 x13)EG-0468 (150 x 13)
MZ-0257 (head probe x 13)
EG-0269: small kelvin clip kitEG-0271: Extra small kelvin clip
EG-0264: Medium kelvin clip kit
EG-0257:5m cable (15 ft)
EC-0316:Staight-in plug
EZ-0082:Medium kelvin clip
EG-0363:25m cable (60 ft)on cable reel
EG-0261: 50m cable (150 ft)EG-0259: 90m cable (270 ft)on cable reel
EG-0270: Big kelvin clip kit
Special Kelvin LeadThis kelvin probe setis used for very pre-cise measurements;3 electrodes tips andone alligator clip areconnected to theAX 6000 through a double cable fitted withconnectors.Banana plugs permit the connection of many dif-ferent measurement tools.
Kelvin Clips
Cable and Reels
Power
Spare parts
EG-0266:Special AnalyseKelvin Probe Set
MB-0147: Front-bag
TZ-0098:Battery pack
E5-0014:AC/DC Adaptor
Kelvin ProbesAll probes are fittedwith a fixed pin and amoving pin.Themoving pin establish the current and the fixedone reads voltage. Measurement is automaticwhen fixed pin touches the part to be measured.A 2 meter cable (6 ft) with the connector and arubber pin protection to the AX 6000.
25 ATEQ - Test instruments for all aircrafts
ELECTRIC
AL
TESTS
LRT 6000
LRT pack
PORTABLEMICRO-OHMMETER LRT6000ANDLOOPRESISTANCETESTER
FORALLAIRCRAFTS
→ FROM 0,1 μΩ TO 200 mΩ→ USB PORT→ EASY TO READ LARGE DISPLAY→ COMBINED CLAMP→ MEMORY OF 2000 READINGS→ COMPACT AND LIGHT WEIGHT(< 2 Kg)
LRT 6000: The right solution for impedanceresistance measurement in compliance with allaircraft specifications on plane, helicopter, rocket,army vehicles for both production andmaintenance.
It is a very easy-to-use and versatile instrument.
Its ergonomics allow the user to use it either placedon the ground or across one’s shoulder or chest.Awideback-lit LCDdisplay combinedwith an intuitivekeyboard ensures simple and easy operation.
Technical characteristicsPresentation 240x120x210 mm (9.4 x 4.7 x 8.3 inch) - < 2kg (6lbs)
International Standards Complies with: CE: 61010-1 ; CEM: 61326-1 and 55011
Temperature Operating: 0° to +50°C (25° to 122°F)
Storage: -20° to +60°C (-4° to 140°F)
Relative humidity < 90% none condensing
Use Portable instrument which can be used on the groundor across one’s shoulder or chest.
Accessories• Transport case
• Bag
• Additional battery
• Additional battery charger
• See accessories for full detailed list
Measurement rangeI Loop range Accuracy Rc range Accuracy
mΩ μΩLoop Resistance 10A 0.1 to 20.00 +/- (10% MV - -
(Loop) Resolution: + 0,02 mΩ)
0.01
Micro ohmmeter 10 to 150 A 0.01 to 20.00 +/-(10% MV 0.1 to 500.0 +/-(10% MV
High Current Resolution: Resolution: + 0.02 mΩ Resolution: +1μΩ)
(HC μΩ) < 100 A: 0.1 0.01
> 100A: 1.
MV = Measured Value
26ATEQ - Test instruments for all aircrafts
ELECTRIC
AL
TESTS
LRT 6000
LRT6000Accessories
Plastic safety caseThe LRT6000 black case can carryall the operator needs to work with:→ LRT6000 loop tester→ AC/DC adaptor CE plug→ Battery pack→ 1 ohm master→ Probes kit + Probes head kit→ 2 Clamps→ Winateq software→ USB cable→ Front bag→ Black case→ User manual
The black case is weatherproof
and shock resistant MB-0505
Front-BagThe LRT front bag free your hands,making it so easy to take measurements;The large LCD screen is at the rightdistance to be read easily.
CLP1
CLP2
Probes kit
Ohm masterWith 3 contacts resistance points
Power
MB-0147: Front-bag
E2-0249
EG-0426 (probe)
MZ-0258 (probe head)
ClampsSmall clamp CLP1, 3meters cable supply with a bag.EG-0425
Big clamp CLP2, 3meters cable supply with a bag.EG-0463
27 ATEQ - Test instruments for all aircrafts
ABOUTATEQATEQ is a worldwide leader in leak testers, operating in 35 countries all over the world.The ATEQ group has been specialized for more than 35 years in Leak, Flow, Electricaltesting, andmore recently TPMS tools (Tire Pressure Monitoring System). ATEQ has madeits fame and reputation on high quality instruments and 24/7 reliable service.
AERONAUTICSDIVISIONATEQ is now a worldwide manufacturer of automated Pitot/Static (ADSE), Pitot/Staticadaptors, leak detectors, bonding, loop and battery testers.For more than 20 years, OMICRON has been specialized in control and measurementsystems for aviation, aerospace, defense, automotive andmedical industries. Its know-howin pressure and electronic measurement led OMICRON to develop aviation on-boardcontrol equipment.In 2008, OMICRON became a member of the ATEQ Group. This merging gives ATEQ anopportunity to provide its customers on-site service, offer equipment most adapted totheir requirements, as well as a fast answers to all their needs.The first priority of ATEQ has always been to provide the highest quality instruments andservice available on the market.