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Name：
Civil Range Air Data Test Set |
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Model：
MPS31C |
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Supplier：DMA-Aero |
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| Contact Info |
11 Old Sugar Hollow Road Danbury, CT 06812
Tel:203 790-8371
Fax:203 743-2051
E-mail:sales@dma-aero.com
Web:www.dma-aero.com |
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Product Introduction： |
| SuPPlying AiR DATA TEST SETS To ThE woRlD |
| DMA traces its origins back to 1938, mainly as a test equipment manu-facturer to support European aviaton requirements. Today DMA sup-ply precision Air Data Test Sets and other aviaton ground support equipment to aircraf manufacturers, repair statons and operators throughout the world. |
| flighT linE TESTER foR DEMAnDing APPliCATionS |
| The MPS31C is a two channel digital technology portable Air Data Test Set incorporatng many standard features normally found on more expensive test instruments. The constructon is both rugged and rainproof for de-manding fight line use. The unit is housed in a single wheeled case with a stowable handle. |
| EASy inTuiTivE inTERfACE |
Using logical key press routnes the MPS31C is easy to use by both beginners and experts. Testng and trouble shootng can be performed via the built-in intuitvely arranged color-coded keypad and large 4 x 20 character back-lit display. For a remote locaton such as the fight- deck, three control optons are available: the Hand Held Remote Control, the Touch Screen Remote Control or a wireless Bluetooth connected PDA. All the important air data functons are simultaneously displayed on all interfaces, constant screen or menu changes are not required. Readings of both commanded and measured test values are displayed.
Laboratory testng can also be performed by a PC connected via RS232 to the remote hand terminal connector. The comprehensive manuals include all the control instructons. ADWIN sofware is available as a ready-to-run PC based interface. |
| ACCuRACy AChiEvED by ThE EnD of SElf TEST |
| A vibratng element absolute transducer is utlized for the statc, alttude channel and a diferental transducer for the Qc/Pt, airspeed channel. Pressure and temperature characterisaton is applied to the sensors ensuring very high accuracy is achieved at all operatng pressure values, without any signifcant warm-up tme. |
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Technical Parameter： |
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PARAMETER |
RANGE |
RESOLUTION |
ACCURACY |
CONTROL STABILITY |
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MEASURE |
CONTROL |
MEASURE |
SETPOINT |
C
I
T
A
T
S |
Alttude (ft) |
-2,000→65,000 |
-2,000→65,000 |
1 |
1 |
± 3 @ SL
± 5 @ 30,000
± 20 @ 60,000 |
± 2 |
Vertcal
speed |
Standard (ft/min) |
0→6,000 |
0→6,000 |
5 @ < ,1500 [2] |
1 |
± 10 ± 1% of reading |
± 10 ± 1% of reading |
| high rate [1] (ft/min) |
0→20,000 |
0→20,000 |
| Statc (inHg abs)(hPa abs) |
1.7→32
56→1089 |
1.7→32
56→1089 |
0.001
0.01 |
0.001
0.01 |
± 0.003
± 0.1 |
± 0.002
± 0.07 |
T
O
T
I
P |
Airspeed |
Standard [3](kts) |
10→700[3] |
10→700[3] |
1 @ < 50
0.1 @ > 50 |
0.1 |
± 0.5 @ 50
± 0.1 @ > 500 |
± 1 @ < 50
± 0.2 @ 300
± 0.1 @ > 500 |
| Ultra low speed functon [4](kts) |
5→200 |
5→200 |
0.1 @ > 20 |
± 0.001 inHg |
± 0.001 inHg |
| Airspeed slew rate (kts/min) |
0→500 |
0→500 |
10 |
10 |
± 10 ± 1% of reading |
± 5% |
| Mach No. (mach) |
0→6 |
0→6 |
0.001 |
0.001 |
< ± 0.002 |
± 0.002 |
| Pitot (Qc) |
Standard (inHg dif)(hPa dif) |
0→30.8
0→1042 |
0→30.8
0→1042 |
0.0001
0.01 |
0.0001
0.01 |
± 0.003
± 0.1 |
± 0.003
± 0.1 |
| Opton I (inHg dif) (hPa dif) |
0→47
0→1592 |
0→47
0→1592 |
± 0.005
± 0.17 |
± 0.005
± 0.17 |
| Engine Pressure Rato (EPR) |
1→2.5 @ SL |
1→2.5 @ SL |
0.001 |
0.001 |
0.001 |
± 0.001 |
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Notes: Control capability on all load volumes : Statc: 0 to 125 cu. in. (2 L), Pitot: 0 to 80 cu. in. (1.3 L). Larger volume
1.High rate achievable into small system volumes
2.10 above 1,500 f/min, 25 above 3,000 f/min, 50 ab
3.Range increase to 830 kts with Opton I
4.Standard mode of test set below 200 kts |
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| Related Document： |
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DownLoad
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