Winter IPK09 User Manual Download Page 16

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IMPORTANT NOTE:

1. The altitude is the pre-set measured value when the ALT / IAS Mode is activated.
2.   If the ALT / IAS Mode was activated when the device was switched off automatically 

or manually, the status will be restored when the device is powered up again, and the 
altitude will be displayed.

3.  When the M203 displays the air speeds and the power is shut off (manually or auto-

matically), also when the Program mode is activated or the „Tare“ key is pressed, the 
device will revert to displaying the altitude when the device is powered up again or the 
gauging mode is selected. This function is intended to prevent errors in the measure-
ment of air speeds and is necessary, since the taring function is used at barometric 
pressure in order to be able to measure the air speeds. The barometric pressure is de-
pendent upon changes in weather conditions. Resetting to altitude measurement when 
the device is shut down, starting the Programming mode or pressing the taring function 
all require that a new taring value be measured prior to each air-speeds measurement.

Test connection (7) – Connect the hose line between the tester and the aircraft
(Warning! In complete installations, the line must always be simultaneously connected to 
the gauging nozzle and to the static via the „T“ connector. Also, one must ensure that no 
additional gauging instrument (e.g. flight-hours counter) is connected to the installation 
without a static connector! 

SIMULTANEOUS TESTING OF THE ALTITUDE DISPLAY UNITS AND 

THE IMPERMEABILITY OF THE ENTIRE INSTALLATION

Please note:
The display device is adjusted based on sea level (QNH) in the altitude display units.

1. Switch on Pump Vacuum (3) 
2.  Vacuum (10) – Set the „pull“ level by turning to the left. Here, it is recommended to 

initially set the value „5“ as the optimum number. The value must be respectively 
increased or decreased according to the length of the particular line and the power 
loss after the activation of the control valve (8); for instance, when altitude changes too 
quickly or when the activation limit is too low, and/or when the altimeter fails to show a 
further change in altitude (stops). Activation of the controller by applying light pressure 
prevents damage to the aircraft and analysis-device systems.

3.  Regulator valve (8) – Triggering of test values and/or comparison of display values 

between the test device and the test object. When the maximum altitude for the re-
spectively installed altimeter is attained – Standard display variants 10,000 ft (3000 m), 
20,000 ft (6000 m) (max. 36,000 ft / 12,000 m), close all valves and turn them to the 
right, then shut off the pump (3) and perform the impermeability test (see Meriam ope-
ration guide) Exposure time  and change in accordance with the test sheet (see Meriam 
operation guide) – System values?

4.  If the nominal values are not attained, the system must be inspected for errors / lea-

kages. This may include the individual inspection of each installed device.

HYSTERESIS TEST

1.  Air escape valve (11) – Triggering of test values and/or comparison of display values 

between the test device and the test object.

TEST AT SEA LEVEL -0-  

1. Switch on Pump Pressure (4).
2. Select the flow rate for the descending-value setting on the valve (9).
3.  Regulator valve (8) – Warning! Triggering of test values and/or comparison of display 

values between the test device and the test object. When the minimum altitude is 
attained (max. -2,000 feet), shut off the pump (4) and open the air escape valve (11). 

PERFORMING ALTITUDE AND AIR-SPEED INDICATOR MEASUREMENTS

1. Main switch (2) – to ON
2. Display device (1) – to ON
3.  Setting the display units (see Meriam operation guide), comparison of the measured 

values.

4.  Test connector (7) – Hose line between the tester and altimeter or the air-speed  

indicator.

5.  Switch on the Vacuum Pump (3) for the altimeter and the pressure pump (4) for the 

air-speed indicator.

6. Valve (10) or (9) – set the flow rate.
7.  Regulator valve (8) – Triggering of test values and/or comparison of display values 

between the test device and the test object. Take special precautions when performing 
the air-speed indicator test!

8. Perform the impermeability test (see Meriam operation guide); shut off pump.
9.  Air escape valve (11) – Triggering of test values and/or comparison of display values 

between the test device and the test object.

10. Shut off pump (3) or pump (4) and open the air escape valve (11).

 
  

Summary of Contents for IPK09

Page 1: ...BEDIENUNGSANLEITUNG USER S MANUAL WINTER IPK09...

Page 2: ...ng der Hysterese 15 Pr fung auf Meeresh he 0 15 Durchf hrung der H hen und Fahrtmesserpr fung 15 Anschlussschemata 16 DISPLAYS AND CONTROLS 20 TECHNICAL DATA 22 TEST PROCESS OPERATION GUIDE Reading th...

Page 3: ...kann bei geschlossenem Deckel aus dem Pr fger t gef hrt werden sodass das Ger t w hrend des Ladens geschlossen bleiben kann 7 TESTANSCHLUSS Anschluss f r die Schlauchleitung zwischen Tester und Flugz...

Page 4: ...0 ft 16000 ft 240 ft 20000 ft 300 ft TECHNISCHE DATEN PR FBEREICHE H he 600 m bis 12000 m 2000 ft bis 36000 ft Fahrt 0 bis 450 km h 250 kts 300 mph GENAUIGKEIT 0 025 vom Messbereichsendwert AKKU 12 V...

Page 5: ...er feet TS 10 210 14 20 30 90 TSO 30 90 NfP 30 90 NFP NFP Messpunkt Toleranz Messpunkt Toleranz 0 m 5 m 0 ft 15 ft 400 m 20 m 5000 ft 100 ft 800 m 20 m 10000 ft 200 ft 1000 m 20 m 15000 ft 300 ft 2000...

Page 6: ...schen Statik und Staudruck Druck im Schlauchverbindungs System f r ca 5 min ausgleichen lassen Die Schlauchleitung en sollten danach nicht mehr ber hrt oder bewegt werden ansonsten droht eine Fehlanze...

Page 7: ...ellte Messung des M203s die H he Durch Dr cken der Tare Taste wird der allgemein g ltige barometrische Druck genullt und die Anzeige zum Anzeigen der Luftgeschwindigkeit ge ndert Um zur H he zur ckzuk...

Page 8: ...i zu schneller H hen nderung oder niederer Ansprech schwelle bzw wenn der H henmesser nicht weitere H hen nderung zeigt stehen bleibt Eine behutsame Bet tigung des Reglers verhindert Besch digungen am...

Page 9: ...ndenz hler Me druck Stat Druck 12 24 V TEK D se ANSCHLUSSSCHEMA IM NORMALEN ZUSTAND FAHRMESSERPR FUNG IM SYSTEM ANSCHLUSSSCHEMA DER FLUGZEUGSYSTEME H henmesser Variometer Fahrtmesser Flugstundenz hler...

Page 10: ...VARIOMETERPR FUNG H henmesser H henmesser Variometer Variometer Fahrtmesser Fahrtmesser Flugstundenz hler Flugstundenz hler Me druck Me druck Stat Druck Stat Druck 12 24 V 12 24 V TEK D se TEK D se Pr...

Page 11: ...e of the automatic battery charger The cable can remain connected also when the testers cover is closed 7 TEST PORT Connector for the hose between tester and unit under test or aircraft Roll up tool f...

Page 12: ...00 m 90 m 12000 ft 180 ft 16000 ft 240 ft 20000 ft 300 ft TECHNICAL DATA RANGE ALTITUDE 600 m to 12000 m 2000 ft to 36000 ft AIRSPEED 0 to 450 km h 250 kts 300mph ACCURACY 0 025 F S BATTERY 12 V 4 2 A...

Page 13: ...meter feet TS 10 210 14 20 30 90 TSO 30 90 NfP 30 90 NFP NFP measuring point tolerance measuring point tolerance 0 m 5 m 0 ft 15 ft 400 m 20 m 5000 ft 100 ft 800 m 20 m 10000 ft 200 ft 1000 m 20 m 150...

Page 14: ...or the impact pressure connector according to the Connect the wiring diagram after the test process T fitting between static and impact pressure Neutralize the pressure in tube system for approx 5 min...

Page 15: ...ce ALT IAS Mode is selected the M203 s default measurement is altitude Pressing the Tare key nulls the prevailing ba rometric pressure and converts the display to air speed indication To revert back t...

Page 16: ...altimeter fails to show a further change in altitude stops Activation of the controller by applying light pressure prevents damage to the aircraft and analysis device systems 3 Regulator valve 8 Trigg...

Page 17: ...YSTEMS Altimeter Variometers Airspeed Indicator Flying hours counter Total Pressure Static Pressure 12 24 V Total Energy Compensating Office Altimeter Variometers Airspeed Indicator Flying hours count...

Page 18: ...speed Indicator Flying hours counter Flying hours counter Total Pressure Total Pressure Static Pressure Static Pressure 12 24 V 12 24 V Total Energy Compensating Office Total Energy Compensating Offic...

Page 19: ...r GmbH Co KG Bordger te f r die Luftfahrt Hauptstr 25 Postfach 6 D 72417 Jungingen Telefon 49 0 74 77 26 2 Fax 49 0 74 77 10 31 info winter instruments de technik winter instruments de www winter inst...

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