background image

Microair Avionics 

EC2002 Altitude Encoder 

16

th

 April 2010 

EC2002 Installation Manual 01R12.doc 

Page  5  of  16 

 

 

 
 

2.0

 

DESCRIPTION 

The EC2002 is housed in a 1mm black anodised case, with 
a mounting flange at each side. 

 

 

Fitted to one end of the case are a DB15 male connector for 
all electrical connections and a female 1/8” NPT fitting for 
connection to the aircraft’s static air pressure system. At the 
opposite  end  is  the  nameplate  showing  the  compliance 
statements, the part number, serial number, and mod status. 

 

 

The  top  of  the  case  is  fitted with  a  label  which  has  the pin 
assignments for the DB-15 connector, and clearly identifies 
the NPT fitting. There are two holes in the top of the case to 
access the HIGH and LOW keys. These keys are used in the 
calibration  of  the  EC2002,  and  are  clearly  marked  on  the 
top cover label. 

 

 

The EC2002 is fitted with a sensitive pressure transducer to 
sense  the  air  pressure  present  at  the  NPT  fitting.  The 
transducer output  is  “digitised”  into  a  numerical  value  and 
outputted as an altitude via the 10 line Gillham interface and 
simultaneously to the serial data interface. The EC2002 will 
typically start outputting altitude data 10  seconds  after being 
turned on. 

 

 

The  maximum  calibration range  is  between  -1000  feet  and 
+35,000  feet. The 

HIGH 

and 

LOW 

keys provide an offset to 

adjust the outputted altitude value up or down in 25ft steps. 

 

 

The EC2002 is temperature controlled to ensure  the pressure 
transducer  is  at  nominal  temperature,  in  an  ambient 
temperature range of -20 to +55 degrees C. A  heater element 
maintains  the  pressure  transducer  core  temperature  within 
operational specification. Power consumption with the heater 
element off is 10mA, and a maximum of 100mA @ 14V or 
200mA @ 28V with the heater element on. The heater will 
be  fully  off  when  ambient  air  temperatures  are  above  15 
degrees C. 

 
 
 
 
 

IMPORTANT NOTE 

The EC2002 will cease outputting altitude data if: 
1.

 

The pressure altitude goes above 35,000 feet 

2.

 

The pressure altitude drops below -1000 feet 

3.

 

The sensor temperature is not within operational range 

Содержание EC2002

Страница 1: ...Microair Avionics Pty Ltd 601 Curtin Ave E Pinkenba QLD 4008 Australia Tel 61 7 4160 8200 e mail support microair aero...

Страница 2: ...Microair Avionics Pty Ltd CURRENT REVISION STATUS Revision Date Change 1 0 23 09 03 Initial Draft 01R2 18 05 07 Specifications and calibration procedures updated 01R3 28 06 07 Minor amendments 01R4 0...

Страница 3: ...DUCTION 4 1 1 ATSO APPROVAL 4 1 2 RTCA COMPLIANCE 4 2 0 DESCRIPTION 5 3 0 INSTALLATION 6 3 1 PHYSICAL REQUIREMENTS 6 3 2 ELECTRICAL REQUIREMENTS 8 4 0 SERIAL ALTITUDE OUTPUT 9 5 0 FIELD CALIBRATION 11...

Страница 4: ...ecification installation methods and calibration procedures of the EC2002 Altitude Encoder 1 1 ATSO Approval Pending 1 2 RTCA Compliance The EC2002 hardware development is compliant to RTCA DO 254 lev...

Страница 5: ...NPT fitting The transducer output is digitised into a numerical value and outputted as an altitude via the 10 line Gillham interface and simultaneously to the serial data interface The EC2002 will typ...

Страница 6: ...he purpose of mounting Microair recommends that the installer should consider the fact that the encoder may have to be dismounted to allow for recalibration periodically The retaining hardware should...

Страница 7: ...y to remove the top cover and set the serial data output switches for the correct data format and resolution The switch settings have no effect on the Gillham output lines Refer to section 4 0 for for...

Страница 8: ...should be clearly labelled as ALTITUDE ENCODER A dedicated ground line should be run from the EC2002 to the transponder and be grounded to the transponder s power ground to ensure correct signal leve...

Страница 9: ...ude digits T 25 checksum carriage return AL 05200T 25D8 CR Magellan 1200bps MGL sign five altitude digits T 25 checksum carriage return MGL 05200T 250C CR Northstar Garmin 2400bps ALT space five altit...

Страница 10: ...ON Garmin Trimble 25 steps ON OFF ON OFF ON ON Microair 100 steps ON OFF OFF OFF ON OFF Microair 25 steps ON OFF ON OFF ON OFF Microair 10 steps ON ON OFF OFF ON OFF Microair 1 steps ON ON ON OFF ON O...

Страница 11: ...ibration check over any altitude range from 1000 feet to 38 000 feet Where the technician is required to adjust the EC2002 refer to section 5 1 IMPORTANT NOTE To complete the calibration process of th...

Страница 12: ...5 050 and note the transition error Step 4 If the average transition error from steps 2 3 is greater than 25ft use an appropriate blunt tool to press either the HIGH or LOW keys to increase or decreas...

Страница 13: ...Microair Avionics EC2002 Altitude Encoder 16th April 2010 EC2002 Installation Manual 01R12 doc Page 13 of 16 6 0 TECHNICAL DRAWING WEIGHT 95g 3 oz...

Страница 14: ...Microair Avionics EC2002 Altitude Encoder 16th April 2010 EC2002 Installation Manual 01R12 doc Page 14 of 16 7 0 WIRING DIAGRAMS 7 1 Gillham Output 7 2 Serial Output...

Страница 15: ...lures due to abuse misuse accident unauthorised alteration or repairs carried out by parties other than Microair Avionics or an approved Microair Avionics Service Centre This warranty does not cover f...

Страница 16: ...Microair Avionics EC2002 Altitude Encoder 16th April 2010 EC2002 Installation Manual 01R12 doc Page 16 of 16 Supplied by...

Отзывы: