TL Electronic TL-3524 Manual de usuario

TL-3524

USER`S MANUAL

TL elektronic

Airport, Building 125, Hradec Kralove

503 41, Czech Republic

TL elektronic

Except as expressly provided below, no part of this manual may be downloaded, transmitted, copied,

reproduced, disseminated or stored in any storage medium, for any purpose without the express prior

written consent of the TL elektronic company.Address your questions about the technical information

to TL elektronic. Other information about sale, distribution should be directed to our exclusive

distributors (see World Distributor list on our website).

Producer‘s address:

TL elektronic Inc.

Airport, Building 125,

503 41 Hradec Kralove, Czech Republic

Fax: +420 49 548 23 94 E-mail: [email protected]

Website Address: www.tl-elektronic.com

Please, send your e-mail address to [email protected] to receive the latest

information about software upgrade.

Send your ideas to innovation@tl-elektronic.com.

We will evaluate your suggestion and provide an update.

Record of revision

Revision Revision Description ECO# Insertion By

date date

A 1/6/03 Initial Release ---

B 1/7/04 Language correction 0001

Windows is registered trademark of Microsoft Corporation.

All trademarks and registered trademarks are acknowledged.

SchecK® is registered trademark of TL elektronic.

iFamily® is registered trademark of TL elektronic.

sModern® is registered trademark of TL elektronic.

All information in this User's manual is subject to change without prior notice.

Page i TL-3524 USER`S MANUAL

Rev. B P/N 03-3524-2003

Page ii TL-3524 USER`S MANUAL

Rev. B P/N 03-3524-2003

TABLE OF CONTENTS

1. GENERAL DESCRIPTION

1.1. Introduction........................................................................................... 1-1

1.2. Instrument Description........................................................................... 1-1

1.3. Technical Specifications............................................................................... 1-2

1.4. Limited Conditions...................................................................................... 1-3

1.5. Limited Warranty......................................................................................... 1-3

1.6. Limited Operation........................................................................................ 1-3

2. INSTALLATION

2.1. Introduction............................................................................................... 2-1

2.2. Rack Consideration.................................................................................... 2-1

2.3. Installation into Panel.................................................................................. 2-1

2.4. Static Pressure Connection........................................................................... 2-1

2.5. Instrument Dimensions................................................................................. 2-2

3. SYSTEM INTERCONNECT

3.1. Pin Function List........................................................................................ 3-1

3.2. TL-3524 Interconnects................................................................................ 3-2

3.3. TL-3524 Connector Location........................................................................ 3-3

4. NAV-MENU DESCRIPTION

4.1. How to Control Instrument via NAV-MENU.................................................. 4-1

5. INSTRUMENT SETUP

5.1. First Instrument Turn-on................................................................................ 4-1

5.2. Main Set-up Functions Description................................................................. 5-1

5.3. How to Select Altitude Units..........................................................................5-2

5.4. How to Select Barometric Pressure Units.......................................................5-2

5.5. Show Altitude in 1 or 10 Unit Resolution.........................................................5-2

5.6. How to Select Default Transition Altitude....................................................... 5-2

5.7. Go to Calibration........................................................................................... 5-3

5.8. Restore Factory Calibration........................................................................... 5-3

5.9. Do Your Calibration.......................................................................................5-3

5.10. Strobe Signal of Transponder........................................................................5-4

5.11. Oxygen Warning..........................................................................................5-4

5.12. User Button................................................................................................ 5-4

5.13. iFamily® and Other Connecting Devices.......................................................5-4

6. OPERATION MANUAL

6.1. Left Menu Description................................................................................. 6-1

6.2. Right Menu Description.................................................................................6-2

6.3. How to Change Configuration........................................................................6-3

6.4. Set Alert Warning......................................................................................... 6-3

6.5. How Alert Warning Works............................................................................ 6-3

6.6. Set MDA or Approach Altitude..................................................................... 6-4

6.7. MDA or Approach Warning.......................................................................... 6-4

6.8. Set Different Transition Altitude.....................................................................6-4

6.9. „TRANSITION ALTITUDE REACHED“ Message...................................... 6-4

6.10. Memory of Maximum Reached Altitude....................................................... 6-5

6.11. Delete Long-term Memory of Altitude.......................................................... 6-5

6.12. „OXYGEN“ Message................................................................................. 6-5

6.13. Measuring Altitude out of Range.................................................................. 6-5

7. SchecK DESCRIPTION

7.1. Method of SchecK® for Storing into Memory................................................. 7-1

8. Transponder Connection

8.1. Table of Transponder Connection................................................................... 8-1

Page 1-1 TL-3524 USER`S MANUAL

Rev. B P/N 03-3524-2003

1. GENERAL DESCRIPTION

1.1. INTRODUCTION

This manual describes the physical, mechanical and electrical features and functions of the TL-3524

Altimeter.

1.2. INSTRUMENT DESCRIPTION

The Altimeter incorporates the new generation of a precise sensor with the temperature and altitude

calibration, which enables measuring the altitude immediately after turning the instrument on, without having

to wait a few minutes. Another part of the Altimeter is an encoder of the altitude for any transponder, see

the table, page 8-1.

The TL-3524 incorporates a 10.000 line long-term memory and SchecK memory (see page 7-1) for

storing the measured values at 0.1 to 60 second sample rate.

The TL-3524 enables the pilot to keep the set altitude. In case of exceeding the set altitude, the pilot will

be warned by the acoustic or visual signalization. It is also possible to set the MDA, the approach altitude

and the transition altitude. When reaching the transition altitude, a message will show on the display.

If the alarm warning has be activated either by the lack of oxygen or by high altitude, the instrument will

display a Service message after the next turn-on to inform the user that the altitude has been exceeded.

The User button can be programmed in the main set-up for the quick display of the maximum reached

altitude or for the display of the currently set barometric pressure.

It is possible to download the measured values from the instrument via the serial cable RS-232c into your

PC.

1.3. TECHNICAL SPECIFICATIONS

The producer guarantees all stated technical parameters only when the instrument is installed by an

authorized service or an aircraft manufacturer.

1.3.1 Physical characteristics

Width 71mm (3.346 inches)

Height 67mm (3.346 inches)

Depth 92mm (3.6220 inches) including connectors with cover

Panel hole 57mm (3.149 inches) diameter

TL-3524 Weight 0.30 kg (0.66 lbs)

TL-3524 Harness 0.05 kg (0.11 lbs)

Page 1-2 TL-3524 USER`S MANUAL

Rev. B P/N 03-3524-2003

1.3.2 General Specifications

Operating Temperature Range -20°C to +70°C

Humidity 95% non-condensing

Altitude Range 4600 meters max.

Power Range 10.0 to 32.0 Volts

Max. Signalization 30 Volts, 1 Ampere

Power Consumption 0.15 Ampere @ 14 VDC

Backlight Consumption 0.08 Ampere max when ext. power is used

Vibration 5 to 500 Hz

Show Rate (LCD Refresh) 1 second

1.3.3 Long-term Memory and Communication

Storing Rate 1 to 60 seconds user selectable

Memory Capacity Scheck® method

Stored Values Altitude

Data Saved Endurance 30 years

Rolling Memory life-time 550 000 hours @ 1 second storing rate

Communication RS-232c

Communication Speed 38400 bps

1.3.4 Encoder

Type of encoder Mode C

Strobe signal from Positive pulse 10 to 32 Volts

the transponder (if positive pulse is applied, the output

encoding data is enabled)

1.3.5 Instrument Measured Range / Resolution

Altitude&encoder -350m to 9700m @ 1013,25 mbar / 1m

(-1150ft to 31.950ft @ 29.92inHg / 2ft)

Page 1-3 TL-3524 USER`S MANUAL

Rev. B P/N 03-3524-2003

1.4. LIMITED CONDITIONS

1.5. LIMITED WARRANTY

The TL elektronic company warrants this product to be free from defects in materials and manufacture for

three years from the date of purchase. TL elektronic will, at its sole option, repair or replace any

components that fail in normal use. Such repairs or replacement will be made at no charge to the customer

for parts or labour. The customer is, however, responsible for any transportation costs. This warranty does

not cover failures due to abuse, misuse, accident or unauthorized alteration or repairs.

THE WARRANTIESAND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU

OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY

LIABILITYARISING UNDER ANY WARRANTY OF ENCHANT ABILITY OR FITNESS FOR A

PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU

SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.

IN NO EVENT SHALL TL ELEKTRONIC BE LIABLE FOR ANY INCIDENTAL, SPECIAL,

INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE,

MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT.

SOME STATES DO NOTALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL

DAMAGES, SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU.

To obtain warranty service, call the TL elektronic Customer Service (+420 49 548 23 92) for a returned

merchandise tracking number. The unit should be securely packaged with the tracking number clearly

marked on the outside of the package and sent freight prepaid and insured to a TL elektronic warranty

service station. A copy of the original sales receipt is required as the proof of purchase for warranty

repairs. TL elektronic retains the exclusive right to repair or replace the unit or software or offer a full

refund of the purchase price at its sole discretion.

SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH

OF WARRANTY.

This product is not TSO approved as a flight instrument, therefore, the manufacturer

will not be held responsible for any damage caused by its use.

The encoder output is only a complement of the Altimeter; therefore, the manufacturer is

responsible neither for using this output, nor for any possible legal consequences resulting

from its use.

1.6. LIMITED OPERATION

Page 2-1 TL-3524 USER`S MANUAL

Rev. B P/N 03-3524-2003

2. INSTALLATION

2.1 INTRODUCTION

Careful planning and consideration of the suggestions in this section are required to achieve the

desired performance and reliability from the TL-3524.

2.2 RACK CONSIDERATION

Plan a location that gives the pilot complete and comfortable access to the entire keypad and that is plainly

visible from the pilot's perspective. Check that there is adequate depth for the rack in the instrument panel.

A location away from heating vents or other sources of heat generation is optimal.

2.3 INSTALLATION INTO PANEL

Connect the cables into the connector and use the connector cover.

Secure the incoming leads to prevent their effect on the connector

in the vertical direction.

Connect the static pressure hose into the fitting. Secure the incoming leads

to prevent their effect on the hose in the vertical and horizontal direction.

2.4 STATIC PRESSURE CONNECTION

The TL-3524 is calibrated in the factory to the pressure datum according to the National

Bureau of Standards. When the TL-3524 has been installed in the aircraft it must be

calibrated to the primary flight altimeter according to Advisory Circular 43-6A so as to

comply with FAR91.36(b) and FAR 91.172 (see the calibration procedure, page 5-9).

Mounting Rack DimensionMounting Rack Dimension

Figure 4. Rack DimensionFigure 4. Rack Dimension

TL-3524 USER'S MANUAL

P/N 03-3524-2003

M3.5 (0.137) 4xM3.5 (0.137) 4x

50 (1.968)50 (1.968)

2 (.007)2 (.007) 40 (1.574)40 (1.574)

67 (2.637)67 (2.637)

71 (2.795)71 (2.795)

57 (2.244)57 (2.244)

23.5 (0.925)23.5 (0.925) 23.5 (0.925)23.5 (0.925)

57 (2.244)57 (2.244)

NOTES:

1. Dimension: mm (INCH)

2. Unit weight: 0.3 kg (0.66 lbs)

3. Mounting Rack & Hardware

weight: 0.05 kg (0.11 lbs)

NOTES:

1. Dimension: mm (INCH)

2. Unit weight: 0.3 kg (0.66 lbs)

3. Mounting Rack & Hardware

weight: 0.05 kg (0.11 lbs)

elektronicelektronic

TL-3524TL-3524

TTLL

ALTIMETERALTIMETER

encoder

Page 2-2

Rev. A

Page 2-2

Rev. A

67 (2.637)67 (2.637)

23.5 (0.925)23.5 (0.925)

Pin Pin Name I/O

1 Transponder -A1 Out

2 Transponder - A2 Out

3 Transponder - STROBE signal In

4 Ground for transponder - -

5 Transponder - A4 Out

6 Transponder - B1 Out

7 Aircraft power In

8 Aircraft ground - -

9 Transponder - B2 Out

10 Transponder - B4 Out

11 Input for backlight In

12 Internal source for backlight Out

13 Transponder - C1 Out

14 Transponder - C2 Out

15 Input for User button In

16 Ground for User button input - -

17 Transponder - C4 Out

18 Do not connect! - reserved for transponder - D4 Out

19 iFamily® communication ISCL I/O

20 iFamily® communication ISDA I/O

21 Signalization unit Out

22 Ground for PC communication (RS-232) - -

23 RXD from PC (RS-232) In

24 TXD to PC (RS-232) Out

Page 3-1 TL-3524 USER`S MANUAL

Rev. B P/N 03-3524-2003

3.1 PIN FUNCTION LIST

P3501

USER BUTTON

GROUND FOR USER BUTTON

10-32V AIRCRAFT POWER

AICRAFT GROUND

SIGNALIZATION UNIT

QUICK PROGRAMMED

USER BUTTON FUSE

FUSE

AIRCRAFT POWER

(Note. 1)

TL-3524

ALTIMETER & ENCODER

DISPLAY BACKLIGHT

Transponder

Unit

Sign.

unit

ALITIUDE OUTPUT - A1

ALITIUDE OUTPUT - A2

ALITIUDE OUTPUT - A4

ALITIUDE OUTPUT - B1

ALITIUDE OUTPUT - B2

ALITIUDE OUTPUT - B4

ALITIUDE OUTPUT - C1

ALITIUDE OUTPUT - C2

ALITIUDE OUTPUT - C4

STROBE SIGNAL

GROUND

Accessories Interconnect

TL-3524 USER'S MANUAL

P/N 03-3524-2003

Figure 5. Accessories interconnect

STROBE

GND

RS 232 RX

IFAMILY® ISCL

ISDA

RS 232 TX

GROUND

IFAMILY®

(Note. 2)

D-SUB 9 pins (female)

for communication with a PC

ISDA

54 3 21

67 8 9

ISCL

Page 3-2

Rev. B

NOTES:

1. Signalization is connected to the aircraft ground

when active.

2. Jumper for the backlight. For the backlight control

install a resistor between the pins 11 and 12.

3. Use the shade cable only and connect it according

to the connection scheme delivered with the sensor.

Connect other

TL elektronic instruments

via the iFamily® Bus

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