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Peregrine – Proprietary Data

 

 

Document No. 

Title 

Page 

E-TX-21-0014 Rev IR  Installation Manual, TXA201 Triaxial Accelerometer 

 

3  EQUIPMENT QUALIFICATION 

3.1  TSO 

The TXA201 triaxial accelerometer meets TSO-C124c requirements and is intended to 

provide data to a flight data recorder (FDR) at a rate and accuracy that is compatible 

with the FDR. 

3.2  Application 

The TXA201 is designed to provide accelerometer inputs for digital flight data recording 

equipment.    

3.3  Environmental 

The accelerometer is environmentally qualified for aircraft applications per RTCA DO-

160G testing as shown in Table 3.  The environmental qualification categories shown 

support typical installations in Part 25 aircraft models.  

Table 1: Environmental Qualifications 

DO-160G Testing Summary 

Conditions 

Section 

Description of Tests Conducted 

Temperature and Altitude 

Low Temperature 

High Temperature 

In-Flight Loss of Cooling 

Altitude 

Decompression 

Overpressure

 

4.0 

4.5.1 

4.5.2 & 4.5.3 

4.5.4 

4.6.1 

4.6.2 

4.6.3

 

Equipment tested to Category F2 

Temperature Variation

 

5.0

 

Equipment tested to Category B.

 

Humidity

 

6.0

 

Equipment tested to Category B.

 

Operational Shock and Crash Safety

 

7.0

 

Equipment tested to Category B.

 

Vibration

 

8.0

 

Equipment tested to Category S and H, 

aircraft zone 1 for fixed wing aircraft fuselage 

using vibration test curves C3 and R.

 

Explosive Atmosphere

 

9.0

 

Equipment identified as Category X  ( no test)

 

Waterproofness

 

10.0

 

Equipment tested to Category W.

 

Fluids Susceptibility

 

11.0

 

Equipment identified as Category X  ( no test)

 

Sand and Dust

 

12.0

 

Equipment identified as Category X  ( no test)

 

Fungus

 

13.0

 

Equipment identified as Category X  ( no test)

 

Salt Fog Test

 

14.0

 

Equipment identified as Category X  ( no test)

 

Magnetic Effect

 

15.0

 

Equipment is Category Z.

 

Power Input

 

16.0

 

Equipment tested to Category A.

 

Voltage Spike

 

17.0

 

Equipment tested to Category B.

 

Audio Frequency Susceptibility

 

18.0

 

Equipment tested to Category B.

 

Induced Signal Susceptibility

 

19.0

 

Equipment tested to Category ZC.

 

Radio Frequency Susceptibility

 

20.0

 

Equipment tested for conducted 

susceptibility to Category T and for radiated 

susceptibility to Category T.

 

Radio Frequency Emission

 

21.0

 

Equipment tested to Category L.

 

Lightning Induced Transient Susceptibility

 

22.0

 

Equipment identified as Category X  ( no test)

 

Lightning Direct Effects

 

23.0

 

Equipment identified as Category X  ( no test)

 

Icing

 

24.0

 

Equipment identified as Category X  ( no test)

 

Electrostatic Discharge

 

25.0

 

Equipment tested to Category A.

 

Fire, Flammability 

26.0 

Equipment identified as Category X  ( no test) 

Содержание TXA201

Страница 1: ...SION STATUS Rev Description Approved Date IR Initial Release T Bailey 7 7 22 Export Control Notice The technical data contained herein is controlled under the U S Export Administration Regulations EAR...

Страница 2: ...N 8 3 1 TSO 8 3 2 Application 8 3 3 Environmental 8 3 4 Installation Approval 9 4 TESTING 9 4 1 Fault Indication 9 4 2 Pre Installation Check 9 4 3 Functional Test Procedure 9 4 4 Post Installation Ch...

Страница 3: ...Center of Gravity DC Direct Current DO Document Order EQ Equipment Qualification ESD Electro Static Discharge FAA Federal Aviation Administration FDR Flight Data Recorder FSO Full Scale Offset MDL Mas...

Страница 4: ...designed to meet ARINC 542A mounting specifications and is sealed to prevent moisture incursion This accelerometer may be utilized as an input to flight data recorder FDR systems such as the Curtiss...

Страница 5: ...to the accelerometer prior to delivery The placard includes a serial number of the format 0000 with the serial number of the first unit being 1001 The placard also serves as an anti tamper device The...

Страница 6: ...ial Accelerometer 6 Location The accelerometer should be mounted within 12 feet longitudinally and 6 feet laterally of the aircraft center of gravity to avoid erroneous readings due to aircraft rotati...

Страница 7: ...5000mV DOWN 3g 200mV FWD 1g 5000mV AFT 1g 200mV RIGHT 1g 5000mV LEFT 1g 200mV Axial Null VERTICAL 1800 mV LONGITUDINAL 2600 mV LATERAL 2600 mV Excitation 18 TO 32 VDC 28 VDC nominal Supply Current 30...

Страница 8: ...tested to Category B Vibration 8 0 Equipment tested to Category S and H aircraft zone 1 for fixed wing aircraft fuselage using vibration test curves C3 and R Explosive Atmosphere 9 0 Equipment identi...

Страница 9: ...rformed using the following procedure Requirements 28VDC Power Supply DC Voltmeter Tooling fixtures or other items that will allow the accelerometer to be rested on each of its six faces in a flat and...

Страница 10: ...a is properly received and is within expected parameters Table 2 Test Orientations and Outputs Axis Orientation Position Arrow UP Gravity Output and Range Vertical 3 0g Pin C 1 800 0036 VDC 1 1g Pin C...

Страница 11: ...and a cotton cloth or swabs A soft bristled brush may also be used 5 3 Repair The TXA201 Accelerometer contains no user serviceable parts and is not designed to be adjusted or repaired by field person...

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