ENGINEERING ORDER N° IM-A319-34/1468 - …webapp.ifrskeyes.com/GED/AMSFSKUPRD/(1468) IM A319-34-1468 REV 3...NOTE: The IFR 6000 Tester has the capability to run automatically ...

ENGINEERING ORDER N° IM-A319-34/1468

Engineering Management Pudahuel, Santiago, Chile

WORK ORDER : …………….

ITEM NUMBER : …………….

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FORMATO 145-38 REV 0

19) PART LIST

ITEM QTY PART NUMBER DESCRIPTION REMARK

20) TOOL LIST

ITEM QTY PART NUMBER DESCRIPTION REMARK 01 01 IFR 6000 ATC Transponder Ramp Test Set

02 01 DPS 350 Tester Air Data Or equivalent

21) TABLE SKY APPLICABILITY





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22) REVISION RECORD

N° REVISION ITEM DESCRIPTION DATE

0

1

2

3

ALL

COVER ITEMS 2

AND 4 AND TASK

DESCRIPTION SHEET 12 OF 14

STEP N

ITEM 19) ART LIST AND TASK DESCRIPTION

STEP J _____________

APPLICABILITY

____________

ALL

ORIGINAL RELEASE

CHANGE DAN 121-1305 (c). FOR 121-

1219(a). (2).

CHANGE THE DECAL P/N CMA 124 FOR P/N R145-53

ADD AIRCRAFT CC-AMP (S/N3171)

CC-AJG (S/N 3331)

1. NEW FORMAT EO 2. CHANGE DAN 121.1219. (a).(2) FOR

DAN 121.1219.(b)

Dic-05-2012 (RG)

Oct-01-2013 (RG)

Jul-25-2014 (AE)

Jun-08-2016 (JF)





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TASK DESCRIPTION MEC

LICENSE & SIGNATURE

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A. ATC SYSTEM TEST.

1. Record the Part Number, Model, Serial Number and Calibrate Due Date of the ATC RAMP TEST SET.

Part Number :_____________ Model :_____________ Serial Number :_____________ Calibrate Due Date :_____________

NOTE: The IFR 6000 Tester has the capability to run automatically

in the AUTO mode and individually in the single test mode. B. PREPARE FOR THE SYSTEM TEST.

NOTE : You must do this test very quickly to prevent interference with air traffic. If the test is long, you must tell the nearest airport of this test.

NOTE : For best test results, buildings, vehicles and other aircraft

must not be in the area of the main antenna lobe (approx. 30 ft.).

REFERENCE DESIGNATION

24-41-00-861-002-A/-A-01 Energize the Aircraft Electrical Circuits

from the External Power or APU. 24-41-00-862-002-A/-A-01 De-energize the Aircraft Electrical

Circuits Supplied from the External Power or APU.

32-69-00-860-001-A Simulation of Flight, with the Aircraft on the

Ground 34-10-00-860-002-A ADIRS Start Procedure 34-10-00-860-005-A ADIRS Stop Procedure

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LICENSE & SIGNATURE

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C. Aircraft Maintenance Configuration

1. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

2. Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).

3. On the center pedestal:

a.- On the ATC/TCAS control unit:

- Start the ATC system 1(2) - Enter the ATC code given by DGAC ATC Control. - Set the STBY/ALT RPTG OFF/XPNDR/TA ONLY/TA-RA switch to XPNDR.

b. On the switching panel 8VU:

- Make sure that the AIR DATA selector switch ia at NORM.

D.- Make sure that this (these) circuit breakers(s) is(are) closed:

PANEL DESIGNATION FIN LOCATION

49VU COM NAV/ATC/1 5SH1 G11

121VU COM NAV/TCAS 4SG K10

121VU COM NAV/ATC/2 5SH2 K07

1. Connect the test antenna to the test set.

2. Put the test antenna in position in the line of sight of the ATC 1

(2) bottom antenna only.

E. Aircraft Maintenance Configuration

1. Power Up to aircraft.

2. On the center pedestal, on one MCDU, get the LGCIU 1 (2) page and simulate a flight condition (Ref. TASK 32-69-00-860-001)

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LICENSE & SIGNATURE

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NOTE: Simulation of flight automatically stops after a period of

time (approx. 5min.). When the aircraft goes back to ground configuration, the bottom antennas no longer transmit squitters.

CAUTION: DO NOT PRESS POWER KEY TO POWER TEST

SET WITHOUT CONNECT DIRECTIONAL ANTENNA. FOR OPTIMUM PERFORMANCE THE AIRCRAFT SHOULD BE OUTSIDE BUILDING, VEHICLES AND OTHER AIRCRAFT SHOULD BE LOCATED AT RIGHT ANGLES TO OR BEHIND ANTENNA. DO NOT USE CODES 7500, 7600, 7677, 7700, 7777. THESE ARE EMERGENCY CODES.

3. Open, safety and tag these circuit breakers

PANEL DESIGNATION FIN LOCATION

49VU L/LGCIU/SYS1/NORM 1GA C09

121VU HYDRAULIC/LGCIU/SYS2 2GA Q35

121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34

4. On ATC control panel select ATC System for operational test

(System 1 or 2).

5. Power Up: Press the POWER Key to power the Test Set

6. Press SETUP Control Key to display XPDR SETUP Screen. Use NEXT PARAM and PREV PARAM soft Key to select each parameter in sequence.

(Ref. IFR 6000 Operation Manual step 2.2)

NOTE: THE TESTER ANTENNA MUST BE WITHIN 95 FEET

(28.96 METERS) OF ANTENNA BEING TESTED.

7. Press XPDR Mode Key to return to XPDR Auto Test Screen.

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LICENSE & SIGNATURE

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8. Press CONFIG Soft Key to display XPDR CONFIG Screen Use

Data Keys to select configuration file. Press SELECT Soft Key to confirm Selection.

For ATC MODE C select ATCRBS CLASS A For ATC MODE S select MODE S. CLASS A.

9. To run a complete DAN 43 Appendix C (FAA FAR Part 43

Appendix F) Test, press RUN TEST soft Key to start Auto Test. When Auto Test completes a PASS or FAIL indication is displayed at the top of the screen.

10. If AUTO TEST PASS for ATC MODE S go to step 12.

11. If AUTO TEST FAIL Change the transponder, send to shop and

install unit serviceable repeat step 7.

Record the following data for the removed and new unit.

P/N OFF__________________ P/N ON ________________ S/N OFF__________________ S/N ON ________________

12. Make sure to read and record the following: A_________

REPLIES = A, C, S, FREQ = 1090 Mhz (+/- 3 Mhz) Read : C_________ S_________ TOP ERP = 51.0 to 57.0 (dBm) MTL = - 73 dBm (+/- 4dBm) Read : ________ Read :__________ BOT ERP = 51.0 to 57.0 (dBm) MTL = - 73 dBm(+/- 4 dBm) Read : _______ Read : ___________ NOTE: Only for TAIL or AA code confirmation, verify with customer operator information. A CODE (similar to select in Control Panel) = Read: _____ C ALT = Read: ______ S CODE (similar to select in Control Panel) = Read :_____ S ALT = Read :______ TAIL = Read :__________________(If used) AA (Aircraft Address) = Read :__________________(If used)

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LICENSE & SIGNATURE

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a. MAKE TEST LIST :

i. Press TEST LIST Soft Key to display Test List. The

configuration the Test List is displayed over two screens

ii. Use DATA Keys to select A/C DECDR / SLS (Side Lobe Suppression ) Press Soft key Select Test

iii. Verify the Suppression test is :

SLS = 0 dB A= PASS C= PASS SLS = -9 dB A= PASS C= PASS

iv. Press Return Soft Key.

v. Use DATA Key to select A/C F1/F2 SPAC / WDTH.

vi. Press Soft key Select Test and verifies the Reply test are:

Mode A Read:_______ REPLY DELAY = A and C = 3.00 us (+/- 0.5 us ) Mode C Read:_______ Mode A Read:_______ REPLY JITTER = A and C = < 0.1 us Mode C Read:_______ Mode A Read:_______ F1 - F2 = A and C = 20.3 us (+/- 0.10 us ) Mode C Read:_______ Mode A Read:_______ F1 WIDTH = A and C = 0.45 us (+/- 0.10 us ) Mode C Read:_______ Mode A Read:_______ F2 WIDTH = A and C = 0.45 us (+/- 0.10 us ) Mode C Read:_______

vii. Press Return Soft Key. viii. Use DATA Key to select POWER / FREQ, Press Soft

key Select Test.

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LICENSE & SIGNATURE

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ix. Verify the MTL and ERP test are:

TOP BOTTOM ATCRBS= -73 DbM +/- 4.0 dBm -73 DbM +/- 4.0 dBm Read:______ Read:______ A – C DIFF MTS = < 1.0 dBm < 1.0 dBm Read:_______ Read:_______ ALL CALL = -73 dBm +/- 4.0 dBm -73 dBm +/- 4.0 dBm Read:_________ Read:_________ MODE S = -73 dB m +/- 4.0 dBm -73 dB m +/- 4.0 dBm Read:________ Read:________ ERP = 51.0 dBm to 57 dBm 51.0 dBm to 57 dBm Read:_____ Read:_____

x. Use DATA Key to select XPDR - S ALL CALL. xi. Press Soft key Select Test. xii. Verify the Reply test is.

Mode A Read:_______ REPLY DELAY = A and C = 128.00 us +/- 0.25 us Mode C Read:_______ Mode A Read:_______ REPLY JITTER = A and C = < 0.08 us Mode C Read:_______ ALL CALL = PASS

xiii. Press Return Soft Key

xiv. Put the aircraft back to ground configuration (Ref. TASK

32-00-00-860-002)

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LICENSE & SIGNATURE

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xv. Press RUN TEST again.

The test sets must show - Interrogation in MODE A - MODE A: no reply - Interrogation in MODE C - MODE C: no reply - Interrogation in MODE S. MODE S aircraft code: XXXXXX Flight number/Flight ID

Acquisition Squitters (PERIOD is between 0.8 second and 2.4 seconds in DF 11 format)

H. ALTITUD REPORTING TEST. FOR ATC MODE C

NOTE: You must do this test very quickly to prevent interference with

air traffic, especially if the aircraft is in the open air. If the test is long you must tell the nearest airport of this test.

REFERENCE DESIGNATION

24-41-00-861-002-A/-A-01 Energize the Aircraft Electrical Circuits

from the External Power or APU 24-41-00-862-002-A/A-01 De-energize the Aircraft Electrical

Circuits Supplied from the External Power or APU

34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure 34-13-00-710-004-A Operational Test of the ALT DYNAMIC

SLEW TEST

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LICENSE & SIGNATURE

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1. Open, safety and tag this(these) circuit breaker(s):

WARNING : OPEN CIRCUIT BREAKER 7XE. THIS WILL

PREVENT A POSSIBLE DEPLOYMENT OF THE RAT IF THE MAIN AC BUS BARS 1XP AND 2XP BECOME ISOLATED.

PANEL DESIGNATION IDENT. LOCATION 105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01

2. Aircraft Maintenance Configuration

a. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-

861-002). b. Do the ADIRS start procedure (Ref. TASK 34-10-00-860-

002). c. Install the ATC ground test unit in the cockpit.

d. Put the antenna of the ATC ground test unit at 50 cm (approx. 2 ft) from the ATC antennas.

e. Connect the antenna to the ATC ground test unit.

f. On the SWITCHING panel 8VU, make sure that the AIR DATA selector switch is at NORM.

g. On the center pedestal, on the ATC/TCAS control unit:

- set the ATC system 1(2) on. - set the STBY/ALT RPTG OFF/XPNDR/TA ONLY/TA-RA

switch is at STBY. - make sure that the display does not show an emergency

code: 7500, 7600 or 7700.

h. On the panel 13VU, on the CAPT and F/O EFIS control sections of the FCU, make sure that the baro displays show STD.

i. Connect TESTER-AIRDATA to the pitot /static system (Ref AMM TASK 34-13-00-710-004).

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LICENSE & SIGNATURE

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3. Start the TESTER AIR DATA

4. Make sure that these Circuit Breakers are close:

PANEL DESIGNATION IDENT. LOCATION 49VU COM NAV/ATC/1 5SH1 G11 121VU COM NAV/ATC/2 5SH2 K07

5. Functional Test of the Altitude Reporting Function

ACTION RESULT

1. On the TESTER AIR DATA : – simulate three altitude values

between 20,000 ft and 25,000 ft

2 On the ATC/TCAS control unit. - set the STBY/ALT RPTG

OFF/XPNDR/TA ONLY/TA-RA switch to XPNDR

On the ATC/TCAS control Unit - The display shows the last code set - The ATC FAULT or FAIL indicator light

stay off.

On the ATC ground test unit, a display shows: - the last selected code. - the standard altitude must be approximately

the same as altitude simulated in step 1.

3 On the PFDs: - read the altitude value and

compare it with the altitude from the ATC transponder

The difference between the altitude shown on the CAPT PFD and the ATC 1 on the ATC ground test unit must not be more than 125 ft. The difference between the altitude shown on the F/O PFD and the ATC 2 on the ATC ground test unit must not be more than 125 ft.

4. On the ATC/TCAS control unit: - set the STBY/ALT RPTG

OFF/XPNDR/TA ONLY/TA-RA SWITCH to STBY

On the ATC/TCAS control unit: - The display stays on.

5. On the air data generator: - slowly decrease pitot and static

pressure until you get atmospheric values

The rate of descent must not be more than 6,000 ft/min

6. Stop and disconnect the air data generator

7. On MCDU: - push the line key adjacent to the

RETURN indication until you get the CFDS menu page.

The flight condition is no longer simulated

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LICENSE & SIGNATURE

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6. Put the aircraft back to its initial configuration.

a. Disconnect the ATC ground test unit.

b. Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005)

c. De-energize the aircraft electrical circuits.

d. Make sure that the work area is clean and clear of tool(s) and

other items.

7. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

7XE.

8. Repeat step 2.f.above with the SWITCHING panel 8VU, make sure that the AIR DATA selector switch is at AIR DATA 3

9. Return the Air Data Switch to NORMAL position

I. CHECK AND RECORD ATC TRANSPONDER.

P/N _______________S/N ____________ POS____________

J. REMOVE ELECTRICAL POWER OF THE AIRPLANE.

K. REMOVE THE ATC RAMP TEST SET.

L. RETURN AIRPLANE BACK TO ORIGINAL CONDITION.

M. RECORD IN FLIGHT LOG “ENGINEERING ORDER IM A319-34/1468 Rev 3 APPLIED TO FULFILL DAN 121.1219 (b) AND DAN 43 APPENDIX “C”.

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Deviation Record Sheet

Paragraph Observation Action Authorized by Performed by





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DISCREPANCY FOUND PARAGRAPH CORRECTIVE ACTION DETAIL MEC LICENSE

& SIGNATURE

INSPECTOR & SIGNATURE

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ENGINEERING ORDER N° IM-A319-34/1468 - …webapp.ifrskeyes.com/GED/AMSFSKUPRD/(1468) IM A319-34-1468 REV 3...NOTE: The IFR 6000 Tester has the capability to run automatically ...

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