Customer : AHK Manual : AMM
Type : A300-600 Selected Effectivity : 001-008
Rev. Date : Jun 01, 2016
GENERAL - ADJUSTMENT/TEST
** ON A/C ALL
22-00-00 PB 501 - GENERAL - ADJUSTMENT/TEST
1. Operational Test
A. Power Supply Cutoff and Restoration Logic
(1) Equipment and materials
-------------------------------------------------------------------------------
ITEM DESIGNATION
-------------------------------------------------------------------------------
Referenced Procedures
- 24-41-00, P. Block 301 AC External Power Control
- 34-25-00, P. Block 501 Inertial Reference System
WARNING: BEFORE POWER IS SUPPLIED TO THE AIRCRAFT, MAKE CERTAIN THAT ELEC-
TRICAL CIRCUITS UPON WHICH WORK IS IN PROGRESS ARE ISOLATED.
(2) Procedure
(a) Job Set-Up
- Energize the aircraft electrical network (Ref. AMM 24-41-00, P. Block 301 ) .
- Make certain that electronics racks ventilation is correct.
- Close overhead panel circuit breakers particularly those associated with AFS, NAVIGATION
and ADS.
- Close L/G PROX DET & RELAYS circuit breakers on panel 133VU (aircraft in ground
configuration).
- Make certain that ADS is operating
- Align the IRS.
- Make certain that EFIS is operating and adjust PFD image brightness on panels 412VU and
413VU.
- On left and right instrument panels make certain that FD pushbutton switches legends are off
- On glareshield, FD/FPV selector switches in ON position
- Close circuit breaker 5RK on panel 22VU, line 204/F27.
(b) Test (5RK: RCDR-CTL)
-------------------------------------------------------------------------------
ACTION RESULT
-------------------------------------------------------------------------------
1. On overhead panel
- place PITCH TRIM 1 engage lever Lever remains in this position.
in ON position Check that the following AFS com-
ponents are energized :
or PITCH TRIM 2 - flight augmentation computers :
SPD LIM out of view on airspeed
scale on PFDs
- flight control computers :
white FD1 indication appears on
captain PFD
White FD2 indication appears on
First Officer PFD
- flight control unit :
all displays show indications
- thrust control computer :
THR LIMIT value appears on TRP
2. Place PITCH TRIM 1 engage lever in Check that, after a few seconds,
Print Date: July 14, 2016 Page 1 of 4
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : AHK Manual : AMM
Type : A300-600 Selected Effectivity : 001-008
Rev. Date : Jun 01, 2016
GENERAL - ADJUSTMENT/TEST
OFF position the following components are de-
energized :
- flight augmentation computers :
SPD LIM message appears on PFDs
- flight control computers :
white FD indication disappears on
PFDs
- flight control unit :
indications disappear
- thrust control computer :
no value on TRP.
3. Place PITCH TRIM 2 levers successi- At engagement, same result as in
vely in ON and then OFF position step 1
At disengagement, same result as
in step 2.
4. On maintenance test panel
- press GROUND SCAN pushbutton Wait for few seconds (safety test
switch (green indicator light duration) then same result as in step
comes on) 1
- press GROUND SCAN pushbutton Same result as in step 2
switch again (indicator light
goes off)
- press AFS TEST/LAND TEST pushbut- Wait for few seconds (safety test du-
ton switch. ration) then same result as in step 1
- press CLEAR pushbutton switch. On MTP display goes off then same re-
sult as in step 2.
5. On panel 22VU
- open circuit breaker 5RK (line Check that the following AFS com-
204/F27) ponents are energized
- flight augmentation computers :
SPD LIM out of view on airspeed
scale on PFDs
- flight control computers :
white FD1 indication appears on
Captain PFD
white FD2 indication appears on
First Officer PFD
- flight control unit :
all displays show indications
- thrust control computer :
TAT value appears on TRP.
- close circuit breaker 5RK Same result as in step 2.
6. On panel 21VU On MTP
- open circuit breaker 306CC1 (line - display comes on for one
103 G/3) second
On flight control unit
- all displays show indications.
- close circuit breaker 306CC1 On flight control unit
- indications disappear after approx.
1 minute.
- open circuit breaker 306CC2 (line On flight control unit
103 G/12) - all displays show indications
- close circuit breaker 306CC2 On flight control unit
- indications disappear after approx.
Print Date: July 14, 2016 Page 2 of 4
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : AHK Manual : AMM
Type : A300-600 Selected Effectivity : 001-008
Rev. Date : Jun 01, 2016
GENERAL - ADJUSTMENT/TEST
1 minute.
NOTE: Energization of AFS components by means of the ANN LT selector switch will be checked
in the next test.
(c) Close-up
- De-energize the aircraft electrical network (Ref. AMM 24-41-00, P. Block 301 ) .
B. AFS Light Test and Display
(1) Reason for the Job
- Test of lighting and display.
- Operational test of windshear warning system through light test with single FWS energized.
- Light test with single FWS energized.
(2) Equipment and materials
-------------------------------------------------------------------------------
ITEM DESIGNATION
-------------------------------------------------------------------------------
Referenced Procedure
- 24-41-00, P. Block 301 AC External Power Control
WARNING: BEFORE POWER IS SUPPLIED TO THE AIRCRAFT, MAKE CERTAIN THAT ELEC-
TRICAL CIRCUITS UPON WHICH WORK IS IN PROGRESS ARE ISOLATED.
(3) Procedure :
(a) Job Set-Up
- Energize the aircraft electrical network (Ref. AMM 24-41-00, P. Block 301 ) .
- Make certain that electronics racks ventilation is correct.
- Close overhead panel circuit breakers particularly those associated with AFS.
- Close L/G PROX DET & RELAYS circuit breakers on panel 133VU (aircraft in ground
configuration).
- Open FWC1 circuit breaker 7WW on panel 21VU, line 108/B8.
(b) Test
NOTE: The test is performed with only FWC2 energized. To perform the test with FWC1 ener-
gized open FWC2 C/B 32WW on panel 21VU, line
109/A8.
-------------------------------------------------------------------------------
ACTION RESULT
-------------------------------------------------------------------------------
1. On overhead panel 436VU Check that the following lights,
- place ANN LT selector switch in displays or indications come on :
TEST position On main instrument panel :
- amber light on altimeter
Two red AUTO-LAND warning lights
** ON A/C ALL
POST SB 22-6055 for A/C ALL
- Open FWC1 circuit breaker 7WW on panel 21VU, line 108/B8.
** ON A/C ALL
(c)
** ON A/C ALL
POST SB 22-6055 for A/C ALL
Test
NOTE: The test is performed with only FWC2 energized. To perform the test with FWC1 ener-
gized open FWC2 C/B 32WW on panel 21VU, line
109/A8.
Print Date: July 14, 2016 Page 3 of 4
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : AHK Manual : AMM
Type : A300-600 Selected Effectivity : 001-008
Rev. Date : Jun 01, 2016
GENERAL - ADJUSTMENT/TEST
-------------------------------------------------------------------------------
ACTION RESULT
-------------------------------------------------------------------------------
1. On overhead panel 436VU Check that the following lights,
- place ANN LT selector switch in displays or indications come on:
TEST position On main instrument panel:
- amber light on altimeter
Two red AUTO-LAND warning lights
Two red RUDDER INPUTS warning lights
** ON A/C ALL
Two red MASTER WARN warning
lights.
On the PFD's :
- red WINDSHEAR legend is
displayed
On CAPT and F/O loudspeakers
- WINDSHEAR is heard 3 times.
On flight control unit :
- SPD/MACH display : 888
- ALT SEL display : 88800
- HDG SEL display : 888
- V/S display : + 88
- PRESET indication
- all pushbutton switches
On L and R instrument panels :
- all pushbutton switches.
On thrust rating panel :
- all pushbutton switches.
- TAT display : + 88
- THR LIMIT display : 8.8.8.8
- LIM MODE display : all segments
used for mode display
- TARGET display : 8.8.8.8
- FLX TO TEMP display : + 88
- place ANN LT selector switch in Check that after a few seconds,
BRT position lights, displays and indications
listed above go off.
(d) Close-up
- De-energize the aircraft electrical network (Ref. AMM 24-41-00, P. Block 301 ) .
End of document
Print Date: July 14, 2016 Page 4 of 4
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
