NUMBER ------------------------------------------------------------------------------
proximity settings
G237 Nose L/G extended interface 1 2 No 18, 58, 70, 71, 1 signal 3 disagrees with BITE 166, 178, A proximity settings
G238 Nose L/G not locked up interface 1 2 No 20, 60, 70, 71, 1 signal 1 disagrees with BITE 168, 178, A proximity settings
H239 Watchdog timer reset failure 1 2 Yes A 1
A240 RH gear uplock prox 1 2 No 57 switch disagreement
A241 LH gear uplock prox 1 2 No 58 switch disagreement
A242 NOSE gear uplock prox 1 2 No 59 switch disagreement
A243 RH gear downlock prox 1 2 No 54 switch disagreement
A244 LH gear downlock prox 1 2 No 55 switch disagreement
A245 NOSE gear downlock prox 1 2 No 56 switch disagreement
A246 Not used
A247 Not used
A248 FWD cargo door lock handle 1 No 60
prox switch disagreement A249 AFT cargo door lock handle 1 No 61 prox switch disagreement A250 FWD cargo door lockshaft 2 No 64 prox switch disagreement A251 AFT cargo door lockshaft 2 No 65 prox switch disagreement A252 FWD cargo door safety mech 1 No 62 prox switch disagreement A253 AFT cargo door safety mech 1 No 63 prox switch disagreement -------------------------------------------------------------------------------
9. BITE Test_________
Not applicable
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LANDING GEAR - BITE - ADJUSTMENT/TEST
_____________________________________
TASK 32-69-00-740-001
BITE Test of the Landing Gear R
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
1. Reason for the Job
__________________
Refer to the MPD TASK: 323100-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
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No specific safety barriers
No specific warning notice
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
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24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears
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3. Job Set-up__________
Subtask 32-69-00-941-052
A. Safety Precautions
R R (1) Put the safety barriers in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).
R R R R (3) On the panel 400VU: - make sure the landing-gear control lever 6GA is in the DOWN position - put a warning notice in position to tell persons not to operate the landing gear controls.
Subtask 32-69-00-865-055
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
Subtask 32-69-00-861-050
C. Energize the Electrical Circuits
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
4. Procedure
_________ Subtask 32-69-00-740-050
A. BITE Test of the Landing Gear NOTE : During the test, indications other than those on the MCDU will
____
occur. You can ignore these other indications.
(1) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
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