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Job Card: 24-92-00-210-808-A - General Visual Inspection of The Braided Conduit End Fittings From Rib 6 To Fus..

This document outlines the job card for a general visual inspection of the braided conduit end fittings from rib 6 to the fuselage on aircraft VT-JWR. It details safety precautions, required tools, materials, and procedures for conducting the inspection, including corrosion protection measures. The task is part of the maintenance program and ensures compliance with safety standards before releasing the aircraft for service.

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linto
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0% found this document useful (0 votes)
32 views6 pages

Job Card: 24-92-00-210-808-A - General Visual Inspection of The Braided Conduit End Fittings From Rib 6 To Fus..

This document outlines the job card for a general visual inspection of the braided conduit end fittings from rib 6 to the fuselage on aircraft VT-JWR. It details safety precautions, required tools, materials, and procedures for conducting the inspection, including corrosion protection measures. The task is part of the maintenance program and ensures compliance with safety standards before releasing the aircraft for service.

Uploaded by

linto
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
You are on page 1/ 6

JOB CARD MPD-TASK: 200001-08

JAI - A330 AMM TASK : 24-92-00-210-808-A


24-92-00 PB 601

TITLE:
A/C Reg.: 24-92-00-210-808-A - General Visual Inspection of
VT-JWR the Braided Conduit End Fittings from Rib 6 to Fus...
CARD: ZONE: INTERVAL:
SKILL: ACCESS:

MECH. INSP.

** ON A/C ALL

TASK 24-92-00-210-808-A
General Visual Inspection of the Braided Conduit End Fittings from Rib 6 to Fuselage

WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES
ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS
AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.

WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL
SURFACES ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A
HYDRAULIC SYSTEM. MOVEMENT OF THE FLIGHT CONTROL SURFACES
CAN BE DANGEROUS AND/OR CAUSE DAMAGE.

1. Reason for the Job


Refer to the MPD TASK: 200001-08
GENERAL VISUAL INSPECTION OF THE FOLLOWING BRAIDED CONDUIT END
FITTINGS, FROM RIB 6 TO FUSELAGE :
- 112QA1-A, 121QA1-A, 122QA1-A, LH SIDE
- 112QA2-A, 121QA2-A, 122QA2-A, RH SIDE
Use this procedure to do a general visual inspection of these braided conduit end-fittings,
from the rib 6 to the fuselage:
· 112QA1-A, 121QA1-A, 122QA1-A, LH side,
· 112QA2-A, 121QA2-A, 122QA2-A, RH side.
2 Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE QTYDESIGNATION
No specific AR ACCESS PLATFORM 3M (10 FT)
No specific AR BRUSH - BRISTLED
No specific AR SAFETY BARRIER(S)
No specific AR WARNING NOTICE(S)
(98D27803000000) 1 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION

B. Consumable Materials

REFERENCE DESIGNATION
(Material No. 08BAA9) Non Aqueous Cleaner-General - -
JCP Title: C-CHECK CERTIFICATE OF TASK / INSPECTION COMPLETION: Page 1 of 6
JCP Ref: C-CHECK DATABASE REV DATE: Apr 01/2017
CERTIFIES THAT THE TASK / INSPECTION HAS BEEN COMPLETED TO THE REQUIRED PRINT DATE: Apr 06/2017 09:20
STANDARD AND SUPPORTS THE FINAL MAINTENANCE RELEASE / CERTIFICATE OF RELEASE
TO SERVICE
JOB CARD MPD-TASK: 200001-08
JAI - A330 AMM TASK : 24-92-00-210-808-A
24-92-00 PB 601

TITLE:
A/C Reg.: 24-92-00-210-808-A - General Visual Inspection of
VT-JWR the Braided Conduit End Fittings from Rib 6 to Fus...
MECH. INSP.

REFERENCE DESIGNATION
(Material No. 12ACB1) Corrosion Preventive Compound-Heavy Duty Hard Film -
(Material No. 14SBA1) Textile-Lint free Cotton -

C. Referenced Information

REFERENCE DESIGNATION
(Ref. 24-41-00-861-801-A). Energize the Aircraft Electrical Circuits from the External
Power A
(Ref. 24-41-00-861-801-A- Energize the Aircraft Electrical Circuits from the APU
01). (APU Started with APU BAT)
(Ref. 24-41-00-861-801-A- Energize the Aircraft Electrical Circuits from the External
03). Power A and B
(Ref. 24-41-00-861-801-A- Energize the Aircraft Electrical Circuits from the APU
04). (APU started with External power A)
(Ref. 24-41-00-861-801-A- Energize the Aircraft Electrical Circuits from the External
05). Power B
(Ref. 24-41-00-862-801-A). De-energize the Aircraft Electrical Circuits from the
External Power A
(Ref. 24-41-00-862-801-A- De-energize the Aircraft Electrical Circuits from the APU
01).
(Ref. 24-41-00-862-801-A- De-energize the Aircraft Electrical Circuits from the
03). External Power A and B
(Ref. 24-41-00-862-801-A- De-energize the Aircraft Electrical Circuits from the
04). External Power B
(Ref. 28-21-49-000-801-A). Removal of the Fuel Pump Fairings
(Ref. 28-21-49-400-801-A). Installation of the Fuel Pump Fairings
(Ref. 29-00-00-864-804-A). Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
Ref. ESPM 20-53-32
Ref. ESPM 20-55-30
Braided Conduit End Fittings from Rib 6 to Fuselage SHEET 1

JCP Title: C-CHECK CERTIFICATE OF TASK / INSPECTION COMPLETION: Page 2 of 6


JCP Ref: C-CHECK DATABASE REV DATE: Apr 01/2017
CERTIFIES THAT THE TASK / INSPECTION HAS BEEN COMPLETED TO THE REQUIRED PRINT DATE: Apr 06/2017 09:20
STANDARD AND SUPPORTS THE FINAL MAINTENANCE RELEASE / CERTIFICATE OF RELEASE
TO SERVICE
JOB CARD MPD-TASK: 200001-08
JAI - A330 AMM TASK : 24-92-00-210-808-A
24-92-00 PB 601

TITLE:
A/C Reg.: 24-92-00-210-808-A - General Visual Inspection of
VT-JWR the Braided Conduit End Fittings from Rib 6 to Fus...
MECH. INSP.

OUTBOAR FUEL PUMP

INBOARD FUEL PUMPS

F_MM_249200_6_NGM0_01_00

Figure 24-92-00-991-02700-00-A / SHEET 1/1 -


Braided Conduit End Fittings from Rib 6 to Fuselage
** ON A/C ALL

JCP Title: C-CHECK CERTIFICATE OF TASK / INSPECTION COMPLETION: Page 3 of 6


JCP Ref: C-CHECK DATABASE REV DATE: Apr 01/2017
CERTIFIES THAT THE TASK / INSPECTION HAS BEEN COMPLETED TO THE REQUIRED PRINT DATE: Apr 06/2017 09:20
STANDARD AND SUPPORTS THE FINAL MAINTENANCE RELEASE / CERTIFICATE OF RELEASE
TO SERVICE
JOB CARD MPD-TASK: 200001-08
JAI - A330 AMM TASK : 24-92-00-210-808-A
24-92-00 PB 601

TITLE:
A/C Reg.: 24-92-00-210-808-A - General Visual Inspection of
VT-JWR the Braided Conduit End Fittings from Rib 6 to Fus...
MECH. INSP.

3. Job Set-up
Subtask 24-92-00-861-058-A
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-801) .
Subtask 24-92-00-941-056-A
B. Safety Precautions
(1) Make sure that the Green hydraulic system is depressurized and put it in the
maintenance configuration.
(Ref. AMM TASK 29-00-00-864-804) .
(2) Make sure that the Yellow hydraulic system is depressurized and put it in the
maintenance configuration.
(Ref. AMM TASK 29-00-00-864-804) .
(3) On the FLAPS control panel 114VU:
· put the LOCKING TOOL-FLAP SLAT LEVER,INT.
POSITION (98D27803000000) on the slat/flap control lever,
· put a WARNING NOTICE(S) in position on the slat/flap control lever to tell
persons not to operate the slats/flaps.
(4) On the FLT CTL control panel 241VU:
· make sure that the PRIM 1 and SEC 1 pushbutton switches are released (the
OFF/R legend of these pushbutton switches is on),
· put a WARNING NOTICE(S) in position to tell persons not to use these
pushbutton switches.
(5) On the FLT CTL section of the panel 212VU:
· make sure that the PRIM 2, PRIM 3 and SEC 2 pushbutton switches are
released (the OFF/R legend of these pushbutton switches is on),
· put a WARNING NOTICE(S) in position to tell persons not to use these
pushbutton switches.
Subtask 24-92-00-010-060-A
C. Get Access
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's
instructions and your local regulations.
(2) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable fuel-
pump fairing.
(3) Remove the applicable fuel-pump fairing (Ref. AMM TASK 28-21-49-000-801) .
4. Procedure
(Ref. Fig. Braided Conduit End Fittings from Rib 6 to Fuselage SHEET 1)
Subtask 24-92-00-210-057-A
A. General Visual Inspection of the Braided Conduit End-Fittings from Rib 6 to the
Fuselage
(1) Do a general visual inspection of the components that follow:
· The bonding leads
· The braided conduits
JCP Title: C-CHECK CERTIFICATE OF TASK / INSPECTION COMPLETION: Page 4 of 6
JCP Ref: C-CHECK DATABASE REV DATE: Apr 01/2017
CERTIFIES THAT THE TASK / INSPECTION HAS BEEN COMPLETED TO THE REQUIRED PRINT DATE: Apr 06/2017 09:20
STANDARD AND SUPPORTS THE FINAL MAINTENANCE RELEASE / CERTIFICATE OF RELEASE
TO SERVICE
JOB CARD MPD-TASK: 200001-08
JAI - A330 AMM TASK : 24-92-00-210-808-A
24-92-00 PB 601

TITLE:
A/C Reg.: 24-92-00-210-808-A - General Visual Inspection of
VT-JWR the Braided Conduit End Fittings from Rib 6 to Fus...
MECH. INSP.

· The clamps that attach the braided conduits


· The electrical connectors at the end fittings of the braided conduits
· The shield of the electrical connectors.
(2) Make sure that there are no signs of contamination Ref. ESPM 20-55-30.
(3) Make sure that there are no signs of corrosion Ref. ESPM 20-53-32.
(4) For corrosion protection, do the steps that follow:

WARNING:BE CAREFUL NOT TO CUT YOUR FINGERS. FLAKES OF NICKEL


ARE SHARP.

CAUTION:MAKE SURE THAT YOU DO NOT APPLY CLEANING AGENTS TO


ELECTRICAL CONDUCTIVE PARTS (PINS, ETC.). IF YOU DO, YOU
CAN CAUSE DAMAGE TO THE EQUIPMENT.

(a) On the electrical connectors, at the end fittings of the braided conduits:
· Use Non Aqueous Cleaner-General - - (Material No. 08BAA9) and a lint-
free cotton cloth Textile-Lint free Cotton - (Material No. 14SBA1) to remove
contamination from the fitting.
· Remove flakes or blisters. Make sure that you do not cause damage to the
base metal while you do this task.

NOTE: A sharp tool is necessary for the removal of the flakes and blisters.

(5) Use a BRUSH - BRISTLED or an airless spray to apply a continuous layer of


Corrosion Preventive Compound-Heavy Duty Hard Film - (Material No. 12ACB1)
with a thickness of 0.03 mm (0.0012 in.). Apply the material on all the fittings,
couplings, backshells, transitions and the space between the crimping sleeve and
the part (if the ESPM 203330 is applicable).
(6) Make sure that the screws are not loose or missing.
5. Close-up
Subtask 24-92-00-410-057-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable fuel-pump fairing (Ref. AMM TASK 28-21-49-400-801) .
(3) On the FLAPS control panel 114VU:
· remove the LOCKING TOOL-FLAP SLAT LEVER,INT.
POSITION (98D27803000000) from the slat/flap control lever.
(4) Remove the warning notice(s).
(5) Remove the safety barriers.
(6) Remove the access platform(s).
Subtask 24-92-00-862-057-A
B. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-801) .

JCP Title: C-CHECK CERTIFICATE OF TASK / INSPECTION COMPLETION: Page 5 of 6


JCP Ref: C-CHECK DATABASE REV DATE: Apr 01/2017
CERTIFIES THAT THE TASK / INSPECTION HAS BEEN COMPLETED TO THE REQUIRED PRINT DATE: Apr 06/2017 09:20
STANDARD AND SUPPORTS THE FINAL MAINTENANCE RELEASE / CERTIFICATE OF RELEASE
TO SERVICE
JOB CARD MPD-TASK: 200001-08
JAI - A330 AMM TASK : 24-92-00-210-808-A
24-92-00 PB 601

TITLE:
A/C Reg.: 24-92-00-210-808-A - General Visual Inspection of
VT-JWR the Braided Conduit End Fittings from Rib 6 to Fus...
MECH. INSP.

*** END OF CARD ***

JCP Title: C-CHECK CERTIFICATE OF TASK / INSPECTION COMPLETION: Page 6 of 6


JCP Ref: C-CHECK DATABASE REV DATE: Apr 01/2017
CERTIFIES THAT THE TASK / INSPECTION HAS BEEN COMPLETED TO THE REQUIRED PRINT DATE: Apr 06/2017 09:20
STANDARD AND SUPPORTS THE FINAL MAINTENANCE RELEASE / CERTIFICATE OF RELEASE
TO SERVICE

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