Visual Inspection of the Junction Box [CFMB]
TASK 72-23-00-210-007-A
Visual Inspection of the Junction Box
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 72-23-00-941-097-A ** ON A/C NOT FOR ALL
Subtask 72-23-00-210-067-A ** ON A/C NOT FOR ALL
Subtask 72-23-00-410-130-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:41:56 UTC
Visual Inspection of the Junction Box
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 1M(3 FT) |
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.CP2242) | RTV 732 |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [1000EM1] (ENGINE-1) | |
| 437AL, 438AR, 451AL, 452AR | |
| FOR [1000EM2] (ENGINE-2) | |
| 447AL, 448AR, 461AL, 462AR | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 71-13-00-010-040-B | Opening of the Fan Cowl Doors |
| TASK 71-13-00-410-040-B | Closing of the Fan Cowl Doors |
| TASK 72-23-00-300-046-A | Replacement of Lateral Bracket Plate on the Junction Box |
| TASK 78-30-00-081-041-B | Make the Thrust Reverser Serviceable after Maintenance |
| TASK 78-30-00-481-041-B | Make the Thrust Reverser Unserviceable for Maintenance |
| TASK 78-36-00-010-040-B | Opening of the Thrust Reverser Doors |
| TASK 78-36-00-410-040-B | Closing of the Thrust Reverser Doors |
Subtask 72-23-00-941-097-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 72-23-00-010-123-A ** ON A/C NOT FOR ALL (1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
B. Get Access
(1) Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
(2) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(3) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(4) Put an ACCESS PLATFORM 1M(3 FT) in position.
Subtask 72-23-00-040-078-A ** ON A/C NOT FOR ALL Subtask 72-23-00-010-136-A ** ON A/C NOT FOR ALL (1) Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
(2) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(3) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(4) Put an ACCESS PLATFORM 1M(3 FT) in position.
D. Open the thrust reverser doors (Ref. AMM TASK 78-36-00-010-040):
(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
4. Procedure(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 72-23-00-210-067-A ** ON A/C NOT FOR ALL
A. Visual Inspection of the Junction Box
Subtask 72-23-00-210-068-A ** ON A/C NOT FOR ALL | INSPECT/CHECK | MAXIMUM SERVICEABLE LIMITS | REMARKS |
|---|---|---|
| 1.Crack on the two lateral bracket plates. | One crack 0.78 in. (20 mm) max length. | Stop crack by drilling a 0.12 in. (3 mm) hole at each end of the crack. Clean the part. Apply RTV 732 (Material No.CP2242) or equivalent to the inner face of the affected area |
| | Any amount | Replace the lateral bracket plate (Ref. AMM TASK 72-23-00-300-046). |
| 2.Loose or missing rivet on the two lateral bracket plates | Not serviceable | Replace the lateral bracket plate (Ref. AMM TASK 72-23-00-300-046). |
B. Visual Inspection of the Junction Box (PRE CFM SB 72-0845)
Subtask 72-23-00-210-069-A ** ON A/C NOT FOR ALL | INSPECT/CHECK | MAXIMUM SERVICEABLE LIMITS | REMARKS |
|---|---|---|
| Crack on the lateral stiffeners. | One crack per stiffener is permitted if the crack is not going over the radius with lateral faces | Stop crack by drilling a 0.12 in. (3 mm) hole at each end of the crack. Clean the part with light duty aqueous cleaning. Apply RTV 732 (Material No.CP2242) or equivalent to the crack and drilled hole |
| Wear on the lateral stiffeners | Any amount if not going through the skin | |
C. Visual Inspection of the Junction Box (POST CFM SB 72-0845)
5. Close-up| INSPECT/CHECK | MAXIMUM SERVICEABLE LIMITS | REMARKS |
|---|---|---|
| Crack on the lateral stiffeners | Not serviceable | |
| Wear on the lateral stiffeners | Any amount if not going through the skin | |
Subtask 72-23-00-410-130-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser doors (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 72-23-00-440-073-A ** ON A/C NOT FOR ALL Subtask 72-23-00-410-115-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser doors (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Junction Box