W DOC AIRBUS | AMM A320F

Inspection of the Stage 2-4 Nozzle Segments [CFMI]


TASK 72-54-00-290-003-A
Inspection of the Stage 2-4 Nozzle Segments


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 60 and 55 lbf.in (0.68 and 0.62 m.daN ) T
856A1320
1
BORESCOPE-KIT
856A1322
1
BORESCOPE-LIGHT SOURCE SET
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2101)
graphite grease
(Material No.CP2619)
Never Seez-Pure Nickel, Special
(Material No.CP8001)
lockwire 0.032 in. (0.8 mm) dia.
(Material No.CP8002)
lockwire 0.032 in. (0.8 mm) dia
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-040-A
Closing of the Fan Cowl Doors
TASK 72-00-00-200-005-A
Over-Serviceable-Limit Extensions
TASK 78-30-00-081-041-A
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-36-00-010-040-A
Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-A
Closing of the Thrust Reverser Doors
3. Job Set-up
Subtask 72-54-00-941-052-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 72-54-00-010-052-A ** ON A/C NOT FOR ALL
B. Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
   (1) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (2) FOR [1000EM2] (ENGINE-2)
447AL 448AR
Subtask 72-54-00-040-052-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 72-54-00-010-062-A ** ON A/C NOT FOR ALL
D. Open the thrust reverser cowl 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
Subtask 72-54-00-010-057-A ** ON A/C NOT FOR ALL
A. Remove the Borescope Plugs
   (1) Let the temperature of the parts decrease to ambient temperature.
   (2) Cut and remove the lockwires and remove the LPT borescope plugs S20, S21 and S22.
NOTE: The borescope plugs S20, S21, S22 are located approximately at 5:00 o'clock (ALF) on the LPT case, and from front to rear, relate to the 2nd, 3rd and 4th stages of the LPT respectively.
Subtask 72-54-00-480-052-A ** ON A/C NOT FOR ALL
B. Install the 856A1320 BORESCOPE-KIT (G01) as follows:
   (1) Connect the power supply.
CAUTION: BEFORE YOU CONNECT THE POWER SUPPLY TO THE POWER SOURCE BE SURE THE ON-OFF SWITCH IS IN THE OFF POSITION AND LIGHT INTENSITY CONTROL IS SET TO MINIMUM. MAKE SURE THAT PROJECTOR AND POWER SUPPLY ARE CORRECTLY GROUNDED.
     (a) Connect the power supply to a grounded power source.
   (2) Connect light source cable to rigid borescope and to port on 856A1322 BORESCOPE-LIGHT SOURCE SET (856A1322/P02/P03/P04/P07/P08).
   (3) Turn light source on; insert borescope and position it as desired for inspection.
Subtask 72-54-00-290-052-A ** ON A/C NOT FOR ALL
C. Inspect the Stage 2-4 Nozzle Segment for the Following
NOTE: For maximum service limits (Ref. AMM TASK 72-00-00-200-005).
NOTE: The following limits are given for nozzle segments you can see near the borescope holes.
INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
1.Cracks in airfoil.
Not serviceable

2.Cracks in leading edge and/or trailing edge.
Any quantity not more than 0.12 in. (3.05 mm) long.
See limit extension (Ref. AMM TASK 72-00-00-200-005).
3.Nicks and/or dents on leading edge and/or trailing edge.
Any quantity, not more than 0.02 in. (0.5 mm) deep.
See limit extensions (Ref. AMM TASK 72-00-00-200-005).
4.Nicks and/or dents on concave and/or convex sides.
Any quantity, not more than 0.01 in. (0.25 mm) deep.
See limit extensions (Ref. AMM TASK 72-00-00-200-005).
5.Burned areas, hot spots.
Up to 1 in.2 (645.2 mm2) per vane segment if separated by 2 unburned vanes.
See limit extensions (Ref. AMM TASK 72-00-00-200-005).
6.Deposit material peeling off on airfoil.
Any quantity, if you see no bowing and/or melting.

Subtask 72-54-00-080-052-A ** ON A/C NOT FOR ALL
D. Removal of the Borescope
   (1) When inspection is complete, turn lamp switch off, leave main light source blower on for a while to cool lamp and housing.
   (2) Remove the borescope.
Subtask 72-54-00-410-054-A ** ON A/C NOT FOR ALL
E. Install the Borescope Plug
   (1) Apply graphite grease (Material No.CP2101) or CP2619Never Seez-Pure Nickel, Special to the threads of the borescope plugs S20, S21, S22 and install on the LPT case.
   (2) TORQUE plugs to between 60 and 55 lbf.in (0.68 and 0.62 m.daN ) T and safety with CP8001lockwire 0.032 in. (0.8 mm) dia. or CP8002lockwire 0.032 in. (0.8 mm) dia.
5. Close-up
Subtask 72-54-00-410-055-A ** ON A/C NOT FOR ALL
Subtask 72-54-00-440-052-A ** ON A/C NOT FOR ALL
B. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 72-54-00-410-062-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 02:39:44 UTC