Installation of Nacelle Anti-Ice (NAI) Duct
TASK 30-21-49-400-807-A
Installation of Nacelle Anti-Ice (NAI) Duct
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 30-21-49-861-087-A ** ON A/C NOT FOR ALL
Subtask 30-21-49-410-125-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 08:18:35 UTC
Installation of Nacelle Anti-Ice (NAI) Duct
WARNING:
BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AND THE ADJACENT COMPONENTS AFTER ENGINE SHUTDOWN. THE ENGINE, THE ENGINE OIL AND THE ADJACENT COMPONENTS CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING:
WEAR APPLICABLE PERSONAL PROTECTIVE EQUIPMENT (PPE) WHEN YOU DO THIS TASK. BEFORE YOU USE PPE, READ, UNDERSTAND AND OBEY ALL INSTRUCTIONS FOR ITS USE. THESE INSTRUCTIONS INCLUDE INSTRUCTIONS FROM THE MANUFACTURER, YOUR EMPLOYER AND GOVERNMENT REGULATIONS. YOU CAN GET INJURED IF YOU DO NOT USE PPE. GET INSTRUCTIONS FROM YOUR EMPLOYER ON WHICH PPE IS NECESSARY.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobNOTE: The NAI duct is an interchangeable part. For the same duct, there are different part numbers with different conditions (form and color). The different part numbers stay fully interchangeable.
2. Job Set-up InformationA. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| P5200 Adhesion Promoter | |
| (Material No.PU1-0001) | Cloth |
| (Material No.PU1-0002) | Cable, Safety |
| (Material No.PU1-0012) | Tape, Thermosetting |
| (Material No.PU1-0012A) | Tape, Glass Cloth |
| (Material No.PU1-0027) | Cable, Safety |
| (Material No.PU2-0001) | Alcohol, Isopropyl |
| (Material No.PU3-0013) | Sealant |
| (Material No.PU3-0034) | Sealant |
| (Material No.PU4-0034) | PR-1200 RTV Clear Prime Coat |
| (Material No.PU5-0003) | Anti-Seize Compound |
| (Material No.PU5-0005) | Anti-Seize Compound |
| (Material No.PU5-0005A) | Anti-Seize Compound |
| (Material No.PU5-0005B) | Anti-Seize Compound |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 400 | POWER PLANT, NACELLES AND PYLONS |
| FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1) | |
| 437AL, 438AR, 451AL, 452AR | |
| FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2) | |
| 447AL, 448AR, 461AL, 462AR | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 30-21-12-400-801-A | Installation of the Nacelle Anti-Ice Sense-Tubes |
| TASK 30-21-51-400-802-A | Installation of the Upper Anti-Ice Valve |
| TASK 30-21-51-400-803-A | Installation of the Lower Anti-Ice Valve |
| TASK 36-11-49-400-822-A | Installation of the Environmental Control System (ECS) Ducts |
| TASK 36-11-52-400-802-A | Installation of the Bleed Pressure-Regulator Valve |
| TASK 71-00-00-790-802-A | Test No. 1 - Pneumatic Leak Test |
| TASK 71-00-00-860-833-A | Procedure to Prevent Engine Motoring |
| TASK 71-13-00-010-802-A | Opening of the Fan Cowl Doors |
| TASK 71-13-00-410-802-A | Closing of the Fan Cowl Doors |
| TASK 71-71-49-400-801-A | Installation of the Engine Drain Tubes and Pylon Drain Hoses |
| TASK 72-21-11-400-801-A | Installation of the Lower BiFi |
| TASK 78-30-00-040-805-A | Deactivation of the Thrust Reverser System for Ground Maintenance |
| TASK 78-30-00-440-805-A | Reactivation of the Thrust Reverser System after Ground Maintenance |
| TASK 78-36-00-010-802-A | Opening of the Thrust Reverser Cowl-Doors |
| TASK 78-36-00-410-802-A | Closing of the Thrust Reverser Cowl-Doors |
Subtask 30-21-49-861-087-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
Subtask 30-21-49-941-113-A ** ON A/C NOT FOR ALL (1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
B. Safety Precautions
(1) Make sure that you did the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
Subtask 30-21-49-865-115-A ** ON A/C NOT FOR ALL (1) Make sure that you did the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 30-21-49-010-157-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENG 1) | |||
| 122VU | ANTI ICE/ENG/1 | 1DN1 | X10 |
| FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2) | |||
| 122VU | ANTI ICE/ENG/2 | 1DN2 | W10 |
D. Get Access
(1) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
Subtask 30-21-49-040-094-A ** ON A/C NOT FOR ALL (1) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
E. Deactivation of the Thrust Reverser System for Ground Maintenance
Subtask 30-21-49-010-158-A ** ON A/C NOT FOR ALL WARNING:
YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE AN INJURY AND/OR DAMAGE.
(1) Make sure that the thrust reverser system is deactivated for ground maintenance (Ref. AMM TASK 78-30-00-040-805). F. Get Access
(1) Make sure that the thrust reverser cowl-doors are open (Ref. AMM TASK 78-36-00-010-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL 462AR
(2) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position.
4. Procedure(1) Make sure that the thrust reverser cowl-doors are open (Ref. AMM TASK 78-36-00-010-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL 462AR
(2) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position.
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
CAUTION:
REMOVE AND INSTALL PROTECTION COVERS AS NECESSARY TO PREVENT DAMAGE TO THE ENGINE AND ADJACENT COMPONENTS.
CAUTION:
WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
Subtask 30-21-49-420-097-A ** ON A/C NOT FOR ALL A. Installation of the Nacelle Anti-Ice (NAI) Ducts
(1) Removal of the protection covers:
(2) If necessary, install the Nacelle Anti-Ice (NAI) bumper plate (23) (Ref. AMM TASK 71-71-49-400-801):
(a) Remove the four bolts (20), eight washers (19), four spacers (21) and four nuts (22) that attach the two middle clamp-block brackets together.
(b) Apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the four nuts (22).
(c) Install the NAI bumper plate (23) on the two middle clamp-block brackets. Use the four bolts (20), eight washers (19), four spacers (21) and four nuts (22).
(a) Install the five link assemblies (9), (10) and (11):
1 Adjust the link assembly (9) to a nominal length of 2.57 in. (65.28 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
2 Adjust the two link assemblies (10) to a nominal length of 2.62 in. (66.55 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
3 Adjust the two link assemblies (11) to a nominal length of 2.50 in. (63.50 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
4 Apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the 11 nuts (8).
1 Adjust the two link assemblies (16) or (52) to a nominal length of 1.786 in. (45.36 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
2 Install the two link assemblies (16) or (52) to the brackets with the two bolts (17), four washers (6), two bushings (7), and two nuts (8).
1 Adjust the link assembly (16) to a nominal length of 1.786 in. (45.36 mm). Make sure that the threads of the link assembly rod covers the inspection hole.
2 Install the link assembly (16) to the bracket with the bolt (37), two washers (6), bushing (7), and nut (8).
1 Adjust the link assembly (36) to a nominal length of 5.475 in. (139.06 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
2 Install the link assembly (36) to the bracket with the bolt (5), two washers(6), bushing (7) and nut (8).
1 Adjust the link assembly (39) to a nominal length of 3.50 in. (88.90 mm).
2 Install the link assembly (39) to the bracket with the bolt (5), two washers (6), bushing (7) and nut (8).
1 Adjust the link assembly (42) to a nominal length of 4.86 in. (123.44 mm).
2 Install the link assembly (42) on the bracket with the bolt (5), two washers (6), bushing (7) and nut (8).
(a) If the thermosetting tape is not on the ducts (15) and (26), install the tape where the clamps will be. Do step 4.A.(4)(c)1_ thru step 4.A.(4)(c)5_, as necessary.
(b) Examine the thermosetting tape for the insulation covers on the ducts (15) and (26). Make sure that the tape is not torn or loose. Make sure that the diameter of the duct and tape are the minimum distances for each location. Refer to step 4.A.(4)(c)1_ through step 4.A.(4)(c)5_ for the minimum distances.
(c) If the tape is damaged or the diameters are too small, remove the thermosetting tape. Install the new tape as follows:
1 WindPU1-0012 Tape, Thermosetting around the middle NAI duct (15) and the forward NAI duct (26) where you will install the two hose clamps (27) for the insulation cover (28). Wind one to six layers of tape on each duct, until the diameter of the duct and tape is a minimum of 1.75 in. (44.4 mm).
PU1-0012 Tape, Thermosetting around the forward NAI duct (26) where clamps on the insulation cover (31) will be. Wind one to six layers of tape at each clamp location, until the diameter of the duct and tape is a minimum of 1.85 in. (47.0 mm).
3 WindPU1-0012 Tape, Thermosetting around the forward NAI duct (26) where you will install the two hose clamps (33) and the hose clamp (51) for the insulation covers (32) and (34). Wind from one to six layers of tape at each clamp location, until the diameter of the duct and tape is a minimum of 1.85 in. (47.0 mm).
4 WindPU1-0012 Tape, Thermosetting around the forward NAI duct (26) where you will install the two hose clamps (33) for the insulation cover (38) or (53). Wind from one to six layers of tape at each clamp location, until the diameter of the duct and tape is a minimum of 1.85 in. (47.0 mm).
5 WindPU1-0012 Tape, Thermosetting around the forward NAI duct (26) where you will install the hose clamps (35), (45) and (46) for the insulation cover (40). Wind from one to six layers of tape at each clamp location, until the diameter of the duct and tape is a minimum of 1.85 in. (47.0 mm).
(5) Install the aft NAI ducts:
(a) Install the aft NAI duct (1):
1 Put the seal (4) in the aft NAI duct (1).
2 Apply Anti-Seize Compound (Material No.PU5-0005) to the threads of the three bolts (2).
1 Attach the short NAI duct (14) to the upper anti-ice valve. Use the V-retainer coupling (12) and seal (13).
2 Turn the V-retainer coupling (12) so that the nut faces outboard from the engine on the aft side of the upper anti-ice valve. Tighten the V-retainer coupling (12) sufficiently to hold the short NAI duct (14) on the upper anti-ice valve.
1 Attach the middle NAI duct (15) to the lower anti-ice valve. Use the V-retainer coupling (12) and seal (13).
2 Turn the V-retainer coupling (12) so that the nut faces down on the outboard side of the lower anti-ice valve. Tighten the V-retainer coupling (12) sufficiently to hold the middle NAI duct (15) on the lower anti-ice valve.
4 Attach the middle NAI duct (15) and igniter cable bracket (18) to the NAI bumper plate (23). Use the four bolts (20), eight washers (19), four spacers (21) and four nuts (22).
a Attach the middle NAI duct (15) to the two link assemblies (16). Use the two bolts (5), four washers (6), two bushings (7) and two nuts (8).
a Attach the middle NAI duct (15) to the two link assemblies (52). Use the two bolts (5), four washers (6), two bushings (7) and two nuts (8).
1 Put the forward NAI duct (26) in the lower bifurcation firewall.
2 Attach the forward NAI duct (26) to the middle NAI duct (15). Use the V-retainer coupling (24) and seal (25).
5 Apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the three bolts (29).
6 Attach the forward NAI duct (26) to the lower bifurcation firewall with the three bolts (29) and three washers (30). Torque the bolts (29) to between 70 and 63 lbf.in (0.79 and 0.71 m.daN )
.
(8) Tighten the bolts (2):
(a) TORQUE the bolts (2) to between 70 and 63 lbf.in (0.79 and 0.71 m.daN )
.
(b) Safety the two bolts (2) with aPU1-0002 Cable, Safety .
PU1-0002 Cable, Safety .
(9) Tighten the V-retainer couplings (12), (24) and (44):
(a) TORQUE the V-retainer couplings (12), (24) and (44) to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
.
(b) Tap around the outer surface of the V-retainer couplings (12), (24) and (44) with a HAMMER - FIBER.
(c) TORQUE the V-retainer couplings (12), (24) and (44) again to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
.
(d) Tap around the outer surface of the V-retainer couplings (12), (24) and (44) with a HAMMER - FIBER.
(e) TORQUE the V-retainer couplings (12), (24) and (44) a third time to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
.
(f) Tap around the outer surface of the V-retainer couplings (12), (24) and (44) with a HAMMER - FIBER.
(g) TORQUE the V-retainer couplings (12), (24) and (44) to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
.
(10) Tighten the XDCR2 sense tube to the forward NAI duct (26) (Ref. AMM TASK 30-21-12-400-801).
(11) Safety the link assembly (36) withPU1-0002 Cable, Safety .
(12) For Configuration 2, do the following:
(a) Safety the two link assemblies (52) withPU1-0002 Cable, Safety .
(13) TORQUE the nuts (8) to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
.
(14) TORQUE the nuts (22) to between 27 and 23 lbf.in (0.31 and 0.26 m.daN )
.
PU2-0001 Alcohol, Isopropyl on a clean Cloth (Material No.PU1-0001) . Remove the PU2-0001 Alcohol, Isopropyl with a clean Cloth (Material No.PU1-0001) before it dries.
(b) Apply a layer of the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) along the longitudinal splitline of the insulation cover (31) and the mating surface of the insulation cover (31) and the lower bifurcation firewall. Let the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) dry for at least 30 minutes, but not more than four hours, before you apply the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer.
PU1-0012 Tape, Thermosetting that you installed in step 4.A.(4)(c)2_. Do not tighten them too much.
(e) Make sure that the Sealant (Material No.PU3-0013) fully cures before the aircraft flies. Refer to the instructions of the manufacturer for cure times.
(f) Disconnect the wire harnesses from the spring clips on the B-flange bracket (50) adjacent to the link assembly (16) attached to the forward NAI duct (26).
(g) Remove the two bolts (49), washers (47) and nuts (48) that attach the B-flange bracket (50) to flange B. Remove the B-flange bracket (50).
PU2-0001 Alcohol, Isopropyl on a clean Cloth (Material No.PU1-0001) . Remove the PU2-0001 Alcohol, Isopropyl with a clean Cloth (Material No.PU1-0001) before it dries.
(i) Apply a layer of PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) where the flaps of the insulation cover (34) make an overlap adjacent to the link assembly (16) and along the splitline. Let the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) dry for at least 30 minutes, but not more than four hours, before you apply the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer.
(l) Install the B-flange bracket (50) to flange B with the two bolts (49), two washers (47) and two nuts (48). Make sure that the bolts go through the holes in the adjacent brackets.
(m) Torque the nuts (48) to between 100 and 90 lbf.in (1.13 and 1.02 m.daN )
.
(n) Attach the wire harnesses to the spring clips on the B-flange bracket (50).
(o) Install the insulation cover (32) and the bottom piece of the insulation cover (34) on the forward NAI duct (26). Use the clamp (46), the two clamps (33) and the clamp (51). Put the insulation cover (32) grommet on the link assembly (36) under the clamp (46). Put the clamps (33) and (51) on thePU1-0012 Tape, Thermosetting that you installed in step 4.A.(4)(c)3_. Tighten the clamp on the insulation cover (32) and the clamps (33), (46) and (51) with your hand until they hold the insulation covers (32) and (34) tightly.
(q) Hold the flaps of the insulation cover (34) together until the Sealant (Material No.PU3-0013) fully cures. Refer to the instructions of the manufacturer for cure times.
PU1-0002 Cable, Safety . Safety the pieces of the insulation cover (34) together with PU1-0002 Cable, Safety .
(s) Install the insulation cover (38) or (53) on the forward NAI duct (26). Use the two clamps (33) and clamp (46). Put the insulation cover (38) or (53) grommet on the link assembly (39) under the clamp (46). Put the clamps (33) on thePU1-0012 Tape, Thermosetting that you installed in step 4.A.(4)(c)4_. Tighten the clamps (33) and clamp (46) with your hand until they hold the insulation cover (38) or (53) tightly.
PU1-0002 Cable, Safety .
(u) Install the insulation cover (41) on the forward NAI duct (26) and inlet cowl anti-ice duct. Tighten the clamp on the insulation cover (41) until it holds the cover tightly. Do not tighten it too much.
(v) Safety the pieces of the insulation cover (41) together withPU1-0002 Cable, Safety .
(w) For PRE SB GRAA320NEO-A-30-21-0001-00001-930A-D, do the following:
1 Install the insulation cover (40) on the forward NAI duct (26). Use the two clamps (46), the clamp (45) and the clamp (35). Put the insulation cover (40) grommets on the link assemblies (10) and (42) under the clamps (46). Put the insulation cover (40) grommet on the XDCR2 sense tube under the clamp (35). Put the two clamps (46), the clamp (45) and the clamp (35) on thePU1-0012 Tape, Thermosetting that you installed in step 4.A.(4)(c)5_. Tighten the clamp on the insulation cover (40) and the clamps (46), (45) and (35) with your hand until they hold the insulation cover (40) tightly.
1 Clean the surface along the splitline of the insulation cover (40) adjacent to the link assembly (10) and the interior of the insulation cover (40) adjacent to the link assembly (10). UsePU2-0001 Alcohol, Isopropyl on a clean Cloth (Material No.PU1-0001) . Remove the PU2-0001 Alcohol, Isopropyl with a clean Cloth (Material No.PU1-0001) before it dries.
2 Apply a layer of PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) along the splitline of the insulation cover (40) adjacent to the link assembly (10) and the interior of the insulation cover (40) adjacent to the link assembly (10). Let the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) dry for at least 30 minutes, but not more than four hours, before you apply the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer.
4 Install the insulation cover (40) on the forward NAI duct (26). Use the clamp (46), the clamp (45) and the clamp (35). Put the insulation cover (40) grommet on the link assembly (42) under the clamp (46). Put the insulation cover (40) grommet on the link assembly (10) adjacent to the end of the cover. Put the insulation cover (40) grommet on the XDCR2 sense tube under the clamp (35). Put the clamp (46), the clamp (45) and the clamp (35) on thePU1-0012 Tape, Thermosetting that you installed in step 4.A.(4)(c)5_. Tighten the clamp on the insulation cover (40) and the clamps (46), (45) and (35) with your hand until they hold the insulation cover (40) tightly.
6 Make sure that the Sealant (Material No.PU3-0013) fully cures before the aircraft flies. Refer to the instructions of the manufacturer for cure times.
(y) Safety the pieces of the insulation cover (40) together withPU1-0002 Cable, Safety .
PU1-0012 Tape, Thermosetting that you installed in step 4.A.(4)(c)1_. Tighten the clamps (27) until they hold the covers tightly. Do not tighten them too much.
(aa) Safety the pieces of the insulation cover (28) together withPU1-0002 Cable, Safety .
(16) Put the ignition cables in the middle NAI duct (15) spring clips.
Subtask 30-21-49-410-127-A ** ON A/C NOT FOR ALL (1) Removal of the protection covers:
CAUTION:
REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY TO PREVENT ENGINE DAMAGE.
(a) Make sure that you remove all the necessary COVER - PROTECTION to prevent damage to the engine and adjacent components.(2) If necessary, install the Nacelle Anti-Ice (NAI) bumper plate (23) (Ref. AMM TASK 71-71-49-400-801):
(a) Remove the four bolts (20), eight washers (19), four spacers (21) and four nuts (22) that attach the two middle clamp-block brackets together.
(b) Apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the four nuts (22).
(c) Install the NAI bumper plate (23) on the two middle clamp-block brackets. Use the four bolts (20), eight washers (19), four spacers (21) and four nuts (22).
NOTE: Do not torque the nuts (22) at this time.
(3) If necessary, install the link assemblies: (a) Install the five link assemblies (9), (10) and (11):
1 Adjust the link assembly (9) to a nominal length of 2.57 in. (65.28 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
2 Adjust the two link assemblies (10) to a nominal length of 2.62 in. (66.55 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
3 Adjust the two link assemblies (11) to a nominal length of 2.50 in. (63.50 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
4 Apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the 11 nuts (8).
NOTE: All the nuts (8) in this procedure must have Anti-Seize Compound (Material No.PU5-0003) on their threads before installation.
5 Install the link assembly (9) to the bracket with the bolt (5), two washers (6), bushing (7) and nut (8). NOTE: Do not torque the nut (8) at this time.
6 Install the two link assemblies (10) to the brackets with the two bolts (5), four washers (6), two bushings (7) and two nuts (8). NOTE: Do not torque the nuts (8) at this time.
7 Install the two link assemblies (11) to the brackets with the two bolts (5),four washers (6), two bushings (7) and two nuts (8). NOTE: Do not torque the nuts (8) at this time.
(b) Install the two link assemblies (16) or (52): 1 Adjust the two link assemblies (16) or (52) to a nominal length of 1.786 in. (45.36 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
2 Install the two link assemblies (16) or (52) to the brackets with the two bolts (17), four washers (6), two bushings (7), and two nuts (8).
NOTE: Do not torque the nuts (8) at this time.
(c) Install the link assembly (16): 1 Adjust the link assembly (16) to a nominal length of 1.786 in. (45.36 mm). Make sure that the threads of the link assembly rod covers the inspection hole.
2 Install the link assembly (16) to the bracket with the bolt (37), two washers (6), bushing (7), and nut (8).
NOTE: Do not torque the nut (8) at this time.
(d) Install the link assembly (36): 1 Adjust the link assembly (36) to a nominal length of 5.475 in. (139.06 mm). Make sure that the threads of the link assembly rods cover the inspection hole.
2 Install the link assembly (36) to the bracket with the bolt (5), two washers(6), bushing (7) and nut (8).
NOTE: Do not torque the nut (8) at this time.
(e) Install the link assembly (39): 1 Adjust the link assembly (39) to a nominal length of 3.50 in. (88.90 mm).
2 Install the link assembly (39) to the bracket with the bolt (5), two washers (6), bushing (7) and nut (8).
NOTE: Do not torque the nut (8) at this time.
(f) Install the link assembly (42): 1 Adjust the link assembly (42) to a nominal length of 4.86 in. (123.44 mm).
2 Install the link assembly (42) on the bracket with the bolt (5), two washers (6), bushing (7) and nut (8).
NOTE: Do not torque the nut (8) at this time.
(4) Examine the thermosetting tape on the ducts (15) and (26):(a) If the thermosetting tape is not on the ducts (15) and (26), install the tape where the clamps will be. Do step 4.A.(4)(c)1_ thru step 4.A.(4)(c)5_, as necessary.
(b) Examine the thermosetting tape for the insulation covers on the ducts (15) and (26). Make sure that the tape is not torn or loose. Make sure that the diameter of the duct and tape are the minimum distances for each location. Refer to step 4.A.(4)(c)1_ through step 4.A.(4)(c)5_ for the minimum distances.
(c) If the tape is damaged or the diameters are too small, remove the thermosetting tape. Install the new tape as follows:
1 Wind
NOTE: You can use PU1-0012A Tape, Glass Cloth as an alternative to PU1-0012 Tape, Thermosetting .
2 Wind 3 Wind
4 Wind
5 Wind
(5) Install the aft NAI ducts:
(a) Install the aft NAI duct (1):
1 Put the seal (4) in the aft NAI duct (1).
2 Apply Anti-Seize Compound (Material No.PU5-0005) to the threads of the three bolts (2).
NOTE: You can use Anti-Seize Compound (Material No.PU5-0005A) or Anti-Seize Compound (Material No.PU5-0005B) as an alternative to Anti-Seize Compound (Material No.PU5-0005) . Refer to the instructions of the manufacturer.
3 Attach the aft NAI duct (1) and seal (4) to the engine case with the three bolts (2) and three washers (3). NOTE: Do not torque the bolts (2) at this time.
4 Apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the 11 nuts (8). NOTE: All the nuts (8) in this procedure must have Anti-Seize Compound (Material No.PU5-0003) on their threads before installation.
5 Attach the aft NAI duct (1) to the three link assemblies (9), (10) and (11). Use the three bolts (5), six washers (6), three bushings (7) and three nuts (8). NOTE: Do not torque the nuts (8) at this time.
(b) Attach the upper anti-ice valve to the aft NAI duct (1). Use the V-retainer coupling (12) and seal (13) (Ref. AMM TASK 30-21-51-400-802). NOTE: Do not torque the V-retainer coupling (12) at this time.
(c) Install the short NAI duct (14): 1 Attach the short NAI duct (14) to the upper anti-ice valve. Use the V-retainer coupling (12) and seal (13).
2 Turn the V-retainer coupling (12) so that the nut faces outboard from the engine on the aft side of the upper anti-ice valve. Tighten the V-retainer coupling (12) sufficiently to hold the short NAI duct (14) on the upper anti-ice valve.
NOTE: Do not torque the V-retainer coupling (12).
3 Attach the short NAI duct (14) to the link assembly (11). Use the bolt (5), two washers (6), bushing (7) and nut (8). NOTE: Do not torque the nut (8) at this time.
(d) Attach the lower anti-ice valve to the short NAI duct (14). Use the V-retainer coupling (12) and the seal (13) (Ref. AMM TASK 30-21-51-400-803). NOTE: Do not torque the V-retainer coupling (12) at this time.
(e) Install the middle NAI duct (15): 1 Attach the middle NAI duct (15) to the lower anti-ice valve. Use the V-retainer coupling (12) and seal (13).
2 Turn the V-retainer coupling (12) so that the nut faces down on the outboard side of the lower anti-ice valve. Tighten the V-retainer coupling (12) sufficiently to hold the middle NAI duct (15) on the lower anti-ice valve.
NOTE: Do not torque the V-retainer coupling (12).
3 If you did not apply the Anti-Seize Compound (Material No.PU5-0003) before in step 4.A.(2)(b), apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the four nuts (22). 4 Attach the middle NAI duct (15) and igniter cable bracket (18) to the NAI bumper plate (23). Use the four bolts (20), eight washers (19), four spacers (21) and four nuts (22).
NOTE: Do not torque the nuts (22) at this time.
5 For Configuration 1, do the following: a Attach the middle NAI duct (15) to the two link assemblies (16). Use the two bolts (5), four washers (6), two bushings (7) and two nuts (8).
NOTE: Do not torque the nuts (8) at this time.
6 For Configuration 2, do the following: a Attach the middle NAI duct (15) to the two link assemblies (52). Use the two bolts (5), four washers (6), two bushings (7) and two nuts (8).
NOTE: Do not torque the nuts (8) at this time.
(f) Install the forward NAI duct (26): 1 Put the forward NAI duct (26) in the lower bifurcation firewall.
2 Attach the forward NAI duct (26) to the middle NAI duct (15). Use the V-retainer coupling (24) and seal (25).
NOTE: Do not torque the V-retainer coupling (24) at this time.
3 Attach the forward NAI duct (26) to the inlet cowl anti-ice duct. Use the V-retainer coupling (44) and seal (43). NOTE: Do not torque the V-retainer coupling (44) at this time.
4 Install the lower bifurcation firewall (Ref. AMM TASK 72-21-11-400-801). 5 Apply a thin layer of Anti-Seize Compound (Material No.PU5-0003) to the threads of the three bolts (29).
6 Attach the forward NAI duct (26) to the lower bifurcation firewall with the three bolts (29) and three washers (30). Torque the bolts (29) to between 70 and 63 lbf.in (0.79 and 0.71 m.daN )
.CAUTION:
MAKE SURE THAT YOU INSTALL THE BOLT(S) IN THE DIRECTION(S) SHOWN IN THE ILLUSTRATION. IF YOU CHANGE THE DIRECTION(S), YOU CAN CAUSE DAMAGE TO THE INSULATION COVER(S).
7 Attach the forward NAI duct (26) to the four link assemblies (10), (36), (39) and (42). Use the four bolts (5), eight washers (6), four bushings (7) and four nuts (8). NOTE: Do not torque the nuts (8) at this time.
CAUTION:
MAKE SURE THAT YOU INSTALL THE BOLT(S) IN THE DIRECTION(S) SHOWN IN THE ILLUSTRATION. IF YOU CHANGE THE DIRECTION(S), YOU CAN CAUSE DAMAGE TO THE INSULATION COVER(S).
8 Attach the forward NAI duct (26) to the link assembly (16). Use the bolt (5), two washers (6), bushing (7) and nut (8). NOTE: Do not torque the nut (8) at this time.
(6) Connect the XDCR2 sense tube to the forward NAI duct (26) (Ref. AMM TASK 30-21-12-400-801). NOTE: Do not torque the XDCR2 sense tube at this time.
(7) Adjustment of the NAI ducts, the XDCR2 sense tube and the link assemblies: CAUTION:
MAKE SURE THAT THERE IS NO TENSION ON THE LINK ASSEMBLIES FOR THE NAI DUCTS. MAKE SURE THE MATING SURFACES BETWEEN THE DUCTS CORRECTLY ALIGN. TENSION AND INCORRECT ALIGNMENT CAN CAUSE AIR LEAKAGE, WHICH CAN CAUSE DAMAGE TO THE EQUIPMENT.
(a) Adjust the NAI ducts (1), (14), (15) and (26), the XDCR2 sense tube and the link assemblies (9), (10), (11), (16), (36), (39) and (42) to keep preload to a minimum. Make sure that the V-retainer couplings (12) and (24) are in the approximate position as shown in the illustration. (8) Tighten the bolts (2):
(a) TORQUE the bolts (2) to between 70 and 63 lbf.in (0.79 and 0.71 m.daN )
. (b) Safety the two bolts (2) with a
NOTE: You can use PU1-0027 Cable, Safety as an alternative to PU1-0002 Cable, Safety .
(c) Safety the bolt (2) and the ECS bolt with a (9) Tighten the V-retainer couplings (12), (24) and (44):
(a) TORQUE the V-retainer couplings (12), (24) and (44) to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
. (b) Tap around the outer surface of the V-retainer couplings (12), (24) and (44) with a HAMMER - FIBER.
(c) TORQUE the V-retainer couplings (12), (24) and (44) again to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
. (d) Tap around the outer surface of the V-retainer couplings (12), (24) and (44) with a HAMMER - FIBER.
(e) TORQUE the V-retainer couplings (12), (24) and (44) a third time to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
. (f) Tap around the outer surface of the V-retainer couplings (12), (24) and (44) with a HAMMER - FIBER.
(g) TORQUE the V-retainer couplings (12), (24) and (44) to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
. (10) Tighten the XDCR2 sense tube to the forward NAI duct (26) (Ref. AMM TASK 30-21-12-400-801).
(11) Safety the link assembly (36) with
(12) For Configuration 2, do the following:
(a) Safety the two link assemblies (52) with
(13) TORQUE the nuts (8) to between 70 and 55 lbf.in (0.79 and 0.62 m.daN )
. (14) TORQUE the nuts (22) to between 27 and 23 lbf.in (0.31 and 0.26 m.daN )
. CAUTION:
WHEN YOU INSTALL THE INSULATION COVERS, BE CAREFUL NOT TO CAUSE DAMAGE TO THEM. DAMAGED, TORN OR RIPPED COVERS MUST BE REPLACED.
(15) Installation of the insulation covers. NOTE: Make sure that the hose clamps are in the positions shown in the illustration or in a position that provides easy access to the hose clamps.
(a) Clean the surface along the longitudinal splitline of the insulation cover (31), the mating surface of the insulation cover (31) and the lower bifurcation firewall. Use (b) Apply a layer of the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) along the longitudinal splitline of the insulation cover (31) and the mating surface of the insulation cover (31) and the lower bifurcation firewall. Let the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) dry for at least 30 minutes, but not more than four hours, before you apply the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer.
NOTE: You can use PU4-0032 P5200 Adhesion Promoter as an alternative to PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) . Refer to the instructions of the manufacturer.
NOTE: If you do not apply the Sealant (Material No.PU3-0013) within four hours after you apply the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) , put a COVER - PROTECTION on the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) . Apply the Sealant (Material No.PU3-0013) within 24 hours of when you applied the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) . If you do not apply the Sealant (Material No.PU3-0013) within 24 hours, remove the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) with PU2-0001 Alcohol, Isopropyl on a clean Cloth (Material No.PU1-0001) . Dry the PU2-0001 Alcohol, Isopropyl off the surface with a clean Cloth (Material No.PU1-0001) and then do step 4.A.(15)(b) again.
(c) Apply the Sealant (Material No.PU3-0013) to the mating surface of the insulation cover (31) and the lower bifurcation firewall. Also apply the sealant to the longitudinal splitline of the insulation cover (31). Refer to the instructions of the manufacturer.NOTE: You can use the Sealant (Material No.PU3-0034) as an alternative to the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer for differences in cure time.
(d) Install the insulation cover (31) on the forward NAI duct (26). Tighten the clamps on the insulation cover (31) until they hold the cover tightly on the (e) Make sure that the Sealant (Material No.PU3-0013) fully cures before the aircraft flies. Refer to the instructions of the manufacturer for cure times.
(f) Disconnect the wire harnesses from the spring clips on the B-flange bracket (50) adjacent to the link assembly (16) attached to the forward NAI duct (26).
(g) Remove the two bolts (49), washers (47) and nuts (48) that attach the B-flange bracket (50) to flange B. Remove the B-flange bracket (50).
NOTE: You must remove the B-flange bracket (50) to have sufficient clearance to install the insulation cover (34).
(h) Clean the surface where the flaps of the insulation cover (34) make an overlap adjacent to the link assembly (16) and along the splitline. Use (i) Apply a layer of PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) where the flaps of the insulation cover (34) make an overlap adjacent to the link assembly (16) and along the splitline. Let the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) dry for at least 30 minutes, but not more than four hours, before you apply the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer.
NOTE: If you do not apply the Sealant (Material No.PU3-0013) within four hours after you apply the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) , put a COVER - PROTECTION on the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) . Apply the Sealant (Material No.PU3-0013) within 24 hours of when you applied the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) . If you do not apply the Sealant (Material No.PU3-0013) within 24 hours, remove the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) with PU2-0001 Alcohol, Isopropyl on a clean Cloth (Material No.PU1-0001) . Dry the PU2-0001 Alcohol, Isopropyl off the surface with a clean Cloth (Material No.PU1-0001) and then do step 4.A.(15)(i) again.
(j) Make sure that the flaps of the insulation cover (34) make an overlap adjacent to the link assembly (16). Put a thick layer between 0.003 in. (0.076 mm) and 0.006 in. (0.152 mm) of the Sealant (Material No.PU3-0013) on the bottom of the top flap adjacent to the link assembly (16) and along the splitline. NOTE: You can put a small bead of the Sealant (Material No.PU3-0013) along the edge of the flaps to make sure you push out some sealant when you push the flaps together.
(k) Install the top piece of the cover (34) on the forward NAI duct (26). (l) Install the B-flange bracket (50) to flange B with the two bolts (49), two washers (47) and two nuts (48). Make sure that the bolts go through the holes in the adjacent brackets.
(m) Torque the nuts (48) to between 100 and 90 lbf.in (1.13 and 1.02 m.daN )
. (n) Attach the wire harnesses to the spring clips on the B-flange bracket (50).
(o) Install the insulation cover (32) and the bottom piece of the insulation cover (34) on the forward NAI duct (26). Use the clamp (46), the two clamps (33) and the clamp (51). Put the insulation cover (32) grommet on the link assembly (36) under the clamp (46). Put the clamps (33) and (51) on the
NOTE: Do not tighten the clamps (33), (46) and (51) more than 18 lbf.in (0.20 m.daN).
(p) Push the flaps of the insulation cover (34) together until you see the Sealant (Material No.PU3-0013) come out from between the flaps. Fair the Sealant (Material No.PU3-0013) you pushed out along the edge of the flaps. Clean the sealant that is more than 0.120 in. (3.05 mm) from the edge of the flaps. (q) Hold the flaps of the insulation cover (34) together until the Sealant (Material No.PU3-0013) fully cures. Refer to the instructions of the manufacturer for cure times.
NOTE: You can use tape or an equivalent mechanical device to hold the insulation cover (34) flaps together.
(r) Safety the pieces of the insulation cover (32) together with (s) Install the insulation cover (38) or (53) on the forward NAI duct (26). Use the two clamps (33) and clamp (46). Put the insulation cover (38) or (53) grommet on the link assembly (39) under the clamp (46). Put the clamps (33) on the
NOTE: Do not tighten the clamps (33) and clamp (46) more than 18 lbf.in (0.20 m.daN).
(t) Safety the pieces of the insulation cover (38) or (53) together with (u) Install the insulation cover (41) on the forward NAI duct (26) and inlet cowl anti-ice duct. Tighten the clamp on the insulation cover (41) until it holds the cover tightly. Do not tighten it too much.
(v) Safety the pieces of the insulation cover (41) together with
(w) For PRE SB GRAA320NEO-A-30-21-0001-00001-930A-D, do the following:
1 Install the insulation cover (40) on the forward NAI duct (26). Use the two clamps (46), the clamp (45) and the clamp (35). Put the insulation cover (40) grommets on the link assemblies (10) and (42) under the clamps (46). Put the insulation cover (40) grommet on the XDCR2 sense tube under the clamp (35). Put the two clamps (46), the clamp (45) and the clamp (35) on the
NOTE: Do not tighten the clamps (35), (45) and (46) more than 18 lbf.in (0.20 m.daN).
(x) For POST SB GRAA320NEO-A-30-21-0001-00001-930A-D, do the following: 1 Clean the surface along the splitline of the insulation cover (40) adjacent to the link assembly (10) and the interior of the insulation cover (40) adjacent to the link assembly (10). Use
2 Apply a layer of PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) along the splitline of the insulation cover (40) adjacent to the link assembly (10) and the interior of the insulation cover (40) adjacent to the link assembly (10). Let the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) dry for at least 30 minutes, but not more than four hours, before you apply the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer.
NOTE: If you do not apply the Sealant (Material No.PU3-0013) within four hours after you apply the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) , put a COVER - PROTECTION on the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) . Apply the Sealant (Material No.PU3-0013) within 24 hours of when you applied the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) . If you do not apply the Sealant (Material No.PU3-0013) within 24 hours, remove the PR-1200 RTV Clear Prime Coat (Material No.PU4-0034) with PU2-0001 Alcohol, Isopropyl on a clean Cloth (Material No.PU1-0001) . Dry the PU2-0001 Alcohol, Isopropyl off the surface with a clean Cloth (Material No.PU1-0001) and then do step 4.A.(15)(x)2_ again.
3 Apply the Sealant (Material No.PU3-0013) along the splitline of the insulation cover (40) adjacent to the link assembly (10). Refer to the instructions of the manufacturer.4 Install the insulation cover (40) on the forward NAI duct (26). Use the clamp (46), the clamp (45) and the clamp (35). Put the insulation cover (40) grommet on the link assembly (42) under the clamp (46). Put the insulation cover (40) grommet on the link assembly (10) adjacent to the end of the cover. Put the insulation cover (40) grommet on the XDCR2 sense tube under the clamp (35). Put the clamp (46), the clamp (45) and the clamp (35) on the
NOTE: Do not tighten the clamps (35), (45) and (46) more than 18 lbf.in (0.203 m.daN).
5 Fill the space between the insulation cover (40) and the link assembly (10) with the Sealant (Material No.PU3-0013) . Refer to the instructions of the manufacturer.6 Make sure that the Sealant (Material No.PU3-0013) fully cures before the aircraft flies. Refer to the instructions of the manufacturer for cure times.
(y) Safety the pieces of the insulation cover (40) together with
CAUTION:
MAKE SURE THAT THE DRAIN HOLE IS AT THE BOTTOM OF THE INSULATION COVER WHEN YOU INSTALL IT. IF THE DRAIN HOLE IS NOT AT THE BOTTOM, IT WILL NOT DRAIN THE LIQUID FROM THE COVER.
(z) Install the insulation cover (28) on the middle NAI duct (15) and forward NAI duct (26). Use the two clamps (27). Put the two clamps (27) on the (aa) Safety the pieces of the insulation cover (28) together with
(16) Put the ignition cables in the middle NAI duct (15) spring clips.
B. Installation of the NAI Sense Tubes
(1) Install the NAI sense tubes (Ref. AMM TASK 30-21-12-400-801).
(a) Attach the middle valve 1, middle valve 2 and XDCR1 sense tubes to the aft NAI duct (1) and the ECS duct.
(b) Connect the aft valve 1 sense tube to the aft NAI duct (1) and upper anti-ice valve.
(c) Connect the aft valve 2 sense tube to the aft NAI duct (1) and lower anti-ice valve.
(2) If necessary, install the ECS starter duct, pressure regulating valve and the ECS mid-Y duct (Ref. AMM TASK 36-11-52-400-802) and (Ref. AMM TASK 36-11-49-400-822).
5. Close-up(1) Install the NAI sense tubes (Ref. AMM TASK 30-21-12-400-801).
(a) Attach the middle valve 1, middle valve 2 and XDCR1 sense tubes to the aft NAI duct (1) and the ECS duct.
(b) Connect the aft valve 1 sense tube to the aft NAI duct (1) and upper anti-ice valve.
(c) Connect the aft valve 2 sense tube to the aft NAI duct (1) and lower anti-ice valve.
(2) If necessary, install the ECS starter duct, pressure regulating valve and the ECS mid-Y duct (Ref. AMM TASK 36-11-52-400-802) and (Ref. AMM TASK 36-11-49-400-822).
Subtask 30-21-49-410-125-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) Remove the access platform(s).
(3) Close the thrust reverser cowl-doors (Ref. AMM TASK 78-36-00-410-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL 462AR
Subtask 30-21-49-440-074-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Close the thrust reverser cowl-doors (Ref. AMM TASK 78-36-00-410-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL 462AR
B. Do the reactivation of the thrust reverser system after ground maintenance (Ref. AMM TASK 78-30-00-440-805).
Subtask 30-21-49-410-126-A ** ON A/C NOT FOR ALL C. Close Access
(1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
(2) Remove the WARNING NOTICE(S).
Subtask 30-21-49-865-116-A ** ON A/C NOT FOR ALL (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
(2) Remove the WARNING NOTICE(S).
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 30-21-49-862-070-A ** ON A/C NOT FOR ALL Subtask 30-21-49-720-055-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENG 1) | |||
| 122VU | ANTI ICE/ENG/1 | 1DN1 | X10 |
| FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2) | |||
| 122VU | ANTI ICE/ENG/2 | 1DN2 | W10 |
F. At the First Engine Start
(1) Do the pneumatic leak test (test N°1) (Ref. AMM TASK 71-00-00-790-802).
(1) Do the pneumatic leak test (test N°1) (Ref. AMM TASK 71-00-00-790-802).
Nacelle Anti-Ice (NAI) Duct