Installation of a Bleed-Air Duct
TASK 36-12-41-400-001-A
Installation of a Bleed-Air Duct
Example of the installation of a bleed-air duct section
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 36-12-41-860-050-A ** ON A/C NOT FOR ALL
Subtask 36-12-41-420-052-A ** ON A/C NOT FOR ALL
Subtask 36-12-41-410-051-C ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 04:54:11 UTC
Installation of a Bleed-Air Duct
WARNING:
MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
1. Reason for the JobExample of the installation of a bleed-air duct section
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.03QBB9) | Dry lubricant-General Assembly Molybdenum Disulfide - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.12ACC1) | Corrosion Preventive Compound-Heavy Duty Soft Film - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 147AB, 147EB, 147FB, 151BW, 161AW, 161BW, 161CW, 161DW, 191BB, 191EB, 191JB, 312AR, 314AR, 315AL, 316AR | |
| 151CW, 151DW, 151EW, 151HW, 151JW | |
| 197BB | |
| 151RW, 197KB | |
| 151SW, 151TW, 151UW, 151VW |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 53 | SEAL | AIPC 36-12-04-50-095 |
| 52 | SEALS | AIPC 36-12-04-50-250 |
| 65 | SEAL | AIPC 36-12-04-50-265 |
| 65 | SEAL | AIPC 36-12-84-36-130 |
| 53 | SEAL | AIPC 36-12-84-36-240 |
| 52 | SEALS | AIPC 36-12-84-36-380 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 20-26-00-910-002-A | Installation of Expansion Joints |
| TASK 20-28-00-912-802-A | Electrical Bonding - General Maintenance Procedure |
| TASK 25-55-11-000-001-A | Removal of the Aft Cargo-Compartment Partition at FR47 |
| TASK 25-55-11-400-001-A | Installation of the Aft Cargo-Compartment Partition at FR47 |
| TASK 25-55-12-000-001-A | Removal of the Aft Cargo-Compartment Partition at FR65 |
| TASK 25-55-12-400-001-A | Installation of the Aft Cargo-Compartment Partition at FR65 |
| TASK 36-12-00-790-001-A | Leak Test of the APU Bleed-Air Supply-System |
| TASK 36-22-17-400-001-A | Installation of the APU Overheat Sensing-Elements |
| TASK 52-30-00-860-001-A | Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
| TASK 52-30-00-860-002-A | Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
Subtask 36-12-41-860-050-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Make sure that the WARNING NOTICE(S) are in position:
(a) For the APU bleed-air ducts between FR35 and FR36:
(b) For the APU bleed-air ducts between FR36 and FR42:
(d) For the APU bleed-air ducts between FR46 and FR70:
(3) Make sure that the access platform is in position below the applicable access panel.
Subtask 36-12-41-860-050-B ** ON A/C NOT FOR ALL (1) Make sure that the WARNING NOTICE(S) are in position:
- in the cockpit on the Engine Control Panel 115VU to tell persons not to start the engine(s),
- in the cockpit on the AIR COND Overhead Control Panel 30VU to tell persons not to push in the APU BLEED pushbutton switch,
- on the HP ground connector to tell persons not to pressurize the pneumatic system.
(a) For the APU bleed-air ducts between FR35 and FR36:
(b) For the APU bleed-air ducts between FR36 and FR42:
- Make sure that the access panel 191JB is removed.
(d) For the APU bleed-air ducts between FR46 and FR70:
- Make sure that the AFT cargo compartment door is open (Ref. AMM TASK 52-30-00-860-001).
- Make sure that the partition panel 151BW is removed (Ref. AMM TASK 25-55-11-000-001).
- Make sure that the access panel 151CW is removed.
- Make sure that the access panel 151DW is removed.
- Make sure that the access panel 151EW is removed.
- Make sure that the access panel 151HW is removed.
- Make sure that the access panel 151JW is removed.
- Make sure that the access panel 161AW is removed.
- Make sure that the access panel 161BW is removed.
- Make sure that the access panel 161CW is removed.
- Make sure that the partition panel 161DW is removed (Ref. AMM TASK 25-55-12-000-001).
- Make sure that the access door 312AR is open.
- Make sure that the access door 314AR is open.
(3) Make sure that the access platform is in position below the applicable access panel.
A. Aircraft Maintenance Configuration
(1) Make sure that the WARNING NOTICE(S) are in position:
(a) For the APU bleed-air ducts between FR35 and FR36:
(b) For the APU bleed-air ducts between FR36 and FR42:
(d) For the APU bleed-air ducts between FR46 and FR70:
(3) Make sure that the access platform is in position below the applicable access panel.
Subtask 36-12-41-860-050-C ** ON A/C NOT FOR ALL (1) Make sure that the WARNING NOTICE(S) are in position:
- in the cockpit on the Engine Control Panel 115VU to tell persons not to start the engine(s),
- in the cockpit on the AIR COND Overhead Control Panel 30VU to tell persons not to push in the APU BLEED pushbutton switch,
- on the HP ground connector to tell persons not to pressurize the pneumatic system.
(a) For the APU bleed-air ducts between FR35 and FR36:
(b) For the APU bleed-air ducts between FR36 and FR42:
- Make sure that the access panel 191JB is removed.
(d) For the APU bleed-air ducts between FR46 and FR70:
- Make sure that the AFT cargo compartment door is open (Ref. AMM TASK 52-30-00-860-001).
- Make sure that the partition panel 151BW is removed (Ref. AMM TASK 25-55-11-000-001).
- Make sure that the access panel 151RW is removed.
- Make sure that the access panel 151CW is removed.
- Make sure that the access panel 151DW is removed.
- Make sure that the access panel 151EW is removed.
- Make sure that the access panel 151HW is removed.
- Make sure that the access panel 151JW is removed.
- Make sure that the access panel 161AW is removed.
- Make sure that the access panel 161BW is removed.
- Make sure that the access panel 161CW is removed.
- Make sure that the partition panel 161DW is removed (Ref. AMM TASK 25-55-12-000-001).
- Make sure that the access door 312AR is open.
- Make sure that the access door 314AR is open.
(3) Make sure that the access platform is in position below the applicable access panel.
A. Aircraft Maintenance Configuration
(1) Make sure that the WARNING NOTICE(S) are in position:
(a) For the APU bleed-air ducts between FR35 and FR36:
(b) For the APU bleed-air ducts between FR36 and FR42:
(d) For the APU bleed-air ducts between FR46 and FR70:
(3) Make sure that the access platform is in position below the applicable access panel.
Subtask 36-12-41-865-051-A (1) Make sure that the WARNING NOTICE(S) are in position:
- in the cockpit on the Engine Control Panel 115VU to tell persons not to start the engine(s),
- in the cockpit on the AIR COND Overhead Control Panel 30VU to tell persons not to push in the APU BLEED pushbutton switch,
- on the HP ground connector to tell persons not to pressurize the pneumatic system.
(a) For the APU bleed-air ducts between FR35 and FR36:
(b) For the APU bleed-air ducts between FR36 and FR42:
- Make sure that the access panel 191JB is removed.
(d) For the APU bleed-air ducts between FR46 and FR70:
- Make sure that the AFT cargo compartment door is open (Ref. AMM TASK 52-30-00-860-001).
- Make sure that the partition panel 151BW is removed (Ref. AMM TASK 25-55-11-000-001).
- Make sure that the access panel 151SW is removed.
- Make sure that the access panel 151TW is removed.
- Make sure that the access panel 151UW is removed.
- Make sure that the access panel 151VW is removed.
- Make sure that the access panel 161AW is removed.
- Make sure that the access panel 161BW is removed.
- Make sure that the access panel 161CW is removed.
- Make sure that the partition panel 161DW is removed (Ref. AMM TASK 25-55-12-000-001).
- Make sure that the access door 312AR is open.
- Make sure that the access door 314AR is open.
(3) Make sure that the access platform is in position below the applicable access panel.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR BLEED/ENG 1/CTL | 3HA1 | D12 |
| 49VU | AIR BLEED/ENG 1/MONG | 2HA1 | D11 |
| ** ON A/C ALL | |||
| 49VU | AIR BLEED/X FEED/VALVE/BAT | 2HV | D13 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR BLEED/ENG 2/MONG | 3HA2 | D12 |
| 49VU | AIR BLEED/ENG 1/CTL | 2HA1 | D11 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR BLEED/ENG 2/CTL | 3HA2 | Z23 |
| 122VU | AIR BLEED/ENG 2/MONG | 2HA2 | Z22 |
| ** ON A/C ALL | |||
| 122VU | AIR BLEED/X FEED VALVE/NORM | 1HV | Z20 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR BLEED/ENG 1/MONG | 3HA1 | Z23 |
| 122VU | AIR BLEED/ENG 2/CTL | 2HA2 | Z22 |
Subtask 36-12-41-420-052-A ** ON A/C NOT FOR ALL
A. Installation of the Bleed Air Ducts between FR35 and FR49:
(1) Clean the component interfaces and the adjacent area with Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts kept from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Installation of the bleed air duct between FR47 and FR49:
(a) Remove the CAP - BLANKING from the bleed air duct in the fuselage.
(b) Put the bleed air duct (40) in position.
(c) Install the clamps (11).
(d) Torque the nut of the clamps to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
.
(5) Installation of the bleed air ducts between FR45 and FR47:
(a) Lubricate the seals (27) and (31) with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
1 Before you apply the lubricant, make a paste with pure water or white spirit.
(c) Put the bleed air duct (26) in position.
(d) Install the washers (28) and the bolts (29).
(e) Tighten the bolts (29).
(f) Install the seal (31) in the bleed air duct (30).
(g) Put the bleed air duct (30) in position.
(h) Install the connecting rods (39) with the bolts (34), the washers (33) and the nuts (32).
(i) Tighten the nuts (32).
(j) Install the clamp (11).
(k) Torque the nut of the clamp to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
.
(l) If necessary adjust the bleed air ducts (30) and (40) with the connecting rods (39):
(n) Torque the nut (36) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
.
(o) Do a check of the electrical bonding (Ref. AMM TASK 20-28-00-912-802).
(p) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to:
(a) Lubricate the seal (20) with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
1 Before you apply the lubricant, make a paste with pure water or white spirit.
(c) Put the bleed air ducts (21) and (25) in position.
(d) Install the bleed air duct (21) with the bolts (22), the washers (23) and the nuts (24).
(e) Tighten the nuts (24).
(f) Install the clamps (11).
(g) Torque the nut of the clamps to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
.
(h) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to:
(a) Remove the CAP - BLANKING from the bleed air duct (10).
(b) Install the bleed air duct (8) into the bleed air duct (10).
(c) Install the connecting rods (9) on the bleed air duct (10) with the bolts (3), the washers (2) and the nuts (1).
(d) Tighten the nuts (1).
(e) If necessary adjust the ducts with the connecting rods (9):
(g) Torque the nut (4) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
.
(h) Do a check of the electrical bonding (Ref. AMM TASK 20-28-00-912-802).
(i) Install the bleed air duct (12) on the bleed air duct (8).
(j) Put the spring rods (15) and (16) in position on the bleed air duct (12).
(k) Connect the spring rods (15) and (16) with the bolts (17), the washers (14) and the nuts (13).
(l) Tighten the nuts (13).
(m) Put the bleed air duct (18) in position.
(n) Install the clamps (11).
(o) Torque the nut of the clamps to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
.
(p) Install the insulation muff (19) and safety it with the velcro strips.
(q) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the clamp (11).
Subtask 36-12-41-420-050-C (1) Clean the component interfaces and the adjacent area with Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts kept from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Installation of the bleed air duct between FR47 and FR49:
(a) Remove the CAP - BLANKING from the bleed air duct in the fuselage.
(b) Put the bleed air duct (40) in position.
(c) Install the clamps (11).
(d) Torque the nut of the clamps to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
. (5) Installation of the bleed air ducts between FR45 and FR47:
(a) Lubricate the seals (27) and (31) with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
1 Before you apply the lubricant, make a paste with pure water or white spirit.
NOTE: This material is a molybdenum disulfide powder.
(b) Install the seal (27) on the bleed air duct (26). (c) Put the bleed air duct (26) in position.
(d) Install the washers (28) and the bolts (29).
(e) Tighten the bolts (29).
(f) Install the seal (31) in the bleed air duct (30).
(g) Put the bleed air duct (30) in position.
(h) Install the connecting rods (39) with the bolts (34), the washers (33) and the nuts (32).
(i) Tighten the nuts (32).
(j) Install the clamp (11).
(k) Torque the nut of the clamp to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
. (l) If necessary adjust the bleed air ducts (30) and (40) with the connecting rods (39):
- Make sure that there is no tension on the bleed air ducts (30) and (40).
(n) Torque the nut (36) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
. (o) Do a check of the electrical bonding (Ref. AMM TASK 20-28-00-912-802).
(p) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to:
- Bolts (29) and washers (28)
- Clamp (11).
(a) Lubricate the seal (20) with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
1 Before you apply the lubricant, make a paste with pure water or white spirit.
NOTE: This material is a molybdenum disulfide powder.
(b) Install the seal (20) on the bleed air duct (21). (c) Put the bleed air ducts (21) and (25) in position.
(d) Install the bleed air duct (21) with the bolts (22), the washers (23) and the nuts (24).
(e) Tighten the nuts (24).
(f) Install the clamps (11).
(g) Torque the nut of the clamps to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
. (h) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to:
- Bolts (22), washers (23) and nuts (24)
- Clamp (11).
(a) Remove the CAP - BLANKING from the bleed air duct (10).
(b) Install the bleed air duct (8) into the bleed air duct (10).
(c) Install the connecting rods (9) on the bleed air duct (10) with the bolts (3), the washers (2) and the nuts (1).
(d) Tighten the nuts (1).
(e) If necessary adjust the ducts with the connecting rods (9):
- Make sure that there is no tension on the bleed air duct (8) and (10).
(g) Torque the nut (4) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
. (h) Do a check of the electrical bonding (Ref. AMM TASK 20-28-00-912-802).
(i) Install the bleed air duct (12) on the bleed air duct (8).
(j) Put the spring rods (15) and (16) in position on the bleed air duct (12).
(k) Connect the spring rods (15) and (16) with the bolts (17), the washers (14) and the nuts (13).
(l) Tighten the nuts (13).
(m) Put the bleed air duct (18) in position.
(n) Install the clamps (11).
(o) Torque the nut of the clamps to between 0.50 and 0.40 m.daN (44.25 and 35.40 lbf.in )
. (p) Install the insulation muff (19) and safety it with the velcro strips.
(q) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the clamp (11).
B. Installation of the Bleed Air Duct between FR49 and FR80:
(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Remove the blanking caps from the bleed-air duct flanges (15) and (19).
(4) Check the bleed-air duct flanges (15) and (19) for correct condition.
(5) Lubricate the seal (16) with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
(7) Install the duct (13).
(8) Install the connecting rods (14) with the bolts (5), the washers (7) and the nuts (8).
(9) Install the clamp (20) and torque the nut with the value given on the clamp.
(10) Install the spring rods (11) with the bolts (12), the washers (10) and the nuts (9).
(11) Make sure that the clearance "X" is parallel around the ducts.
(14) Install the APU overheat sensing elements (6) (Ref. AMM TASK 36-22-17-400-001).
Subtask 36-12-41-420-053-B (1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Remove the blanking caps from the bleed-air duct flanges (15) and (19).
(4) Check the bleed-air duct flanges (15) and (19) for correct condition.
(5) Lubricate the seal (16) with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
NOTE: This material is a molybdenum disulfide powder. Before you can apply it, you must make a paste. To do this, mix the powder with pure water or white spirit.
(6) Install the seal (16) in the duct (13) (Ref. AMM TASK 20-26-00-910-002). (7) Install the duct (13).
(8) Install the connecting rods (14) with the bolts (5), the washers (7) and the nuts (8).
(9) Install the clamp (20) and torque the nut with the value given on the clamp.
(10) Install the spring rods (11) with the bolts (12), the washers (10) and the nuts (9).
(11) Make sure that the clearance "X" is parallel around the ducts.
NOTE: A deviation of 1.5 mm (0.0591 in.) for a 3.5 in. (88.8998 mm) and 1.8 mm (0.0709 in.) for a 4.0 in. (101.5998 mm) duct is permitted.
(12) If necessary adjust the ducts with the connecting rods (14). NOTE: Make sure that there is no tension on the ducts.
(13) Install the bonding straps (2) with the bolt (1), the washer (3) and the nut (4) (Ref. AMM TASK 20-28-00-912-802). (14) Install the APU overheat sensing elements (6) (Ref. AMM TASK 36-22-17-400-001).
C. Installation of the Bleed Air Duct between FR80 and FR82
(1) Install the bleed air ducts between FR80 and FR82 as follows:
(a) Clean the component interfaces and the adjacent area.
(b) Do an inspection of the component interfaces and the adjacent area.
(c) Make sure that the parts retained from the removed component are clean and in the correct condition.
(d) Lubricate the new seals that follow with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) :
(e) Remove the CAP - BLANKING from the flanges of the bleed air duct (61) and (67).
(f) Make sure that the flanges of the bleed air duct (61) and (67) in the correct condition.
(g) Align the bleed air duct (42) with the bleed air duct (67).
(h) Install the clamp (66) on the bleed air duct (42) and (67).
(i) TORQUE the screw of the clamp (66) to between 5.35 and 4.85 m.N (47.35 and 42.92 lbf.in )
.
(j) Install the new seal (65) on the bleed air duct (42).
(k) Align the bleed air duct (35) with the bleed air duct (42).
(l) Install the connecting rods (43), bolts (41), washers (44) and nuts (45).
(m) TORQUE the nuts (45) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )
.
(n) Install the bonding strap (49), bolt (48), washer (47) and nut (46).
(o) TORQUE the nut (46) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
.
(p) Install the new seal (53) on the bleed air duct (31).
(q) Align the bleed air duct (31) with the bleed air duct (35).
(r) Install the spring rod (55), bolt (54), washer (56) and nut (57) on the bleed air duct (31).
(s) TORQUE the nut (57) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )
.
(t) Install the connecting rods (34), bolts (36), washers (32) and nuts (33).
(u) TORQUE the nuts (33) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )
.
(v) Install the bonding strap (39), bolt (40), washer (38) and nut (37).
(w) TORQUE the nut (37) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
.
(x) Install the new seals (52) on the bleed air duct (31).
(y) Install the plates (58) and (59) on the flange (60).
(z) Install the flange (60) on the bleed air duct (31) and the aircraft structure.
(aa) Install the washers (50), bolts (51), washers (64), plates (63) and nuts (62).
(ab) TORQUE the nuts (62) to between 0.63 and 0.57 m.N (5.58 and 5.04 lbf.in )
.
(ac) Do the electrical bonding check (Ref. AMM TASK 20-28-00-912-802).
Subtask 36-12-41-865-052-A (1) Install the bleed air ducts between FR80 and FR82 as follows:
(a) Clean the component interfaces and the adjacent area.
(b) Do an inspection of the component interfaces and the adjacent area.
(c) Make sure that the parts retained from the removed component are clean and in the correct condition.
(d) Lubricate the new seals that follow with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) :
- AIPC 36-12-04-50-250 SEALS (52) or AIPC 36-12-84-36-380 SEALS (52)
- AIPC 36-12-04-50-095 SEAL (53) or AIPC 36-12-84-36-240 SEAL (53)
- AIPC 36-12-04-50-265 SEAL (65) or AIPC 36-12-84-36-130 SEAL (65):
(e) Remove the CAP - BLANKING from the flanges of the bleed air duct (61) and (67).
(f) Make sure that the flanges of the bleed air duct (61) and (67) in the correct condition.
(g) Align the bleed air duct (42) with the bleed air duct (67).
(h) Install the clamp (66) on the bleed air duct (42) and (67).
(i) TORQUE the screw of the clamp (66) to between 5.35 and 4.85 m.N (47.35 and 42.92 lbf.in )
.(j) Install the new seal (65) on the bleed air duct (42).
(k) Align the bleed air duct (35) with the bleed air duct (42).
(l) Install the connecting rods (43), bolts (41), washers (44) and nuts (45).
(m) TORQUE the nuts (45) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )
.(n) Install the bonding strap (49), bolt (48), washer (47) and nut (46).
(o) TORQUE the nut (46) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
.(p) Install the new seal (53) on the bleed air duct (31).
(q) Align the bleed air duct (31) with the bleed air duct (35).
(r) Install the spring rod (55), bolt (54), washer (56) and nut (57) on the bleed air duct (31).
(s) TORQUE the nut (57) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )
.(t) Install the connecting rods (34), bolts (36), washers (32) and nuts (33).
(u) TORQUE the nuts (33) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in )
.(v) Install the bonding strap (39), bolt (40), washer (38) and nut (37).
(w) TORQUE the nut (37) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
.(x) Install the new seals (52) on the bleed air duct (31).
(y) Install the plates (58) and (59) on the flange (60).
(z) Install the flange (60) on the bleed air duct (31) and the aircraft structure.
(aa) Install the washers (50), bolts (51), washers (64), plates (63) and nuts (62).
(ab) TORQUE the nuts (62) to between 0.63 and 0.57 m.N (5.58 and 5.04 lbf.in )
.(ac) Do the electrical bonding check (Ref. AMM TASK 20-28-00-912-802).
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 36-12-41-710-050-A 5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR BLEED/ENG 1/CTL | 3HA1 | D12 |
| 49VU | AIR BLEED/ENG 1/MONG | 2HA1 | D11 |
| ** ON A/C ALL | |||
| 49VU | AIR BLEED/X FEED/VALVE/BAT | 2HV | D13 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR BLEED/ENG 2/MONG | 3HA2 | D12 |
| 49VU | AIR BLEED/ENG 1/CTL | 2HA1 | D11 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR BLEED/ENG 2/CTL | 3HA2 | Z23 |
| 122VU | AIR BLEED/ENG 2/MONG | 2HA2 | Z22 |
| ** ON A/C ALL | |||
| 122VU | AIR BLEED/X FEED VALVE/NORM | 1HV | Z20 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR BLEED/ENG 1/MONG | 3HA1 | Z23 |
| 122VU | AIR BLEED/ENG 2/CTL | 2HA2 | Z22 |
Subtask 36-12-41-410-051-C ** 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) For the APU bleed-air ducts between FR35 and FR36:
(a) Install the access panels 191BB and 191EB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 191BB and 191EB.
(3) For the APU bleed-air ducts between FR36 and FR42:
(a) Install the access panel 191JB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panel 191JB.
(4) For the APU bleed-air ducts between FR42 and FR50:
(a) Install the access panels 147AB, 147EB, 147FB and 197BB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 147AB, 147EB, 147FB and 197BB.
(5) For the APU bleed-air ducts between the FR46 and FR47:
(a) Install the partition panel 151BW (Ref. AMM TASK 25-55-11-400-001).
(6) For the APU bleed-air ducts between the FR47 and FR49:
(16) For the APU bleed-air ducts between the FR70 and FR77:
(19) Remove the ACCESS PLATFORM 3M (10 FT) from below the rear fuselage.
(20) Remove the WARNING NOTICE(S).
Subtask 36-12-41-410-051-D ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) For the APU bleed-air ducts between FR35 and FR36:
(a) Install the access panels 191BB and 191EB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 191BB and 191EB.
(3) For the APU bleed-air ducts between FR36 and FR42:
(a) Install the access panel 191JB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panel 191JB.
(4) For the APU bleed-air ducts between FR42 and FR50:
(a) Install the access panels 147AB, 147EB, 147FB and 197BB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 147AB, 147EB, 147FB and 197BB.
(5) For the APU bleed-air ducts between the FR46 and FR47:
(a) Install the partition panel 151BW (Ref. AMM TASK 25-55-11-400-001).
(6) For the APU bleed-air ducts between the FR47 and FR49:
- Install the access panel 151CW.
- Install the access panel 151DW.
- Install the access panel 151EW.
- Install the access panel 151HW.
- Install the access panel 151JW.
- Install the access panel 161AW.
- Install the access panel 161BW.
- Install the access panel 161CW.
- Install the partition panel 161DW (Ref. AMM TASK 25-55-12-400-001).
(16) For the APU bleed-air ducts between the FR70 and FR77:
- Close the access door 312AR.
- Close the access door 314AR.
(19) Remove the ACCESS PLATFORM 3M (10 FT) from below the rear fuselage.
(20) Remove the WARNING NOTICE(S).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) For the APU bleed-air ducts between FR35 and FR36:
(a) Install the access panels 191BB and 191EB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 191BB and 191EB.
(3) For the APU bleed-air ducts between FR36 and FR42:
(a) Install the access panel 191JB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panel 191JB.
(4) For the APU bleed-air ducts between FR42 and FR50:
(a) Install the access panels 147AB, 147EB, 147FB and 197KB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 147AB, 147EB, 147FB and 197KB.
(5) For the APU bleed-air ducts between the FR46 and FR47:
(17) For the APU bleed-air ducts between the FR70 and FR77:
(20) Remove the ACCESS PLATFORM 3M (10 FT) from below the rear fuselage.
(21) Remove the WARNING NOTICE(S).
Subtask 36-12-41-410-051-E ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) For the APU bleed-air ducts between FR35 and FR36:
(a) Install the access panels 191BB and 191EB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 191BB and 191EB.
(3) For the APU bleed-air ducts between FR36 and FR42:
(a) Install the access panel 191JB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panel 191JB.
(4) For the APU bleed-air ducts between FR42 and FR50:
(a) Install the access panels 147AB, 147EB, 147FB and 197KB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 147AB, 147EB, 147FB and 197KB.
(5) For the APU bleed-air ducts between the FR46 and FR47:
- Install the partition panel 151BW (Ref. AMM TASK 25-55-11-400-001).
- Install the access panel 151RW.
- Install the access panel 151CW.
- Install the access panel 151DW.
- Install the access panel 151EW.
- Install the access panel 151HW.
- Install the access panel 151JW.
- Install the access panel 161AW.
- Install the access panel 161BW.
- Install the access panel 161CW.
- Install the partition panel 161DW (Ref. AMM TASK 25-55-12-400-001).
(17) For the APU bleed-air ducts between the FR70 and FR77:
- Close the access door 312AR.
- Close the access door 314AR.
(20) Remove the ACCESS PLATFORM 3M (10 FT) from below the rear fuselage.
(21) Remove the WARNING NOTICE(S).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) For the APU bleed-air ducts between FR35 and FR36:
(a) Install the access panels 191BB and 191EB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 191BB and 191EB.
(3) For the APU bleed-air ducts between FR36 and FR42:
(a) Install the access panel 191JB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panel 191JB.
(4) For the APU bleed-air ducts between FR42 and FR50:
(a) Install the access panels 147AB, 147EB, 147FB and 197BB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 147AB, 147EB, 147FB and 197BB.
(5) For the APU bleed-air ducts between the FR46 and FR53:
(14) For the APU bleed-air ducts between the FR70 and FR77:
(17) Remove the ACCESS PLATFORM 3M (10 FT) from below the rear fuselage.
(18) If Additional Center Tanks (ACT) were removed, do the steps that follow:
(a) If the Additional Center Tank No1 (ACT1) was removed, install the ACT1 (Ref. AMM D/O 28-11-27-40).
(b) If the Additional Center Tank No2 (ACT2) was removed, install the ACT2 (Ref. AMM D/O 28-11-27-40).
(c) If the Additional Center Tank No3 (ACT3) was removed, install the ACT3 (Ref. AMM D/O 28-11-27-40).
(d) If the Additional Center Tank No4 (ACT4) was removed, install the ACT4 (Ref. AMM D/O 28-11-27-40).
(e) If the Additional Center Tank No5 (ACT5) was removed, install the ACT5 (Ref. AMM D/O 28-11-27-40).
(f) If the Additional Center Tank No6 (ACT6) was removed, install the ACT6 (Ref. AMM D/O 28-11-27-40).
(19) Remove the WARNING NOTICE(S).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) For the APU bleed-air ducts between FR35 and FR36:
(a) Install the access panels 191BB and 191EB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 191BB and 191EB.
(3) For the APU bleed-air ducts between FR36 and FR42:
(a) Install the access panel 191JB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panel 191JB.
(4) For the APU bleed-air ducts between FR42 and FR50:
(a) Install the access panels 147AB, 147EB, 147FB and 197BB.
(b) Remove the ACCESS PLATFORM 2M (6 FT) from below the access panels 147AB, 147EB, 147FB and 197BB.
(5) For the APU bleed-air ducts between the FR46 and FR53:
- Install the partition panel 151BW (Ref. AMM TASK 25-55-11-400-001).
- Install the access panel 151SW.
- Install the access panel 151TW.
- Install the access panel 151UW.
- Install the access panel 151VW.
- Install the access panel 161AW.
- Install the access panel 161BW.
- Install the access panel 161CW.
- Install the partition panel 161DW (Ref. AMM TASK 25-55-12-400-001).
(14) For the APU bleed-air ducts between the FR70 and FR77:
- Close the access door 312AR.
- Close the access door 314AR.
(17) Remove the ACCESS PLATFORM 3M (10 FT) from below the rear fuselage.
(18) If Additional Center Tanks (ACT) were removed, do the steps that follow:
(a) If the Additional Center Tank No1 (ACT1) was removed, install the ACT1 (Ref. AMM D/O 28-11-27-40).
(b) If the Additional Center Tank No2 (ACT2) was removed, install the ACT2 (Ref. AMM D/O 28-11-27-40).
(c) If the Additional Center Tank No3 (ACT3) was removed, install the ACT3 (Ref. AMM D/O 28-11-27-40).
(d) If the Additional Center Tank No4 (ACT4) was removed, install the ACT4 (Ref. AMM D/O 28-11-27-40).
(e) If the Additional Center Tank No5 (ACT5) was removed, install the ACT5 (Ref. AMM D/O 28-11-27-40).
(f) If the Additional Center Tank No6 (ACT6) was removed, install the ACT6 (Ref. AMM D/O 28-11-27-40).
(19) Remove the WARNING NOTICE(S).
APU Bleed-Air Ducts