DMC:V2500-A5-72-00-4000-05C-720A-B|Issue No:001|Issue Date:2013-11-01

Export Control

EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.

Copyright

© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).

Applicability

V2500-A5

Common Information

TASK 72-00-40-420-005-B00 HP System Module - Install The Components, Ducts, Electrical Harnesses, And Tubes To The HPC Case Vertical Splitline, Installation-008

General

This TASK gives the procedure to install the electrical harnesses, the tubes and the brackets on to the HP compressor/diffuser case assembly. Refer to the TASKs which follow for other related procedures.

TASK 72-00-40-420-004-B00 - Install the initial HP system module components and air off-take ducts.

TASK 72-00-40-420-006-B00 - Install and connect the components, the electrical harnesses and the tubes on the front of the HP compressor case.

TASK 72-00-40-420-007-B00 - Install the components, the electrical harnesses, tubes and brackets to the HP turbine.

For lockwire data and procedures refer to the SPM TASK 70-42-05-400-501.

SBE 70-0813

For safety cable data and procedures refer to the SPM TASK 70-42-08-400-501.

Safety the threaded fasteners in this TASK with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT for the ATA Chapter/Section/Subjects which follow:

A5 series engines:
71-51-41	71-52-43	72-41-34
73-22-49	75-23-49	75-31-42
75-31-43	75-32-42

Transportation covers/blanks must be removed immediately before the installation of components and tubes.

Fig./item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the Service Bulletin alpha variants refer to the IPC.

For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig./item number.

For standard torque data and procedures refer to the SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-400-501.

Special torque data is identified with the symbol * after the torque value.

Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS approved engine oil unless other lubricants are referred to in the procedure.

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flanges and attach parts. Use the correct color of air drying enamel. Refer to the SPM TASK 70-38-21-380-501.

The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.

Refer to the V2500 Illustrated Tool and Equipment Manual (ITE-V2500-1IA) for the illustrations of the special tools given in this procedure.

Do not remove the special plastic caps from the electrical connectors until immediately before they are installed. This will give protection from unwanted fluids and materials.

NOTE

To identify the consumable materials refer to the PCI.

NOTE

SBE 70-0813: Announcement of introduction of safety cable as a preferred method to lockwire.

NOTE

Safety the threaded fasteners in this TASK with safety cable for the ATA Chapter/Section/Subjects detailed in 2. General.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

Name	Manufacturer	Part Number / Identification	Quantity	Remark
ACR Torq-Set bit 212-1/4-ACR	LOCAL	Torq-Set

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 02-126 LOCKWIRE	LOCAL	CoMat 02-126
CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)	LOCAL	CoMat 02-148
CoMat 02-274 SAFETY CABLE KIT	LOCAL	CoMat 02-274
CoMat 02-275 SAFETY CABLE KIT	LOCAL	CoMat 02-275
CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE	LOCAL	CoMat 04-005
CoMat 07-038 AIR DRYING ENAMEL	K3504	CoMat 07-038
CoMat 10-031 ANTI-GALLING COMPOUND	0AM53	CoMat 10-031
CoMat 10-077 APPROVED ENGINE OILS	LOCAL	CoMat 10-077
CoMat 10-129 ANTI-SEIZE PASTE	34568	CoMat 10-129

Spares

NONE

Safety Requirements

NONE

Procedure

1. Refer to Figure, Figure and Figure.
2. 1. Attach the tube 21 to the diffuser case adapter.
  2. Install the clip, the bolt, the washer and the clipnut to attach tube 21 to the bracket at clip position 5569.
  3. Torque the diffuser case adapter nut to 257 to 283 lbf.in (29 to 32 Nm). Safety with CoMat 02-126 LOCKWIRE.
3. 1. Attach the bracket OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-090) to the bracket HPC Assembly (72-41-00, 03-510) with the two bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-094) and the two nuts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-092) at clip position 5664. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  2. Lightly lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-116) seal ring with CoMat 10-077 APPROVED ENGINE OILS and install it on the tube 21.
  3. Install the filter OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-080) in to the tube 21.
  4. Put a thin layer of CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE on to the bracket OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-070) where it touches tube 24.
  5. Attach the tube 24 to the tube 21 with the bracket, the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-114) and the three nuts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-110). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
  6. Install the clip, the clipnut, the spacer, the washer and the bolt at the clip position 5591. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  7. Install the clip, the clipnut, the washer and the bolt at the clip position 5664. Torque the bolt to, 36 to 45 lbf.in (4 to 5 Nm).
  8. Install the clips, the bolt, the washer and the clipnut at the clip position 5768. Torque the nut to, 36 to 45 lbf.in (4 to 5 Nm).
4. 1. Put the tube 23 in position.
  2. Install the clips, the clipnuts, the washers and the bolts at the clip positions 5665 and 5659.
1. Refer to Figure, Figure and Figure.
2. 1. Attach the tube 21 to the diffuser case adapter.
  2. Install the clip, the bolt, the washer and the clipnut to attach tube 21 to the bracket at clip position 5569.
  3. Torque the diffuser case adapter nut to 257 to 283 lbf.in (29 to 32 Nm). Safety with CoMat 02-126 LOCKWIRE.
3. 1. Attach the bracket OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-090) to the bracket HPC Assembly (72-41-00, 03-510) with the two bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-094) and the two nuts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-092) at clip position 5664. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  2. Lightly lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-116) seal ring with CoMat 10-077 APPROVED ENGINE OILS and install it on the tube 21.
  3. Install the filter OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-080) in to the tube 21.
  4. Put a thin layer of CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE on to the bracket OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-070) where it touches tube 24.
  5. Attach the tube 24 to the tube 21 with the bracket, the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-114) and the three nuts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-110). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
  6. Install the clip, the clipnut, the spacer, the washer and the bolt at the clip position 5591. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  7. Install the clip, the clipnut and the bolt at the clip position 5664. Torque the bolt to, 36 to 45 lbf.in (4 to 5 Nm).
  8. Install the clips, the bolt, the washer and the clipnut at the clip position 5768. Torque the nut to, 36 to 45 lbf.in (4 to 5 Nm).
4. 1. Put the tube 23 in position.
  2. Install the clip, the clipnut and the bolt to the bracket Engine Air Off-Take Air Ducts (75-00-49, 01-680) at the clip position 6087.
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. 1. Put the duct in position on the HP compressor case (with the angle duct to the top) at the 8 o'clock position and align the bolt holes.
  2. Install the 12 bolts Engine Air Off-Take Air Ducts (75-00-49, 01-252) together with the three brackets Engine Air Off-Take Air Ducts (75-00-49, 01-235), Engine Air Off-Take Air Ducts (75-00-49, 01-240) and Engine Air Off-Take Air Ducts (75-00-49, 01-242). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
  3. Install the clipnut, the clip, the washer and the bolt at the clip position 5569. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
3. 1. Put one of the ducts in position on the compressor case at the 2 o'clock position and align the bolts holes.
  2. Install 12 of the bolts Engine Air Off-Take Air Ducts (75-00-49, 01-102) together with the brackets Engine Air Off-Take Air Ducts (75-00-49, 01-090). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
  3. Put the remaining duct in position on the compressor case at the 4 o'clock position and align the bolt holes.
  4. Install the bracket ENGINE FUEL AND CONTROL-FUEL DISTRIBUTION VALVE (73-13-43, 01-042) on the flange of the air offtake duct with the four bolts Engine Air Off-Take Air Ducts (75-00-49, 01-106) at the 5, 6, 7 and 8 o'clock locations. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
  5. Install the 8 bolts Engine Air Off-Take Air Ducts (75-00-49, 01-104) together with the bracket Engine Air Off-Take Air Ducts (75-00-49, 01-090) on the flange of the air offtake duct. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. Put a bleed valve HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) in position on the air off-take duct Engine Air Off-Take Air Ducts (75-00-49, 01-100) at the 2 o'clock position. Make sure that bleed valve actuation connection is at the 4 o'clock position and align the bolt holes.
3. Install the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-104) and the nuts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-102) and torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
4. Pre SBE 75-0071: Attach the silencer HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-250) and the seal assembly HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-265) to the bleed valve with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-268) and the 12 nuts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-266). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
5. SBE 75-0071, Pre SBE 75-0092: Attach the silencer assembly HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-250) to the bleed valve with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-268) and the 12 nuts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-266). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
6. SBE 75-0092, Pre SBE 75-0093: Attach the silencer assembly HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-250) and the spacer HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-230) to the bleed valve with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-268) and the 12 nuts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-266). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
7. SBE 75-0093: Attach the silencer assembly HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-250) to the bleed valve with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-268) and the 12 nuts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-266). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
8. Put a bleed valve HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) in position on the air off-take duct Engine Air Off-Take Air Ducts (75-00-49, 01-100) at the 4 o'clock position. Make sure the bleed valve actuation connection is at the 10 o'clock position and align the bolt holes.
9. Install 12 of the bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-104) and the nuts No. 2 Bearing (72-32-52, 01-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
10. Attach the seal assembly HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-465) to the bleed valve with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-468) and the 12 nuts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-466). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
11. Put the remaining bleed valve No. 2 Bearing (72-32-52, 01-100) through the seal assembly HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-070) on to the air off-take duct Engine Air Off-Take Air Ducts (75-00-49, 01-250). Make sure the bleed valve actuation connection is at the 6 o'clock position and align the bolt holes.
12. Install the other 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-104) and torque them to 85 to 105 lbf.in (10 to 12 Nm).
13. Pre SBE 75-0071: Attach the silencer HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-060) and the seal assembly to the bleed valve with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-062). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
14. SBE 75-0071: Attach the silencer assembly HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-060) to the bleed valve with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-062). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
  .
1. Refer to Figure, Figure and Figure.
2. 1. Attach the tube 49 to the stage 10 bleed valve at the 3 o'clock position.
  2. Attach the tube 50 to the stage 7 bleed valve at the 2 o'clock position.
  3. Attach the tube 51 to the stage 7 bleed valve at the 4 o'clock position.
  4. Install the clip, the clipnut, the washer and the bolt at the clip position 5397. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the washer, the bolt and the nut at the clip position 5643. Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).
  6. Install the clip, the washer and the bolt at the clip position 5642. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  7. Torque the tube nuts in Step, Step and Step to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.
3. 1. Attach the tube 63 to the tube 50.
  2. Attach the tube 64 to the tube 49.
  3. Attach the tube 65 to the tube 51.
  4. Install the clip, the clipnut, the spacer, the washer and the bolt at the clip position 5641. Torque the bolt to 36 to 45 lbfin (4 to 5 Nm).
  5. Torque the tube nuts in Step, Step and Step to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.
4. Attach the tube 32 to the stage 7 bleed valve at the 8 o'clock position. Torque the tube nut to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure and Figure.
2. 1. Attach the tube 49 to the stage 10 bleed valve at the 3 o'clock position.
  2. Attach the tube 50 to the stage 7 bleed valve at the 2 o'clock position.
  3. Attach the tube 51 to the stage 7 bleed valve at the 4 o'clock position.
  4. Install the clip, the clipnut, the washer and the bolt at the clip position 5397. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the bolt and the nut at the clip position 5643. Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).
  6. NOTE
    The SBE 71-0199 clip position 6073 is assembled in TASK 72-00-40-420-006-C00.
    Pre SBE 71-0199: Install the clip, the clipnut and the bolt to the bracket HPC Assembly (72-41-00, 03-575) at the clip position 6073. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  7. Torque the tube nuts in Step, Step and Step to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.
3. 1. Attach the tube 63 to the tube 50.
  2. Attach the tube 64 to the tube 49.
  3. Attach the tube 65 to the tube 51.
  4. Install the clips, the clipnuts, the spacer and the bolts at the clip position 6089 and 6093. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm).
  5. Torque the tube nuts in Step, Step and Step to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.
4. Attach the tube 32 to the stage 7 bleed valve at the 8 o'clock position. Torque the tube nut to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.
1. Refer to Figure.
2. During the installation procedure make sure the harnesses are held temporarily along their different lengths. Always install the datum clip positions when you install each electrical connector. This will give correct installation of the different harnesses, prevent too much strain on the electrical connectors and give the necessary drip loops (the drip loop makes sure moisture or fluids do not go in to the electrical connector).
3. Because of the differences between the harness diameters, the specified clip could be too large or too small. You can use a clip from a range of six clips that have the same part numbers. If the harness diameter is between two of the clips in the range, use the larger clip. When you do this use CoMat 02-148 ADHESIVE TAPE (ELECTRICAL) to increase the harness diameter.
4. For the data on the electrical connectors refer to the SPM TASK 70-43-00-400-501 and the SPM TASK 70-43-01-400-501.
1. Refer to Figure, Figure, Figure and Figure.
2. 1. Connect the No. 2 high energy ignition harness to the No. 2 igniter plug.
  2. Install the clips, the clipnut, the washer and the bolt at the clip positions 5450. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  3. Install the clip, the clipnut, the washer and the bolt at the clip position 5759. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  4. Install the clips, the washer, the bolt and the nut at the clip position 5758. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).
  5. Torque the high energy ignition harness to between 140 and 160 lbf.in (15.82 and 18.08 Nm).
  6. Install the two shrouds (Ignition Leads (74-21-43, 02-070) and Ignition Leads (74-21-43, 02-075)) and the two clamps (Ignition Leads (74-21-43, 02-055) and Ignition Leads (74-21-43, 02-060)) on to the igniter plug end of the harness. Torque the clamp screws to 40 to 50 * lbf.in (4.52 to 5.65 Nm).
3. 1. Connect the No. 1 high energy ignition harness to the No. 1 igniter plug.
  2. Install the clips, the clipnuts, the spacers, the washers and the bolts at the clip positions 5757 and 5760. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm).
  3. Install the clips, the clipnuts, the washers and the bolts at the clip positions 5564, 5566 and 5756. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm).
  4. Torque the high energy ignition harness to between 140 and 160 lbf.in (15.82 and 18.08 Nm).
  5. Install the two shrouds (IGNITION-IGNITION LEADS (74-21-43, 01-070) and IGNITION-IGNITION LEADS (74-21-43, 01-075)) and the two clamps (IGNITION-IGNITION LEADS (74-21-43, 01-055) and IGNITION-IGNITION LEADS (74-21-43, 01-060)) on to the igniter plug end of the harness. Torque the clamp screws to 40 to 50 * lbf.in (4.52 to 5.65 Nm).
1. 1. Put the harness in the correct position for installation.
  2. Connect the electrical connector 4001HA-A to the pressure regulator valve. Tighten the connector with your fingers plus a one-eighth turn.
  3. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5913, 5925 and 5924. Torque the nuts to 36 to 45 lbf.in. (4 to 5 Nm).
  4. Attach the four earth leads to the bracket HPC Assembly (72-41-00, 03-760) with the four bolts and the four nuts. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5922, 6066, 5923, 6064, 5921, 5652, 5763, 5764, 5905 and 5904. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  6. Connect the electrical connector 4000HA-A to the high pressure bleed valve. Tighten the connector with your fingers plus a one-eighth turn.
  7. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5919, 5920, 5766, 5918, 5901 and 5804. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.
2. 1. Put the harness in the correct position for installation.
  2. Connect the electrical connector 4001HA-A to the pressure regulator valve. Tighten the connector with your fingers plus a one-eighth turn.
  3. Install the clips, the washers, the spacers, the bolts and the nuts at the clip positions 5913, 5925 and 5924.
  4. Attach the four earth leads to the bracket HPC Assembly (72-41-00, 03-760) with the four bolts and the four nuts. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5922, 6066, 5923, 6064, 5921, 5652, 5763, 5764, 5905 and 5648. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  6. Connect the electrical connector 4000HA-A to the high pressure bleed valve. Tighten the connector with your fingers plus a one-eighth turn.
  7. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 6098, 5940, 5766, 6112, 6088, 6084, 6079 and 6075.
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.
2. 1. Put the harness in the correct position for installation.
  2. Connect the electrical connector 4001HA-A to the pressure regulator valve. Tighten the connector with your fingers plus a one-eighth turn.
  3. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5913, 5925 and 5924. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  4. Attach the four earth leads to the bracket HPC Assembly (72-41-00, 03-760) with the four bolts and the four nuts. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5922, 6066, 5923, 6064, 5921, 5652, 5763, 5764, 5765 and 5648. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  6. Connect the electrical connector 4000HA-A to the high pressure bleed valve. Tighten the connector with your fingers plus a one-eighth turn.
  7. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5941, 6098, 5940, 5766, 5939 and 5938. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.
2. 1. Put the harness in the correct position for installation.
  2. Connect the electrical connector 4001HA-A to the pressure regulator valve. Tighten the connector with your fingers plus a one-eighth turn.
  3. Install the clips, the washers, the spacers, the bolts and the nuts at the clip positions 5913, 5925 and 5924. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  4. Attach the four earth leads to the bracket HPC Assembly (72-41-00, 03-760) with the four bolts and the four nuts. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the washers, the spacers, the bolts and the nuts at the clip positions 5922, 6066, 5923, 6064, 5921, 5652, 5763, 5764, 5765 and 5648. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  6. Connect the electrical connector 4000HA-A to the high pressure bleed valve. Tighten the connector with your fingers plus a one eighth turn.
  7. Install the clips, the washers, the spacers, the bolts and the nuts at the clip positions 6098, 5940, 5766, 6112, 6088, 6084, 6079 and 6075. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.
2. 1. Put the harness in the correct position for installation.
  2. Connect the electrical connector 4001HA-A to the pressure regulator valve. Tighten the connector with your fingers plus a one-eighth turn.
  3. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5990, 5925 and 5924. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  4. Attach the four earth leads to the bracket HPC Assembly (72-41-00, 03-760) with the four bolts and the four nuts. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5922, 6066, 5923, 6064, 5921, 5652, 6107, 6058, 5747 and 5904. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  6. Connect the electrical connector 4000HA-A to the high pressure bleed valve. Tighten the connector with your fingers plus a one-eighth turn.
  7. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5919, 5920, 5766, 5918, 5901 and 5804. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure .
2. 1. Put the harness in the correct position for installation.
  2. Connect the electrical connector 4001HA-A to the pressure regulator valve. Tighten the connector with your fingers plus a one-eighth turn.
  3. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5990, 5925 and 5924. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  4. Attach the four earth leads to the bracket HPC Assembly(72-41-00,03-760) with the four bolts and the four nuts. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  5. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5922, 6066, 5923, 6064, 5921, 5652, 6107, 6058, 5747 and 5948. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
  6. Connect the electrical connector 4000HA-A to the high pressure bleed valve. Tighten the connector with your fingers plus a one-eighth turn.
  7. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 6098, 5940, 5766, 6112, 6088, 6084, 6079 and 6075. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure.
2. 1. Attach the support tube to the bracket HP SYSTEM MODULE (72-00-40, 01-280) with the bolt Ignition Exciters (74-11-38, 01-765) and the clipnut Ignition Exciters (74-11-38, 01-770).
  2. Attach the support tube to the bracket HPC Assembly (72-41-00, 03-310) with the bolt Ignition Exciters (74-11-38, 01-765) and the clipnut Ignition Exciters (74-11-38, 01-770).
  3. Torque the bolts to 85 to 105 lbfin (10 to 12 Nm).
3. 1. Attach the support tube to the bracket HP SYSTEM MODULE (72-00-40, 01-310) with the bolt Ignition Exciters (74-11-38, 01-365) and the clipnut Ignition Exciters (74-11-38, 01-370).
  2. Attach the support tube to the bracket HPC Assembly (72-41-00, 03-280) with the bolt Ignition Exciters (74-11-38, 01-365) and the clipnut Ignition Exciters (74-11-38, 01-370).
  3. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
4. 1. Attach the cross bracket to the lower support bracket HPC Assembly (72-41-00, 04-650) with the two screws Ignition Exciters (74-11-38, 01-690) and the two clipnuts Ignition Exciters (74-11-38, 01-695). Use the ACR Torq-Set bit 212-1/4-ACR 1 off to install the two screws.
  2. Attach the cross bracket to the support tube, together with the bracket Ignition Exciters (74-11-38, 01-595) with the bolt Ignition Exciters (74-11-38, 01-680).
  3. Torque the bolt to 85 to 105 lbf.in (10 to 12 Nm).
  4. Use the ACR Torq-Set bit 212-1/4-ACR 1 off to torque the screws to 85 to 105 lbf.in (10 to 12 Nm).
5. 1. Attach the cross bracket to the lower support bracket HPC Assembly (72-41-00, 04-650) with the bolt Ignition Exciters (74-11-38, 01-610) and the clipnut Ignition Exciters (74-11-38, 01-625).
  2. Attach the cross bracket to the support tube, together with the bracket Ignition Exciters (74-11-38, 01-590), with the bolt Ignition Exciters (74-11-38, 01-620).
  3. Torque the two bolts to 85 to 105 lbf.in (10 to 12 Nm).
6. 1. Attach the cross bracket to the upper support bracket HPC Assembly (72-41-00, 04-600) with the two screws Ignition Exciters (74-11-38, 01-290) and the two clipnuts Ignition Exciters (74-11-38, 01-295). Use the ACR Torq-Set bit 212-1/4-ACR 1 off to install the two screws.
  2. Attach the cross bracket to the support tube with the bolt Ignition Exciters (74-11-38, 01-280).
  3. Torque the bolt to 85 to 105 lbf.in (10 to 12 Nm).
  4. Use the ACR Torq-Set bit 212-1/4-ACR 1 off to torque the screws to 85 to 105 lbf.in (10 to 12 Nm).
7. 1. Attach the cross bracket to the upper support bracket HPC Assembly (72-41-00, 04-600) with the bolt Ignition Exciters (74-11-38, 01-220) and the clipnut Ignition Exciters (74-11-38, 01-225).
  2. Attach the cross bracket to the support tube with the bolt Ignition Exciters (74-11-38, 01-210).
  3. Torque the two bolts to 85 to 105 lbf.in (10 to 12 Nm).
1. Refer to Figure.
2. 1. Attach the bracket Ignition Exciters (74-11-38, 01-470) to the brackets HPC Assembly (72-41-00, 04-620) and HPC Assembly (72-41-00, 04-670) installed in TASK 72-41-00-440-002-B00 with two bolts Ignition Exciters (74-11-38, 01-472) and two clipnuts Ignition Exciters (74-11-38, 01-473).
  2. Attach the bracket Ignition Exciters (74-11-38, 01-470) to the brackets HPC Assembly (72-41-00, 04-600) and HPC Assembly(72-41-00,04-650) installed in TASK 72-41-00-440-002-B00 with two bolts Ignition Exciters (74-11-38, 01-472) and two clipnuts Ignition Exciters (74-11-38, 01-473).
  3. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm.).
3. 1. Attach the brackets Ignition Exciters (74-11-38, 01-170) and Ignition Exciters (74-11-38, 01-570) to the flange face using existing nuts, bolts and washers.
  2. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm.).
4. 1. Attach the brackets Ignition Exciters (74-11-38, 01-180 and (74-11-38, 01-580) to the flange face using existing nuts and bolts.
  2. Torque the bolts to 180 to 220 lbf.in (20 to 25 Nm.).
5. 1. Attach the bracket Ignition Exciters (74-11-38, 01-170) to the bracket Ignition Exciters (74-11-38, 01-180) with the bolts Ignition Exciters (74-11-38, 01-172) and the clipnuts Ignition Exciters (74-11-38, 01-174).
  2. Attach the bracket Ignition Exciters (74-11-38, 01-570) to the bracket Ignition Exciters (74-11-38, 01-580) with the bolts Ignition Exciters (74-11-38, 01-572) and the clipnuts Ignition Exciters (74-11-38, 01-574).
  3. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm.).
6. 1. Attach the bracket Ignition Exciters (74-11-38, 01-200) to the bracket Ignition Exciters (74-11-38, 01-470) with the two bolts Ignition Exciters (74-11-38, 01-214) and Ignition Exciters (74-11-38, 01-216) and the two clipnuts Ignition Exciters (74-11-38, 01-215 and (74-11-38, 01-474).
  2. Attach the bracket Ignition Exciters (74-11-38, 01-600) to the bracket Ignition Exciters (74-11-38, 01-470) with the two bolts Ignition Exciters (74-11-38, 01-612) and Ignition Exciters (74-11-38, 01-614) and the two clipnuts Ignition Exciters (74-11-38, 01-613) and Ignition Exciters (74-11-38, 01-474).
  3. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm.).
  4. Attach the bracket Ignition Exciters (74-11-38, 01-200) to the bracket Ignition Exciters (74-11-38, 01-180) with the two bolts Ignition Exciters (74-11-38, 01-210) and Ignition Exciters (74-11-38, 01-212).
  5. Attach the bracket Ignition Exciters (74-11-38, 01-600) to the bracket Ignition Exciters (74-11-38, 01-580) with the two bolts Ignition Exciters (74-11-38, 01-610).
  6. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm.).
1. Refer to Figure and Figure.
2. NOTE
  Refer to SPM TASK 70-47-01-470-501 for the procedure to install v-band couplings.
  Do not tighten or torque the duct v-band couplings until all the ducts, valves, couplings and tubes are installed in the correct position, refer to SUBTASK 72-00-40-420-228.
3. 1. Install the seal PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-110) onto the HP7 bleed valve/cabin air duct.
  2. Attach the IP bleed check valve to the HP7 bleed valve/cabin air duct with the coupling PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-100). Tighten the v-band coupling nut.
4. 1. Install the seal PNEUMATIC-HP BLEED VALVE (36-11-51, 01-110) on to the HP10 cabin air duct.
  2. Attach the HP bleed valve to the HP10 cabin air duct with the coupling PNEUMATIC-HP BLEED VALVE (36-11-51, 01-100). Tighten the v-band coupling nut.
  3. Connect the electrical connector 4000HA-A to the HP bleed valve and torque to 13 * lbf.in (1.5 Nm).
5. 1. Install the seal PNEUMATIC-HP BLEED VALVE (36-11-51, 01-110) on to the HP bleed valve.
  2. Attach the lower duct assembly to the HP bleed valve with the coupling PNEUMATIC-HP BLEED VALVE (36-11-51, 01-100). Tighten the v-band coupling nut.
6. 1. Install the seal PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-320) on to the lower duct assembly.
  2. Install the seal PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-110) on to the IP bleed check valve.
  3. Attach the Y-duct to the IP bleed check valve with the coupling PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-100) and the lower duct assembly with the coupling PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-310). Tighten the v-band coupling nut.
7. 1. Install the seal Bleed Pressure Regulator Valve (36-11-52, 01-110) PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-340 on to the Y-duct.
  2. Attach the pressure bleed valve to the Y-duct with the coupling Bleed Pressure Regulator Valve (36-11-52, 01-100), PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-330). Tighten the v-band coupling nut.
  3. Connect the electrical connector 4001HA-A to the pressure bleed valve and torque to 13 * lbf.in (1.5 Nm).
8. 1. Install the seal Bleed Pressure Regulator Valve (36-11-52, 01-110) on to the pressure bleed valve.
  2. Attach the upper duct assembly to the pressure bleed valve with the coupling Bleed Pressure Regulator Valve (36-11-52, 01-100). Tighten the v-band coupling nut.
  3. Attach the link bearing PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-230), nut PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-232) and keywasher PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-233) to the link bearing PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-220). Adjust the length of the link bearing to align its holes with the holes in the upper duct assembly lugs and the brackets HPC Module - Attaching Parts (72-40-00, 01-760) and HPC Module - Attaching Parts (72-40-00, 01-770).
  4. Attach the link bearings to the upper duct assembly lugs and the brackets with the two flanged bushes PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-210), the two bolts PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-180), the two washers PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-200) and the two nuts PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-190).
  5. Attach the two link bearings PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-160), nut PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-172) and keywasher PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-173) to the connecting rod PNEUMATIC-BLEED AIR DUCTS (36-11-49 ,01-170). Adjust the length of the connecting rod assembly to align its holes with the holes in the upper duct assembly lugs and the bracket HPC Assembly (72-41-00, 03-770).
  6. Attach the connecting rod assembly to the upper duct assembly lugs and the bracket with the two flanged bushings PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-150), the two bolts PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-120), the two washers PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-140) and the two nuts PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-130).
  7. NOTE
    Final adjust and secure the link assemblies when the engine is installed on the pylon.
    Lock the link bearing and the connecting rod assembly in position.
  8. Torque the nuts in steps (4) and (6) to 85 to 105 lbf.in (10 to 12 Nm).
1. Refer to Figure, Figure, Figure, Figure, Figure and Figure.
2. 1. NOTE
    Refer to the SPM TASK 70-41-02-400-501 for the torque loading procedures.
    Apply CoMat 10-129 ANTI-SEIZE PASTE to one of the mating thread surfaces of the pressure sense tubes, hoses and union before you connect the components, as follows:
    Cabin Bleed Air System Sense Tubes (36-21-49)
    IPC Fig./item
    01-100
    01-500
    01-510
    02-200
    02-500
    02-650
    02-700
    02-725
  2. Do not tighten or torque the tube nuts or attaching parts until all the tubes are installed in their correct position.
  3. Install the K seal PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-655) and the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650) in the duct PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-300). Torque the union to 168-181 lbf.in (19-20.50 Nm).
  4. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) to the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650).
  5. Connect the hose PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-700) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) and the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-725).
  6. Attach the hose PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-200) to the tube connected to the pressure regulator bleed valve Bleed Pressure Regulator Valve (36-11-52, 01-050).
  7. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) and the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005) to the lug at the tube 38 at clip position 5923 with the bolt, spacer PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-562), spacer and the nut.
  8. Pre SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-500), the clip Fuel System Air Tubes (73-22-49, 05-336) at the tube Fuel System Air Tubes (73-22-49, 05-300) and the clips Turbine Cooling Air (TCA) Controlled Air Tubes (75-23-48, 03-568) and Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-160) at tubes 37 and 38 to the bracket HPC Assembly (72-41-00, 03-850) at the clip position 6064 with the bolt Fuel System Air Tubes (73-22-49, 05-333), washer Fuel System Air Tubes (73-22-49, 05-334), spacer Fuel System Air Tubes (73-22-49, 05-338), spacer Fuel System Air Tubes (73-22-49, 05-337) and nut Fuel System Air Tubes (73-22-49, 05-340).
  9. SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-500), the clip Fuel System Air Tubes (73-22-49, 05-336) at the tube Fuel System Air Tubes (73-22-49, 05-300) and the clip Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-160) at tube 38 to the bracket HPC Assembly (72-41-00, 03-850) at the clip position 6064 with the bolt Fuel System Air Tubes (73-22-49, 05-333), washer Fuel System Air Tubes (73-22-49, 05-334), spacer Fuel System Air Tubes (73-22-49, 05-338), spacer Fuel System Air Tubes (73-22-49, 05-337) and nut Fuel System Air Tubes (73-22-49, 05-340).
  10. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) to the pressure regulator bleed valve Bleed Pressure Regulator Valve (36-11-52, 01-050).
  11. Pre SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) with the clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-560) and the tube 52 Fuel System Air Tubes (73-22-49, 05-100) with the clip Fuel System Air Tubes (73-22-49, 05-128) to the bracket AIR-STAGE 10 TO HPT AIR VALVE (75-23-51, 01-010) at the clip position 5433 with the bolt Fuel System Air Tubes (73-22-49, 05-125), the washer Fuel System Air Tubes (73-22-49, 05-126) and the clipnut Fuel System Air Tubes (73-22-49, 05-132).
  12. SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) with the clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-562) and the tube 52 Fuel System Air Tubes (73-22-49, 05-100) with the clip Fuel System Air Tubes (73-22-49, 05-160) to the bracket Turbine Cooling Air (TCA) Controlled Air Tubes (75-23-48, 04-390) at the clip position 6108 with the bolt Fuel System Air Tubes (73-22-49, 05-157), the spacer Fuel System Air Tubes (73-22-49 ,05-162) and the nut Fuel System Air Tubes (73-22-49 ,05-164).
  13. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500).
  14. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500) to the bracket HPC Module - Attaching Parts (72-40-00, 01-740) at clip position 5865 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-525), washer PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-531), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-529) and the nut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-532).
  15. NOTE
    Refer to TASK 72-00-40-420-004 for the installation procedure for the tubes at support bracket G (clip position 5997).
    Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500), the clip Fuel Nozzle Supply Fuel Manifolds (73-11-41, 03-460) at the tube 80 at clip position 5997 to the bracket HPC Module - Attaching Parts (72-40-00, 01-060) with the bolt, clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-555) and the nut.
  16. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500) to the bracket HPC Module - Attaching Parts (72-40-00, 01-740) at clip position 5495 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-532), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-535), spacer PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-534) and clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-540).
  17. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) to the bracket HPC Module - Attaching Parts (72-40-00, 01-780) at clip position 5996 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-133), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-579) and clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-140).
  18. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500) and to the HP bleed valve PNEUMATIC-HP BLEED VALVE (36-11-51, 01-050).
  19. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to the bracket Engine Air Off-Take Air Ducts (75-00-49, 01-240) at clip position 5862 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-133), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-137) and the clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-140).
  20. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to the bracket Engine Air Off-Take Air Ducts (75-00-49, 01-242) at clip position 5931 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-150), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-514) and the clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-158).
  21. Torque the tube nuts on the tubes PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49,02-510) and PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to 135-145 lbf.in (15-16 Nm).
  22. Torque the bolts at the clip positions to 36-45 llbf.in (4-5 Nm). Wipe off excess paste.
3. 1. Torque the couplings installed in Step: PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-100), PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-310), PNEUMATIC-HP BLEED VALVE (36-11-51, 01-100), Bleed Pressure Regulator Valve (36-11-52, 01-100)) to 75-85 lbf.in (8.5-9.6 Nm). Use a soft faced hammer and tap around the outside of the couplings.
  2. Torque the couplings using the above procedure two more times.
  3. Torque the couplings (for the final time) to 75-85 lbf.in (8.5-9.6 Nm).
  4. Keep the coupling PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-110) for installation of the cabin bleed air duct on the pylon.
1. Refer to Figure, Figure, Figure, Fig. 72-00-40-457-005, Figure and Figure.
2. 1. Apply CoMat 10-031 ANTI-GALLING COMPOUND to one of the mating thread surfaces of the pressure sense tubes, hoses and union before you connect the components, as follows:
  2. NOTE
    Refer to SPM TASK 70-41-02-400-501 for the torque loading procedures.
    Cabin Bleed Air System Sense Tubes (36-21-49)
    IPC Fig./item
    01-100
    01-500
    01-510
    02-200
    02-500
    02-650
    02-700
    02-725
  3. NOTE
    Refer to SPM TASK 70-41-02-400-501 for the torque loading procedures.
    Do not tighten or torque the tube nuts or attaching parts until all the tubes are installed in their correct position.
  4. Install the K seal PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-655) and the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650) in the duct PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-300). Torque the union to 168-181 lbf.in (19-20.50 Nm).
  5. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) to the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650).
  6. Connect the hose PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-700) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) and the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-725).
  7. Attach the hose PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-200) to the tube connected to the pressure regulator bleed valve Bleed Pressure Regulator Valve (36-11-52, 01-050).
  8. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) and the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005) to the lug at the tube 38 at clip position 5923 with the bolt, spacer PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-562), spacer and the nut.
  9. Pre SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-500), the clip Fuel System Air Tubes (73-22-49, 05-336) at the tube Fuel System Air Tubes (73-22-49, 05-300) and the clips Turbine Cooling Air (TCA) Controlled Air Tubes (75-23-48, 03-568) and Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-160) at tubes 37 and 38 to the bracket HPC Assembly (72-41-00, 03-850) at the clip position 6064 with the bolt Fuel System Air Tubes (73-22-49, 05-333), washer Fuel System Air Tubes (73-22-49, 05-334), spacer Fuel System Air Tubes (73-22-49, 05-338), spacer Fuel System Air Tubes (73-22-49, 05-337) and nut Fuel System Air Tubes (73-22-49, 05-340).
  10. SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-500), the clip Fuel System Air Tubes (73-22-49, 05-336) at the tube Fuel System Air Tubes (73-22-49, 05-300) and the clip Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-160) at tube 38 to the bracket HPC Assembly (72-41-00, 03-850) at the clip position 6064 with the bolt Fuel System Air Tubes (73-22-49, 05-333), washer Fuel System Air Tubes (73-22-49, 05-334), spacer Fuel System Air Tubes (73-22-49, 05-338), spacer Fuel System Air Tubes (73-22-49, 05-337) and nut Fuel System Air Tubes (73-22-49, 05-340).
  11. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) to the pressure regulator bleed valve Bleed Pressure Regulator Valve (36-11-52, 01-050).
  12. Pre SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) with the clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-560) and the tube 52 Fuel System Air Tubes (73-22-49, 05-100) with the clip Fuel System Air Tubes (73-22-49, 05-128) to the bracket AIR-STAGE 10 TO HPT AIR VALVE (75-23-51, 01-010) at the clip position 5433 with the bolt Fuel System Air Tubes (73-22-49, 05-125), the washer Fuel System Air Tubes (73-22-49, 05-126) and the clipnut Fuel System Air Tubes (73-22-49, 05-132).
  13. SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) with the clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-562) and the tube 52 Fuel System Air Tubes (73-22-49, 05-100) with the clip Fuel System Air Tubes (73-22-49, 05-160) to the bracket Turbine Cooling Air (TCA) Controlled Air Tubes (75-23-48, 04-390) at the clip position 6108 with the bolt Fuel System Air Tubes (73-22-49, 05-157), the spacer Fuel System Air Tubes (73-22-49, 05-162) and the nut Fuel System Air Tubes (73-22-49, 05-164).
  14. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500).
  15. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500) to the bracket HPC Module - Attaching Parts (72-40-00, 01-740) at clip position 5865 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-525), washer PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-531), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-529) and the nut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-532).
  16. NOTE
    Refer to TASK 72-00-40-420-004 for the installation procedure for the tubes at support bracket G (clip position 5997).
    Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500), the clip Fuel Nozzle Supply Fuel Manifolds (73-11-41, 03-460) at the tube 80 at clip position 5997 to the bracket HPC Module - Attaching Parts (72-40-00, 01-060) with the bolt, clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-555) and the nut.
  17. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500) to the bracket HPC Module - Attaching Parts (72-40-00, 01-740) at clip position 5495 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-532), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-535), spacer PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-534) and clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-540).
  18. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) to the bracket HPC Module - Attaching Parts (72-40-00, 01-780) at clip position 5996 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-133), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-579) and clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-140).
  19. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500) and to the HP bleed valve PNEUMATIC-HP BLEED VALVE (36-11-51, 01-050).
  20. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to the bracket Engine Air Off-Take Air Ducts (75-00-49, 01-240) at clip position 5862 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-133), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-137) and the clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-140).
  21. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to the bracket Engine Air Off-Take Air Ducts (75-00-49, 01-242) at clip position 5931 with the bolt PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-150), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-514) and the clipnut PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-158).
  22. Torque the tube nuts on the tubes PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-150) and PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-100) to 135-145 lbf.in (15-16 Nm).
  23. Torque the bolts at the clip positions to 36-45 llbf.in (4-5 Nm).
3. 1. Torque the couplings installed in Step: PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-100), PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-310), PNEUMATIC-HP BLEED VALVE (36-11-51, 01-100), Bleed Pressure Regulator Valve (36-11-52, 01-100) to 75-85 lbf.in (8.5-9.6 Nm). Use a soft faced hammer and tap around the outside of the couplings.
  2. Torque the couplings using the above procedure two more times.
  3. Torque the couplings (for the final time) to 75-85 lbf.in (8.5-9.6 Nm).
  4. Keep the coupling PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-110) for installation of the cabin bleed air duct on the pylon.
1. Refer to Figure and Figure.
2. 1. Apply CoMat 10-031 ANTI-GALLING COMPOUND to one of the mating thread surfaces of the pressure sense tubes, hoses and union before you connect the components, as follows:
  2. NOTE
    Refer to the SPM TASK 70-41-02-400-501 for the torque loading procedures.
    NOTE
    Refer to the SPM TASK 70-41-02-400-501 for the torque loading procedures.
    Cabin Bleed Air System Sense Tubes (36-21-49)
    IPC Fig./item
    01-100
    01-500
    01-510
    02-200
    02-500
    02-650
    02-700
    02-725
    Do not tighten or torque the tube nuts or attaching parts until all the tubes are installed in their correct position.
  3. Install the K seal PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-655) and the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650) in the duct PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-300). Torque the union to 168-181 lbf.in (19-20,50 Nm).
  4. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) to the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650).
  5. Connect the hose PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-700) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) and the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-725).
  6. Attach the hose PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-050) to the tube connected to the pressure regulator bleed valve Bleed Pressure Regulator Valve (36-11-52, 01-050).
  7. Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) and the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005) to the lug at the tube 38 at clip position 5923 with the bolt, spacer PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-562), spacer and the nut.
  8. Pre SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-500), the clip Fuel System Air Tubes (73-22-49, 05-336) at the tube Fuel System Air Tubes (73-22-49, 05-300) and the clips Turbine Cooling Air (TCA) Controlled Air Tubes (75-23-48, 03-568) and Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-160) at tubes 37 and 38 to the bracket HPC Assembly (72-41-00, 03-850) at the clip position 6064 with the bolt Fuel System Air Tubes (73-22-49, 05-333), washer Fuel System Air Tubes (73-22-49, 05-334), spacer Fuel System Air Tubes (73-22-49, 05-338), spacer Fuel System Air Tubes (73-22-49, 05-337) and nut Fuel System Air Tubes (73-22-49, 05-340).
  9. SBE 75-0081: Attach the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500), the clip at the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-500), the clip Fuel System Air Tubes (73-22-49, 05-336) at the tube Fuel System Air Tubes (73-22-49, 05-300) and the clip Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-160) at tube 38 to the bracket HPC Assembly (72-41-00, 03-850) at the clip position 6064 with the bolt Fuel System Air Tubes (73-22-49, 05-333), washer Fuel System Air Tubes (73-22-49, 05-334), spacer Fuel System Air Tubes (73-22-49, 05-338), spacer Fuel System Air Tubes (73-22-49, 05-337) and nut Fuel System Air Tubes (73-22-49, 05-340).
  10. Attach the tube assembly PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-600), and the clip Fuel System Air Tubes (73-22-49, 05-944) at the raceway Fuel System Air Tubes (73-22-49, 05-900) to the bracket HPC Assembly (72-41-00, 03-720) at clip position 5657 with the bolt Fuel System Air Tubes (73-22-49, 05-941), washer Fuel System Air Tubes (73-22-49, 05-942), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-620), spacer Fuel System Air Tubes (73-22-49, 05-946) and clipnut Fuel System Air Tubes (73-22-49, 05-948).
  11. Attach the tube assembly PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-600), the clip Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-544) at tube 69 Bearing Compartment Cooling And Sealing Air Tubes (75-22-49, 05-500) and the clip Fuel System Air Tubes (73-22-49, 05-560) at tube 53 Fuel System Air Tubes (73-22-49, 05-500) to the bracket HPC Assembly (72-41-00, 03-550) at clip position 5647 with the bolt Fuel System Air Tubes (73-22-49, 05-557), washer Fuel System Air Tubes (73-22-49, 05-558), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-630), spacer Fuel System Air Tubes (73-22-49, 05-563) and clipnut Fuel System Air Tubes (73-22-49, 05-564).
  12. Attach the tube assembly PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-600), the clip OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-144) at tube 21 OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-100) to the bracket HPC Assembly (72-41-00, 03-530) at clip position 5591 with the bolt OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-141), washer OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-142), clip PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-640), spacer OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-146) and clipnut OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-148).
  13. Torque the tube nuts on the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-600) to 135-145 lbf.in (15-16 Nm).
  14. Torque the bolts at the clip positions to 36-45 llbf.in (4-5 Nm).
3. 1. Torque the couplings installed in Step PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-100), PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-310), PNEUMATIC-HP BLEED VALVE (36-11-51, 01-100), Bleed Pressure Regulator Valve (36-11-52, 01-100) to 75-85 lbf.in (8.5 - 9.6 Nm). Use a soft faced hammer and tap around the outside of the couplings.
  2. Torque the couplings using the above procedure two more times.
  3. Torque the couplings (for the final time) to 75-85 lbf.in (8.5 -9.6 Nm).
  4. Keep the coupling PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-110) for installation of the cabin bleed air duct on the pylon.
1. Refer to Figure.
2. Connect the tube 48 to the cabin air conditioning control tube.
3. Install the clips, the washers, the bolt and the nut at the clip positions 5782 and 5783. Torque the nut and bolt to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. Connect the tube 48 to the cabin air conditioning control tube.
3. SBE 73-0128: Install the clips, the washers, the bolt and the nut at the clip positions 6094. Torque the nut and bolt to 36 to 45 lbfin (4 to 5 Nm).
4. NOTE
  CP6097 is finally assembled in TASK 72-00-40-420-006-C00.
  Install the clips, the washers, the bolt and the nut at the clip positions, 6095, 6096 and 6098. Torque the nut and bolt to 36 to 45 lbf.in (4 to 5 Nm).
1. 1. The general clearance must be a minimum of 0.250 in. (6.35 mm).
  2. To check the clearance, push the harness with a light pressure of the thumb then release. The harness must spring back and give the minimum clearance. The harness must not move through the adjacent clips.
  3. The harness can touch the smooth parts of brackets if the harness is clipped to them. The harness must be held so there is no movement between the harness and the bracket.
2. Adjust the harnesses (if necessary) to get the minimum clearance and torque the clip position nut or bolt to 36 to 45 lbf.in (4 to 5 Nm).
  .
1. Refer to Figure.
2. Make sure that all the applicable connectors, backshells and cable clamps are secure.
3. Make sure that all the applicable backshells and cable clamps are safetied with CoMat 02-126 LOCKWIRE. Refer to the SPM TASK 70-42-05-400-501.

Cabin Bleed Air System Sense Tubes (36-21-49) IPC Fig./item
01-100	01-500	01-510	02-200	02-500	02-650	02-700	02-725

Cabin Bleed Air System Sense Tubes (36-21-49) IPC Fig./item
01-100	01-500	01-510	02-200	02-500	02-650	02-700	02-725

Cabin Bleed Air System Sense Tubes (36-21-49) IPC Fig./item
01-100	01-500	01-510	02-200	02-500	02-650	02-700	02-725

Sheet 1

Sheet 2

Sheet 3

Sheet 4

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Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 7

Sheet 8

Electrical Harness Installation

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 7

Sheet 8

Sheet 9

Sheet 10

Sheet 11

Sheet 12

Sheet 13

Sheet 14

Sheet 15

Sheet 16

Sheet 17

Sheet 18

Sheet 19

Sheet 20

Sheet 21

Sheet 1

Sheet 2

Sheet 1

Sheet 2

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Sheet 4

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Sheet 6

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Sheet 8

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Sheet 2

Sheet 3

Visually Inspect the Backshells and Cable Clamps

Requirements After Job Completion

Follow-On Conditions

NONE

Manufacturer Code:	0AM53
Enterprise Name:	IAE INTERNATIONAL AERO ENGINES AG
BU Name:	NULL
Building:	SUITE 400
Street:	628 HEBRON AVENUE
City:	GLASTONBURY
State:	CT
Zip Code:	06033
Country:	USA

Manufacturer Code:	34568
Enterprise Name:	TIODIZE CO., INC.
BU Name:	TIODIZE CO., INC.
Street:	5858 ENGINEER DRIVE
City:	HUNTINGTON BEACH
State:	CA
Zip Code:	92649
Country:	USA
Phone Number:	1-714-898-4377
Fax Number:	1-714-891-7467
Internet:	www.tiodize.com

Manufacturer Code:	K3504
Enterprise Name:	INDESTRUCTIBLE PAINT CO LTD
BU Name:	NULL
Street:	25 PENTOS DRIVE
City:	SPARKHILL
Province:	BIRMINGHAM
Zip Code:	B11 3TA
Country:	GREAT BRITAIN
Phone Number:	44-121-7022485
Fax Number:	44-121-7784338
Email:	sales@indestructible.co.uk
Internet:	www.indestructible.co.uk

Manufacturer Code:	LOCAL
Enterprise Name:	LOCALLY SUPPLIED

Manufacturer Code:	LOCAL
Tool Number:	Torq-Set
Tool Name:	ACR Torq-Set bit 212-1/4-ACR

TASK 72-00-40-420-005-B00 HP System Module - Install The Components, Ducts, Electrical Harnesses, And Tubes To The HPC Case Vertical Splitline, Installation-008

Export Control

Copyright

Applicability

Common Information

TASK 72-00-40-420-005-B00 HP System Module - Install The Components, Ducts, Electrical Harnesses, And Tubes To The HPC Case Vertical Splitline, Installation-008

General

NOTE

NOTE

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-00-40-420-219-A00 Install the Oil Feed Tubes (21, 23 and 24) (Pre SBE 72-0189)

SUBTASK 72-00-40-420-219-B00 Install the Oil Feed Tubes (21, 23 and 24) (SBE 72-0189)

SUBTASK 72-00-40-420-220 Install the Stage 7 Air Off-Take Ducts

SUBTASK 72-00-40-420-221 Install the Stage 7 Bleed Valves, the Seal Assemblies and the Silencers (Pre SBE 75-0071, Pre SBE 75-0092, Pre SBE 75-0093, SBE 75-0071, SBE 75-0092 and SBE 75-0093)

SUBTASK 72-00-40-420-222-A00 Install the HP Compressor Bleed Valve Air Tubes (Pre SBE 72-0189)

SUBTASK 72-00-40-420-222-B00 Install the HP Compressor Bleed Valve Air Tubes (SBE 72-0189)

NOTE

SUBTASK 72-00-40-420-223 Electrical Harness Installation Procedure

SUBTASK 72-00-40-420-224 Install the High Energy Ignition Harness

CAUTION

SUBTASK 72-00-40-420-225-A00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (Pre SBE 72-0189 and Pre SBN 71-0273)

NOTE

SUBTASK 72-00-40-420-225-B00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (Pre SBE 72-0189 and SBN 71-0273)

SUBTASK 72-00-40-420-225-C00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (SBE 72-0189, Pre SBE 75-0081 and Pre SBN 71-0273)

SUBTASK 72-00-40-420-225-D00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (SBE 72-0189, SBN 71-0273 and Pre SBE 75-0081)

SUBTASK 72-00-40-420-225-E00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (SBE 75-0081, SBE 72-0189 and Pre SBN 71-0273)

SUBTASK 72-00-40-420-225-F00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (SBE 75-0081, SBE 72-0189 and SBN 71-0273)

SUBTASK 72-00-40-420-226-A00 Install the Support Tubes and the Cross Brackets for the Ignition Exciters (Pre SBE 74-0001)

SUBTASK 72-00-40-420-226-B00 Install the Brackets for the Ignition Exciters (SBE 74-0001)

SUBTASK 72-00-40-420-227 Install the Cabin Bleed Air System Ducts and Valves

NOTE

NOTE

NOTE

NOTE

SUBTASK 72-00-40-420-228-A00 Install the Cabin Bleed Air System Sense Tubes (Pre SBE 36-0007, Pre SBN 70-0468, SBN 71-0273, Pre SBE 75-0081 and SBE 75-0081)

NOTE

NOTE

NOTE

SUBTASK 72-00-40-420-228-B00 Install the Cabin Bleed Air System Sense Tubes (Pre SBE 36-0007, SBN 70-0468, SBN 71-0273, Pre SBE 75-0081 and SBE 75-0081)

NOTE

NOTE

NOTE

NOTE

SUBTASK 72-00-40-420-228-C00 Install the Cabin Bleed Air System Sense Tubes (Pre SBE 75-0081, SBE 36-0007 and SBE 75-0081)

NOTE

NOTE

NOTE

SUBTASK 72-00-40-420-229-A00 Install the HP Bleed Control Air Tube (48) (Pre SBE 72-0189)

SUBTASK 72-00-40-420-229-B00 Install the HP Bleed Control Air Tube (48) (SBE 72-0189 and SBE 73-0128)

NOTE

SUBTASK 72-00-40-220-136 Measure the Harness Clearances and Examine the Harness Routing

SUBTASK 72-00-40-210-063 Visually Inspect the Electrical Backshells and Cable Clamps

Figure: Pre SBE 72-0189: Install the Oil Feed Tubes

Sheet 1

Figure: SBE 72-0189: Install the Oil Feed Tubes

Sheet 2

Figure: Install the Oil Feed Tubes

Sheet 3

Figure: Install the Oil Feed Tubes

Sheet 4

Figure: Pre SBE 75-0092 and Pre SBE 75-0093: Install the Stage 7 HP Compressor Bleed Valve Assemblies and the Air Off-take Ducts

Sheet 1

Figure: Pre SBE 75-0093 and SBE 75-0092: Install the Stage 7 HP Compressor Bleed Valve Assemblies and the Air Off-take Ducts

Sheet 2

Figure: SBE 75-0093: Install the Stage 7 HP Compressor Bleed Valve Assemblies and the Air Off-take Ducts

Sheet 3

Figure: Install the Stage 7 HP Compressor Bleed Valve Assemblies and the Air Off-take Ducts

Sheet 4

Figure: Install the Stage 7 HP Compressor Bleed Valve Assemblies and the Air Off-take Ducts

Sheet 5

Figure: Pre SBE 72-0189: Install the HP Compressor Bleed Valve Air Tubes

Sheet 1

Figure: SBE 72-0189: Install the HP compressor bleed valve air tubes