TASK 72-00-40-420-005-C00 HP System Module - Install The Components, Ducts, Electrical Harnesses, And Tubes To The HPC Case Vertical Splitline, Installation-008 - SBE 79-0088

DMC:V2500-A5-72-00-4000-05D-720A-B|Issue No:001.00|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 and /SBE 79-0088

Common Information

TASK 72-00-40-420-005-C00 HP System Module - Install The Components, Ducts, Electrical Harnesses, And Tubes To The HPC Case Vertical Splitline, Installation-008 - SBE 79-0088

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 (INSTALLATION-007) Install the initial components, the air off-take ducts and the tubes to the HP system module.

TASK 72-00-40-420-006-B00 (INSTALLATION-009, CONFIG-002) Install and connect the components, the electrical harnesses and the tubes to the front of the HP compressor case.

TASK 72-00-40-420-007-B00 (INSTALLATION-010, CONFIG-002) Install the components, the electrical harnesses and the tubes to the HP turbine.

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

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 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

NameManufacturerPart Number / IdentificationQuantityRemark
ACR Torq-Set bit 212-1/4-ACRLOCALTorq-Set

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-126 LOCKWIRELOCALCoMat 02-126
CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)LOCALCoMat 02-148
CoMat 02-274 SAFETY CABLE KITLOCALCoMat 02-274
CoMat 02-275 SAFETY CABLE KITLOCALCoMat 02-275
CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADELOCALCoMat 04-005
CoMat 07-038 AIR DRYING ENAMELK3504CoMat 07-038
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077
CoMat 10-031 ANTI-GALLING COMPOUND0AM53CoMat 10-031

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-40-420-415 Install the Oil Feed Tubes (21, 23 and 24)

    1. Refer to Figure, Figure and Figure.

      2. Install the tube 21 OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 14-100).

      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. Install the tube 24 OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-100).

      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 lbfin (4 to 5 Nm).

      2. Lightly lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 13-116) seal ring 1 off 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. Install the tube 23 Engine Pressure Oil Tubes (79-21-49, 12-100).

      1. Put the tube 23 in position.

      2. Install the clip, the clipnut, the washer and the bolt to the bracket Engine Air Off-Take Air Ducts (75-00-49, 01-680) at the clip position 6087.

    2. SUBTASK 72-00-40-420-416 Install the Stage 7 Air Off-Take Ducts

      2. Install the stage 7 air off-take duct Engine Air Off-Take Air Ducts (75-00-49, 01-250).

      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. Install the two stage 7 air off-take ducts Engine Air Off-Take Air Ducts (75-00-49, 01-100).

      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). 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.

      5. Install the remaining 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 12 bolts to 85 to 105 lbf.in (10 to 12 Nm).

    3. SUBTASK 72-00-40-420-417 Install the Stage 7 Bleed Valves, the Seal Assemblies and the Silencers (Pre SBE 75-0071, SBE 75-0071, Pre SBE 75-0092, SBE 75-0092, Pre SBE 75-0093, SBE 75-0093, Pre SBE 75-0105 and SBE 75-0105)

    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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) 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 and 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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) 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 and 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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) 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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) 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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-102). Torque the nuts to 85 to 105 lbfin (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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-070) to the bleed valve HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) 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 HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-100) with the 12 bolts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-062) and the 12 nuts HPC Stage 7 Bleed Outlet Duct, Seal Assembly And Silencer Assemblies (75-32-52, 01-061). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).

    4. SUBTASK 72-00-40-420-418 Install the tubes 63, 64, 65 and 32, the HP Compressor Bleed Valve Air Tubes

    1. Refer to Figure, Figure and Figure.

      2. Install the tubes 63, 64 and 65, the stage 7 and 10 air bleed tubes:

      1. Attach the tube 63 to the stage 7 bleed valve at the 2 o'clock position.

      2. Attach the tube 65 to the stage 7 bleed valve at the 4 o'clock position.

      3. Attach the tube 64 to the stage 10 bleed valve at the 3 o'clock position.

      4. Install the clips, the clipnuts, the washers and the bolts at the clip positions 5397 and 5675.

      5. Install the clip, the bolt, the washer and the nut at the clip position 5643.

      6. Torque the tube nuts to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-274 SAFETY CABLE KIT lockwire.

      7. Torque the bolt at clip positions 5397 and 5675 to 36 to 45 lbf.in (4 to 5 Nm).

      8. Torque the nut at clip position 5643 to 36 to 45 lbf.in (4 to 5 Nm).

      3. Install the tube 32, the HPC stage 7 air bleed tube:

      1. Attach the tube 32 to the stage 7 bleed valve at the 8 o'clock position.

      2. Install the clip, the bolt, the washer and the nut at the clip position 6081.

      3. Torque the tube nut to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at clip position 6081 to 36 to 45 lbf.in (4 to 5 Nm).

    5. SUBTASK 72-00-40-420-419 Electrical Harness Installation Procedure

    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 SPM TASK 70-43-01-700-501.

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

      CAUTION

      DO NOT BEND THE HIGH ENERGY IGNITION HARNESS MORE THAN IS NECESSARY, YOU CAN DAMAGE THE CONDUIT.

    1. Refer to Figure, Figure, Figure and Figure.

      2. Install the No. 2 high energy ignition harness Ignition Leads (74-21-43, 02-100).

      1. Connect the No. 2 high energy ignition harness to the No. 2 igniter plug.

      2. Install the clip, 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. NOTE

        The installation of clip position 5758 is completed in TASK 72-00-40-420-007-B00.

        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. Install the No.1 high energy ignition harness IGNITION-IGNITION LEADS (74-21-43, 01-100).

      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).

    7. SUBTASK 72-00-40-420-421-A00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (Pre SBE 75-0081, Pre SBN 71-0273 and SBN 71-0273)

    1. Refer to Figure.

      2. Install the fire detection (system A), nacelle temperature and cabin services harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005).

      1. Put the harness in to position.

      2. 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).

      3. Pre SBN 71-0273: Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 5938, 5939, 5766, 5940, 5941, 6098, 5648, 5765, 5764, 5763, 5652, 5921, 5922, 6064, 5923, 6066, 5924, 5925 and 5913. Torque the nuts to 36 to 45 lbfin. (4 to 5 Nm).

        Refer to Figure. Figure. Figure and Figure.

      4. SBN 71-0273: Install the clips, the washers, the spacers, the bolts and the nuts at the clip positions 6075, 6079, 6084, 6088, 6112, 5766, 5940, 6098, 5648, 5765, 5764, 5763, 5652, 5921, 5922, 6064, 5923, 6066, 5924, 5925 and 5913.

        Refer to Figure, Figure, Figure and Figure.

    8. SUBTASK 72-00-40-420-421-B00 Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harnesses and the Core Overheat Detector (SBE 75-0081 and SBN 71-0273)

    1. Refer to Figure.

      2. Install the fire detection (system A), nacelle temperature and cabin services harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005).

      1. Put the harness in to position.

      2. 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).

      3. Install the clips, the washers, the spacers, the bolts and the nuts at clip positions 6075, 6079, 6084, 6088, 6112, 5766, 5940, 6098, 5648, 5747, 6058, 6107, 5652, 5921, 5922, 6064, 5923, 6066, 5924, 5925 and 5990. Torque the nuts to 36 to 45 lbfin (4 to 5 Nm). Refer to Figure. Figure. Figure and Figure.

    9. SUBTASK 72-00-40-420-422-A00 Install the Support Tubes and the Cross Brackets for the Ignition Exciters (Pre SBE 74-0001)

    1. Refer to Figure.

      2. Install the lower support tube Ignition Exciters (74-11-38, 01-755).

      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 lbf.in (10 to 12 Nm).

      3. Install the upper support tube Ignition Exciters (74-11-38, 01-355).

      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. Install the lower, forward cross bracket Ignition Exciters (74-11-38, 01-670).

      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. Install the lower, rear cross bracket Ignition Exciters (74-11-38, 01-600).

      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. Install the upper, forward cross bracket Ignition Exciters (74-11-38, 01-270).

      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. Install the upper, rear cross bracket Ignition Exciters (74-11-38, 01-200).

      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).

    10. SUBTASK 72-00-40-420-422-B00 Install the Brackets for the Ignition Exciters (SBE 74-0001)

    1. Refer to Figure.

      2. Install the brackets Ignition Exciters (74-11-38, 01-470).

      1. Attach the bracket Ignition Exciters (74-11-38, 01-470) to the brackets HPC Assembly (72-41-00, 04-620 and HPC Assembly 04-670) fitted 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 Assembly04-650) fitted 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. Install the brackets Ignition Exciters (74-11-38, 01-170 and Ignition Exciters 01-570).

      1. Attach the brackets Ignition Exciters (74-11-38, 01-170 and Ignition Exciters 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. Install the brackets Ignition Exciters (74-11-38, 01-180 and Ignition Exciters01-580).

      1. Attach the brackets Ignition Exciters (74-11-38, 01-180 and Ignition Exciters 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. Assemble the brackets Ignition Exciters (74-11-38, 01-170 and Ignition Exciters 01-180) and Ignition Exciters (74-11-38, 01-570 and Ignition Exciters 01-580).

      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. Install the brackets Ignition Exciters (74-11-38, 01-200 and Ignition Exciters 01-600).

      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 01-216) and the two clipnuts Ignition Exciters (74-11-38, 01-215 and Ignition Exciters 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 01-614) and the two clipnuts Ignition Exciters (74-11-38, 01-613 and Ignition Exciters 01-474).

      3. Torque the bolts to 85 to 105 lbfin (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 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.).

    11. SUBTASK 72-00-40-420-423 Install the Cabin Bleed Air System Ducts and Valves

    1. NOTE

      Pre SBE 36-0007: It is quicker to loose install the two cabin bleed air system sense tubes PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510 and PNEUMATIC-PRESSURE INDICATING TUBES 36-21-49, 01-500) before you install the cabin bleed air ducts.

      Refer to Figure and Figure.

    2. NOTE

      Refer to the 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. Install the IP bleed check valve PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-050).

      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. Install the HP bleed valve PNEUMATIC-HP BLEED VALVE (36-11-51, 01-050).

      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. Install the lower duct assembly PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-500).

      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. Install the Y-duct PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-300).

      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. Install the pressure regulator bleed valve Bleed Pressure Regulator Valve (36-11-52, 01-050).

      1. Install the seal Bleed Pressure Regulator Valve (36-11-52, 01-110) PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-340 ref.) 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. NOTE

        Final adjust and secure the link assemblies when the engine is installed on the pylon.

        Install the upper duct assembly PNEUMATIC-BLEED AIR DUCTS (36-11-49, 01-100).

      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 01-770). Refer to Figure.

      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 Step and Step to 85 to 105 lbf.in (10 to 12 Nm).

    12. SUBTASK 72-00-40-420-424-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)

      2. Install the cabin bleed air system sense tubes (36-21-49).

      1. NOTE

        Refer to SPM TASK 70-41-02-400-501 for the torque loading procedures.

        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:

        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 V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-333), washer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-334), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49,05-338), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-337) and nut V2500-A5-36-21-49-05A-941A-D (36-21-49, 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 V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-333), washer V2500-A5-36-21-49-05A-941A-D (36-21-49,05-334), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49,05-338), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-337) and nut V2500-A5-36-21-49-05A-941A-D (36-21-49, 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 (72-00-40 Installation-07) 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 lbf.in (4-5 Nm).

      3. NOTE

        Refer to SPM TASK 70-47-01-470-501 for the procedure to install v-band couplings.

        Torque the cabin bleed air system duct couplings.

      1. Torque the couplings installed in SUBTASK 72-00-40-420-227PNEUMATIC-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.

    13. SUBTASK 72-00-40-420-424-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)

      2. Install the cabin bleed air system sense tubes (36-21-49).

      1. 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.

      2. 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).

      3. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) to the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650).

      4. 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).

      5. 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).

      6. 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.

      7. 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 V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-333), washer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-334), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-338), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-337) and nut V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-340).

      8. 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 V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-333), washer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-334), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49,05-338), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-337) and nut V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-340).

      9. 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).

      10. 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).

      11. 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).

      12. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-510) to the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-500).

      13. 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).

      14. NOTE

        Refer to TASK 72-00-40-420-004 (72-00-40 Installation-07) 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.

      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 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).

      16. 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).

      17. 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).

      18. 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).

      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, 01-242) 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).

      20. 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).

      21. Torque the bolts at the clip positions to 36-45 lbf.in (4-5 Nm).

      3. NOTE

        Refer to SPM TASK 70-47-01-470-501 for the procedure to install v-band couplings.

        Torque the cabin bleed air system duct couplings.

      1. Torque the couplings installed in SUBTASK 72-00-40-420-227PNEUMATIC-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.

    14. SUBTASK 72-00-40-420-424-C00 Install the Cabin Bleed Air System Sense Tubes (SBE 36-0007)

    1. Refer to Figure.

      2. Install the cabin bleed air system sense tubes (36-21-49).

      1. NOTE

        Refer to the 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.

      2. 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).

      3. Connect the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-500) to the union PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 02-650).

      4. 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).

      5. 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).

      6. 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.

      7. 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 V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-333), washer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-334), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-338), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-337) and nut V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-340).

      8. 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 V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-333), washer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-334), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-338), spacer V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-337) and nut V2500-A5-36-21-49-05A-941A-D (36-21-49, 05-340).

      9. 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).

      10. 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).

      11. Torque the tube nuts on the tube PNEUMATIC-PRESSURE INDICATING TUBES (36-21-49, 01-600) to 135-145 lbf.in (15-16 Nm).

      12. Torque the bolts at the clip positions to 36-45 llbf.in (4-5 Nm).

      3. NOTE

        Refer to SPM TASK 70-47-01-470-501 for the procedure to install v-band couplings.

        Torque the cabin bleed air system duct couplings.

      1. Torque the couplings installed in SUBTASK 72-00-40-420-227PNEUMATIC-IP BLEED AIR CHECK VALVE (36-11-41, 01-100 , PNEUMATIC-BLEED AIR DUCTS36-11-49, 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.

    15. SUBTASK 72-00-40-420-425 Install the HP Bleed Control Air Tube (48)

    1. Refer to Figure, Figure and Figure.

    2. Connect the tube 48 to the cabin air conditioning control tube.

    3. NOTE

      CP6098 is finally assembled in TASK 72-00-40-420-006-C00 Installation-09.

      Install the clips, the washers, the bolts and the nuts at the clip positions, 6094, 6096 and 6098. Torque the nut and bolt to 36 to 45 lbf.in (4 to 5 Nm).

    16. SUBTASK 72-00-40-220-149 Measure the Harness Clearances and Examine the Harness Routing

      1. Measure the clearance between all the different harnesses and the engine parts:

      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).

    17. SUBTASK 72-00-40-210-081 Visually Inspect the Electrical Backshells and Cable Clamps

    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.

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

    Sheet 1

    Legend
    SBE 72-0189: Install the Oil Feed Tubes

    Sheet 1

    Close

    Figure: Install the Oil Feed Tubes

    Sheet 2

    Legend
    Install the Oil Feed Tubes

    Sheet 2

    Close

    Figure: Install the Oil Feed Tubes

    Sheet 3

    Legend
    Install the Oil Feed Tubes

    Sheet 3

    Close

    Figure: Install the Oil Feed Tubes

    Sheet 4

    Legend
    Install the Oil Feed Tubes

    Sheet 4

    Close

    Figure: Pre SBE 75-0071, SBE 75-0071, Pre SBE 75-0092 and Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 1

    Legend
    Pre SBE 75-0071, SBE 75-0071, Pre SBE 75-0092 and Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 1

    Close

    Figure: Pre SBE 75-0071, SBE 75-0071, SBE 75-0092, Pre SBE 75-0093 and Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 2

    Legend
    Pre SBE 75-0071, SBE 75-0071, SBE 75-0092, Pre SBE 75-0093 and Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 2

    Close

    Figure: SBE 75-0071, SBE 75-0093, Pre SBE 75-0092 and SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 3

    Legend
    SBE 75-0071, SBE 75-0093, Pre SBE 75-0092 and SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 3

    Close

    Figure: Pre SBE 75-0093, SBE 75-0071, SBE 75-0092 and SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 4

    Legend
    Pre SBE 75-0093, SBE 75-0071, SBE 75-0092 and SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 4

    Close

    Figure: SBE 75-0093, SBE 75-0071 and SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 5

    Legend
    SBE 75-0093, SBE 75-0071 and SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 5

    Close

    Figure: Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 6

    Legend
    Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 6

    Close

    Figure: SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 7

    Legend
    SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 7

    Close

    Figure: Pre SBE 75-0071, SBE 75-0071 and Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 8

    Legend
    Pre SBE 75-0071, SBE 75-0071 and Pre SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 8

    Close

    Figure: SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 9

    Legend
    SBE 75-0105: Install the Stage 7 HPC Bleed Valve Assemblies and the Air Off-Take Ducts

    Sheet 9

    Close

    Figure: Install the HP Compressor Bleed Valve Air Tubes

    Sheet 1

    Legend
    Install the HP Compressor Bleed Valve Air Tubes

    Sheet 1

    Close

    Figure: Install the HP Compressor Bleed Valve Air Tubes

    Sheet 2

    Legend
    Install the HP Compressor Bleed Valve Air Tubes

    Sheet 2

    Close

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

    Sheet 3

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

    Sheet 3

    Close

    Figure: Electrical Harness Installation

    Electrical Harness Installation

    Figure: Install the High Energy Ignition Harness

    Sheet 1

    Legend
    Install the High Energy Ignition Harness

    Sheet 1

    Close

    Figure: Install the High Energy Ignition Harness

    Sheet 2

    Legend
    Install the High Energy Ignition Harness

    Sheet 2

    Close

    Figure: Install the High Energy Ignition Harness

    Sheet 3

    Legend
    Install the High Energy Ignition Harness

    Sheet 3

    Close

    Figure: Install the High Energy Ignition Harness

    Sheet 4

    Legend
    Install the High Energy Ignition Harness

    Sheet 4

    Close

    Figure: Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 1

    Legend
    Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 1

    Close

    Figure: Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 2

    Legend
    Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 2

    Close

    Figure: Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 3

    Legend
    Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 3

    Close

    Figure: Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 4

    Legend
    Install the Fire Detection, the Nacelle Temperature and the Cabin Services Harnesses

    Sheet 4

    Close

    Figure: Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harness

    Sheet 5

    Legend
    Install the Fire Detection Harnesses, the Nacelle Temperature and Cabin Services Harness

    Sheet 5

    Close

    Figure: Pre SBE 74-0001: Install the Ignition Exciter Cross Brackets and the Support Tubes

    Sheet 1

    Legend
    Pre SBE 74-0001: Install the Ignition Exciter Cross Brackets and the Support Tubes

    Sheet 1

    Close

    Figure: SBE 74-0001: Install the Ignition Exciter Support Brackets

    Sheet 2

    Legend
    SBE 74-0001: Install the Ignition Exciter Support Brackets

    Sheet 2

    Close

    Figure: Install the Cabin Bleed Air System Ducts and the Valves

    Sheet 1

    Legend
    Install the Cabin Bleed Air System Ducts and the Valves

    Sheet 1

    Close

    Figure: Install the Cabin Bleed Air System Ducts and the Valves

    Sheet 2

    Legend
    Install the Cabin Bleed Air System Ducts and the Valves

    Sheet 2

    Close

    Figure: Pre SBE 36-0007: Install the Cabin Bleed Air System Sense Tubes

    Sheet 1

    Legend
    Pre SBE 36-0007: Install the Cabin Bleed Air System Sense Tubes

    Sheet 1

    Close

    Figure: SBE 36-0007: Install the Cabin Bleed Air System Sense Tubes

    Sheet 2

    Legend
    SBE 36-0007: Install the Cabin Bleed Air System Sense Tubes

    Sheet 2

    Close

    Figure: Install the Cabin Bleed Air System Sense Tubes

    Sheet 3

    Legend
    Install the Cabin Bleed Air System Sense Tubes

    Sheet 3

    Close

    Figure: Pre SBE 36-0007, Pre SBE 75-0081: Install the Cabin Bleed Air System Sense Tubes

    Sheet 4

    Legend
    Pre SBE 36-0007, Pre SBE 75-0081: Install the Cabin Bleed Air System Sense Tubes

    Sheet 4

    Close

    Figure: SBE 75-0081: Install the Cabin Bleed Air System Sense Tubes

    Sheet 5

    Legend
    SBE 75-0081: Install the Cabin Bleed Air System Sense Tubes

    Sheet 5

    Close

    Figure: Pre SBE 36-0007: Install the Cabin Bleed Air System Sense Tubes

    Sheet 6

    Legend
    Pre SBE 36-0007: Install the Cabin Bleed Air System Sense Tubes

    Sheet 6

    Close

    Figure: Pre SBE 36-0007, SBN 71-0273: Install the Cabin Bleed Air System Sense Tubes

    Sheet 7

    Legend
    Pre SBE 36-0007, SBN 71-0273: Install the Cabin Bleed Air System Sense Tubes

    Sheet 7

    Close

    Figure: Install the Cabin Bleed Air System Sense Tubes

    Sheet 8

    Legend
    Install the Cabin Bleed Air System Sense Tubes

    Sheet 8

    Close

    Figure: Install the HP Bleed Control Air Tube (48)

    Sheet 1

    Legend
    Install the HP Bleed Control Air Tube (48)

    Sheet 1

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the HP Bleed Control Air Tube (48)

    Sheet 2

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the HP Bleed Control Air Tube (48)

    Sheet 2

    Close

    Figure: Install the HP Bleed Control Air Tube (48)

    Sheet 3

    Legend
    Install the HP Bleed Control Air Tube (48)

    Sheet 3

    Close

    Figure: Visually Inspect the Backshells and Cable Clamps

    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: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:K6835
Supply Number:CoMat 02-126
Type:sp01
Supply Short Name:CoMat 02-126 LOCKWIRE
Supply Name:CoMat 02-126 LOCKWIRE
Specification Groups:
Doc NumberType
DTD 189A, 0.028 TO 0.032 IN DIA
Suppliers:
ManufacturerRemarks
K6835
KB362
LOCAL
U06C8
Manufacturer Code:LOCAL
Supply Number:CoMat 02-148
Type:sp01
Supply Short Name:CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)
Supply Name:CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)
Specification Groups:
Doc NumberType
OMAT: 296SCOTCH NO. 69 (WHITE)
Suppliers:
ManufacturerRemarks
LOCAL
76381
94960
K0993
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 02-274
Type:sp01
Supply Short Name:CoMat 02-274 SAFETY CABLE KIT
Supply Name:CoMat 02-274 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
SAE AS3510-0218K (DIA 0,032 IN LENGTH 18IN)
Suppliers:
ManufacturerRemarks
LOCAL
11851
U0419
70958
H7503
SA221
V384V
Manufacturer Code:X111X
Supply Number:CoMat 02-275
Type:sp01
Supply Short Name:CoMat 02-275 SAFETY CABLE KIT
Supply Name:CoMat 02-275 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
Deleted. Use CoMat 02-274.
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:LOCAL
Supply Number:CoMat 04-005
Type:sp01
Supply Short Name:CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE
Supply Name:CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE
Specification Groups:
Doc NumberType
OMAT: 4/47 (RR REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
JCR-026 (JAEC REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
DTD 900/4586 (RR REF, MOD UK REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
MSRR 9055 (RR REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
Suppliers:
ManufacturerRemarks
LOCAL
460Y4
CJ731
K3237
Manufacturer Code:00BB6
Supply Number:CoMat 07-038
Type:sp01
Supply Short Name:CoMat 07-038 AIR DRYING ENAMEL
Supply Name:CoMat 07-038 AIR DRYING ENAMEL
Specification Groups:
Doc NumberType
OMAT:7/22B (RR REF)IP9138 R1
JCR-029 (JAEC REF)
Suppliers:
ManufacturerRemarks
00BB6
K3504
Manufacturer Code:0AM53
Supply Number:CoMat 10-031
Type:sp01
Supply Short Name:CoMat 10-031 ANTI-GALLING COMPOUND
Supply Name:CoMat 10-031 ANTI-GALLING COMPOUND
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
0AM53
Manufacturer Code:X333X
Supply Number:CoMat 10-077
Type:sp01
Supply Short Name:CoMat 10-077 APPROVED ENGINE OILS
Supply Name:CoMat 10-077 APPROVED ENGINE OILS
Specification Groups:
Doc NumberType
For V2500-A1/A5/D5 models - Refer to V2500 Service Bulletin ENG-79-0108
For V2500-E5 model - Refer to Service Bulletin E5-79-0001
Suppliers:
ManufacturerRemarks
X333X
Manufacturer Code:LOCAL
Tool Number:Torq-Set
Tool Name:ACR Torq-Set bit 212-1/4-ACR