Preliminary Requirements

Procedure

1. SUBTASK 72-00-45-220-100 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly to Location 2225

   1. Refer to Figure or Figure.

   2. Reference clearance at location 2225. If required, use the data written as a note in TASK 72-41-13-200-000 (INSPECTION-000) and TASK 72-40-00-200-000 (INSPECTION-000).

      Table 1. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2225
      HPC drive turbine shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850), Journal Diameter
      No. 4 Bearing Spacer (72-40-00, 03-003 thru 03-035), Bore
      HPC Drive Turbine Shaft	5.107	Clear
      Journal Diameter	5.108	0.003
      Spacer Bore	5.111	0.006
      	5.113	Clear

      Table 2. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2225
      HPC Drive Turbine Shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850), Journal Diameter
      No. 4 Bearing Spacer ENGINE-ATTACH PARTS & FITTINGS-HP SYSTEM (72-40-00, 03-003 thru 03-035), Bore
      HPC Turbine Drive Shaft Journal Diameter	129.718	Clear
      	129.743	0.077
      Spacer Bore	129.819	0.152
      	129.870	Clear

2. SUBTASK 72-00-45-220-101 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2246

   1. Refer to Figure or Figure.

   2. Reference interference at location 2246. If required, use the data written as a note in TASK 72-45-11-200-000 (INSPECTION-000) and TASK 72-41-13-200-000 (INSPECTION-000).

      Table 3. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2246
      Front Turbine Hub HPT Stage 1 Hub (72-45-11, 01-011), Bore
      HPC Drive Turbine Shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850), Location Diameter
      Hub bore	5.1022	Intf
      	5.101	0.005
      Shaft location diameter	5.108	0.0072
      	5.107	Intf

      Table 4. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2246
      Front turbine hub HPT Stage 1 Hub (72-45-11, 01-011), Bore
      HPC Drive Turbine Shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850), Location Diameter
      Hub Bore	129.596	Intf
      	129.565	0.127
      Shaft Location Diameter	129.743	0.1778
      	129.718	Intf

3. SUBTASK 72-00-45-220-104 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2249

   1. Refer to Figure or Figure.

   2. Reference interference at location 2249. If required, use the data written as a note in TASK 72-41-13-200-000 (INSPECTION-000) and TASK 72-45-31-200-000 (INSPECTION-000).

      Table 5. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Select)	REJECT IF MORE THAN
      LOCATION 2249
      HPC Drive Turbine Shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850), Location Diameter
      Stage 2 Turbine Hub ENGINE-STAGE 2 TURBINE HUB (72-45-31, 01-010), Bore
      Shaft Location Diameter	4.842	Intf	4.842	Intf
      	4.841	0.005	4.841	0.0046
      Hub Bore	4.836	0.007	4.8364	0.007
      	4.835	Intf	4.8345	Intf

      Table 6. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Select)	REJECT IF MORE THAN
      LOCATION 2249
      HPC Drive Turbine Shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850), Location Diameter
      Stage 2 Turbine Hub ENGINE-STAGE 2 TURBINE HUB (72-45-31, 01-010), Bore
      Shaft Location Diameter	122.987	Intf	122.987	Intf
      	122.962	0.128	122.962	0.117
      Hub Bore	122.834	0.178	122.844	0.178
      	122.809	Intf	122.796	Intf

4. SUBTASK 72-00-45-220-105 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2250

   1. Refer to Figure or Figure.

   2. Reference clearance at location 2250. If required, use the data written as a note in TASK 72-41-13-200-000 (INSPECTION-000) and TASK 72-40-00-200-000 (INSPECTION-000).

      Table 7. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2250
      HPC Drive Turbine Shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850)
      HPC Drive Turbine Nut ENGINE-ATTACH PARTS & FITTINGS-HP SYSTEM (72-40-00, 04-020)
      Shaft Diameter	4.819	Clear	4.819	Clear
      	4.821	0.002	4.821	0.002
      Nut Diameter	4.823	0.006	4.823	0.009
      	4.825	Clear	4.828	Clear

      Table 8. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2250
      HPC Drive Turbine Shaft HPC Rear Shaft And Heatshield Assembly (72-41-13, 01-850)
      HPC Drive Turbine Nut ENGINE-ATTACH PARTS & FITTINGS-HP SYSTEM (72-40-00, 04-020)
      Shaft Diameter	122.403	Clear	122.403	Clear
      	122.453	0.051	122.453	0.051
      Nut Diameter	122.505	0.152	122.505	0.229
      	122.555	Clear	122.631	Clear

5. SUBTASK 72-00-45-220-106 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2253

   1. Refer to Figure or Figure.

   2. Reference interference at location 2253. If required, use the data written as a note in TASK 72-45-21-200-000 (INSPECTION-000) and TASK 72-44-10-200-000 (INSPECTION-000).

      Table 9. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2253
      Turbine Case Assembly HPT Case And Related Parts (72-45-21, 01-010), Location Diameter
      Stage 1 HPT Support Assembly HPT Stage 1 Support Assembly And Support Seal (72-44-10, 01-010), Location Diameter
      Case Assembly Location Diameter	28.233	Intf	28.233	Intf
      	28.227	0.002	28.222	0.002
      Support Assembly Location Diameter	28.241	0.014	28.241	0.019
      	28.235	Intf	28.230	Intf

      Table 10. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2253
      Turbine Case Assembly HPT Case And Related Parts (72-45-21, 01-010), Location Diameter
      Stage 1 HPT Support Assembly HPT Stage 1 Support Assembly And Support Seal (72-44-10, 01-010), Location Diameter
      Case Assembly Location Diameter	717.118	Intf	717.118	Intf
      	716.966	0.05	716.839	0.050
      Support Assembly Location Diameter	717.321	0.36	717.321	0.483
      	717.169	Intf	717.040	Intf

6. SUBTASK 72-00-45-220-107 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 5624

   1. Refer to Figure or Figure.

   2. Reference interference at location 5624. If required, use the data written as a note in TASK 72-50-21-200-000 (INSPECTION-000) and TASK 72-45-27-200-000 (INSPECTION-000).

      Table 11. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 5624
      LPT Case Assembly LPT Case, Heat Shields, And Seal Segments (72-50-21, 01-010), Location Diameter
      Stage 2 HPT Support Assembly ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27, 01-010), Location Diameter
      Case Diameter	28.533	Intf
      	28.527	0.002
      Support Diameter	28.541	0.014
      	28.535	Intf

      Table 12. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 5624
      LPT Case Assembly LPT Case, Heat Shields, And Seal Segments (72-50-21, 01-010), Location Diameter
      Stage 2 HPT Support Assembly ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27, 01-010), Location Diameter
      Case Diameter	724.738	Intf
      	724.586	0.05
      Support Diameter	724.941	0.36
      	724.789	Intf

7. SUBTASK 72-00-45-220-108 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 5623

   1. Refer to Figure or Figure.

   2. Calculate the clearance at Location 5623.

      Table 13. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Select)	REJECT IF MORE THAN
      LOCATION 5623
      Stage 2 Blade Retaining Plate HPT Stage 2 Blade Retaining Plate And Related Parts (72-45-33, 01-020), Knife-edge Outside Diameter
      Inner Turbine Duct LPT Inner Diffuser Duct And Related Parts (72-50-24, 01-010), Inside Diameter
      Knife-edge Outside Diameter	19.804	Clear	19.797	Clear
      	19.812	0.084	19.812	0.084
      Turbine Duct Inside Diameter	19.896	0.121	19.896	0.121
      	19.925	Clear	19.925	Clear

      Table 14. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Select)	REJECT IF MORE THAN
      LOCATION 5623
      Stage 2 Blade Retaining Plate HPT Stage 2 Blade Retaining Plate And Related Parts (72-45-33, 01-020), Knife-edge Outside Diameter
      Inner Turbine Duct LPT Inner Diffuser Duct And Related Parts (72-50-24, 01-010), Inside Diameter
      Knife-edge Outside Diameter	503.10	Clear	502.84	Clear
      	503.22	2.13	503.22	2.13
      Turbine Duct Inside Diameter	505.36	3.07	505.36	3.07
      	506.10	Clear	506.10	Clear

8. SUBTASK 72-00-45-220-109 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2256

   1. Refer to Figure or Figure.

   2. Reference clearance at location 2256. If required, use the data written as a note in TASK 72-44-60-200-000 (INSPECTION-000) and TASK 72-45-11-200-000 (INSPECTION-000).

      Table 15. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2256
      Radial Clearance
      Stage 1 HPT Duct Segment ENGINE-STAGE 1 HPT SEGMENT (72-44-60, 01-010)
      Stage 1 HPT Hub HPT Stage 1 Hub (72-45-11, 01-011) And Blade HPT Stage 1 Blade And Related Parts (72-45-14, 01-010) Assembly
      Stage 1 HPT Duct Segment	10.693	Clear
      	10.735	0.047
      Stage 1 HPT Hub And Blade Assembly	10.782	0.103
      	10.796	Clear

      Table 16. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2256
      Radial clearance
      Stage 1 HPT Duct Segment ENGINE-STAGE 1 HPT SEGMENT (72-44-60, 01-010)
      Stage 1 HPT Hub HPT Stage 1 Hub (72-45-11, 01-011) And Blade HPT Stage 1 Blade And Related Parts (72-45-14, 01-010) Assembly
      Stage 1 HPT Duct Segment	271.60	Clear
      	272.67	1.19
      Stage 1 HPT Hub And Blade Assembly	273.86	2.62
      	274.22	Clear

9. SUBTASK 72-00-45-220-110 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2257

   1. Refer to Figure or Figure.

   2. Reference clearance at location 2257. If required, use the data written as a note in TASK 72-45-12-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

      Table 17. Fits and Clearances (all dimensions are in inches)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2257
      Stage 1 And 2 HPT Airseal ENGINE-STAGE 1 HPT AIR SEAL (OUTER) (72-45-12, 01-040), knife-edge outside diameter
      Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
      Knife Edge Outsisde Diameter	11.381	Clear
      	11.397	0.018
      Seal Land Inside Diameter	11.415	0.064
      	11.445	Clear

      Table 18. Fits and Clearances (all dimensions are in millimeters)

      	NEW PART		WORN PART
      	DIMENSIONS		DIMENSIONS
      PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
      LOCATION 2257
      Stage 1 And 2 HPT Airseal ENGINE-STAGE 1 HPT AIR SEAL (OUTER) (72-45-12, 01-040), Knife-edge Outside Diameter
      Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
      Knife-edge Outsisde Diameter	289.08	Clear
      	289.48	0.46
      Seal Land Inside Diameter	289.94	1.63
      	290.70	Clear

10. SUBTASK 72-00-45-220-111 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2258

    1. Refer to Figure or Figure.

    2. Reference clearance at location 2258. If required, use the data written as a note in TASK 72-45-12-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

       Table 19. Fits and Clearances (all dimensions are in inches)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2258
       Stage 1 And 2 HPT Airseal ENGINE-STAGE 1 HPT AIR SEAL (OUTER) (72-45-12, 01-040), Knife-edge Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outsisde Diameter	11.481	Clear
       	11.497	0.018
       Seal Land Inside Diameter	11.515	0.064
       	11.545	Clear

       Table 20. Fits and Clearances (all dimensions are in millimeters)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2258
       Stage 1 And 2 HPT Airseal ENGINE-STAGE 1 HPT AIR SEAL (OUTER) (72-45-12, 01-040), Knife-edge Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	291.62	Clear
       	292.02	0.46
       Seal Land Inside Diameter	292.48	1.63
       	293.24	Clear

11. SUBTASK 72-00-45-220-112 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at location 2259

    1. Refer to Figure or Figure.

    2. Reference clearance at location 2259. If required, use the data written as a note in TASK 72-45-12-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

       Table 21. Fits and Clearances (all dimensions are in inches)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2259
       Stage 1 And 2 HPT Airseal ENGINE-STAGE 1 HPT AIR SEAL (OUTER) (72-45-12, 01-040), Knife-edge Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	11.581	Clear
       	11.597	0.018
       Seal Land ID	11.615	0.064
       	11.645	Clear

       Table 22. Fits and Clearances (all dimensions are in millimeters)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2259
       Stage 1 And 2 HPT Airseal ENGINE-STAGE 1 HPT AIR SEAL (OUTER) (72-45-12, 01-040), Knife-edge Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	294.16	Clear
       	294.56	0.46
       Seal Land Inside Diameter	295.02	1.63
       	295.78	Clear

12. SUBTASK 72-00-45-220-113 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2260. (Pre SBE 72-0180)

    NOTE

    There is no SBE 72-0180 condition at this location.

    1. Refer to Figure.

    2. Reference clearance at location 2260. If required, use the data written as a note in TASK 72-45-13-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

       Table 23. Fits and Clearances (all dimensions are in inches)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2260
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	8.927	Clear	8.921	Clear
       	8.933	0.022	8.933	0.022
       Seal Land Inside Diameter	8.955	0.038	8.955	0.038
       	8.965	Clear	8.965	Clear

       Table 24. Fits and Clearances (all dimensions are in millimeters)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2260
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	226.746	Clear	226.593	Clear
       	226.898	0.56	226.898	0.56
       Seal Land Inside Diameter	227.46	0.97	227.46	0.97
       	227.71	Clear	227.71	Clear

13. SUBTASK 72-00-45-220-114-A00 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2261 (Pre SBE 72-0511)

    1. Refer to Figure.

    2. Reference clearance at location 2261. If required, use the data written as a note in TASK 72-45-13-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

       Table 25. Fits and Clearances (all dimensions are in inches)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2261
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	9.027	Clear	9.021	Clear
       	9.033	0.022	9.033	0.022
       Seal Land Inside Diameter	9.055	0.038	9.055	0.038
       	9.065	Clear	9.065	Clear

       Table 26. Fits and Clearances (all dimensions are in millimeters)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2261
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	229.286	Clear	229.133	Clear
       	229,438	0.56	229.438	0.56
       Seal Land Inside Diameter	230.00	0.97	230.00	0.97
       	230.25	Clear	230.25	Clear

14. SUBTASK 72-00-45-220-114-B00 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2261 (SBE 72-0511)

    1. Refer to Figure.

    2. Reference clearance at location 2261. If required, use the data written as a note in TASK 72-45-13-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

       Table 27. Fits and Clearances (all dimensions are in inches)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2261
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	9.031	Clear
       	9.037	0.018
       Seal Land Inside Diameter	9.055	0.034
       	9.065	Clear

       Table 28. Fits and Clearances (all dimensions are in millimeters)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2261
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	229.39	Clear
       	229.54	0.457
       Seal Land Inside Diameter	230.00	0.864
       	230.25	Clear

15. SUBTASK 72-00-45-220-115-A00 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2262 (Pre SBE 72-0511)

    1. Refer to Figure or Figure.

    2. Reference clearance at location 2262. If required, use the data written as a note in TASK 72-45-13-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

       Table 29. Fits and Clearances (all dimensions are in inches)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2262
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	9.127	Clear	9.121	Clear
       	9.133	0.022	9.133	0.022
       Seal Land Inside Diameter	9.155	0.038	9.155	0.038
       	9.165	Clear	9.165	Clear

       Table 30. Fits and Clearances (all dimensions are in millimeters)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2262
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	231.826	Clear	231.673	Clear
       	231.978	0.56	231.978	0.56
       Seal Land Inside Diameter	232.54	0.97	232.54	0.97
       	232.79	Clear	232.79	Clear

16. SUBTASK 72-00-45-220-115-B00 Reference Fits and Clearances of the HP Turbine Rotor and Stator Assembly at Location 2262 (SBE 72-0511)

    1. Refer to Figure.

    2. Reference clearance at location 2262. If required, use the data written as a note in TASK 72-45-13-200-000 (INSPECTION-000) and TASK 72-44-50-200-000 (INSPECTION-000).

       Table 31. Fits and Clearances (all dimensions are in inches)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2262
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50, 01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	9.131	Clear	9.125	Clear
       	9.137	0.018	9.137	0.018
       Seal Land Inside Diameter	9.155	0.034	9.155	0.034
       	9.165	Clear	9.165	Clear

       Table 32. Fits and Clearances (all dimensions are in millimeters)

       	NEW PART		WORN PART
       	DIMENSIONS		DIMENSIONS
       PART IDENT	Size	Clearance	(Non-select)	REJECT IF MORE THAN
       LOCATION 2262
       Stage 1 HPT Airseal HPT Stage 1 Rotating Inner Air Seal And Damper (72-45-13, 01-020), Outside Diameter
       Stage 1 HPT Cooling Duct Assembly HPT Stage 1 Cooling (TOBI) Duct And Duct Deflector (72-44-50,01-010), Seal Land Inside Diameter
       Knife-edge Outside Diameter	231.927	Clear	231.775	Clear
       	232.080	0.457	232.080	0.457
       Seal Land Inside Diameter	232.54	0.864	232.54	0.864
       	232.79	Clear	232.79	Clear

17. SUBTASK 72-00-45-420-058 Install the Tooling to the HPT Rotor and Stator Assembly

    1. Refer to Figure and Figure.

    2. Install the IAE 1P16046 Removal/Installation fixture or IAE 1P16543 Removal/Installation fixture 1 off.

       1. Remove the cover from the Stage 1 Turbine Nozzle Assembly.

       2. Attach a standard two cable sling to the hoist rings on the fixture and attach the sling to a hoist.

       3. Release the hand knobs and move the center ring of the fixture to the rear until the flanged end is in line with the front surface of the hub of the fixture.

       4. Tighten two of the hand knobs (one in each row) to hold the center ring in this position.

       5. Lift the fixture and install onto the HP Turbine Rotor And Stator Assembly with the offset hole in the fixture over the dowel pin in the HP Turbine Case Flange. Remove the sling and the hoist.

       6. Attach the fixture with the two rings against the HP Turbine Case rear flange front face and the large offset hole over the flare of the dowel pin. Hold in position with the 25 bolts and nuts.

       7. Hold the center ring of the fixture and release the hand knobs.

       8. Move the center ring of the fixture down until it touches the rear face of the stage 2 Turbine Hub.

    3. Install the IAE 1P17022 Removal/installation jaws assembly 1 off.

       1. Install the four jaws into the Stage 2 Turbine Hub Bore.

       2. Move the jaws radially out so the lip on the jaws engages the groove on the hub and the socket head capscrews engage the flange of the fixture center ring.

       3. Install the jaw assembly sleeve into the jaws to move the jaws out.

       4. Align the slots in the sleeve with the large socket head capscrews.

       5. Install the sleeve until the flange contacts the jaws.

       6. Attach the jaws to the sleeve with the eight capscrews. Tighten the capscrews.

       7. Check to see if the HP Turbine Rotor And Stator Assembly is in the proper running position.

          1. NOTE

             Make sure when you take the measurements that the vernier does not go into the slots that are located on the hub flange.

             Measure the distance from the two machined areas of the fixture to the rear flange of the Stage 2 Hub. Use a depth vernier, Figure.

          2. To get dimensions D, add the two measurements together and do an average of total measurement.

          3. Subtract dimensions D from the dimension marked on the machined surface of the fixture.

          4. This dimension must be 1.194 in. to 1.214 in. (30.33 mm to 30.84 mm). This is the HP Turbine Assembly running distance.

          5. If necessary, adjust the center pedestal of the build stand to get this running distance dimension.

          6. Tighten the hand knobs on the hub of the fixture to hold the pedestal of the build stand in position.

    4. Install the scalloped plate, of the IAE 1P16272 Adapter 1 off, to the rear inner flange of the fixture and install and tighten the bolts.

    5. Attach the IAE 1F10052 Two cables sling 1 off to the turning spools on the fixture.

    6. Attach a hoist to the sling and lift the assembly.

    7. Turn the HP Turbine Rotor And Stator Assembly to the horizontal position.

18. SUBTASK 72-00-45-420-059 Get the No. 4 Bearing Spacer Dimension

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

    2. Measure the distance from the HP Turbine Case front flange front face to the front flange face of the stage 1 HP Turbine Airseal (inner). Write this dimension as dimension B.

    3. Measure the distance from the rear face of the stage 1 HP Turbine Support Assembly Flange to the rear face of the No. 4 bearing rear seal seat. Write this dimension as dimension C.

    4. Subtract dimension B from dimension C and the result will be the required No. 4 bearing spacer dimension.

       1. Usually, the necessary spacer will be a class 11 or 12. After you subtract dimension B from dimension C, if a different class is necessary, check the measurements and do the calculation again.

          1. Use the guidelines for correct bearing tolerances that follow so you can meet the final assembly check:

             1. If the C - B calculation results in a class 9 or 10 spacer - Install a class 11 spacer.

             2. If the C - B calculation results in a class spacer that is less than 9 - Install a class 10 spacer.

             3. If the C - B calculation results in a class 13 or 14 spacer - Install a class 12 spacer.

             4. If the C - B calculation results in a class spacer that is more than 14 - Install a class 13 spacer.

    5. Use the table to find the correct class of the spacer, refer to Figure.

       1. If the correct class spacer is not available, you can machine a larger (numerically higher) class spacer to a smaller (numerically lower) class spacer as follows:

          1. Find the necessary thickness from Figure and machine the spacer to that thickness. Refer to Figure for the machining requirements.

          2. After you have machined the spacer, mark the new class number at the location shown in Figure. Cross off old class marking. Refer to SPM TASK 70-09-00-400-501. Use vibration peen method. Remove high metal.

    6. Install the spacer (72-40-00, 03-003 thru 03-035) over the HP Compressor rear hub with the puller groove to the rear of the engine.

    7. The spacer must touch the No. 4 bearing rear seal seat.

    8. Position the spacer with the IAE 1P16470 Drift 1 off. Refer to Figure.

    9. Apply CoMat 10-129 ANTI-SEIZE PASTE to the mating surface on the HPC rear hub, Figure. Wipe off excess paste.

19. SUBTASK 72-00-45-420-060 Install the HP Turbine Rotor and Stator Assembly onto the Heater

    1. Refer to Figure.

    2. Remove the pin and remove the cover from the IAE 1P16040 Heater 1 off.

    3. 

       CAUTION

       REMOVE THE THERMOCOUPLE FROM THE HEATER BEFORE THE HP TURBINE ROTOR AND STATOR ASSEMBLY IS INSTALLED. IF THIS IS NOT DONE, DAMAGE TO THE THERMOCOUPLE MAY RESULT.

       Turn the HP Turbine Rotor And Stator Assembly to the front end down position and lower onto the heater until the case flange rests on the heater flange.

    4. Install the heater thermocouple to the heater and adjust the length to touch the rotor.

    5. Attach the heater to the IAE 6F10027 Heater control unit 1 off. Heat the HP turbine rotor and stator assembly to 400 °F (204 °C).

20. SUBTASK 72-00-45-420-061 Install the Puller into the HP Compressor Rear Hub

    1. Refer to Figure.

    2. Remove the puller rod if it is on the end of the IAE 1P17017 Puller 1 off.

    3. Install the puller to the HP Compressor rear hub.

       1. Turn the capscrew out to move the jaws into be in line with the surface of the puller.

       2. Install the puller to the HP Compressor rear hub until the stops touch the rear face of the hub.

       3. Install the puck onto the tool shaft and into the hub. Hold in place with the shaft nut. Tighten by hand only. Do not tighten too tight.

       4. 

          CAUTION

          YOU MUST MAKE SURE THE JAWS ARE FULLY EXTENDED TO THE LIMIT TO PREVENT DAMAGE TO THE ENGINE PARTS.

          Hold the shaft at the wrench flats and turn the capscrew into extend the jaws. The jaws will be fully extended when the capscrew can no longer move freely.

       5. Install the puller rod onto the puller shaft until the pin in the puller rod touches the capscrew in the puller shaft.

21. SUBTASK 72-00-45-420-062 Install the HP Turbine Rotor and Stator Assembly to the HP Compressor Rear Hub

    1. Refer to Figure.

    2. When the HP Turbine Rotor And Stator Assembly is at the correct temperature remove the heater thermocouple.

    3. Lift the assembly from the heater, turn to the horizontal position, and install over the puller and the HP Compressor rear hub.

    4. Align the dowel pin in the case flange with the offset hole in the diffuser case flange and the stage 1 HP Turbine Support Assembly and align the Stage 1 Turbine Hub Splines with the splines on the HP Compressor rear hub.

       1. Make sure the splines are engaged correctly.

          1. The hub splines are correctly engaged if the distance T is 0.625 in. (15.875 mm) or less. Refer to Figure.

          2. If the splines are correctly engaged, continue the installation procedure.

          3. If the splines are not correctly engaged, remove the HP Turbine Rotor And Stator Assembly and do the installation again.

    5. Install several bolts around the case flanges. Do not tighten the bolts.

    6. Install the threaded plate, of the IAE 1P16272 Adapter 1 off over the puller rod and into the scalloped plate detail of the adapter.

    7. Install the hydraulic cylinder with the threaded end away from the engine and attach with the washer and the nut.

    8. Attach the IAE 1F10026 Hydraulic hand pump 1 off to the hydraulic cylinder.

    9. Operate the hand pump and tighten the bolts in the flange to pull the HP Turbine Rotor And Stator Assembly into the proper position.

    10. NOTE

        Do not let the HP Turbine Rotor And Stator Assembly cool sufficiently before the installation has been completed.

        Apply a 30,000 lbf (133446.7 N) load with the hydraulic cylinder.

    11. Let the HP turbine disks cool to the touch with load on.

22. SUBTASK 72-00-45-420-063 Remove the Tooling from the HP Turbine Rotor and Stator Assembly

    1. Refer to Figure.

    2. Remove the hand pump, the hydraulic cylinder and the adapter.

       1. Release pressure on the hand pump. Remove the hand pump.

       2. Remove the nut and the washer from the puller rod and remove the hydraulic cylinder.

       3. Remove the threaded plate from the center of the scalloped plate.

       4. Remove the 12 bolts and remove the scalloped plate from the rear of the fixture.

    3. Remove the jaws assembly.

       1. Remove the eight capscrews which secure the sleeve to the jaws. Remove the sleeve.

       2. Release the large socket head capscrews and remove the four jaws from the fixture.

23. SUBTASK 72-00-45-420-064 Install the Bearing Retaining Nut

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

    2. NOTE

       This cover is used to prevent damage to the Rotor Assembly when the tools are installed to torque the bearing retaining nut.

       Install the IAE 1P17509 Protective cover 1 off to the rear flange of the HP Turbine Rotor And Stator Assembly.

    3. NOTE

       1. Bake step for the anti-galling compound after it has been applied is not necessary.

          The bearing retaining nut must be silver plated when you install or remove the nut more than five times or engine operation has occurred.

       Apply CoMat 10-031 ANTI-GALLING COMPOUND to the mating surface of the bearing retaining nut ENGINE-ATTACH PARTS & FITTINGS-HP SYSTEM (72-40-00, 04-020).

    4. Engage the slots of the retaining nut with the teeth of the IAE 1P16284 Hand wrench 1 off and install the bearing nut.

    5. Tighten the retaining nut hand tight with the hand wrench.

    6. Remove the hand wrench.

    7. Install IAE 1P17023 Torque adapter 1 off in the slots of the bearing retaining nut.

    8. Install the scalloped plate of the IAE 1P16272 Adapter 1 off over the puller rod and into the rear flange of the fixture.

    9. Attach the plate with the 12 bolts and tighten.

    10. Install the threaded plate of the adapter over the puller rod and into the scalloped plate of the adapter.

    11. Install the hydraulic cylinder over the puller rod with the hydraulic cylinder connector to the rear of the engine and attach with the washer and nut.

    12. Install the IAE 1P16341 Torque adapter 1 off over the hydraulic cylinder and engage the four pins in the flange holes of the torque adapter.

    13. Tighten the nut that attaches the hydraulic cyinder to the puller rod.

    14. Connect the IAE 1F10026 Hydraulic hand pump 1 off to the hydraulic cylinder.

    15. Apply a 30,000 lbf (133446.7 N) load to the hydraulic cylinder with the hand pump. Keep the hydraulic load on the cylinder until the torque is complete.

    16. Install a torque wrench into the rear of the torque adapter and torque the retaining nut to 500 lbfin (56.493 Nm).

        1. NOTE

           Keep the hydraulic load applied when you move the torque adapter to a new set of holes.

           If necessary to get the correct torque, remove the torque adapter and position the adapter into a new set of four holes in the IAE 1P17023 Torque adapter to provide the proper clearance with the hydraulic cylinder connector.

    17. Release the hydraulic load and disconnect and remove the hand pump.

    18. Remove the tooling from the HP Turbine Rotor And Stator Assembly.

        1. Remove the two torque adapters.

        2. Remove the nut and the washer from the puller rod and remove the hydraulic cylinder.

        3. Remove the threaded plate from the center of the scalloped plate.

        4. Remove the 12 bolts from the scalloped plate and remove the plate from the rear of the fixture.

        5. Remove the sling from the turning spools on the fixture.

        6. Attach a hoist to one of the two hoist rings on the fixture.

        7. Remove the bolts, the nuts and the two piece ring from the HP Turbine Case rear flange.

        8. Remove the fixture from the HP Turbine Rotor And Stator Assembly and put on a stand or a pallet. Remove the sling and the hoist.

        9. Remove the puller from the HP Compressor rear hub.

           1. Remove the puller rod from the puller shaft with two wrenches.

           2. Turn out, the hexagon head screws in the end of the puller shaft until the jaws are released.

           3. Remove the puller from the HP Compressor rear hub.

    19. Install the tools to do the last bearing retaining nut torque.

        1. Loosen the wingnuts on the four clamp assemblies on the IAE 1P17025 Adapter or IAE 1P17047 Adapter.

        2. Move the clamps in the clockwise direction (opposite direction of the arrows).

        3. Pull out the clamps until the clamp foot makes a continuous surface with the surface of the tooth on the adapter. Tighten the wingnuts to hold the clamps in this position.

        4. Attach a nylon strap to one of the slots in the side of the adapter and a hoist.

        5. 

           CAUTION

           TURN THE ADAPTER TO LOCATE THE SLOTS WITH THE LOCKS BETWEEN THE TEETH OF THE ADAPTER. MAKE SURE THE SLOTS AND THE TEETH OF THE ADAPTER ARE ALIGNED TO PREVENT DAMAGE TO THE SIDES OF THE SLOT.

           Lift the adapter in position and engage the teeth of the adapter with the slots of the Stage 2 Turbine Hub.

        6. Loosen the wing nuts and push the clamps in until the clamp foot touches the hub.

        7. Move the clamp assemblies in the counterclockwise direction (direction of arrows) and tighten the wingnuts.

        8. Install the IAE 1P16011 Wrench 1 off through the adapter to engage the retaining nut splines.

        9. NOTE

           You can use IAE 1F10016 Mechanical wrench as an alternative to IAE 1F10015 Hydraulic wrench.

           Attach a hoist to the IAE 1F10015 Hydraulic wrench 1 off and install over the wrench.

        10. Engage the anti-rotation pins on the wrench with the holes in the adapter. Tighten the hexagon head bolts to attach the wrench to the adapter.

    20. Torque the bearing retaining nuts with the hydraulic wrench.

        1. Turn the retaining nut an angle of turn of 80 degrees plus or minus two degrees.

    21. Remove the bearing retaining nut tools.

        1. Loosen the hexagon head bolts and remove the hydraulic wrench from the adapter.

        2. Remove the wrench from the nut.

        3. Loosen all the wingnuts on the clamp assemblies.

        4. Move the clamp assemblies in the clockwise direction (opposite direction of the arrows).

        5. Pull the clamps assemblies out and tighten the wingnuts, touches the hub.

        6. Remove the adapter from the Stage 2 Turbine Hub.

    22. Install the No. 4 bearing lock ENGINE-ATTACH PARTS & FITTINGS-HP SYSTEM (72-40-00, 04-060).

        1. 

           CAUTION

           THE NO. 4 BEARING LOCK CAN BE INSTALLED IN THREE DIFFERENT POSITIONS WHEN YOU LOOK FROM THE REAR OF THE ENGINE. IF THE LOCK IS NOT INSTALLED IN THE CORRECT POSITION, THE BEARING RETAINING NUT CAN BECOME LOOSE.

           NOTE

           This position will keep the bearing retaining nut at the correct torque.

           Position and install the clockwise side of the rear lock tabs nearest to the counterclockwise side of the tabs on the bearing and install the lock.

    23. Install the retaining ring ENGINE-ATTACH PARTS & FITTINGS-HP SYSTEM (72-40-00, 04-040) to attach the lock in position.

    24. Remove the protective cover.

    25. NOTE

        The tool bolts and nuts must be removed as the engine bolts and nuts are installed.

        Install all the bolts and nuts and the brackets to the HP Turbine Case front flange.

    26. Torque the nuts to 180 lbfin to 200 lbfin (20.337 Nm to 22.597 Nm).

24. SUBTASK 72-00-45-220-217 Examine the HPC Rear Shaft for Surface Damage

    1. Refer to Figure.

    2. Examine the rear shaft inner bore at the inspection area given in the figure.

       1. Surface damage not more than 0.003 in. (0.08 mm) in depth.

          1. Accept.

       2. Other than Step.

          1. Reject.

25. SUBTASK 72-00-45-220-116 Check the HP Turbine Assembly Running Distance

    1. Refer to Figure.

    2. Load the HP turbine assembly as follows:

       1. Install the IAE 1P16187 Loading fixture 1 off to the rear of the HP turbine.

       2. Attach the stage 2 HP Turbine Support rear flange face with the 12 socket head capscrews, through the rear flange from the front, and the nuts.

       3. Turn the handle to push the ring which touches the stage 2 turbine hub rear face and apply a load of 700 lbs to 1000 lbs (3113.8 N to 4448.2 N) on the fixture gage.

    3. Install the IAE 1P17515 Gage 1 off.

       1. Before the checking fixture is used, move the digital indicator to the machined area on the gage and set the digital indicator to zero. The dimension of the indicator rod when the digital indicator is zero is 1.194 in. (30.328 mm).

       2. With the correct load put on the HP Turbine, install the fixture to the rear of the turbine with the end position in the slots of the loading fixture and the digital indicator rod on the Stage 2 Turbine Hub Lug End Faces.

       3. Measure the distance to the lugs on the Stage 2 Turbine Hub at three equally spaced positions.

          1. At each measurement, add or substract the digital indicator reading to the 1.194 in. (30.328 mm) dimension.

          2. Average the three measurements.

          3. The running distance must be 1.194 in. to 1.214 in. (30.33 mm to 30.84 mm).

    4. Remove the gage and the loading fixture from the rear of the HP Turbine Assembly.

    5. Install the IAE 1P16060 Protective cover 1 off or the IAE 1P17758 Protective cover 1 off to the rear flange of the HP turbine rotor and stator assembly. Put equal hand pressure on the outer edge of the cover to hold in position.

26. SUBTASK 72-00-45-220-221 Examine the Stage 2 Turbine Hub for Damage

    1. Examine the Stage 2 Turbine Hub for dents, nicks and scratches that occurred during the assembly process.

       1. Dents, nicks and scratches.

          1. Diassemble. Refer to TASK 72-00-45-020-001-B01; then Repair, VRS3238 TASK 72-45-31-300-001 (REPAIR-001).

Figure: Pre SBE 72-0180, Pre SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances

Pre SBE 72-0180, Pre SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances



Figure: Pre SBE 72-0180, Pre SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances

Pre SBE 72-0180, Pre SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances



Figure: SBE 72-0180, SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances

SBE 72-0180, SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances



Figure: SBE 72-0180, SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances

SBE 72-0180, SBE 72-0511: The HP Turbine Rotor and Stator Assembly - Fits and Clearances



Figure: HP Turbine Assembly and Related Parts

HP Turbine Assembly and Related Parts



Figure: Installation Tooling for the HP Turbine Assembly

Installation Tooling for the HP Turbine Assembly



Figure: Engine Dimension

Engine Dimension



Figure: Pre SBE 72-0180: HP Turbine Assembly Dimensions

Pre SBE 72-0180: HP Turbine Assembly Dimensions



Figure: SBE 72-0180: HP Turbine Assembly Dimensions

SBE 72-0180: HP Turbine Assembly Dimensions



Figure: Thickness of Spacer

Thickness of Spacer



Figure: Machine the Thickness of the Spacer

Machine the Thickness of the Spacer



Figure: No.4 Bearing Spacer Installation

No.4 Bearing Spacer Installation



Figure: Install the HP Turbine Assembly onto the Heater

Install the HP Turbine Assembly onto the Heater



Figure: Puller Installed in HP Compressor Rear Hub

Puller Installed in HP Compressor Rear Hub



Figure: Install the HP Turbine Assembly to the Engine

Install the HP Turbine Assembly to the Engine



Figure: Bearing Retaining Nut

Bearing Retaining Nut



Figure: Install the Bearing Nut Tooling

Install the Bearing Nut Tooling



Figure: Retaining Nut Angle of Turn Tooling

Retaining Nut Angle of Turn Tooling



Figure: Hydraulic Wrench Package

Hydraulic Wrench Package



Figure: HPC Rear Shaft Inspection Location for Surface Damage

HPC Rear Shaft Inspection Location for Surface Damage



Figure: Install the Load Fixture and Gage

Install the Load Fixture and Gage