MAL_0325

WORK ITEM 1: 2950-01-118-7979, Turbocharger, Repair

1. SCOPE

1.1 Intent. This specification covers the requirements for the receipt, disassembly, inspection, condition/test reports, overhaul, reassembly, testing, preservation, packing and marking of Alco

Turbochargers used on U.S. Coast Guard 251 Series Alco Diesel Engines.

1.2 Government-furnished property.

MTI ITEM DESCRIPTION NSN

P/N

QTY

(EA.)

APPLICATION

Y ***Turbocharger, Model 165

NSN: 2950-01-118-7979

PN: 22602128-2

1 WMEC 270 A/B

*Government-loaned property, which shall be returned to the Coast Guard upon completion of the contract.

**New or refurbished equipment that the Government may provide for installation in place of existing equipment.

***Government-furnished property, which is to be supplied by the Coast Guard.

2. REFERENCES

COAST GUARD DRAWINGS

None

COAST GUARD PUBLICATIONS

None

OTHER REFERENCES

Alco Maintenance Manual MI-11209A for Turbocharger Model 165 Dated May 1973

ASQ/ANSI/ISO 9001, Dated 20 Nov 2015, Quality Management Systems - Requirements

ASTM D7478/D7478MD6251M, Dated 1 Nov 2011 (R2017), Standard Specification for Heavy

Duty Sheathed Wood Crates

ISO/IEC 16388-2007, May 15 2007 Information technology — Automatic identification and data capture techniques — Code 39 bar code symbology specification

ISO/IEC 17025:2017, Dated 2017, General Requirements for the Competence of Testing and

Calibration Laboratories

MIL-PRF-21260E Dated July 31, 1998 Lubricating Oil, Internal Combustion Engine, Preservative Break-In

MIL-PRF-16173E w/ Int. Amendment 1, Sep 2006, Corrosion Preventive Compound, Solvent

Cutback, Cold- Application

MIL-STD-129R, 27 Sep 2019 Military Marking for Shipment and Storage

MIL-STD-2073-1E Change 4, 22 Apr 2019 Standard Practice for Military Packaging

NAVSEA T9074-AS-GIB-010/271, Dated February 16, 1999, Requirements for Nondestructive

Testing Methods.

NAVSEA TT-P-28H, Dated 1 Jul 2021, Coating, Heat Resisting

SAE AMS-STD-595A, Dated Feb 2017, Colors Used in Government Procurement

SSPC-PAINT 25, Dated May 1, 1997, Editorial Changes November 1, 2004, Zinc Oxide, Alkyd, Linseed Oil Primer for Use Over Hand Cleaned Steel (Without Lead and Chromate

Pigments-Red Iron Oxide)

2.1 Document availability. The documents listed in this section are referenced in sections 3, 4 and 5 of this work item and drawings stated in this Work Item. To obtain the referenced documents see section

6.1.

2.2 Specification order of precedence. The Applicable Documents described are required to be adhered to in fulfilling the contract. In the event of a conflict between the text of this specification and the references cited herein, this work item shall take precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

3. REQUIREMENTS

3.1 General. Inspections, repair/overhaul and testing of each turbocharger shall be accomplished in accordance with all applicable documents listed in section 2.0 of this specification.

3.1.1 Tech rep.

None.

3.2 Government furnished property (GFP). The Contractor shall provide protective storage for the GFP when not in use, and safe handling when in use.

3.2.1 The storage area shall at a minimum be closed on all sides, dry, and locked when the equipment is not in use.

3.3 Arrival inspection/disassembly inspection. Each turbocharger received by the Contractor shall be disassembled and inspected. A detailed report shall be completed and submitted to the Contracting

Officer to include the following information:

• Date of inspection

• Inspectors name

• Identification of units by serial number, part number, and stock number

• Condition of the shipping crate and any cost of repair

• List Mandatory parts as priced in the contract as one line and a total price (Appendix A)

• List of contingency parts by part number & CLIN, and their applicable prices (Appendix B)

• Cost of overhaul labor as applicable

• Comments if any pertaining to unusual observations during inspection & disassembly

• Dimensional inspection of bearing bores, rotor shaft journal areas, seal areas, disc fit and impeller fit areas using clearance table in Appendix C and D as applicable

• A list of defective or worn parts recommended for repair/refurbishment vice replacement and the associated cost to accomplish

• If not previously condemned, each rotor disk, impeller, inducer, and gas inlet of each turbocharger shall be dye penetrant tested in accordance with NAVSEA T9074-AS-GIB-

010/271 and the results provided in the initial report with discrepancies highlighted

3.3.1 No further work shall be accomplished until the report is approved by the Contracting Officer.

3.4 Overhauls. Each turbocharger shall be overhauled in accordance with the documents cited in section

2.0 and appendices A through C as applicable.

3.4.1 Replacement parts. All replacement parts shall be new and manufactured in accordance with Alco specifications and standards, the Original Equipment Manufacturer (OEM).

3.4.1.1 Defective or worn parts may be repaired/refurbished if the Contractor deems it more economical than replacement. The performance and function of the repaired parts shall be equal to that of a new part.

A listing of all parts recommended for repair shall be part of the Arrival Inspection as required in section

3.3 of this specification.

3.4.1.2. Metallic ID Plate. If the metallic ID Plate is missing or ineligible it shall be replaced with a new

ID Plate. New Metallic ID Plates shall be marked with the Serial Number, Part Number, Model Number, Size and OEM information.

3.4.2 Mandatory repairs. The following shall be accomplished on each turbocharger inducted for repair/overhaul:

• Cleaning/repairing of all bolt holes

• Rotor Balancing

• Installation of Mandatory Replacement Parts

• Cleaning and Painting (see section 3.6)

3.5 Mandatory replacement parts. The following parts are mandatory to replace.

• Model 165 as per Appendix A

3.6 Surface cleaning & painting.

3.6.1 Cleaning.

• All scale and paint shall be removed

• All surfaces shall be solvent cleaned of all grease and oil

3.6.2 Painting.

3.6.2.1 These items shall be masked or plugged and not painted:

• Oil inlet and drain openings

• Hoses, hose connections or openings

• Identification plate

• Air inlet and discharge openings and flanges, exhaust inlet and discharge openings and flanges

• Water inlet and discharge openings

• Any other openings that will permit foreign material to enter the turbocharger

3.6.2.2 All external areas not exposed to temperature that normally exceeds 300 degrees F., while turbocharger is in operation, shall be coated as follows:

• One coat, 2-3 mils thickness with Primer in accordance with SSPC-PAINT 25

• Two coats, at least 2 mils thick total, of high gloss Equipment Enamel, MIL-E-15090C, Formula 111, Type I, Class 1, light gray, Color No. 16492 per SAE-AMS Standard 595

3.6.2.3 All external surfaces normally exposed to temperatures that exceeds 300 degree F. shall be painted with 2 coats, 2 mils total thickness of Heat-Resistant Aluminum Paint, NAVSEA Specification TT-P-28H

3.6.2.4 When all paint is dry, the masking shall be removed.

3.7 Reassembly report/test report. The Contractor shall submit a Reassembly Report/Test Report to the

Contracting Officer for approval.

3.7.1 The Reassembly Report/Test Report shall include all inspections and tests specified herein and all other inspections and tests needed to verify conformance to the requirements.

3.7.2 The Reassembly Report/Test Report shall include (unless otherwise noted), but not be limited to:

• Time and date of test or inspection

• A chronological listing of the tests and inspections performed

• Step-by-step inspection procedures for the assembly and pass/fail criteria

• Assembly dimensions, tolerances, thrust, adjustments, torque specs, and balance records observed, and all deficiencies found and the corrective action taken. Any deficiencies noted shall be highlighted

• A complete listing of all measuring test equipment (MTE) used with MTE serial numbers

• Dimensional inspection report with tolerances. Any deficiencies noted shall be highlighted

• Rotor assembly balance record, with tolerances o The rotor assemblies shall be spun-balanced at the OEM recommended RPM.

o The rate of unbalance for each model of Turbocharger shall not exceed the following

Specified amounts.

▪ Model 165 - 0.02 in. oz.

• Date and signatures of test or inspection personnel

• Signature of Government witness, if any

3.8 Notifications & inspections. The Contractor shall notify the Contracting Officer a minimum of ten

(10) calendar days prior to any inspections or testing required herein.

4. QUALITY ASSURANCE

4.1 Responsibility for inspection. The Contractor shall be responsible for the performance of all inspection requirements specified herein. The Contractor shall provide space, personnel and test equipment for the conduct of all inspection requirements. All inspection and testing shall be performed at the Contractor's plant or at other facilities acceptable to the Coast Guard. The Coast Guard reserves the right to verify or have performed any of the inspections set forth in this specification where such inspections are deemed necessary to assure that supplies and services conform to the prescribed requirements.

4.2 Responsibility for compliance. All items shall meet the requirements of sections 3 and 5. The inspections set forth in this specification shall become part of the contractor's overall inspection system or quality program. The absence of any inspection requirements in this specification shall not relieve the contractor of the responsibility of assuring that all products or services submitted to the government for acceptance comply with all requirements of the contract. Sampling for quality conformance does not authorize submission of known defective material (either indicated or actual) nor does it commit the government to acceptance of defective material.

4.3 Quality system. The contractor shall maintain a documented Quality System in accordance with

ASQ/ANSI/ISO 9001. A copy of this program shall be submitted to the Contracting Officer for approval within 15 calendar days after contract award.

4.4 Inspections. The inspections required herein are the minimum required and are not intended to replace any controls, examinations, inspections or tests normally employed by the Contractor to assure the quality of the equipment. The following are required and will be monitored by a Government Quality Assurance

Representative.

4.4.1 Rotor balancing inspection in accordance with section 3.7.2.g of this specification

4.4.2 Preservation, packing, and marking in accordance with section 5.0 of this specification.

4.5 Calibration system. The Contractor shall maintain a test equipment calibration program conforming to

ISO/IEC 17025:2017. The Contractor shall have a copy of the calibration program readily available during the term of this contract for review by any Coast Guard personnel upon request.

4.5.1 Calibration system records. The calibration system records shall be maintained for inspection for the duration of any contract referencing this specification.

4.6 Noncompliance. Shall mean any single failure of any individual part or subsystem during inspection or testing.

4.6.1 The Contractor shall replace the failed part with new and continue testing.

4.6.2 If, during assembly any noises, rubbing, or grinding are heard or felt indicating potential problems the entire test procedure shall be repeated after replacement of the failed part(s).

4.6.3 Any flaws detected in materials or construction methods which reduces the usefulness of the turbochargers to the Coast Guard shall be resolved before completing any further work.

4.6.4 Any unusual noises or other non-compliances, as determined by the Coast Guard Inspector, will require re-testing and shall be cause for failure.

4.7 Test and inspection reports. One copy of any inspection or test report approved for use from submittal shall be sent to the Contracting Officer for approval. A copy shall also be given to the Coast Guard

Quality Assurance Representative upon his arrival at the Contractor's facility.

4.8 Records. The Contractor shall maintain records by serial number of all inspections and tests.

4.8.1 The records shall indicate the nature and number of observations made, the number and type of deficiencies found, and the corrective action taken.

4.8.2 Copies of all records shall be maintained for Coast Guard inspection at any time during the duration of any Contract referencing this specification.

4.9 Discarded parts. All parts scrapped by the Contractor shall be saved until rendered scrap by a Coast

Guard representative.

4.10 Packing inspection. The Contractor shall notify the Contracting Officer a minimum of ten (10) calendar days prior to the scheduled preservation, packing, and marking of the completed units.

5. PRESERVATION, PACKAGING, PACKING, MARKING, AND SHIPPING

5.1 General. Each Turbocharger shall be cleaned, preserved, packaged, packed, marked and bar-coded as specified herein. Preservation, packaging, packing, marking and bar-coding will be inspected by SFLC

QA personnel at Contractor’s facility.

5.2 Preservation. The Contractor shall preserve all Turbochargers in accordance with MIL-SPEC-2073-

1E, Method 20.

5.2.1 Internal.

5.2.1.1 Internal oil passages and bearings shall be spray/fogged and drained with Code 10, Grade 30 preservative as specified by MIL-STD-2073-1E APPENDIX J, TABLE J.III.

5.2.1.2 Internal water passages shall be spray/fogged and drained with Grade 3 preservative as specified by MIL-PRF-16173E(SH).

5.2.2 External. Unpainted surfaces shall be coated with Code 19, Grade 4, corrosion preventative as specified by MIL-STD-2073-1E APPENDIX J, TABLE J.III.

5.2.2.1 All fittings or openings that would allow foreign material to enter the unit shall be plugged or capped.

5.2.2.2 All pipe plugs must have the plugs removed. The hole and plug threads shall be cleaned with a tap and dye set. The pipe plug shall be replaced as a Contingency Item, if necessary. All pipe plugs shall be reinstalled and hand tightened. Red tag shall be applied to unit identifying plugs as being hand tight only.

5.2.2.2.1 VPI paper shall be placed between the flanges and the bolted on cap.

5.3 Packing. Each Turbocharger shall be individually packed in its own wooden box in accordance with accordance with ASTM D7478/D7478M, Class 2, Style A.

5.3.1 Top, side and end panels shall be fabricated and assembled (screwed vice nailed) to each other as specified for Type I, and the combination fastened (bolted) to skid as specified for Type II.

5.3.2 Each turbocharger shall be supplied with a gasket installation kit to facilitate installation using the correct gaskets and seals. This kit shall be made part of the package. The contents shall be in a plastic bag and placed in a cardboard and clearly marked “installation gasket kit”.

5.4 Marking. Shipping container shall be stenciled with the information laid out below. Markings shall be placed on each side of the two longest sides of the container so it will be visible to a forklift driver during storage and shipment. Stencil shall be applied directly on the container and a minimum of 1inch height black characters on a highly contrasting painted background, using permanent waterproof ink or enamel paint. Marking is in accordance with MIL-STD-129R.

5.4.1 All previous markings and labels shall be completely removed from the reusable shipping container prior to the applications of any new markings.

5.4.2 Marking layout (ready for issue) “A” condition Model 165 turbocharger.

NATIONAL STOCK NUMBER

2950-01-118-7979

ITEM NAME

TURBOCHARGER

MODEL NUMBER

PART NUMBER

22602128-2

SERIAL NUMBER

As per enclosed item

CONTRACT NUMBER (See Contract)

DELIVERY ORDER NUMBER

(See Contract)

SHIPPING DATE

"The Delivery Date to SFLC"

WARRANTY EXPIRATION

DATE

As Determined by Contractor

SHIPPING WEIGHT (LBS)

As Determined by Contractor

QUANTITY & UNIT OF ISSUE 1 - EA

CONDITION

CONDITION A

OTHER DATA AS DIRECTED

COAST GUARD SFLC MATERIAL

REUSABLE CONTAINER, DO NOT

DESTROY,

REMOVE BOLTS, LIFT CRATE FROM

SKID.

5.5 Bar coding. U.S. Coast Guard requires bar coding of the NSN, IAW ISO/IEC 16388-2007 Code 39

Symbology.

5.5.1 Bar coding label. Can be applied separately or as part of the marking required in 5.4.

5.6 Shipping. The Contractor shall ship and deliver the repaired diesel engine turbocharger to the government address specified in paragraph. 5.6.1 Notice the Contracting Officer representative (COR) and KO about the shipment 7 days in advance. Provide timely shipping information to COR including the name of the shipping company, date of shipment leaving Contractor’s facility, and expecting arrival date and time at the government facility. No shipment shall arrive outside of government normal business hours as determined by the KO.

5.6.1 Unless otherwise specified, the Contractor shall ship, and deliver the diesel engine turbocharger(s) to the following government address:

U.S. Coast Guard

Surface Forces Logistics Center

2401 Hawkins Point Rd, Bldg. 88

Baltimore, MD 21226

NOTE

Normal deliver hours at the warehouse are Monday through Friday 0730-

1300. If delivery is needed to be made outside that delivery window the

Contractor shall notify the Contracting Officer.

6 NOTES

6.1 Document sources.

6.1.1 Government document sources.

• Department of Defense Single Stock Point (DODSSP)

Building 4, Section D

700 Robbins Avenue

Philadelphia, PA 19111-5094

215-697-2667/2179

FAX 215-697-1462

• DOD & Navy Publications & Forms (Other Than DODSSP)

Naval Publication and Forms Center

5801 Tabor Ave.

Philadelphia, PA 19120

215-697-2000

• ASSIST (Database for Military Specifications) https://assist.dla.mil/online/start/ http://quicksearch.dl.mil Assist Service Desk: PH: 215-737-8000 https://assist.dla.mil/online/start/ http://quicksearch.dl.mil/

• USCG Surface Forces Logistics Center

2401 Hawkins Point Road

Baltimore, MD. 21226-5000

Phone: 410-762-6474

ATTN: Yvette Rene Johnson

6.1.2 Commercial document sources.

• American National Standards Institute (ANSI)

1899 L St. NW 11th Floor

Washington, DC 20036

Phone: 202-293-8020 www.astm.org

• American Society for Quality (ASQ)

600 North Plankinton Avenue

Milwaukee, WI 53203

Phone: 414-272-8575

Fax: 414-272-1734

• ASTM International

1916 Race Street

Philadelphia, PA 19103-1187

Phone: 215-299-5585

Fax: 215-977-9679

• International Standard Organization (ISO)

1, ch. De la Voie-Creuse

CP 56 - CH-1211 Geneva 20

Switzerland

Phone: +41 22 749 01 11

Fax: +41 22 733 34 306.1

• Society for Protective Coatings

Steel Structures Painting Council (SSPC)

800 Trumbull Drive

Pittsburgh, PA 15205

PH: 412-281-2331

http://www.astm.org/

APPENDIX A

MANDATORY REPLACEMENT PARTS - MODEL 165

Part Number Description Quantity

21526719-1 O-Ring 1

2153654-2 Gasket, Connector 8

2154432-2 Gasket, Cover Plate 2

215267260 (21526726) O-Ring 1

226120213 (22610213) Shim, Turbo to Support 1

22610223-1 Ship, Air Seal 1

22610224 Shim, Bearing Carrier 1

22610225-1 Shim, Oil Seal 1

22611310-1 Thrust Washer, Small 1

2261139-1 Thrust Washer 1

2612012-1 (22612012-1) Bearing 1

22612120-1 Oil Seal 1

22612121-1 Oil Seal 1

2261527-1 Floating Bushing 2

2261631-1 Air Seal 1

APPENDIX B

CONTINGENCY REPLACEMENT PARTS - MODEL 165

Part Number Description Quantity

24023642 Elbow 2

16393718 Pipe Plug 1

1639374 Pipe Plug 1

16394015-1 Tube 1

21511010-1 Dowel 1

21512863 Capscrew 8

2151312-1 Lockwasher 24

2151313-1 Lockwasher 41

2151319-1 Lockwasher 4

21513513-1 Capscrew 20

21514218 Stud 21

2151495-1 Washer 4

2151697-1 Nut 21

21517741 Guide Pin 3

21517744-1 Dowel 6

2152866 Capscrew 10

21529624 Machine Screw 2

2154765 Straight Dowel 2

2154961 Capscrew 6

2154962 Capscrew 8

21549629 Capscrew 13

21549632 Capscrew 6

21549549 Capscrew 8

21549715 Capscrew 10

21553616 Capscrew 4

21555893 Capscrew 24

22600723 Blower Casing 1

22600434 Gas Inlet Casing 1

22600722 Blower Casing 1

22600437 Gas Inlet Casing 1

22600526-4 Rotor 1

22600540-2 Rotor 1

2260161-1 Bearing Assembly 1

2260162-1 Bearing Assembly 1

22610459-1 Nozzle Clamp Ring 1

22610460 Diffuser 1

22610464-1 Air Nozzle 1

22610480-2 Nozzle Ring 1

22610533 Air Inlet Casing 1

22610534 Air Inlet Casing 1

22611311-1 Retainer Washer 1

2261221-2 Dowel 2

2261222-1 Dowel 2

22612312 Bearing Retainer 1

2261237 Bearing Retainer Ring 1

2261238 Retainer Ring 1

2261239 Retainer Ring 1

22612710-1 Main Casing 1

22613011-2 Cover Plate 1

22613012-1 Cover Plate 1

2261474-1 Bearing Carrier 1

2261476-2 Bearing Housing 1

2261477-1 Bearing Carrier 1

2261614 Shroud Ring 1

2261674 Diffuser 1

2401298-1 Tube Clamp 1

4401079 Tube Clamp 1

APPENDIX C

TABLE OF CLEARANCES FOR MODEL 165

REFER TO ILLUSTRATION #3

Measurement Location Minimum Maximum

1) Nozzle Ring and Gas Inlet Casing (Outside) Dia. Cl. 0.085” 0.105”

2) Nozzle Ring and Gas Inlet Casing (Inside) Dia. Cl. 0.002” 0.008”

3) Turbine Disc and Oil Seal Long. Cl. 0.018” 0.024”

4) Turbine End Oil Seal and Main Casing Dia. Cl. 0.0005” 0.0035”

5) Shaft and Bearing Carrier Long. Cl. 0.085” 0.132”

6) Shaft and Oil Seal Dia. Cl. 0.020” 0.025”

7) Bearing Outer Race and Floating Bushing Long. Cl. 0.006” 0.020”

8) Shaft and Carrier Shaft and Outer Race Dia. Cl. 0.015” 0.018”

9) Bearing Carrier and Main Casing Dia. Cl. 0.0005” 0.0010”

10) Air Nozzle and Shaft Long. Cl. 5/16” ¼”

11) Turbine Disc and Oil Seal (Radial Clearance) Rad. Cl. 1/8”

12) Nozzle Ring and Clamp (Inner) Dia. Cl. 0.035” 0.047”

13) Nozzle Ring and Clamp (Outer) Dia. Cl. 0.035” 0.055”

14) Nozzle Ring and Shroud Long. Cl. 0.015” 0.022”

15) Shroud Ring and Main Casing (Inside) Dia. Cl. 0.002” 0.006”

16) Bearing Housing and Retaining Washer Rad. Cl. 0.005” 0.0065”

17) Impeller and Main Casing Dia. Cl. 0.230” 0.238”

18) Diffuser and Air Discharge Casing

(Cold)

Dia. Cl. 0.002” 0.010”

19) Impeller and Casing b. Datum - 0.005 0.005”

20) Air Discharge Casing and Impeller Cl. 0.045” 0.078”

21) Inducer and Air Discharge Casing Dia. Cl. 0.060” 0.070”

22) Oil Slinger and Oil Seal Dia. Cl. 0.016” 0.021”

23) Thrust Washer and Bearing Housing Dia. Cl. 0.002” 0.005”

24) Bearing Carrier and Main Casing Dia. Cl. 0.001” 0.005”

25) thrust Washer and Shaft Dia. Cl. 0.059” 0.064”

26) Retainer and Floating Bushing Dia. Cl. 0.040” 0.055”

27) Oil Slinger and Floating Bushing Dia. Cl. 0.0030” 0.0045”

28) Oil Slinger and Bearing Housing Dia. Cl. 0.015” 0.021”

29) Bearing Carrier and Shaft Dia. Cl. 0.018” 0.021”

30) Thrust Washer and Thrust Collar Long. Cl. 0.005” 0.012”

31) Retainer Washer and Bloating Bushing Long. Cl. 0.006” 0.030”

32) Retainer Washer and Retainer Long. Cl. 0.006” 0.020”

33) Retainer and Bearing Housing Int. 0.000” 0.0015”

34) Main Casing and Bearing Housing Dia. Cl. 0.002” 0.006”

35) Thrust Washer and Bearing Carrier Dia. Cl. 0.0025” 0.0070”

36) Floating Bushing and Outer Race Dia. Cl. 0.0040” 0.0055”

37) Floating Bushing and Shaft Dia. Cl. 0.0030” 0.0045”

38) Outer Race and Bearing Carrier Int. 0.0000” 0.0015”

39) Retaining Ring and Shaft Dia. Cl. 0.015” 0.018”

40) Impeller and Inducer Long. Cl. 0.010” 0.020”

41) Air Seal and Impeller Long. Cl. 0.014” 0.020”

42) Main and Air Discharge Casing Dia. Cl. 0.001” 0.005”

43) Main and Air Discharge Casings (Nuts Loose) Dia. Cl. 0.004” 0.014”

44) Main and Gas Inlet Casings Dia. Cl. 0.002” 0.008”

45) Turbine Disc and Shroud Dia. Cl. 0.062” 0.070”

46) Nozzle ring Clamp Long. Cl. 0.000” 0.006”

47) Nozzle ring and Turbine Disc Tablock Dia. Cl. 0.020” 0.070”

Note: All diametrical clearances to be equalized radially.

APPENDIX D

MODEL 165 TURBOCHARGER ROTOR ASSEMBLY TABLE OF CLEARANCES

REFER TO ILLUSTRATION #4

1. Turbine Disc 7. Ring Nut 12. Turbine Blade

2. Shaft 8. Lockwasher 13. Ferrule

3. Thrust Collar 9. Blower End Oil Slinger 14. Stub Shaft

4. Air Impeller Slinger (Screw type) 15. Nut and Cotter Pin

5. Inducer 10. Impeller Insert 16. Key

6. Nose Piece 11. Tablock

Measurement Location Minimum Maximum

A) Ferrule and Stub Shaft and Ferrule and Turbine

Disc

Dia. Cl. 0.005” 0.010”

B) Turbine Disc and Shaft Int. 0.000” 0.002”

C) Air Impeller and Inducer Long.

Cl.

0.010” 0.020”

D) Air Impeller and Inducer Int. 0.000” 0.002”

E) Bearing Sleeve and Shaft Dia. Cl. 0.0116” 0.0169”

F) Nose Piece and Shaft Dia. Cl. 0.0000” 0.0006”

G) Air Impeller Insert and Shaft Dia. Cl. 0.0000” 0.0006”

H) Oil Slinger and Shaft Int. 0.0000” 0.0006”

I) Thrust Collar and Shaft Dia. Cl. 0.0003” 0.0009”

J) Inducer and Shaft Dia. Cl. 0.029” 0.079”

K) Key and Impeller Insert Long.

Cl.

0.0005” 0.0085”

L) Key and Impeller Insert Long.

Cl.

0.000” 0.004”