Attachment 0010 - AED CSI AX9M9025AX.pdf

07/09/2018

7-114110011 3110 01 179 - 7335

N NN

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, Roller, TaperedNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

7-211411089 5315 01 163 - 4614

Y NN Age per AMS5844

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Pin, Link Attach, M/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/15/1989CSI Date

7-211411089-3 5315 01 433 - 8524

Y

N

N

N

N

Y

Heat treat and Age per AMS5844

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Pin, Link Attach, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-211411149-5 -

Y NN Assembly contains Critical Safety Items

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Strap Assy, M/R HubNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

01/09/2002CSI Date

7-211411149-7 -

Y NN Assembly contains Critical Safety Items

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Strap Assy, M/R HubNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

11/17/2000CSI Date

7-211411150-5 1615 01 434 - 1505

Y NN Fabricate per EPB 4-231 (NOTE 9)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Straps, Matched Set, M/R HubNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-211411150-9 1615 01 434 - 1506

Y NN Fabricate per EPB 4-231 (NOTE 9)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Straps, Matched Set, M/R HubNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

03/30/1995CSI Date

7-211411155-29 3040 01 433 - 8522

Y NY Shot peening

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Link, Lead LagNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

03/30/1995CSI Date

7-211411155-31 3040 01 433 - 8523

Y NY Shot peening

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Link Assy, Lead LagNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

03/30/1995CSI Date

7-211411186-5 3120 01 170 - 5299

N NN

09455

97613

RBC Transport Dynamics Corporation

Sargent Aerospace & Defense, LLC

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, Plain, Rod EndNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

7-211411199 1615 01 163 - 4514

Y NY Assembly contains CSI. See P/N 7-211411089-3 for CCs.

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Pin Assy, Link AttachNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/15/1989CSI Date

7-211411199-3 1615 01 163 - 4514

Y NY Assembly contains CSI. See P/N 7-211411089-3 for CCs.

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Pin Assy, Link AttachNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/24/1995CSI Date

7-311411003-625 1615 01 512 - 0889

Y NY Assy contains CSI. See PN 7-211411199, 7-311411015-7, 7-311411045-3, 7-311411080-7, 7-311411088-9, 7-311411096-3, 7-311411146-7, 7-311411155-9/-11, 7-311411193-15, 7-311411215-19, 7-311411202-5, 7-311411045-3 for CC.

08XL0

82001

8V613

Professional Aircraft Accessories Inc

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Head Assy, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved M&O Sources

08/16/2004CSI Date

7-311411009-3 1615 01 433 - 8517

Y NN Heat treat

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Hub, M/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-311411009-5 1615 01 433 - 5594

Y

Y

Y

N

N

N

N

N

N

N

N

Y

Conductivity

Hardness

Heat treat

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Hub, M/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-311411015-5 1615 01 323 - 4381

Y

N

N

N

Y

Y

Assembly contains Critical Safety Items

Visual inspection for heat oxidation (discoloration)

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Hub Sub-Assy, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

05/13/1997CSI Date

7-311411015-7 1615 01 323 - 4381

Y

N

N

N

Y

Y

Assembly contains Critical Safety Items

Visual inspection for heat oxidation (discoloration)

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Hub Sub-Assy, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

09/23/1996CSI Date

7-311411045 5307 01 163 - 4676

Y

Y

N

N

N

N

N

N

Y

Hardness

Heat treat

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Stud, PlainNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/15/1989CSI Date

7-311411045-3 5307 01 163 - 4676

Y

Y

N

N

N

N

N

N

Y

Heat treat per note 16 of the parts list.

Verify hardness of 45 HRC per notes 17 and 18 of the parts list.

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Stud, PlainNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/01/1994CSI Date

7-311411080 1615 01 164 - 3848

Y

Y

Y

N

N

N

Y

N

N

Assembly contains CSI

Hardness

Heat treat

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Plate Assy, Lwr, Hub, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

7-311411080-3 1560 01 433 - 8515

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Hardness (Notes 23 & 24)

Heat treat

Magnetic particle inspection

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Plate Assy, Lwr, Hub, M/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-311411080-7 1615 01 164 - 3848

Y

Y

Y

N

N

N

Y

N

N

Assembly contains CSI

Hardness

Heat treat

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Plate Assy, Lwr, Hub, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/01/1994CSI Date

7-311411080-9 1560 01 433 - 5599

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Hardness (Notes 22, 23 & 24)

Heat treat

Magnetic particle inspection

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Plate, Lwr, Hub, M/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-311411088-7 1615 01 245 - 9826

Y

Y

Y

N

N

N

N

N

N

N

N

Y

Conductivity (forging)

Hardness (forging)

Heat treat (forging)

Visual inspection for heat oxidation (discoloration)

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Shoe Assy, Lower, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

7-311411088-9 1615 01 245 - 9826

Y

Y

N

N

N

N

N

N

Y

Hardness (forging)

Heat treat and conductivity (forging)

Visual inspection for heat oxidation (discoloration)

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Shoe Assy, Lower, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/01/1994CSI Date

7-311411096 1615 01 164 - 3847

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Hardness

Heat treat

Magnetic particle inspection

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Load Plate, Upper, Hub, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

7-311411096-3 1615 01 164 - 3847

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Hardness

Heat treat

Magnetic particle inspection

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Load Plate, Upper, Hub, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/24/1995CSI Date

7-311411110 1615 01 219 - 8658

N NN

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Damper Assy, Lead LagNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

7-311411146-5 1615 01 154 - 7076

Y

Y

N

N

Y

Y

Assembly contains Critical Safety Items

Fixed process control for finishing holes, edges and surfaces of stainless steel laminates

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Strap Assy, Stretched, M/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-311411146-7 1615 01 154 - 7076

Y

Y

N

N

Y

Y

Assembly contains Critical Safety Items

Fixed process control for finishing holes, edges and surfaces of stainless steel laminates

1CA38

8V613

KSD Inc

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Strap Assy, M/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/01/1994CSI Date

7-311411155 3040 01 147 - 4772

Y NY Assembly contains Critical Safety Items

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

LINK ASSY, LEAD LAGNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

7-311411155-11 3040 01 352 - 1531

Y NY Assembly contains Critical Safety Items

82001

8V613

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Link Assy, Lead LagNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/24/1995CSI Date

7-311411155-9 3040 01 432 - 8240

Y NY Assembly contains Critical Safety Items

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

LINK ASSY, LEAD LAGNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-311411164-7 3120 01 509 - 9129

Y

Y

N

Y

Y

N

N

N

N

N

Y

Y

Y

N

Y

Fluorescent penetrant inspection per HP6-13

Shot Peen as noted per HP4-36, 200% coverage, intensity .006-.010A, Shot size S230-S330.

Surface finish shall be RMS 20 or less on O.D. (2.4980-, 2.4965) of the stem.

Surface finish should be RMS 16 on O.D. (2.4980-2.4965) of, the stem to be kept as the final minimum acceptable surface, finish after all operations.

Surface finish should be RMS 32 on I.D. 1.5025 - 1.5015) of the stem to be kept as the final minimum acceptable surface finish after all operations

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, Lead Lag LinkNoun YCritical Safety

NSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

01/31/2006CSI Date

7-311411187 1615 01 170 - 5243

N NN

09455

50632

8V613

97613

RBC Transport Dynamics Corporation

Kamatics Corporation (Sub of Kaman Corp)

The Boeing Company

Sargent Aerospace & Defense, LLC

CAGE

Critical CharacteristicsM ID

Part No NSN

Trunnion, Damper M/RNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

7-311411193-11 3110 01 249 - 3982

Y

Y

Y

N

N

N

N

N

N

N

N

Y

Conductivity

Hardness

Heat treat

Visual inspection for heat oxidation (discoloration)

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing Assy, FeatheringNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

7-311411193-15 3110 01 249 - 3982

Y

Y

Y

N

N

N

N

N

N

N

N

Y

Conductivity

Hardness

Heat treat

Visual inspection for heat oxidation (discoloration)

30061

8V613

Lord Corp Mechanical Products Division

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing Assy, FeatheringNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/01/1994CSI Date

7-311411202 3110 01 215 - 4794

Y

Y

Y

Y

N

N

N

N

N

N

N

N

N

N

Y

Hardness

Heat treat

Maximum surface roughness (per Parts List note 1G of Revision E)

Profile of all Rollers shall be inspected (per Parts List note 8 of Revision E)

Visual inspection for heat oxidation (discoloration)

32828

8V613

Kaydon Corporation

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, Roller, TaperedNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

7-311411202-5 3110 01 215 - 4794

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

N

N

N

N

N

N

N

Y

Hardness

Heat treat

Magnetic Particle Inspection

Maximum surface roughness (per Parts List note 1G of Revision E)

Nital Etch Inspection

Profile of all Rollers shall be inspected (per Parts List note 8 of Revision E)

Visual inspection for heat oxidation (discoloration)

32828

8V613

Kaydon Corporation

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, Roller, TaperedNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

07/20/1995CSI Date

7-311411215-19 1615 01 507 - 5295

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Hardness & conductivity verification per drwg note 39

Heat treat

Shot peen

Visual inspection for heat oxidation (discoloration)

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Housing Assy, Pitch, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

11/13/2003CSI Date

7-311411215-21 1615 01 507 - 5295

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Hardness & conductivity verification per drawing note 39

Heat treat

Shot peen

Visual inspection for heat oxidation (discoloration)

15152

82001

8V613

Timken Aerospace Drive Systems, LLC

PCX Aerostructures, LLC - Newington

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Housing, Pitch, M/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

12/03/2015CSI Date

7-511411146-3 1615 01 501 - 7715

Y

Y

Y

Y

N

N

N

N

Y

N

N

Y

Assembly contains Critical Safety Items.

Bolt elongation dimension as defined on engineering drawing.

Bolt elongation process as defined on engineering drawing.

Fixed process control for finishing holes, edges, and surfaces of stainless steel laminates.

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

MR Strap Pack AssemblyNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

02/26/2004CSI Date

7-511411160-3 -

N

Y

N

N

Y

N

Measured ID: 1.515 inch maximum ID measured in 3 locations:, 1) 0.5 inches into the bore from the top., 2) 0.5 inches into the bore from the Bottom., 3) Center of the Bore from the Top and Bottom.

Shot peen as defined on engineering drawing.

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bolt, Outboard, Pitch ConeNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/11/2007CSI Date

7-511411160-5 -

N

Y

N

N

Y

N

Measured ID: 1.515 inch maximum ID measured in 3 locations:, 1) 0.5 inches into the bore from the top., 2) 0.5 inches into the bore from the Bottom., 3) Center of the Bore from the Top and Bottom.

Shot peen as defined on engineering drawing.

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bolt, Outboard, Pitch ConeNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/11/2007CSI Date

7-511411161-3 -

Y

Y

Y

Y

N

N

N

N

N

N

N

N

Hardness per Engineering Drawings

Heat Treat per Engineering Drawings

Magnetic Particle Inspection

Shot Peening

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Nut, Strap PackNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

03/03/2017CSI Date