Attachment_0020_-_Critical_Characteristics.pdf

07/06/2016

19E203-7ACL95 3130 01 631 - 7822

Y

Y

Y

Y

Y

N

N

N

N

N

Y

Y

Y

Y

Y

ATP/ATS per Vendor or DMWR approved plan.

Dynamic balance both input flange & output flange to 0.007 ounce-inch.

Input flange (2494075) & output flange (2494445) with five 1/4" bolt holes and five 1/2" balancing holes must not be used (SOF AH-64-00-01) Static test at 11,464 (+100,-0) in-lbs for 5 seconds

Torque self-locking nut (NAS1022C14) between 700 & 800 in-lbs above running torque

8V613

99551

The Boeing Company

Goodrich Corporation, Power Transmission Systems

CAGE

Critical CharacteristicsM ID

Part No NSN

Hanger Assy, Fwd BearingNoun YCritical Safety

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

Approved M&O Sources

11/12/2014CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

2882673 3010 01 336 - 0783

Y

Y

Y

N

N

N

Y

N

N

Dynamic balance to 0.007 oz-in

Heat treat with final hardness of Rc 36-40

UT inspection IAW MIL-S-2154 Class A

8V613

99551

The Boeing Company

Goodrich Corporation, Power Transmission Systems

CAGE

Critical CharacteristicsM ID

Part No NSN

Flange, InputNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/11/2006CSI Date

2882674 3010 01 336 - 0784

Y

Y

Y

N

N

N

Y

N

N

Dynamic balance to 0.007 oz-in

Heat treat with final hardness of Rc 36-40

UT inspection IAW MIL-S-2154 Class A

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Flange, OutputNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/07/2006CSI Date

2888438 3010 01 336 - 0783

Y

Y

Y

N

N

N

Y

N

N

Dynamic balance to 0.007 oz-in

Heat treat with final hardness of Rc 36-40

UT inspection IAW MIL-S-2154 Class A

8V613

99551

The Boeing Company

Goodrich Corporation, Power Transmission Systems

CAGE

Critical CharacteristicsM ID

Part No NSN

Flange, InputNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/11/2006CSI Date

2888439 3010 01 336 - 0784

Y

Y

Y

N

N

N

Y

N

N

Dynamic balance to 0.007 oz-in

Heat treat with final hardness of Rc 36-40

UT inspection IAW MIL-S-2154 Class A

8V613 The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Flange, OutputNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/11/2006CSI Date

7-311350008-7 3130 01 631 - 7822

Y

Y

Y

Y

Y

N

N

N

N

N

Y

Y

Y

Y

Y

ATP/ATS per Vendor or DMWR approved plan.

Dynamic balance both input flange & output flange to 0.007 ounce-inch.

Input flange (2494075) & output flange (2494445) with five 1/4" bolt holes and five 1/2" balancing holes must not be used (SOF AH-64-00-01) Static test at 11,464 (+100,-0) in-lbs for 5 seconds

Torque self-locking nut (NAS1022C14) between 700 & 800 in-lbs above running torque

8V613

99551

The Boeing Company

Goodrich Corporation, Power Transmission Systems

CAGE

Critical CharacteristicsM ID

Part No NSN

Hanger Assy, Fwd BearingNoun YCritical Safety

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

Approved Replacement (Spares) Sources

11/03/2014CSI Date