Solicitation_Attachment_0013_-_Critical_Characteristics_BB856-1.pdf

12/09/2016

274600-1048 -

Y

Y

Y

N

N

N

Y

Y

Y

Acceptance of swaging of NAS1446 and NAS1448 lockbolts and NAS1080 collars using, NAS1563 inspection gauges (4 places Ref: Dwg 274600, Sheets 10 and 11) Acceptance of swaging of NAS1446 and NAS1448 lockbolts and NAS1080 collars using, NAS1563 inspection gauges (6 places Ref: Dwg 274600, Sheets 8,10 and 11) Verification of proper assembly, torquing, and safetying of 274647 rod end (360 in-lbs max)and, 274646 rod end (270 in-lbs max. on NAS6509 nut) to 274645 piston per Bertea boost actuator, assembly drawing 274640 (Ref:

Sheet 4, note 9 and Sheet 2 F/D)

78286

82106

Sikorsky Aircraft Corp

PARKER-HANNIFIN CORPORATION

CAGE

Critical CharacteristicsM ID

Part No NSN

Servo Assy, Boost, CollectivNoun YCritical Safety

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

Approved Replacement (Spares) Sources

03/11/2014CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

274600-1049 1650 01 624 - 9557

Y NY Assembly Contains CSI.

78286

82106

Sikorsky Aircraft Corp

Parker-Hannifin Corp (Aerospace Group) Controls Systems Div

CAGE

Critical CharacteristicsM ID

Part No NSN

Servo Assy, CollectiveNoun YCritical Safety

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

Approved M&O Sources

03/11/2014CSI Date

274640-1029 -

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Proper installation of locking device NAS1193K7CP.

Torque NAS509-7C nut to 240-270 inch-lbs, and lockwire nut.

Torque of output rod end to 340-360 inch pounds.

Verify proper alignment of input rod end with output rod end.

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Actuator, AssemblyNoun YCritical Safety

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

Approved Replacement (Spares) Sources

01/06/2010CSI Date

274640-1031 -

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Proper installation of locking device NAS1193K7CP.

Torque NAS509-7C nut to 240-270 inch-lbs, and lockwire nut.

Torque of output rod end to 340-360 inch pounds.

Verify proper alignment of input rod end with output rod end.

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Actuator, AssemblyNoun YCritical Safety

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

Approved Replacement (Spares) Sources

01/06/2010CSI Date

274640-1033 1650 01 137 - 5790

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Proper installation of locking device NAS1193K7CP.

Torque NAS509-7C nut to 240-270 inch-lbs, and lockwire nut.

Torque of output rod end to 340-360 inch pounds.

Verify proper alignment of input rod end with output rod end.

82106 Parker-Hannifin Corp (Aerospace Group) Controls Systems Div

CAGE

Critical CharacteristicsM ID

Part No NSN

Cylinder, Assembly, LinearNoun YCritical Safety

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

Approved Replacement (Spares) Sources

01/06/2010CSI Date

274640-1037 1650 01 625 - 5920

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Proper installation of locking device NAS1193K7CP.

Torque NAS509-7C nut to 240-270 inch-lbs, and lockwire nut.

Torque of output rod end to 340-360 inch pounds.

Verify proper alignment of input rod end with output rod end.

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Cylinder, Assembly, LinearNoun YCritical Safety

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

Approved Replacement (Spares) Sources

11/03/2014CSI Date

70410-02334-045 3040 01 281 - 4589

Y

Y

N

N

N

N

Penetrant Inspection, reference Note 9 on Sikorsky drawing 70410-02334

Verify IAW SS8013, that the heat treatment process was properly performed Reference Note 8 on Sikorsky drawing 70410-02334

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Link Assy, Connecting, RigidNoun YCritical Safety

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

Approved Replacement (Spares) Sources

05/16/2001CSI Date

70410-02900-127 -

Y

Y

Y

N

N

N

Y

Y

Y

Acceptance of swaging of NAS1446 and NAS1448 lockbolts and NAS1080 collars using, NAS1563 inspection gauges (4 places Ref: Dwg 274600, Sheets 10 and 11) Acceptance of swaging of NAS1446 and NAS1448 lockbolts and NAS1080 collars using, NAS1563 inspection gauges (6 places Ref: Dwg 274600, Sheets 8,10 and 11) Verification of proper assembly, torquing, and safetying of 274647 rod end (360 in-lbs max)and, 274646 rod end (270 in-lbs max. on NAS6509 nut) to 274645 piston per Bertea boost actuator, assembly drawing 274640 (Ref:

Sheet 4, note 9 and Sheet 2 F/D)

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Servo Assy, Boost, CollectivNoun YCritical Safety

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

Approved Replacement (Spares) Sources

03/11/2014CSI Date

70410-02920-054 1650 01 624 - 9557

Y NY Assembly Contains CSI

78286

82106

Sikorsky Aircraft Corp

Parker-Hannifin Corp (Aerospace Group) Controls Systems Div

CAGE

Critical CharacteristicsM ID

Part No NSN

Servo Assy, CollectiveNoun YCritical Safety

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

Approved Replacement (Spares) Sources

03/11/2014CSI Date