Attachment 0008 - M and O CSI.pdf

02/13/2020

114CS123-1 3120 00 110 - 8542

Y

Y

Y

Y

N

N

N

N

N

N

N

N

100% Minimum Shot peen coverage over the area defined on the drawing.

Bake within 4 hours of Cadmium plating at 375 degrees Fahrenheit plus or minus 25 degrees Fahrenheit for a minimum of 12 hours.

Magnetic Particle Inspection per BAC5424 or equivalent.

Rockwell Hardness shall conform to range specified on drawing after final heat treating and machining (if applicable) of the surface being tested. Hardness testing as specified per BAC5650 or equivalent.

09455

77272

RBC Transport Dynamics Corporation

The Boeing Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, Spherical, Rod EndNoun YCritical Safety

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

Approved Replacement (Spares) Sources

01/21/1992CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

02/13/2020

145CS114-2 1680 01 120 - 7641

Y

Y

N

Y

Y

Y

Assembly contains Critical Safety Items. Subcomponent CSI is 114CS123-1.

Proper orientation of the lower rod end. The lower rod end has a flat side and a tabbed side (anti-rotation lugs).

The rod end shall be installed with the flat side facing the motor side of the actuator (tabs facing away from the motor).

08XL0 Professional Aircraft Accessories Inc

CAGE

Critical CharacteristicsM ID

Part No NSN

Actuator AssemblyNoun YCritical Safety

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

Approved M&O Sources

01/01/1987CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS