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W/O Non-Routine Task Card Express, Damage Tab - Corrosion

Corrosion:

From the General tab, 'Corrosion' is selected as the Damage Type.

Damage_Corrosion_1

Notice that the Damage tab reads 'Corrosion.'

Damage_Corrosion_2

 

The following fields are available to describe the Corrosion:

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Cause

The reason/cause of the damage.

Previously Blended (Yes/No) radio buttons

Select the Yes radio button if the area had a previously blended repair. Select No if the area has not had a previously blended repair.

Corrosion Area

The area where the corrosion occurred.

Corrosion Level

The level of corrosion that occurred.

Location of Damage section

Section - To Section - The section(s) covering the damage area.

Station - To Station - The Station(s) of the aircraft. This is a physical location on the aircraft in inches from a datum point.

Stringer - To Stringer - In aircraft construction, a Stringer (also known as Longeron) is a thin strip of wood or metal to which the skin of the aircraft is fastened.

Plus - Enter any additional dimensional information regarding the station(s). This can be measured through different Units of Measurement (UOM) which can be input to the right of each Plus field.

Water Line - To Water Line - A horizontal line through the center of the aircraft in its flying position. Water lines are drawn parallel to one another in three to six inch intervals. This is a range between two numbers.

Buttock Line - To Buttock Line - Lines that are determined by looking at the plan view of the aircraft. A centerline of the aircraft is established and labeled 'buttock line 0.' This is a range between two numbers.

Structural Category

The Structural Category Code.

Damage Description

Enter a brief description of the damages to the aircraft. This field is copied from the N/R T/C Description field from the General tab.

Action Taken section

In Limits radio buttons - Select whether the corrosion is within allowable limits.

Blend Repair (Yes/No) radio buttons - Select the Yes radio button if there was any blending done to the repair.

Note: If the Yes radio button is selected, the Original Material Thickness and Remaining Thickness fields become available.

Original Material Thickness - The original thickness of the material before blending. This field is only available when Blend Repair is set to Yes.

Remaining Thickness - The remaining thickness of the blended area. This field is only available when Blend Repair is set to Yes.

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See Also

W/O Non-Routine Task Card Express, Damage Tab

W/O Non-Routine Task Card Express, Damage Tab - Dent

W/O Non-Routine Task Card Express, Damage Tab - Airframe Crack

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