CLASSIFICATION OF FUSELAGE DAMAGE AND TYPES OF REPAIR

TM 1-1520-238-23 2-46 Change 2 2.12. CLASSIFICATION OF FUSELAGE DAMAGE AND TYPES OF REPAIR Category Action Limits z. Strut End Fittings Nicks or Scratches A Not applicable. ------- B Maximum 0.005 INCH. Must be blended out. C Exceeds B. Replace. 2.12.6. Abrasion Damage Category Limits Action a. Left Hand and Right Hand Tailboom Fuselage Stringer Splice Plate A Abrasion length is less than 0.125 INCH width is less than 0.125 INCH and/or depth is less than 0.020 INCH. Blend abraded area of airframe splice plate to eliminate any sharp edges or sudden contour changes. Refinish plate blended area (TM 55-1500-345-23). B Abrasion length is more than 0.800 INCH and depth is less than 0.060 INCH. Blend abraded area of airframe splice plate to eliminate any sharp edges or sudden contour changes. Refinish plate blended area (TM 55-1500-345-23). B Abrasion width is less than 0.350 INCH depth is less than 0.060 INCH and/or length is less than 0.800 INCH. Blend abraded area of airframe splice plate to eliminate any sharp edges or sudden contour changes. Refinish splice blended area (TM 55-1500-345-23). INBD FWD 1.68 A A AA DEPTH WEAR AREA TYPICAL WEAR AREA WIDTH BL 11.640 LENGTH FS370.00 STRINGER SPLICE PLATE - 7-311113604-1/2 M04-4514-1 GO TO NEXT PAGE