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CLASSIFICATION OF FUSELAGE DAMAGE AND TYPES OF REPAIR – continued
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TM-1-1520-238-23-2 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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CLASSIFICATION OF FUSELAGE DAMAGE AND TYPES OF REPAIR – continued

TM 1-1520-238-23 2-44 Change 4 2.12. CLASSIFICATION OF FUSELAGE DAMAGE AND TYPES OF REPAIR – continued Category Action Limits p.   Kevlar/Epoxy Fairings Cracks B No longer than 25 PERCENT of shortest skin dimension. Repair (para 2.30). C Exceeds B or extends from one end of part through other end. Replace. q.   Kevlar/Epoxy Fairings Erosion B Any broken resin or exposed fibers. Repair (para 2.30). r.   Repair seal on armor side panel. A Cracks, tears, punctures. Replace. s.   Boron Carbide Cracks (e.g., nontransparent barrier) C Any cracking. Replace. t.   Area Weapon Support Structure (F.S. 91.7) A Single crack less than 0.75 INCH. Repair (TM 1-1500-204-23). B Total of all cracks on one side of bulkhead - less than 1.75 INCHES. Repair (TM 1-1500-204-23). Total of all cracks on bulkhead - less than 1.75 INCHES. Repair (TM 1-1500-204-23). Single crack greater than 0.75 INCH. Ground helicopter until repaired. Total of all cracks on one side of bulkhead - greater than 1.75 INCHES. Ground helicopter until repaired. Total of all cracks on bulkhead - greater than 1.75 INCHES. Ground helicopter until repaired. u.   Fuselage Frame Assembly (F.S. 547.15) (includes attached stringers within 6 INCHES of attachment to this frame.) A Single crack less than 1.50 INCHES. Continue operation of helicopter - INSPECT DAILY. B Any crack greater than A. Contact local LAR Representative for repair. Any crack within 0.25 INCH of thin-to-thick wall transition flange. Contact local LAR Representative for repair. C Greater than B. Replace. GO TO NEXT PAGE

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