Figure 3-22. Tape Application, Main Rotor (OH-58A/C)

Figure 3-21. Tape Alignment, Main Rotor (OH-58A/C)

Section V. DESCRIPTION AND APPLICATION PROCEDURES FOR THE OH-58D AIRCRAFT

TB-1-1615-351-23 Rotor Blade Erosion Protection Manual
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ALL TAPE PIECES ARE 2 INCHES

ON TOP AND 2 INCHES ON BOTTOM

Figure 3-22. Tape Application, Main Rotor (OH-58A/C)

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