TB 1-1615-351-23
TAPING APPLICATION, ROTOR BLADE EROSION PROTECTION
Section I. GENERAL
Figure 3-1 depicts general taping procedures applicable to
all aircraft.
Table 3-1 gives a
detailed listing of
item quantities, used for the individual aircraft systems, when applying
tape for rotor blade erosion protection.
Table 3-2 identifies the quantity of
aircraft each kit can modify/supp ort.
NOTE
Refer to Chapter 4 for detaping procedures of rotor blades for the AH-1, AH-64,
CH-47, OH-58, UH-1 and UH-60 helicopters returning from Southwest Asia.