Specific Location

Area

Specific L ocation

COCKPIT

Internal area of fuselage from STA 120.00 forward

CABIN

Internal area of fuselage from STA 120.00 aft to STA 482.00

RAMP

Internal area of fuselage STA 482.00 aft to STA 630.50

RIGHT FUSELAGE

External fuselage from STA 630.50 forward to STA 120.00,

including bottom of fuselage, excluding forward and aft pylons,

rotors, and tunnel area

NOSE

External area of fuselage from STA 120.00 RH to STA 120.00 LH,

excluding forward rotor and pylon area

LEFT FUSELAGE

External Area of fuselage from STA 120.00 aft to STA 630.50,

including bottom of fuselage, excluding forward and aft pylons,

rotors, and tunnel area

No. 1 ENGINE (Lower)

No. 1 engine, and engine and transmission covers (cowling)

No. 2 ENGINE (Lower)

No. 2 engine, and engine and transmission covers (cowling)

No. 2 ENGINE (Upper)

No. 2 engine, and engine and transmission covers (cowling)

AFT ROTOR and

Internal and external area of upper fuselage from STA 630.50

PYLON (Right Side)

forward to STA 440.00 and right of BL 0.0

No. 1 Engine (Upper)

No. 1 engine, and engine and transmission covers (cowling)

AFT ROTOR and

Internal and external area of upper fuselage from STA 630.50

PYLON (Left Side)

forward to STA 440.00 and left of BL 0.0

TUNNEL

Internal and external area of upper fuselage from STA 440.00

forward to STA 160.00

FWD ROTOR and

Internal and external area of upper fuselage from STA 160.00

PYLON (Left Side)

forward and left of BL 0.0

TM 55-1520-240-PMD