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Figure 1. Are Diagram
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TM-55-1520-240-PMD CH-47D Helicopter Manual
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Specific Location (Cont)
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
4

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