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66 AFMAN 11-217V1 3 JANUARY 2005 Figure 4.14. Short Final Approach. 4.5.1.4. Point In Space. While the point in space approach (Figure 4.15) is rare, it does illustrate how approach design takes advantage of helicopter capability. This approach (see AFJMAN 11-226 TERPS) places the helicopter up to 2,600 feet from the landing pad, and the pilot is expected to proceed visually, by ground reference, to the pad. If planning to use this type of approach, pay careful attention to weather conditions upon arrival, as VMC conditions are required to maneuver.
AFMAN 11-217V1 3 JANUARY 2005 67 Figure 4.15. Point in Space Approach. 4.5.1.5. Review Missed Approach. Review the published missed approach departure instruction to ensure you can achieve the published climb gradient. For copter only procedures, the missed approach is based on a climb gradient of at least 304 feet per mile; twice the angle used for fixed-wing instrument approach procedures (IAP). If a 90 knot missed approach is performed, then this climb gradient equates to a 456 foot per minute minimum rate of climb, no wind. 4.5.1.6. RNAV Departure Procedures. Helicopter-only GPS departure procedures are to be flown at 70 knots or less since turning areas and segment lengths are based on this speed. 4.6. Altimeter Setting Procedures. The altitude indicated on the altimeter may be in error if the altimeter check is conducted with the rotors turning. This error is due to the difference in pressure caused by the rotor downwash. The difference in pressure causes the altimeter to
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