SH.V.D.R9

From the FAA library

• Helicopter Flying Handbookp. 11-20
  Chapter 11: Helicopter Emergencies and Hazards › System Malfunctions › Loss of Tail Rotor Effectiveness (LTE)

  The key is not to put the helicopter in a compromising condition…

• Helicopter Flying Handbookp. 11-16
  Chapter 11: Helicopter Emergencies and Hazards › Low Rotor RPM and Rotor Stall

  Other causes of a power-on low rotor rpm condition include the pilot rolling the throttle the wrong way in helicopters not equipped with a governor or a governor failure in helicopters so equipped. As the rpm decreases, the amount ... horsepower the engine can produce also decreases. Engine horsepower is directly proportional to its rpm, so a 10 percent loss in rpm due to overpitching, or one of the other scenarios above, will result in a 10 percent loss…

• Helicopter Flying Handbookp. 10-6
  Chapter 10: Advanced Flight Maneuvers › Steep Approach › Technique

  closure with the cyclic, and trim with antitorque pedals. The helicopter should be kept in trim just prior to loss of effective translational lift (approximately 25 knots). Below 100 feet above ground level (AGL), the antitorque pedals should be adjusted ... align the helicopter with the intended touchdown point. Visualize the location of the tail rotor behind the helicopter and fly the landing gear to 3 feet above the intended landing point. In small confined areas, the pilot must precisely position…

• Helicopter Flying Handbookp. 3-3
  Chapter 3: Helicopter Flight Controls › Antitorque Pedals

  This results in maximum downward deflection of the rotor blade in front of the helicopter and maximum upward deflection behind it, causing the rotor disk to tilt forward. Figure 3-4. The cyclic pitch control may be mounted vertically between ... located on the cabin floor by the pilot’s feet, control the pitch and therefore the thrust of the tail rotor blades or other antitorque system. See Chapter 5, Helicopter Components, Sections, and Systems, for a discussion on these other…

• Small Unmanned Aircraft System (Small UAS)p. 6-2
  CHAPTER 6. PART 107 SUBPART C, REMOTE PILOT CERTIFICATION › 6.4 Application Process › 6.4.1 Remote Pilot Applicants Without Part 61 Certificates

  Once the applicant completes the online application in IACRA, the applicant signs the application electronically and submits it to the Airman Registry for processing. No FAA representative will be required to sign the application if the applicant was able ... self-certify. Note: When an applicant seeking a Remote Pilot Certificate uses this online option, the application transmits electronically from the applicant to the Airman Registry. The only electronic signature reflected on the IACRA application will be the applicant…