Faa rotorcraft flight manual

the Rotorcraft Flight Manual weight and balance section as well as the limitations section to determine that all loads will remain within the CG limits throughout the entire operation. Pilots will be aware of fuel burn effects on the center of gravity of the aircraft. Rotorcraft Flight Manual. In accordance with § , a pilot operating a civil aircraft (rotorcraft) must comply with the operating limitations specified in the approved Rotorcraft Flight Manual. b. Cockpit Check Procedure/Checklist. A pilot should use a cockpit check procedure or checklist appropriate to the aircraft and operation. FAA APPROVED ROTORCRAFT FLIGHT MANUAL Type Certificate No. H3WE Approved By r, Flight Test Branch, ANM−L Federal Aviation Administration Los Angeles Aircraft Certification Office Transport Airplane Directorate Original Approval Date: 25 October Reissue #1: 14 August

Airplane Flight Manual (AFM): The AFM is a document developed by the airplane manufacturer and approved by the Federal Aviation Administration (FAA) It is specific to a particular make and model airplane by serial number and it contains operating procedures and limitations which meet the requirements of FAR ; Pilot Operating Handbook (POH). This supplement must be attached to the appropriate FAA approved Airbus Helicopters Rotorcraft Flight Manual when an Onboard Systems P/N , , , or Cargo Hook Swing Suspension is installed in accordance with Supplemental Type Certificate (STC) NO. SRSE. Rotorcraft Flight Manual (RFM): A document developed by the rotorcraft manufacturer and approved by the Federal Aviation Administration (FAA). It is specific to a particular make and model rotorcraft by serial number and it contains operating procedures and limitations. source: FAA Helicopter Flying Handbook (FAA-HA).

Maximum Rotorcraft - Load Combinations operating gross weight is published in the Rotorcraft Flight Manual (FAR ). Refer to the Rotorcraft Flight Manual for Gross Weight Center of Gravity Limits for external load operations. The dual cargo hook system load limit is lbs. ( kg) with the Y-rope attached to both cargo hooks. This Rotorcraft Flight Manual Supplement MUST be used in conjunction with Section IX Optional Equipment of the Rotorcraft Flight Manual. The Dual Cargo Hook System for the MDHI series and N model helicopters provides a means to transport human external cargo (HEC). When the Dual Cargo Hook System is installed, an owner or operator holding a valid Rotorcraft. FAA APPROVED ROTORCRAFT FLIGHT MANUAL Type Certificate No. H3WE Approved By r, Flight Test Branch, ANM−L Federal Aviation Administration Los Angeles Aircraft Certification Office Transport Airplane Directorate Original Approval Date: 25 October Reissue #1: 14 August