Rotorcraft flight manual : chapter 5 - helicopter
Page 1:
Introduction to Title 14 of the Code of Federal Regulations (14 CFR) part 91
Requirement for pilot compliance with operating limitations specified in approved rotorcraft flight manuals, markings, and placards
Evolution of flight manuals with the acceptance of the General Aviation Manufacturers Association (GAMA) specification for a Pilot's Operating Handbook (POH)
Use of the term "Pilot's Operating Handbook (POH)" interchangeably with "Rotorcraft Flight Manual (RFM)"
Chapter 5 of the Rotorcraft Flight Manual
Page 2:
Description of the RFM as a regulatory document
Inclusion of a statement on the title page indicating FAA approval if using "Pilot's Operating Handbook" as the main title
Structure of an FAA-approved RFM with up to ten sections
Importance of including the serial number and registration on the title page to identify the specific aircraft
Inclusion of a table of contents and section dividers in looseleaf form
General Information section providing descriptive information on the rotorcraft and powerplant
Operating Limitations section containing necessary limitations for safe operation
Preliminary Pages:
Variation in RFMs for different aircraft models due to specific information included
Inclusion of serial number and registration for identification
Table of contents for the entire manual and each section
Page numbers reflecting the section being read
Use of divider tabs for section identification
Red tab for quick identification of the emergency procedures section
General Information (Section 1):
Descriptive information on the rotorcraft and powerplant
Three-view drawing of the rotorcraft with dimensions of various components
Importance of familiarizing pilots with the dimensions of the helicopter for operational purposes
Definitions, abbreviations, symbology, and terminology explanations at the end of the section
Optional inclusion of metric and other conversion tables
Operating Limitations (Section 2):
Inclusion of limitations required by regulation or necessary for safe operation
Instrument markings, color coding, and basic placards
Areas covered: airspeed, altitude, rotor, powerplant limitations, weight and loading distribution, and flight limitations
Instrument Markings:
Green, red, and yellow ranges indicating safe operation
Green for continuous operation, red for maximum or minimum operation, yellow for caution or transition area
Airspeed Limitations:
Color coding on the airspeed indicator and placards/graphs in the aircraft
Red line indicating the never exceed speed (VNE)
Green arc for normal operating speed range
Blue line for maximum safe autorotation speed
Page 3:
Typical airspeed indicator limitations and markings
Dual-needle tachometer markings in a reciprocating-engine helicopter
Torque and turbine outlet temperature (TOT) gauges used with turbine-powered aircraft
Altitude limitations based on maximum operating density altitude
Rotor rpm limitations with minimum and maximum values
Power-on and power-off rotor rpm limitations
Powerplant limitations including rpm range, power limitations, operating temperatures, and fuel and oil requirements
Maximum power and maximum continuous power ratings for engines
Yellow and green arcs indicating power ranges on engine power instruments
Manifold pressure gauge indicating maximum power and warning of pressures approaching the limit
Page 4:
Weight and Loading Distribution
Contains maximum certificated weights and center of gravity (CG) range
Location of reference datum used in balance computations should be included
Weight and balance computations are provided in the weight and balance section of the FAA-approved RFM
Flight Limitations
Lists prohibited maneuvers (acrobatic flight, flight into known icing conditions)
Notes if rotorcraft can only be flown in visual flight rules (VFR) conditions
Includes minimum crew requirements and pilot seat location for solo flights
Placards
All rotorcraft have one or more placards with important safety information
Placards are located in a conspicuous place within the cabin, usually in the limitations section
VNE placard can be found in all helicopters
Emergency Procedures (Section 3)
Concise checklists for various types of emergencies or critical situations
Covers engine failure, tail rotor failures, fires, systems failures, restarting an engine, and ditching in water
Manufacturers may show emergencies checklists in an abbreviated form followed by amplified checklists
Page 5:
Performance (Section 5)
Contains information required by regulations and additional performance information
Operating outside the performance section can be hazardous or dangerous
Includes calibrated versus indicated airspeed conversion graph, hovering ceiling versus gross weight charts, and height-velocity diagram
Weight and Balance (Section 6)
Contains information required by the FAA for calculating weight and balance
Includes sample problems to help compute proper data
Aircraft and Systems Description (Section 7)
Describes all the systems found on an aircraft
Should be understandable to most pilots, but may assume higher knowledge for larger, more complex helicopters
Handling, Servicing, and Maintenance (Section 8)
Describes recommended maintenance and inspections
Includes airworthiness directive (AD) compliance procedures
Provides suggestions for ensuring proper work and preventative maintenance
Describes recommended ground handling procedures and storage procedures for the helicopter
Page 6: Supplements (Section 9)
Supplements section provides information on optional equipment installed on the helicopter
Information may come from the aircraft manufacturer or the maker of the optional equipment
The information is inserted into the flight manual when the equipment is installed
Civilian manuals are not updated as frequently as military manuals
Pilots must learn to read the supplements and amend their checklists accordingly
Air carriers must provide checklists to their crews
Checklists must include procedures for all installed equipment and approved company procedures
Page 6: Safety and Operational Tips (Section 10)
Safety and operational tips section is optional
Contains information to enhance the safety of the operation
Examples of covered information: physiological factors, general weather information, fuel conservation procedures, external load warnings, low rotor rpm considerations
Recommendations in this section are important to prevent emergencies
Chapter Summary
The chapter provides an overview of the RFM (Rotorcraft Flight Manual)
Explains each section of the manual
Emphasizes the importance of following and understanding the flight manual for enhanced safety of flight