Aircraft became a practical means of transportation when accurate flight instruments freed the pilot from the necessity of maintaining visual contact with the ground
Flight instruments are crucial to conducting safe flight operations and it is important that the pilot have a basic understanding of their operation
Various types of air navigation aids are in use today, each serving a special purpose
These aids have varied owners and operators, namely: the Federal Aviation Administration (FAA), the military services, private organizations, individual states and foreign governments
The FAA has the statutory authority to establish, operate, maintain air navigation facilities and to prescribe standards for the operation of any of these aids which are used for instrument flight in federally controlled airspace as tabulated in the Chart Supplement U.S.
Basic Six-Pack:
The core of the instruments in an aircraft center around what is often referred to as "the six-pack"
These instruments enable the pilot to maintain spatial orientation during flight
Airspeed Indicator:
The airspeed indicator provides the pilot with a means of determining the speed of the aircraft
Generally, altimeters are configured to show height above sea level (an aviation standard) however, other types of altimeters do exist which can measure other heights, such as height above ground
Attitude Indicator:
Attitude indicators display the orientation of the aircraft with regards to its roll (angle of the wings) and pitch (angle of the nose)
Heading Indicator:
Heading Indicators, also called a directional gyros, are instruments used to determine aircraft direction to aid the pilot in navigation
The navigation instruments indicate the position of the aircraft in relation to a selected navigation facility or fix. This group of instruments includes various types of course indicators, range indicators, glideslope indicators, and bearing pointers. Newer aircraft with more technologically advanced instrumentation provide blended information, giving the pilot more accurate positional information. Navigation instruments are comprised of indicators that display GPS, very high frequency (VHF) omni-directional radio range (VOR), nondirectional beacon (NDB), and instrument landing system (ILS) information. The instruments indicate the position of the aircraft relative to a selected navigation facility or fix. They also provide pilotage information so the aircraft can be maneuvered to keep it on a predetermined path. The pilotage information can be in either two or three dimensions relative to the ground-based or space-based navigation information
Satellite-Based Navigation Systems:
The Global Positioning System (GPS) is U.S.-based satellite-based navigation system composed of a network of satellites placed into orbit by the United States Department of Defense (DOD)
GPS provides a very precise, global navigation service, which is unaffected by weather, allowing for point-to-point navigation
In conjunction with GPS, another system called the Wide Area Augmentation System is used as well
Since the development of the first GNSS by the US, other countries have followed with regional and global systems:
Russia: Global Navigation Satellite System (GLONASS)
China: BeiDou
European Union: Galileo
India: Indian Regional Navigation Satellite System (IRNSS)
Ground-Based Navigation Systems:
Non-Directional Beacon (NDB):
Non-Directional Beacons are all but gone within the United States, but remain prolific across the world due to their low cost and high reliability in remote areas
Users of the National Airspace System (NAS) can render valuable assistance in the early correction of NAVAID malfunctions or GNSS problems and are encouraged to report their observations of undesirable avionics performance
Although NAVAIDs are monitored by electronic detectors, adverse effects of electronic interference, new obstructions or changes in terrain near the NAVAID can exist without detection by the ground monitors
Some of the characteristics of malfunction or deteriorating performance which should be reported are: erratic course or bearing indications; intermittent, or full, flag alarm; garbled, missing or obviously improper coded identification; poor quality communications reception; or, in the case of frequency interference, an audible hum or tone accompanying radio communications or NAVAID identification
GNSS problems are often characterized by navigation degradation or service loss indications
Pilots conducting operations in areas where there is GNSS interference may be unable to use GPS for navigation, and ADS-B may be unavailable for surveillance
Radio frequency interference may affect both navigation for the pilot and surveillance by the air traffic controller
Depending on the equipment and integration, either an advisory light or message may alert the pilot
Air traffic controllers monitoring ADS-B reports may stop receiving ADS-B position messages and associated aircraft tracks
Malfunctioning, faulty, inappropriately installed, operated, or modified GPS re-radiator systems, intended to be used for aircraft maintenance activities, have resulted in unintentional disruption of aviation GPS receivers. This type of disruption could result in unflagged, erroneous position-information output to primary flight displays/indicators and to other aircraft and air traffic control systems. Since Receiver Autonomous Integrity Monitoring (RAIM) is only partially effective against this type of disruption (effectively a "signal spoofing"), the pilot may not be aware of any erroneous navigation indications; ATC may be the only means available to identify these disruptions and detect unexpected aircraft positions while monitoring aircraft for IFR separation
Pilots encountering navigation error events should transition to another source of navigation and request amended clearances from ATC as necessary
Pilots are encouraged to submit detailed reports of NAVAID or GPS anomaly as soon as practical. Pilot reports of navigation error events should contain the following information:
Date and time the anomaly was observed, and NAVAID ID (or GPS)
Location of the aircraft at the time the anomaly started and ended (e.g., latitude/longitude or bearing/distance from a reference point)
Heading, altitude, type of aircraft (make/model/call sign)
Type of avionics/receivers in use (e.g., make/model/software series or version)
Number of satellites being tracked, if applicable
Description of the position/navigation/timing anomaly observed, and duration of the event
Consequences/operational impact(s) of the NAVAID or GPS anomaly
Actions taken to mitigate the anomaly and/or remedy provided by the ATC facility
Post-flight pilot/maintenance actions taken
Pilots operating an aircraft in controlled airspace under IFR shall comply with CFR 91.187 and promptly report as soon as practical to ATC any malfunctions of navigational equipment occurring in flight; pilots should submit initial reports:
Immediately, by radio to the controlling ATC facility or FSS
By telephone to the nearest ATC facility controlling the airspace where the disruption was experienced
Additionally, GPS problems should be reported, post flight, by Internet via the GPS Anomaly Reporting Form at http://www.faa.gov/air_traffic/nas/gps_reports/
To minimize ATC workload, GPS anomalies associated with known testing NOTAMs should NOT be reported in-flight to ATC in detail; EXCEPT when:
GPS degradation is experienced outside the NOTAMed area
Pilot observes any unexpected consequences (e.g., equipment failure, suspected spoofing, failure of unexpected aircraft systems, such as TAWS)
"Real-time precision, shared situational awareness, advanced applications for pilots and controllers alike – these are the hallmarks of ADS-B NextGen surveillance"
Emergency Locator Transmitter:
Safety is the primary concern with everything aviation
The Emergency Locator Transmitter (ELT) was designed with safety in mind, when luck is at its worst, allowing pilots to broadcast their position when in distress
Angle of Attack Indicator:
An angle of attack indicator is a more accurate measurement of the aircraft's performance
These systems incorporate a numeric value to be read in flight while also using stick shakers to avoid the pilot putting the aircraft into an unsafe situation
The Earth is a huge magnet, spinning in space, surrounded by a magnetic field made up of invisible lines of flux
These lines leave the surface at the magnetic North Pole and reenter at the magnetic South Pole
Lines of magnetic flux have two important characteristics:
Any magnet that is free to rotate will align with them, and
An electrical current is induced into any conductor that cuts across them
Most direction indicators installed in aircraft make use of one of these two characteristics
One of the most common types of magnetic direction indicators is the Magnetic Compass
Instrumentation: Moving into the Future:
Until recently, most GA aircraft were equipped with individual instruments utilized collectively to safely operate and maneuver the aircraft. With the release of the electronic flight display (EFD) system, conventional instruments have been replaced by multiple liquid crystal display (LCD) screens
The first screen is installed in front of the pilot position and is referred to as the primary flight display (PFD)
The second screen, positioned approximately in the center of the instrument panel, is referred to as the multi-function display (MFD)
These solid state instruments have a failure rate far less than those of conventional analog instrumentation. [Figure 3-18]
With today's improvements in avionics and the introduction of EFDs, pilots at any level of experience need an astute knowledge of the onboard flight control systems, as well as an understanding of how automation melds with Aeronautical Decision-Making (ADM)
Training for avionics:
Companies often create simulators which can be downloaded on their websites:
Whether an aircraft has analog or digital (glass) instruments, the instrumentation falls into three different categories:
Performance
Control
Navigation
Performance Instruments:
The performance instruments indicate the aircraft's actual performance. Performance is determined by reference to the altimeter, airspeed or vertical speed indicator (VSI), heading indicator, and turn-and-slip indicator. The performance instruments directly reflect the performance the aircraft is achieving. The speed of the aircraft can be referenced on the airspeed indicator. The altitude can be referenced on the altimeter. The aircraft's climb performance can be determined by referencing the VSI. Other performance instruments available are the heading indicator, angle of attack indicator, and the slip-skid indicator [Figure 2]
Control Instruments:
The control instruments display immediate attitude and power changes and are calibrated to permit adjustments in precise increments. The instrument for attitude display is the attitude indicator. The control instruments do not indicate aircraft speed or altitude. In order to determine these variables and others, a pilot must reference the performance instruments [Figure 3]
Avionics Frequencies:
The 960-1164 MHz band is part of the 960-1215 MHz band allocated on a primary basis to the Federal Government for the aeronautical radionavigation service (ARNS)
The Federal Aviation Administration (FAA) domestically manages the 960-1164 MHz band
Ground-based and airborne systems that operate in this band control civilian and military aircraft in the National Air Space (NAS)
The Distance Measuring Equipment (DME) system and its military version, the Tactical Air Navigation (TACAN) system operates throughout the band
The Air Traffic Control Radar Beacon System (ATCRBS) and the Mode Select (Mode S) system have a ground-based and airborne component and operate on the frequencies of 1030 MHz and 1090 MHz
Identification Friend or Foe (IFF) system is the primary positive means of aircraft identification in air defense operations
An IFF transponder receives interrogation pulses at one frequency (1030 MHz), and sends the reply pulses at a different frequency (1090 MHz)
Proper use of IFF facilitates rapid engagement of enemy aircraft, conserves air defense assets, and reduces risk to friendly aircraft
The Traffic Alert and Collision Avoidance System (TCAS) operates at 1030 and 1090 MHz and is independent of any ground system
The International Telecommunication Union 2007 World Radiocommunication Conference allocated the band 960-1164 MHz to aeronautical mobile (route) service (AM(R)S)
The Automatic Dependent Surveillance-Broadcast (ADS-B) system and the Universal Access Transceiver (UAT) operate on the frequencies of 978 MHz and 1090 MHz
In addition to the ARNS and AM(R)S systems, the Department of Defense (DOD) operates a communication system, the Joint Tactical Information Distribution System (JTIDS) in this band on a coordinated basis
Conclusion:
Avionics are tools, not crutches
While very useful, they can be rendered less so by not maintaing software versions or obstruction databases