Emergency Locator Transmitters (ELTs) are expensive devices (average cost for aviation use is $1500–3000). In commercial aircraft, a
cockpit voice recorder or
flight data recorder must contain an
underwater locator beacon. In the US, ELTs are required to be permanently installed in most general aviation aircraft, depending upon the type or location of operation. The specifications for the design of ELTs are published by the
RTCA, and in the specification the alarm signal is defined as an AM signal (A3X and/or N0N emissions), containing a swept tone ranging from 1600 Hz to 300 Hz (downwards), with 2-4 sweeps per second. When activated, 406 MHz units transmit a 0.5 second, 5-watt digital burst every 50 seconds, varying within a span of ±2.5 seconds somewhat randomly, so as to avoid multiple ELTs always having their beacons synchronized. As per 14 CFR 91.207.a.1, ELTs built according to TSO-C91 (of the type described below as "
Traditional ELT, unregistered") have not been permitted for new installations since June 21, 1995; the replacing standard was TSO-C91a. Furthermore, TSO-C91/91a ELTs are being replaced / supplemented by the TSO C126 406 MHz ELT, a far superior unit. ELTs are unique among distress radiobeacons in that they have
impact monitors and are activated by
g-force. Although monitoring of 121.5 and 243 MHz (Class B) distress signals by satellite ceased in February 2009, the FAA has not mandated an upgrade of older ELT units to 406 MHz in United States aircraft. Transport Canada has put forward a proposed regulatory requirement that requires upgrade to Canadian registered aircraft to either a 406 MHz ELT or an alternate means system; however, elected officials have overruled the recommendation of Transport Canada for the regulation and have asked for a looser regulation to be drafted by Transport Canada. Recent information indicates Transport Canada may permit private, general aviation flight with only an existing 121.5 MHz ELT if there is a placard visible to all passengers stating to the effect that the aircraft does not comply with international recommendations for the carriage of the 406 MHz emergency alerting device and is not detectable by satellites in the event of a crash. In the case of 121.5 MHz beacons, the frequency is known in aviation as the "VHF Guard" emergency frequency, and all U.S. civilian pilots (private and commercial) are required, by FAA policy, to monitor this frequency when it is possible to do so. The frequency can be used by
Automatic Direction Finder (ADF) radionavigation equipment, which is being phased out in favor of
VOR and
GPS but is still found on many aircraft. ELTs are relatively large, and would fit in a cube about on a side, and weigh . ELTs were first mandated in 1973 by FAA technical standard order (TSO-C91). The original TSO-C91, and updated TSO-C91A were officially deprecated as of February 2, 2009, when reception of the 121.5 MHz signal was deactivated on all of the SAR satellite, in favor of the C126 ELT models, with their 406 MHz
Cospas-Sarsat beacons. However, the 121.5 MHz signal is still used for close-in direction finding of a downed aircraft.
ELT activation Automatic ELTs have
impact monitors activated by
g-force. Numerous activities, such as
aerobatics, hard landings, movement by ground crews and aircraft maintenances, can generate false alarms, which can interfere with and cannot be distinguished from genuine emergency transmissions.
ELT sub-classification Emergency locator transmitters (ELTs) for aircraft may be classed as follows: • A: automatically ejected • AD: automatic deployable • F: Fixed • AF: automatic fixed • AP: automatic portable • W: water activated • S: survival Within these classes, an ELT may be either a digital 406 MHz beacon, or an analog beacon (
see below).
Obsolete ELTs • Any ELT that is not a 406 MHz ELT with a Hex Code became obsolete February 1, 2009. According to the U.S.
Federal Aviation Administration, ground testing of A-, B-, and S-type ELTs is to be done within the first 5 minutes of each hour. Testing is restricted to three audio sweeps. Type I and II devices (those transmitting at 406 MHz) have a self test function and must not be activated except in an actual emergency.
Timeline of ELT development • Automatic SOS radios were developed as early as the 1930s. • The
United States Air Force institutes development of a "Crash-Locator Beacon" and a "Crash-Locator Bearing Recorder" in the early 1950s. • In the UK, by 1959 the first automatic beacon for liferafts had been produced by
Ultra Electronics, and at the same time Burndept produced the TALBE (Talk and Listen Beacon Equipment) - VHF, and SARBE - Search-And-Rescue-Beacon Equipment (UHF) range of beacons which were used by the
Fleet Air Arm and later,
Royal Air Force. Later, SARBE beacons included a radio for voice communication by the survivor with the rescuing personnel. • Jan 9 1964: FAA Advisory Circular 170-4 investigated ELTs • Mar 17 1969: FAA Advisory Circular 91-19 advised pilots to install ELTs • A
Saturday Evening Post article covered the death of 16-year-old Carla Corbus, who survived, though badly injured, along with her mother, for 54 days after the plane her step-dad was flying crashed in the Trinity Alps of California in March 1967. He was lost and died in the woods looking for rescue. • The winter 1969 search for the
Hawthorne Nevada Airlines Flight 708 "Gamblers' Special"
DC-3 that crashed on February 18, 1969 in the Sierra Nevada Mountains. Five aircraft crashed and five searchers were killed while trying to find Flight 708. • Carriage requirements for emergency locator beacons on most US non-jet powered fixed-wing civil aircraft became law on December 29, 1970, with the signing of Senate bill S.2193, "The Occupational Safety and Health Act of 1970," Public Law 91-596. as a last-minute rider to the Occupational Safety and Health Act.
Senator Peter Dominick (R-Colorado) added the unrelated beacon language as a rider to the bill, which became section 31 of the law. (Earlier in the session he tried to add the requirements as an amendment to House bill H.R. 14465, the "Airport and Airways Development Act of 1969," but was unsuccessful.) It required most general aviation aircraft to install ELTs by Dec. 30, 1973, and it preempted all the state ELT laws. The federal ELT law left the matter of alerting vague, although the initial idea was alerting by over flying aircraft which could receive an ELT's 75-milliwatt signal from 50 nautical miles away. The law set the compliance dates as one year after passage for newly manufactured or imported aircraft (December 30, 1971), and three years for existing aircraft (December 30, 1973). In response to the law, the
Federal Aviation Administration (FAA) published on March 13, 1971, Notice of Proposed Rule Making (NPRM) 71–7 with the proposed amendments to the
Federal Aviation Regulations (FAR). After public comment, the final rules were published in the Federal Register on September 21, 1971. • The disappearance of U.S. Congressmen
Hale Boggs and
Nick Begich in a general aviation aircraft on October 16, 1972 sparked the then largest ever search and rescue effort, which proved fruitless. This high-profile event further hastened the mandating of ELTs aboard aircraft. • The RTCA published DO-145, DO-146, and DO-147, which the FAA then adopted the three DO documents as Technical Standard Order TSO C91. • After problems with the C-91 ELTs, The FAA responded to the defective early ELTs by outlawing the installation of C-91 ELTs and certifying C91a ELTs with an improved gravity switch, improved crash and fire-worthy casing, and batteries that work in colder temperatures. • March 16, 1973: AC 20–85, Emergency Locator Transmitters and Receivers • Dec 23, 1992: TSO-C126, 406 MHz Emergency Locator Transmitter (ELT) defines the 406 MHz ELT == Emergency Position-Indicating Radio Beacon ==