Flight data recorder

From Wikipedia, the free encyclopedia

An example of an FDR (Flight Data Recorder). (English translation: FLIGHT RECORDER DO NOT OPEN)
An example of an FDR (Flight Data Recorder). (English translation: FLIGHT RECORDER DO NOT OPEN)
Flight data recorder and Cockpit voice recorder
Flight data recorder and Cockpit voice recorder

The flight data recorder (FDR) or Black Box is a flight recorder used to record specific aircraft performance parameters. A separate device is the cockpit voice recorder (CVR), although some versions (including the original) combine both in one unit. Popularly, though almost always falsely, known as the black box used for aircraft mishap analysis, the FDR is also used to study air safety issues, material degradation, and jet engine performance. These ICAO regulated "black box" devices are often used as an aid in investigating aircraft mishaps, and its recovery is second only in importance to the recovery of survivors and victims' bodies. The device's shroud is usually painted bright orange and generally located in the tail section of the aircraft. It is also designed to withstand intense heat and pressure.

Contents

[edit] History

The first prototype FDR was produced in 1956 by Dr. David Warren of the then Aeronautical Research Laboratories of Melbourne, Australia. In 1953 and 1954, a series of fatal accidents involving the De Havilland DH106 Comet prompted the grounding of the entire fleet pending an investigation. Dr. Warren, a chemist specializing in aircraft fuels, was involved in a professional committee discussing the possible causes. Since there had been neither witnesses nor survivors, Dr. Warren conceived of a crash-survivable method to record the flight crew's conversation (and other pre-crash data), reasoning they would greatly assist in determining a cause and enabling the prevention of future, avoidable accidents of the same type.

Despite his 1954 report entitled "A Device for Assisting Investigation into Aircraft Accidents" and a 1957 prototype FDR called "The ARL Flight Memory Unit", aviation authorities from around the world were largely uninterested. This changed in 1958 when Sir Robert Hardingham, the Secretary of the UK Air Registration Board, visited the ARL and was introduced to Warren.

1962 ARL encoder/recorder units by Lane Sear and Wally Boswell.
1962 ARL encoder/recorder units by Lane Sear and Wally Boswell.

The Aeronautical Research Laboratory allocated Dr. Warren an engineering team to develop the prototype to airborne stage. The team, consisting of electronics engineers Lane Sear, Wally Boswell and Ken Fraser developed a working design incorporating a fire and shockproof case, a reliable system for encoding and recording aircraft instrument readings and voice on one wire, and a ground-based decoding device.

The ARL system became the "Red Egg", the world's first commercial FDR, made by the British firm of S. Davall & Son. The "Red Egg" got its name from its shape and bright red color.

The term "Black Box" came from a meeting about the "Red Egg", when afterwards a journalist told Dr. Warren, "This is a wonderful black box." The unit itself was based on an EMI Minifon wire recorder (originally a 1950's espionage gadget from the west-german manufacterer Protona Monske) fitted into a perspex box firmly screwed together.[citation needed]

[edit] Design

The design of today's FDR is governed by the internationally recognised standards and recommended practices relating to flight recorders which are contained in ICAO Annex 6 which makes reference to industry crashworthiness and fire protection specifications such as those to be found in the European Organisation for Civil Aviation Equipment[1] documents EUROCAE ED55, ED56A and ED112 (Minimum Operational Performance Specification for Crash Protected Airborne Recorder Systems). In the United States, the Federal Aviation Administration (FAA) regulates all aspects of U.S. aviation, and cites design requirements in their Technical Standard Order,[2] based on the EUROCAE documents (as do the aviation authorities of many other countries).

After the crash of Gol Transportes Aéreos Flight 1907, Brazilian Air Force personnel recover the flight data recorder of PR-GTD, the Boeing 737-8EH used for the flight, in the Amazon Rainforest in Mato Grosso, Brazil.
After the crash of Gol Transportes Aéreos Flight 1907, Brazilian Air Force personnel recover the flight data recorder of PR-GTD, the Boeing 737-8EH used for the flight, in the Amazon Rainforest in Mato Grosso, Brazil.

Currently, EUROCAE specifies that a recorder must be able to withstand an acceleration of 3400 g (33 km/s²) for 6.5 milliseconds. This is roughly equivalent to an impact velocity of 270 knots and a deceleration or crushing distance of 450 cm. Additionally, there are requirements for penetration resistance, static crush, high and low temperature fires, deep sea pressure, sea water immersion, and fluid immersion.

Modern day FDRs are typically plugged into the aircraft's fly-by-wire main data bus. They record significant flight parameters, including the control and actuator positions, engine information and time of day. There are 88 parameters required as a minimum under current U.S. federal regulations (only 29 were required until 2002), but some systems monitor many more variables. Generally each parameter is recorded a few times per second, though some units store "bursts" of data at a much higher frequency if the data begins to change quickly. Most FDRs record aproximatley 17-25 hours worth of data in a continuous loop.

This has also given rise to flight data monitoring programs, whereby flights are analyzed for optimum fuel consumption and dangerous flight crew habits. The data from the FDR is transferred, in situ, to a solid state recording device and then periodically analyzed with some of the same technology used for accident investigations.

FDRs are usually located in the rear of the aircraft, typically in the tail. In this position, the entire front of the aircraft acts as a "crush zone" to reduce the shock that reaches the recorder. Also, modern FDRs are typically double wrapped, in strong corrosion-resistant stainless steel or titanium, with high-temperature insulation inside.

[edit] Future devices

Since the recorders can sometimes be crushed into unreadable pieces, or even never located in deep water, some modern units are self-ejecting (taking advantage of kinetic energy at impact to separate themselves from the aircraft) and also equipped with radio and sonar beacons (see emergency locator transmitter) to aid in their location.

Alternatively other aircraft such as the Space Shuttle Orbiter do not possess an FDR, but instead use down-links to transfer such data. This kind of system could potentially see wider use in aviation in modified form.

On 19 July 2005, the Safe Aviation and Flight Enhancement Act of 2005 was introduced and referred to the Committee on Transportation and Infrastructure of the U.S. House of Representatives. This bill would require installation of a second cockpit voice recorder, digital flight data recorder system and emergency locator transmitter that utilizes combination deployable recorder technology in each commercial passenger aircraft, currently required to carry each of those recorders. The deployable recorder system would be ejected from the rear of the aircraft at the moment of an accident. The bill was referred to the Subcommittee on Aviation and has not progressed since.[3][4] One problem for the military is that these commercial devices offer no protection of the data that has been recorded thus have the potential for exposing military secrets if the device is captured by non-friendly forces and exploited.

[edit] Flight Data Recorders for Radio Controlled Models

RC FDR
RC FDR

Reductions in the cost and size of electronic components, coupled with the increased sophistication and popularity of radio controlled vehicles, have led to the development of miniature, low cost RC Flight Data Recorders which measure many of the same parameters logged by full sized Recorders.

An example of one of these recorders (pictured) measures altitude, airspeed, motor RPM, temperatures, servo positions, and several other parameters, and weighs less than 30 grams (1 ounce).

[edit] See also

[edit] References

  1. ^ European Organisation for Civil Aviation Equipment
  2. ^ TSO-C124a FAA Regs.
  3. ^ Search Results - THOMAS (Library of Congress)
  4. ^ Search Results - THOMAS (Library of Congress)

[edit] External links

Wikimedia Commons has media related to:

[edit] General information

[edit] Dr David Warren

This article contains material that originally came from an NTSB website. According to their site usage guidelines, "Text appearing on NTSB Web pages, in reports, recommendation, and public dockets, unless otherwise noted, was prepared by employees of the United States Government as part of their official duties and, therefore, is not subject to copyright." For more information, please review NTSB's use policies.