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Standard

FLIGHT DATA RECORDER

2011-06-07
CURRENT
ARIC747-3
This document provides design guidance for the development and installation of Flight Data Recorders (FDR) which may utilize solid state memory and which may employ some means of data compression. The Flight Data Recorder will be utilized with a Flight Data Acquisition Unit (FDAU) (ARINC Characteristic 573) or a Digital Flight Data Acquisition Unit (DFDAU) (ARINC Characteristic 717) to accommodate mandatory flight data recording and other flight data acquisition needs. ...This document provides design guidance for the development and installation of Flight Data Recorders (FDR) which may utilize solid state memory and which may employ some means of data compression. ...The Flight Data Recorder will be utilized with a Flight Data Acquisition Unit (FDAU) (ARINC Characteristic 573) or a Digital Flight Data Acquisition Unit (DFDAU) (ARINC Characteristic 717) to accommodate mandatory flight data recording and other flight data acquisition needs.
Technical Paper

Flight Test and Evaluation of Fluidic Flight Control

1987-10-01
871864
This paper presents the results of a multi-year project by the Naval Air Development Center to design, fabricate, evaluate, and flight test a fluidic flight control system in a Navy T-2C, a twin-jet carrier aircraft. The work leading to this flight test began with component design to the aircraft installation constraints and to flight requirements, continued through fabrication, laboratory testing and system installation, and culminated with man-in-the-loop evaluation of the system installed in the aircraft, ground tests, and flight. ...The work leading to this flight test began with component design to the aircraft installation constraints and to flight requirements, continued through fabrication, laboratory testing and system installation, and culminated with man-in-the-loop evaluation of the system installed in the aircraft, ground tests, and flight. ...The work leading to this flight test began with component design to the aircraft installation constraints and to flight requirements, continued through fabrication, laboratory testing and system installation, and culminated with man-in-the-loop evaluation of the system installed in the aircraft, ground tests, and flight. The results of these tests demonstrate the successful integration of three advanced technologies: 8000-psi actuationcontrolled both by fluidics and fly-by-wirewhich the Naval Air Development Center has brought to fruition.
Technical Paper

The Impact of Automation on Flight Test

1982-02-01
821450
This paper will emphasize the changing methodology of the FAA certification process with some specific examples of recent flight test programs.
Technical Paper

YJ101/YF-17 Flight Test Experience

1976-02-01
760932
A description is presented of the YJ101 engine as well as the unique development program leading to flight qualification. Two specific achievements are reviewed; first, the inlet-engine compatibility, and second, engine life evaluation. ...Realistic engine development testing is recognized as a key requirement for the engine industry. Correlation of factory testing with service usage is important to the development of a methodology for engine testing. ...Correlation of factory testing with service usage is important to the development of a methodology for engine testing. An analysis of the actual YF-17 engine operation is made and compared to factory development testing.
Technical Paper

Human Factors Analysis of Naval Transport Aircraft Maintenance and Flight Line Related Incidents

1999-08-10
1999-01-2981
To study maintainer error, the Naval Safety Center’s Human Factors Accident Classification System (HFACS) was adapted for Maintenance Related Mishaps (MRMs). The HFACS Maintenance Extension (ME) successfully profiled the errors present Naval Aviation Class A MRMs. In order to assess its suitability for studying major and minor airline accidents, a post hoc analysis was conducted on 124 Naval Fleet Logistics Support (VR) Wing maintenance related mishap, hazard, and injury reports. Two judges separately coded the 124 VR Wing incidents; a Cohen’s kappa of .78 was achieved, indicating an “excellent” level of agreement. Generally, HFACS-ME was able to profile maintainer errors found in more minor incidents and the factors that contribute to them. Common factors observed include errors attributed to third party maintenance, inadequate supervision, failed communications, skill-based errors, and procedural violations.
Standard

ENHANCED AIRBORNE FLIGHT RECORDER

2017-05-29
CURRENT
ARIC767-1
The EAFR standard addresses combinations of any or all of the following in a single Line Replaceable Unit (LRU), a Digital Flight Data Recorder (DFDR) function, a Cockpit Voice Recorder (CVR) function, a data link recording function, and an image recording function. ...This document is intended to provide design guidance for the development and installation of an Enhanced Airborne Flight Recorder (EAFR). The EAFR standard addresses combinations of any or all of the following in a single Line Replaceable Unit (LRU), a Digital Flight Data Recorder (DFDR) function, a Cockpit Voice Recorder (CVR) function, a data link recording function, and an image recording function. ...This document does not address the overall flight data recorder system requirements but considers interface and system standards. This document does not replace ARINC Characteristic 747 which defines DFDRs.
Standard

DIGITAL FLIGHT DATA RECORDER

1988-01-21
CURRENT
ARIC542A
This standard includes specific requirements necessary to support flight data recording and other flight data acquisition needs. Design details necessary to ensure interchangeability of equipment in a standard aircraft installation is included.
Standard

ELECTRONIC FLIGHT INSTRUMENTS (EFI)

2013-06-01
CURRENT
ARIC725-2
The EFI provides display functions that include Attitude Director Indicator (ADI), Horizontal Situation Indicator (HSI), Air Data, Map display, Weather display, Radio Altitude data, Flight Control Mode annunciation, Flight Path information, and Flight Warning display.
Standard

Flight Management System (FMS)

2001-12-14
CURRENT
ARP4102/9A
This document recommends criteria and requirements for a Flight Management System (FMS) for transport aircraft. The FMS shall provide the functions of Lateral Navigation, Vertical Navigation, and Performance Management and may include Time of Arrival Control.
Standard

FLIGHT WARNING COMPUTER SYSTEM

1981-09-10
CURRENT
ARIC726-1
It is intended to process caution and warning inputs for visual and/or audible presentation to the flight crew.
Standard

FLIGHT CONTROL COMPUTER SYSTEM

1983-04-01
CURRENT
ARIC701-1
This standard sets forth the characteristics of a FCCS within an Automatic Flight System. The FCCS is intended to provide autoland capability for commercial aircraft. The document provides design guidance for the development and installation of a FCCS.
Standard

FLIGHT MANAGEMENT COMPUTER SYSTEM

1994-06-01
CURRENT
ARIC702-6
The FMCS provides performance data, performance computations, fuel management functions, and navigation and guidance to a desired flight plan.
Standard

Recommended Insertion Loss Test Methods for EMI Power Line Filters

2012-08-10
CURRENT
ARP4244A
This document presents standard methods to evaluate the common mode and differential mode insertion loss of passive electromagnetic interference power line filters from 10 kHz through 10 GHz. Insertion loss test methods for both quality assurance and performance prediction purposes are described. ...The performance prediction tests are selected to more closely approximate operating impedances. They are not intended to be inclusive or to represent worst case conditions.
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