NATIONAL TRANSPORTATION SAFETY BOARD WASHINGTON, D.C. SAFETY RECOMMENDATION LETTER TO THE FAA dated NOVEMBER 21, 1994, AND RESPONSES.

Similar documents
UNITED STATES OF AMERICA NATIONAL TRANSPORTATION SAFETY BOARD WASHINGTON, D.C.

SA A NATIONAL TRANSPORTATION SAFETY BOARD. Airplane Performance Study Korean Air Flight 801 DCA97MA058. Docket No. Exhibit No. WASHINGTON, D.C.

MetConsole LLWAS (Low Level Wind Shear Alert System)

NATIONAL TRANSPORTATION SAFETY BOARD Office of Research and Engineering Vehicle Performance Division (RE60) Washmgton, D.C

METEOROLOGY PANEL (METP) WORKING GROUP- METEOROLOGICAL OPERATION GROUP (MOG) FIRST MEETING

A Path to Shed Light on the Windshear. Enhancing the windshear alerting systems in airports by integrating a LiDAR-based system.

AERODROMES PANEL (AP) VISUAL AIDS WORKING GROUP (VAWG) FIFTH MEETING. Montréal, Canada, 25 to 27 June 2008

QNH: With this setting set on your altimeter you will be reading altitude above mean sea level based on the local station pressure.

Section 7: Hazard Avoidance

Doppler Weather Radars and Weather Decision Support for DP Vessels

Real-Time defenses. FlightOPS

Gleim Private Pilot FAA Knowledge Test 2015 Edition, 1st Printing Updates July 2015

Advances in Weather Technology

National Transportation Safety Board Aviation Accident Final Report

NCAR UCAR. 50 th Anniversary Lecture

Use of radar to detect weather

HEIGHT ALTITUDE FLIGHT LEVEL

AWOS Level Descriptions

Inspection of. Aerodrome Lighting Federal Aviation 1. Administration

Airport Wind Observations Architectural Analysis

M o d u l e k A i r c r a f t A e r o d y n a m i c s, S t r u c t u r e s a n d S y s t e m s

Analysis of Ground-Based Radar Low- Altitude Wind-Shear Detection in OEP Terminal Airspace for NextGen

The Montague Doppler Radar, An Overview

SAMPLE. SITE SPECIFIC WEATHER ANALYSIS Rainfall Report. Bevens Engineering, Inc. Susan M. Benedict REFERENCE:

Example of Aircraft Climb and Maneuvering Performance. Dr. Antonio A. Trani Professor

A Bayesian. Network Model of Pilot Response to TCAS RAs. MIT Lincoln Laboratory. Robert Moss & Ted Londner. Federal Aviation Administration

Applying GIS Data to Radar Video Maps Air Traffic Control Towers

SAMPLE. SITE SPECIFIC WEATHER ANALYSIS Wind Report. Robinson, Smith & Walsh. John Smith REFERENCE:

MetConsole AWOS. (Automated Weather Observation System) Make the most of your energy SM

MK V and MK VII Enhanced Ground Proximity Warning System Pilot's Guide Rev. D - March 2000 MK V & MK VII EGPWS Pilot Guide 1

BEFORE THE PUBLIC SERVICE COMMISSION OF MARYLAND

Three-Dimensional Aerial Zoning around a Lebanese Airport

SUMMARY. information from

Technical Assessment of the Impact of Decommissioning the TDWR on Terminal Weather Services

Aircraft Icing FAR/CS-25, Appendix O and P charts

SCOPE: Outlines standard techniques for setting up and conducting voice communication and broadcasting ATIS at Hong Kong VACC

TERMS OF REFERENCE Special Committee (SC) 230 Airborne Weather Detection Systems Revision 5

CHAPTER 26 PLANNING AND ZONING ARTICLE XIV. AIRPORT OVERLAY ZONING

EMADDC. towards operational collection of Mode-S EHS observations in Europe

Pursuant to Section 205 of the Federal Power Act ( FPA ) 1 and the Commission s

P1.1 THE NATIONAL AVIATION WEATHER PROGRAM: AN UPDATE ON IMPLEMENTATION

HIGH DENSITY EN ROUTE AIRSPACE SAFETY LEVEL AND COLLISION RISK ESTIMATION BASED ON STORED AIRCRAFT TRACKS

Human Factors Assessment of Runway Status Lights (RWSL) and Final Approach Runway Occupancy Signal (FAROS) Maria Picardi Kuffner

Lightning Safety in a Flash / VAISALA AIRPORT LIGHTNING INFORMATION SYSTEM (ALIS)

Published by the Hong Kong Observatory, Hong Kong Special Administrative Region Government.

Appendix A Zoning Ordinance

SCOPE: Outlines standard techniques for setting up and conducting voice communication and broadcasting ATIS at Hong Kong VACC

METEOROLOGICAL WARNINGS STUDY GROUP (METWSG)

DE PUBLIC SERVICE COMPANY OF NEW HAMPSHIRE

Guidance on Aeronautical Meteorological Observer Competency Standards

LANDMARK TM. Class B TAWS

Responsibilities: Effective Date: November Revision Date: February 8, VP, Facilities and Construction Management. Issuing Authority:

July 13, 2017 Session #1 In Lieu of the Surface Observation Including EWINS Authority, RTMA, Web Cams, and Remote Observation Systems

Acquisition of Multi-Function Equipment at DIA: Conditions, Factors, Considerations & Integration. Presented by Mike Carlson September 20, 2012

SOLAR PHOTOVOLTAIC ENERGY FACILITIES: ASSESSMENT OF POTENTIAL FOR IMPACT ON AVIATION. January Report No.10/344/RPS/1

8.7 Calculation of windshear hazard factor based on Doppler LIDAR data. P.W. Chan * Hong Kong Observatory, Hong Kong, China

Deutscher Wetterdienst

AERODROME METEOROLOGICAL OBSERVATION AND FORECAST STUDY GROUP (AMOFSG)

Flight Operations Briefing Notes

A compilation of key maintenance and performance articles taken from the former Lycoming Flyer Newsletter. Lycoming Flyer Key Reprints

DISCLAIMER NOTICE BEST AVAILABLE COPY

Hong Kong Collection

StormReady Supporter Application Form updated by NWS Chanhassen on April 7, Name of Applying Entity: Point of Contact: Title:

NATIONAL TRANSPORTATION SAFETY BOARD WASHINGTON, D.C.

All Weather Wind Monitoring with Integrated Radar and Lidar

INTEGRATED TURBULENCE FORECASTING ALGORITHM 2001 METEOROLOGICAL EVALUATION

The current status, functions, challenges and needs of South Sudan Meteorological Department (SSMD)

AERODROME METEOROLOGICAL OBSERVATION AND FORECAST STUDY GROUP (AMOFSG)

Vaisala Blitzdetektion. Michael Kalkum

TERMS OF REFERENCE Special Committee (SC) 230 Airborne Weather Detection Systems Revision 2

Which instrument will become inoperative if the pitot tube becomes clogged?

STANDARD OPERATING PROCEDURES

GPS and Mean Sea Level in ESRI ArcPad

AOPA. Mitigating Turbulence Impacts in Aviation Operations. General Aviation Perspective

IMS4 ARWIS. Airport Runway Weather Information System. Real-time data, forecasts and early warnings

Learning. Goals. of pressure. aircraft. Altimeter knob. Page 1 of 8. Document : V1.1

A tail strike event of an aircraft due to terrain-induced wind shear at the Hong Kong International Airport

P R E A M B L E. The module is run with the following pattern over 3 weeks. Introduction (1 hour) Facilitated Practical Class (2 hours)

WIND DATA REPORT FOR THE YAKUTAT JULY 2004 APRIL 2005

9.4 INITIAL DEPLOYMENT OF THE TERMINAL DOPPLER WEATHER RADAR SUPPLEMENTAL PRODUCT GENERATOR FOR NWS OPERATIONS

SAMPLE. SITE SPECIFIC WEATHER ANALYSIS Wind Report. Robinson, Smith & Walsh. John Smith. July 1, 2017 REFERENCE: 1 Maple Street, Houston, TX 77034

CHAPTER 3 HELIPORT AND HELICOPTER STAGEFIELD LIGHTING SYSTEMS

AVIATION INVESTIGATION REPORT A04A0057 WING SCRAPE DURING A REJECTED LANDING

COMPARISON OF DOPPLER LIDAR OBSERVATIONS OF SEVERE TURBULENCE AND AIRCRAFT DATA. S.T. Chan * and C.W. Mok Hong Kong Observatory, Hong Kong

Safety in Numbers SKYWATCH 497. The affordable original.

Observations from Plant City Municipal Airport during the time period of interest are summarized below:

EXHIBIT H LOT 317 GRADING AND SITE PLAN

The PEAC-WMD Gamma Radiation Dose Calculator

An Application of the Improved Models for Risk Assessment of Runway Excursion in Korea

Hazard Communications

National Transportation Safety Board Office of Aviation Safety Washington, D.C December 10, 2012 WEATHER STUDY DCA13RA025

P474 SYDNEY AIRPORT WIND SHEAR ENCOUNTER - 15 APRIL 2007

Comprehensive Winter Maintenance Management System BORRMA-web MDSS inside to increase Road Safety and Traffic Flow

Fume Hood Face Velocity Can it Ensure Safe Containment?

Robert Barron*, National Center for Atmospheric Research, and Vaughn Yates, Federal Aviation Administration

Operational Applications of Awos Network in Turkey

Remote Sensing of Windshear under Tropical Cyclone Conditions in Hong Kong

Review of Anemometer Calibration Standards

SERIOUS INCIDENT. Aircraft Type and Registration: 2) Embraer EMB 121 Xingu F-TEZZ. Date & Time (UTC): 1 June 2010 at 1000 hrs.

UN-GGIM: Europe ExCom 1 June 2016 Francfort Work Group A «Core Data» Status and Progress François Chirié, France

Transcription:

DOCKET NO.: SA-517 EXHIBIT NO. 3-R NATIONAL TRANSPORTATION SAFETY BOARD WASHINGTON, D.C. SAFETY RECOMMENDATION LETTER TO THE FAA dated NOVEMBER 21, 1994, AND RESPONSES (22 pages)

/ /7 8!?>3 @. National Transportation Safety Board g 2.$ Washington, D.C. 20594 %. && Safety Recommendation FILE COPY Date: November 21, 1994 In reply refer to: A-94-186 through -188 Honorable David R. Hinson Administrator Federal Aviation Administration Washington, D.C. 20591 The National Transportation Safety Board s investigation of a recent accident involving a landing approach, in instrument meteorological conditions, at Washington Dunes International Airport (IAD), has revealed software discrepancies with the minimum safe altitude warning system (MSAW) and low level windshear alert system (LLWAS) operating at IAD at the time of the accident. The discrepancies are believed to affect the accuracy of the warning systems. The Safety Board believes that action is required to correct the discrepancies at IAD, and may be required to correct similar discrepancies at other airports throughout the country. The investigation found two apparent discrepancies in the site variables used in the MSAW program at IAD. Both were identified from the Absolute Assembly of MSAWD for A305-L0 Dunes (IAD) document, dated October 29, 1993. The first discrepancy was found in the document on page 9, line 6570. This site variable is the definition of the runway 1R threshold in Cartesian coordinates (distance) relative to the air surveillance radar antenna. The Safety Board was informed by the Federal Aviation Administration (FAA) that the Automated Radar Terminal System (ARTS) III software at IAD was programmed for a 10 west variation, which is the current angular difference between true north and magnetic north at the Dunes airport. However, when a 10 variation was applied to establish the coordinate 6473 ~-t

2 reference, the resultant position for the runway lr threshold did not correlate to the actual geographic runway location. It was found that the radar established position was 700 feet to the northeast from the actual runway threshold. It was determined that when a 7 west variation was used to establish the radar coordinate reference (instead of the correct 10 west variation) the coordinates for the runway 1R threshold corresponded to the actual location. The apparen radar position for the runway lr threshold resulted in a sinul g=e%~k radar MSAW capture box from its intended position with respect to the actual approach path to runway 1 R. This displacement might compromise the protective intent of the MSAW system. Although the Safety Board examined the coordinates for the runway lr threshold only, the Board believes that similar discrepancies exist in the radar locations for the other runway thresholds at Dunes. The second discrepancy identified in the MSAW program was the defined minimum descent altitude (MDA) for the runway 1R capture box. Document NAS- MD-633, Section 3.2 states: ILS localizer only MDA should not be used where another nonprecision approach exists. Nevertheless, some locations may, because of particular operational characteristics; e.g., absence of another nonprecision approach to a runway, need to adapt ILS localizer only MDA. The lower limit for the runway lr capture box was 267 feet above ground level (agl). This altitude was derived by subtracting the 3 13-foot field elevation and a 100-foot margin from the localizer-only MDA of 680 feet mean sea level (msl). However, runway lr has a nondirectional beacon (NDB) approach with an MDA of 760 feet msl. Based on the information and criteria provided to the Safety Board, it appears that the NDB approach MDA should have been used in establishing the runway lr capture box lower limit. This would produce an alarm at 347 feet agl, 80 feet higher than the existing capture box. The Safety Board has not been provided with a written rationale, if one exists, for using the 267-foot base rather than a 347-foot base for the capture box. The offset of the MSAW capture box should be corrected, and it would seem prudent to conduct a one-time campaign of all MSAW programs to ensure that they are correctly configured. In addition, the q-z

3 lower limit of the MSAW capture box should conform to published criteria, or documentation that details the allowable deviations from the criteria should be published. An FAA memorandum dated July 7, 1994, responding to an official investigative request for information about the IAD LLWAS, stated that the geometric configuration fiie (GCF) in use was actually the GCF for Tampa International Airport Florida. The memorandum further stated: It seems likely that IAD was using the incorrect LLWAS configuration at the time of the incident. However, IAD is currently using the correct configuration file. Although the Safety Board function of LLWAS would be Environmental Support Engineering believes that the basic windshear detection unaffected by the discrepancy, the FAA Branch (AOS-220) advised us that to realize the capability of the enhanced Phase II LLWAS software, to provide optimum microburst detection, it is necessary to input an appropriate GCF that is distinct and unique to the airport of concern. The Safety Board notes that the GCF at IAD has been corrected, but it is concerned that other airports with LLWAS installations may also have installed inappropriate configuration files. As a result of its investigation of this accident the National Transportation Safety Board recommends that the Federal Aviation Administration Review the calculations establishing the runway threshold coordinates for all runways at IAD with respect to the air surveillance radar to verify proper alignment of the MSAW capture boxes. (Class II, Priority Action) (A-94-186) Conduct a complete national review of all radar environments using MSAW systems. This review should address all user-defined site variables for the MSAW programs that control general terrain warnings, as well as runway capture boxes, to ensure compliance with prescribed procedures. (Class II, Priority Action) (A-94-187) R-3

4 Ensure that all airports equipped with the Phase II (enhanced) LLWAS are using geometric configuration files appropriate to those facilities. (Class II Priority Action) (A-94-188) Chairman HALL, and Members LAUBER, HAMMERSCHMIDT and VOGT concurred in these recommendations. By &4 Jun H an 44( m.