DOCSLIB.ORG

Runway Collision, United Express Flight 5925 and Beechcraft King Air

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Runway Collision, United Express Flight 5925 and Beechcraft King Air / PB97-910404 NTSB/AAR-97/04 DCA97MA009A/B NATIONAL TRANSPORTATION SAFETY BOARD WASHINGTON, D.C. 20594 AIRCRAFT ACCIDENT REPORT RUNWAY COLLISION UNITED EXPRESS FLIGHT 5925 AND BEECHCRAFT KING AIR A90 QUINCY MUNICIPAL AIRPORT QUINCY, ILLINOIS NOVEMBER 19,1996 The National Transportation Safety Board is an independent Federal agency dedicated to promoting aviation, railroad, highway, marine, pipeline, and hazardous materials safety. Established in 1967, the agency is mandated by Congress through the Independent Safety Board Act of 1974 to investigate transportation accidents, determine the probable causes of the accidents, issue safety recommendations, study transportation safety issues, and evaluate the safety effectiveness of government agencies involved in transportation. The Safety Board makes public its actions and decisions through accident reports, safety studies, special investigation reports, safety recommendations, and statistical reviews. Information about available publications may be obtained by contacting: National Transportation Safety Board Public Inquiries Section, RE-51 490 L’Enfant Plaza, S.W. Washington, D.C. 20594 (202)314-6551 (800)877-6799 Safety Board publications may be purchased, by individual copy or by subscription, from: National Technical Information Service 5285 Port Royal Road Sprin~leld, Virginia 22161 (703)487-4600 NTSB/AAR-97/04 PB97-910404 NATIONAL TRANSPORTATION SAFETY BOARD WASHINGTON, D.C. 20594 AIRCRAFT ACCIDENT REPORT RUNWAY COLLISION UNITED EXPRESS FLIGHT 5925 AND BEECHCRAFT KING AIR A90 QUINCY MUNICIPAL AIRPORT QUINCY, ILLINOIS NOVEMBER 19, 1996 Adopted: July 1, 1997 Notation 6793C Abstract: This report explains the accident involving United Express flight 5925, a Beechcraft 1900C, and a Beechcraft King Air A90 that collided at the intersection of runway 13 and runway 04 at Quincy Municipal Airport, near Quincy, Illinois, on November 19, 1996. Safety issues in the report include the importance of emphasizing careful scanning techniques during flight training, Beech 1900C certification standards and compliance with requirements on door jamming, the certification of small airports used by scheduled commuter airlines, and aircraft rescue and fire fighting protection on scheduled commuter aircraft having 10 seats or more. Safety recommendations concerning these issues were made to the Federal Aviation Administration. September 5, 2000 The National Transportation Safety Board adopted revisions to the findings and probable cause for this accident, as indicated below. For more information, see Response to Petition for Reconsideration Finding 15 In the findings list and the accident report text (Section 2.5, “Survival Aspects,” on page 48, sixth paragraph), replaced “the occupants of the Beech 1900C did not escape because the air stair door could not be opened and the left overwing exit hatch was not opened” with “the occupants of the Beech 1900C did not escape because the air stair door and the left overwing exit hatch were not opened for undetermined reasons.” Finding 16 In the findings list, deleted “the most likely reason that the air stair door could not be opened is that the accident caused deformation of the door/frame system and created slack in the door control cable.” Renumbered the remaining findings accordingly. In the accident report text (Section 2.5.1, “Air Stair Door,” on page 49, fifth paragraph), deleted “the Safety Board concludes that the most likely reason that the air stair door could not be opened is that the accident caused deformation of the door/frame system and created slack in the door control cable. The Safety Board is concerned that the design and testing of the door did not account for minimal permanent deformation that could introduce slack into the door control system and ultimately disable the door.” In the accident report text (Section 2.5.1, “Air Stair Door,” on page 49, sixth paragraph), replaced “the Safety Board is further concerned that even though the impact forces from the accident were so mild that both airplanes came to rest on their landing gear and the occupants of the Beech 1900C sustained little or no injuries as a result, those same forces were apparently sufficient to cause the Beech 1900C’s air stair door to jam, preventing the occupants from using it to escape” with “the Safety Board is further concerned that, even though the impact forces from the accident were such that both airplanes came to rest on their landing gear and the occupants of the Beech 1900C did not sustain blunt force trauma injuries as a result, the door was not opened by any of the occupants for undetermined reasons.” a-1 Finding 17 In the findings list, deleted “the methods for showing compliance with the FAA’s certification requirement that external doors be reasonably free from jamming as a result of fuselage deformation are not clearly defined.” Renumbered the remaining findings accordingly. In the accident report text (Section 2.5.1, “Air Stair Door,” on page 50, second complete paragraph), deleted “the Safety Board concludes that the methods for showing compliance with the FAA’s certification requirement that external doors be reasonably free from jamming as a result of fuselage deformation are not clearly defined.” Finding 18 In the findings list, deleted “the FAA’s freedom from jamming certification standards may be inadequate.” Renumbered the remaining findings accordingly. In the accident report text (Section 2.5.1, “Air Stair Door,” on page 50, third complete paragraph), deleted “further, because the air stair door on the accident airplane jammed as a result of an impact that caused little or no injury to the occupants of the airplane, the Safety Board concludes that the FAA’s freedom from jamming certification standards may be inadequate.” Probable Cause Replaced “contributing to the severity of the accident and the loss of life were the lack of adequate aircraft rescue and firefighting services, and the failure of the air stair door on the Beech 1900C to open” with “contributing to the severity of the accident and the loss of life were the lack of adequate aircraft rescue and firefighting services and the failure of the air stair door on the Beech 1900C to be opened.” a-2 This page intentionally left blank CONTENTS EXECUTIVE SUMMARY............................................................................................................vi 1. FACTUAL INFORMATION.....................................................................................................1 1.1 History of Flight....................................................................................................................1 1.2 Injuries to Persons.................................................................................................................4 1.3 Damage to Airplane...............................................................................................................4 1.4 Other Damage........................................................................................................................4 1.5 Personnel Information...........................................................................................................4 1.5.1 Flight 5925 Flightcrew.......................................................................................................4 1.5.1.1 Captain Information........................................................................................................4 1.5.1.2 First Officer Information.................................................................................................7 1.5.2 King Air Occupants............................................................................................................7 1.5.2.1 King Air Pilot-in-Command............................................................................................7 1.5.2.2 King Air Pilot/Passenger.................................................................................................8 1.6 Airplane Information.............................................................................................................9 1.6.1 Beech 1900C......................................................................................................................9 1.6.1.1 Beech 1900C Emergency Exit Door Certification – Freedom from Jamming..............10 1.6.2 King Air A90....................................................................................................................13 1.7 Meteorological Information................................................................................................14 1.8 Aids to Navigation..............................................................................................................14 1.9 Communications.................................................................................................................14 1.10 Airport Information...........................................................................................................15 1.11 Flight Recorders................................................................................................................15 1.12 Wreckage and Impact Information....................................................................................18 1.12.1 Beech 1900C Wreckage Information.............................................................................18 1.12.2 King Air A90 Wreckage Information.............................................................................18 1.13 Medical and Pathological Information..............................................................................19
Load more

Recommended publications
  • Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft
    Air s.Pace ELectric Innovative Commuter Aircraft D2.1 Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft Name Function Date Author: Maximilian Spangenberg (ASP) WP2 Co-Lead 31.03.2020 Approved by: Markus Wellensiek (ASP) WP2 Lead 31.03.2020 Approved by: Dr. Qinyin Zhang (RRD) Project Lead 31.03.2020 D2.1 Economic Feasibility Study page 1 of 81 Clean Sky 2 Grant Agreement No. 864551 © ELICA Consortium No export-controlled data Non-Confidential Air s.Pace Table of contents 1 Executive summary .........................................................................................................................3 2 References ........................................................................................................................................4 2.1 Abbreviations ...............................................................................................................................4 2.2 List of figures ................................................................................................................................5 2.3 List of tables .................................................................................................................................6 3 Introduction ......................................................................................................................................8 4 ELICA market study ...................................................................................................................... 12 4.1 Turboprop and piston engine
    [Show full text]
  • TCDS A.064 ANNEX - Airbus A318, A319, A320, A321 - Special Conditions
    TCDS A.064 ANNEX - Airbus A318, A319, A320, A321 - Special Conditions This annex to the EASA TCDS A.064 was created to publish selected Special Conditions, Equivalent Safety Findings that are part of the applicable certification basis and particular Interpretative Material: Table of Content: D-0306-000: Application of Heat Release and Smoke Density Requirements to Seat Materials 2 D-0322-001: Installation of suite type seating .................................................................. 3 E10: High Altitude Airport Operations (up to 14,100 ft) ...................................................... 5 E-18: Improved flammability standards for thermal / acoustic insulation materials - ESF to JAR 25.853(b) and 25.855(d) ............................................................................ 6 E-2105: Type III Overwing Emergency Exit Access ............................................................ 7 E-2107: Passenger Extension to 180 ................................................................................ 9 E-34: Seats with Inflatable Restraints .............................................................................10 E-3002: Reclassification of doors 2 & 3 to type III ............................................................12 E-4001: Exit configuration .............................................................................................13 G-1006: ETOPS ............................................................................................................14 H-01: Enhanced Airworthiness Programme
    [Show full text]
  • Beechcraft Accessories
    BEECHCRAFT ACCESSORIES BEECHCRAFT ACCESSORIES CESSNA GOLDEN EAGLE YOKE EMBLEM Designed & built by real-world pilots, manufactured to the highest Replace Your Original, Damaged, Or Missing standards. These products are built for those incomparable Beechcraft. Yoke Inserts With Our New Faux Carbon Fiber CM Years of experience and the highest quality materials and construction Insert! Includes Beautiful Domed Golden result in the best products available for Bonanzas & Barons. All have Eagle Emblem (Does NOT Include Yoke or FAA STC/PMA as applicable. Padded Surround) Faux Carbon Fiber Insert Is BONANZA/BARON CONTROL YOKE LOCK Same Size As Your Original Piece - Installation Protect your investment with this heat treated lock. It Instructions Included. installs quickly and simply ( no modification is needed) P/N 09-03786 .........$137.75 WP but cannot be removed without being unlocked. It is a permanent, direct replacement for the original equip- BEECH BONANZA YOKE EMBLEM ment. Complete with the highest quality lock, instruc- This Is A Beautiful Domed tions, and all hardware. ...............................P/N 05-00649 .........$376.00 Black and Gold Emblem, Optional clipboard for clearances or notes makes a stable flight center. Approximately 1.1” High, ME Spring-loaded, it snaps out of the way in seconds. 7.3” Wide, 1/32” Thick, For P/N 05-01335 .........$202.95 Peel ‘n Stick Application. BEECH THROTTLE, MIXTURE, PROP KNOB SET The Classic Beech “B” Is A Real Eye-Catcher! Designed Especially For These high-strength knobs for Bonanzas are a big improve- Bonanza Yokes, This Piece Can Be Applied Almost Anywhere! ment over old, cracked original equipment and likely the P/N 09-03868 ...........$33.50 HA best replacement knobs on the market.
    [Show full text]
  • Federal Register / Vol. 60, No. 23 / Friday, February 3, 1995 / Rules
    6652 Federal Register / Vol. 60, No. 23 / Friday, February 3, 1995 / Rules and Regulations decision on whether to grant or deny the Federal Aviation Administration (FAA) (SB) No. 2255, Revision V, dated request. has received several reports of these October 1993. improved design trusses cracking in Interested persons have been afforded PART 339ÐFUNCTIONS AND DUTIES Area A (as specified in the service an opportunity to participate in the OF CLERKS OF COURT REGARDING information) of the engine truss. This making of this amendment. Due NATURALIZATION PROCEEDINGS action retains the currently required consideration has been given to the two repetitive inspections, but shortens the comments received. 14. The authority citation for part 339 One commenter concurs with the continues to read as follows: repetitive inspection interval in Area A and eliminates the inspection- proposal as written. Authority: 8 U.S.C. 1103, 1433, 1448. terminating replacement option; and The other commenter concurs with 15. Section 339.2 is amended by also incorporates the Beech Models the actions specified in the proposal, adding a new paragraph (e) to read as 1900C and 1900D airplanes that have but states that the engine trusses on the follows: engine trusses of this same type design Beech Model 1900 airplanes are hard to installed at manufacture. The actions identify. This commenter states that § 339.2 Monthly reports. specified by this AD are intended to Beechcraft 1900 Airliner Communique * * * * * prevent failure of the engine truss No. 27, dated February 1993, presents (e) Use of reports for accounting assembly caused by a cracked engine information that helps identify the older purposes.
    [Show full text]
  • Aircraft Accident Report: American Airlines, Inc., Mcdonnell Douglas
    Explosive decompression, American Airlines, Inc., McDonnell Douglas DC-10-10, N103AA, Near Windsor, Ontario, Canada, June 12, 1972 Micro-summary: On climb, this McDonnell Douglas DC-10-10 experienced an opening of a cargo door, explosive decompression, and a main cabin floor collapse, disrupting the flight control system. Event Date: 1972-06-12 at 1925 EST Investigative Body: National Transportation Safety Board (NTSB), USA Investigative Body's Web Site: http://www.ntsb.gov/ Cautions: 1. Accident reports can be and sometimes are revised. Be sure to consult the investigative agency for the latest version before basing anything significant on content (e.g., thesis, research, etc). 2. Readers are advised that each report is a glimpse of events at specific points in time. While broad themes permeate the causal events leading up to crashes, and we can learn from those, the specific regulatory and technological environments can and do change. Your company's flight operations manual is the final authority as to the safe operation of your aircraft! 3. Reports may or may not represent reality. Many many non-scientific factors go into an investigation, including the magnitude of the event, the experience of the investigator, the political climate, relationship with the regulatory authority, technological and recovery capabilities, etc. It is recommended that the reader review all reports analytically. Even a "bad" report can be a very useful launching point for learning. 4. Contact us before reproducing or redistributing a report from this anthology. Individual countries have very differing views on copyright! We can advise you on the steps to follow.
    [Show full text]
  • Aircraft Library 
    Interagency Aviation Training Aircraft Library Disclaimer: The information provided in the Aircraft Library is intended to provide basic information for mission planning purposes and should NOT be used for flight planning. Due to variances in Make and Model, along with aircraft configuration and performance variability, it is necessary acquire the specific technical information for an aircraft from the operator when planning a flight. Revised: June 2021 Interagency Aviation Training—Aircraft Library This document includes information on Fixed-Wing aircraft (small, large, air tankers) and Rotor-Wing aircraft/Helicopters (Type 1, 2, 3) to assist in aviation mission planning. Click on any Make/Model listed in the different categories to view information about that aircraft. Fixed-Wing Aircraft - SMALL Make /Model High Low Single Multi Fleet Vendor Passenger Wing Wing engine engine seats Aero Commander XX XX XX 5 500 / 680 FL Aero Commander XX XX XX 7 680V / 690 American Champion X XX XX 1 8GCBC Scout American Rockwell XX XX 0 OV-10 Bronco Aviat A1 Husky XX XX X XX 1 Beechcraft A36/A36TC XX XX XX 6 B36TC Bonanza Beechcraft C99 XX XX XX 19 Beechcraft XX XX XX 7 90/100 King Air Beechcraft 200 XX XX XX XX 7 Super King Air Britten-Norman X X X 9 BN-2 Islander Cessna 172 XX XX XX 3 Skyhawk Cessna 180 XX XX XX 3 Skywagon Cessna 182 XX XX XX XX 3 Skylane Cessna 185 XX XX XX XX 4 Skywagon Cessna 205/206 XX XX XX XX 5 Stationair Cessna 207 Skywagon/ XX XX XX 6 Stationair Cessna/Texron XX XX XX 7 - 10 208 Caravan Cessna 210 X X x 5 Centurion Fixed-Wing Aircraft - SMALL—cont’d.
    [Show full text]
  • Sensory Overload
    AeroSafety WORLD 1,500 HOURS Are you really experienced? FIRST RESPONDERS Flight attendants and safety SKY’S THE LIMIT Single European Sky lags FIGHTING FOR ATTENTION SENSORY OVERLOAD THE JOURNAL OF FLIGHT SAFETY FOUNDATION DECEMBER 2012–JANUARY 2013 AIR ad2 v1a.pdf 1 2012-11-16 12:55 PM The AIR Group Specializing in Safety Systems Product Development and Aircraft Accident Investigation Consultancy Affordably Priced - Highly Capable Flight Analysis System (FASET Animation) Our Animation System is based on over twenty years of R&D in the field of aircraft accident/incident, Flight Data Monitoring and flight simulation, flight visualization technology. It was developed by industry leaders in flight animation systems. Seamlessly integrate into existing third party flight analysis systems or as a stand alone product. FASET will meet your needs and exceed your expectations. C M Y CM MY CY Thinking of adding animation or upgrading your current system, think FASET CMY K Flight Data Monitoring (FDM/FOQA) Services The AIR Group can assist with: • Full implementation of a managed service, eliminating the need for highly specialized internal FDM technical expertise. • Customized service to suit client specific operations. • Investigative assistance for significant flight safety events. • Producing standard or customized reports • Highly qualified experts who can design new measurements and assist with staff training. Aircraft Accident and Serious Incident support services • Post-Accident and Incident Reconstruction • Data Integration and Reconstruction • Technical Reporting, Critical Commentary • Safety and Defect Analysis Applied Informatics and Research Inc. / Accident Investigation and Research Inc. All Operators believe they are safe; however, the AIR Group offers comprehensive safety tools and capabilities to help you to confirm that you are safe.
    [Show full text]
  • Where's the Exit?
    CABINSAFETY Despite a briefing and illustrated safety cards, passengers on an Embraer 195 were unsure of what to do while using an overwing exit. © Daniel Guerra/Airliners.net BY LINDA WERFELMAN he U.K. Air Accidents Investigation Man. Five of the 95 people in the air- concerned about the possibility of fire, Branch (AAIB) has recommended plane received minor injuries during declared an emergency and diverted to design reviews and modifica- the evacuation. Ronaldsway. The fumes and smoke in- tions of emergency exits on public About 10 minutes after takeoff on a tensified during the surveillance radar Ttransport aircraft following an emer- scheduled passenger flight from Man- approach, and the captain “considered gency landing in which passengers in chester, England, to Belfast, Northern that he would probably conduct an an Embraer 195 became confused about Ireland, the no. 1 air cycle machine evacuation on landing,” the report said. how to use an overwing exit. (ACM) failed, sending fumes onto the He did not notify the cabin crew or The AAIB issued the safety recom- flight deck. The cabin crew reported air traffic control because “he thought mendations as a result of its investiga- an unusual odor and a haze in parts of that to tell them anything at this late tion of the Aug. 1, 2008, incident that the cabin. stage of the flight might cause confu- prompted the emergency landing at The pilots donned oxygen masks sion should he decide not to order an Ronaldsway Airport on the Isle of and, because the commander was evacuation,” the report said.
    [Show full text]
  • Planned Ground Evacuation
    Cabin Operations Flight Operations Briefing Notes Planned Ground Evacuation Flight Operations Briefing Notes Cabin Operations Planned Ground Evacuation I Introduction A planned ground evacuation can be defined as an evacuation that enables the cabin crew to review procedures, and to inform and prepare passengers for an emergency landing. The cabin crew provide passengers with brace instructions, guidance on exit usage, and information on how and when exits should be operated. Effective communication between the crewmembers and the passengers is necessary for a timely, effective, and orderly response. II Background Information A safety study by the US NTSB (National Transportation Safety Board) in 2000, entitled “Emergency Evacuation of Commercial Airplanes”, cites examples of planned evacuations where the cabin crewmembers were able to provide passengers with a detailed briefing. The cabin preparation and briefing resulted in an orderly, timely evacuation with few to no injuries. III Emergency Checklist Emergency checklists are useful tools that enable cabin crew to prepare the cabin for a planned emergency. It contains all the steps required to prepare the cabin for an emergency, and lists the steps to be completed in order of priority. Many Operators have developed checklists in the form of laminated cards that are distributed to each cabin crew, or are stowed near the cabin crew’s seats. These types of checklists should be readily accessible to the cabin crew. Page 1 of 12 Cabin Operations Flight Operations Briefing Notes Planned Ground Evacuation Emergency checklists are designed to provide support to cabin crewmembers in a planned emergency, and to help them complete all the necessary steps without forgetting anything.
    [Show full text]
  • Emergency Evacuation of Commercial Passenger Aeroplanes Second Edition 2020
    JUNE 2020 EMERGENCY EVACUATION OF COMMERCIAL PASSENGER AEROPLANES SECOND EDITION 2020 @aerosociety A specialist paper from the Royal Aeronautical Society www.aerosociety.com About the Royal Aeronautical Society (RAeS) The Royal Aeronautical Society (‘the Society’) is the world’s only professional body and learned society dedicated to the entire aerospace community. Established in 1866 to further the art, science and engineering of aeronautics, the Society has been at the forefront of developments in aerospace ever since. The Society seeks to; (i) promote the highest possible standards in aerospace disciplines; (ii) provide specialist information and act as a central forum for the exchange of ideas; and (iii) play a leading role in influencing opinion on aerospace matters. The Society has a range of specialist interest groups covering all aspects of the aerospace world, from airworthiness and maintenance, unmanned aircraft systems and aerodynamics to avionics and systems, general aviation and air traffic management, to name a few. These groups consider developments in their fields and are instrumental in providing industry-leading expert opinion and evidence from their respective fields. About the Honourable Company of Air Pilots (Incorporating Air Navigators) Who we are The Company was established as a Guild in 1929 in order to ensure that pilots and navigators of the (then) fledgling aviation industry were accepted and regarded as professionals. From the beginning, the Guild was modelled on the lines of the Livery Companies of the City of London, which were originally established to protect the interests and standards of those involved in their respective trades or professions. In 1956, the Guild was formally recognised as a Livery Company.
    [Show full text]
  • SYNOPTIC REPORT SERIOUS INCIDENT Airbus, A320-214, EI-GAL Cork Airport 2 November 2017
    Air Accident Investigation Unit Ireland SYNOPTIC REPORT SERIOUS INCIDENT Airbus, A320-214, EI-GAL Cork Airport 2 November 2017 Airbus, A320-214, EI-GAL Cork Airport (EICK) 2 November 2017 FINAL REPORT Foreword This safety investigation is exclusively of a technical nature and the Final Report reflects the determination of the AAIU regarding the circumstances of this occurrence and its probable causes. In accordance with the provisions of Annex 131 to the Convention on International Civil Aviation, Regulation (EU) No 996/20102 and Statutory Instrument No. 460 of 20093, safety investigations are in no case concerned with apportioning blame or liability. They are independent of, separate from and without prejudice to any judicial or administrative proceedings to apportion blame or liability. The sole objective of this safety investigation and Final Report is the prevention of accidents and incidents. Accordingly, it is inappropriate that AAIU Reports should be used to assign fault or blame or determine liability, since neither the safety investigation nor the reporting process has 1 been undertaken for that purpose. Extracts from this Report may be published providing that the source is acknowledged, the material is accurately reproduced and that it is not used in a derogatory or misleading context. 1 Annex 13: International Civil Aviation Organization (ICAO), Annex 13, Aircraft Accident and Incident Investigation. 2 Regulation (EU) No 996/2010 of the European Parliament and of the Council of 20 October 2010 on the investigation and prevention of accidents and incidents in civil aviation. 3 Statutory Instrument (SI) No. 460 of 2009: Air Navigation (Notification and Investigation of Accidents, Serious Incidents and Incidents) Regulations 2009.
    [Show full text]
  • List of Avionics Design and Modification
    List of Avionics Design and Modification - Aerovation’s Past Performance 15-Oct-2017, Rev IR Aerovation, Inc. 7005 S. Plumer Ave Tucson, AZ 85756 - USA Tel. (520) 308-6409 Fax (520) 844-8785 www.AerovationInc.com This document may contain commercial or financial information, or trade secrets, of Aerovation, Inc., which are confidential and exempt from disclosure to the public under the Freedom of Information Act, 5 U.S.C. 552(b)(4), and unlawful disclosure thereof is a violation of the Trade Secrets Act, 18 U.S.C. 1905 Public disclosure of any such information or trade secrets shall not be made without the prior written permission of Aerovation, Inc List of Avionics Project Company Project Year Aircraft Basic Description AAC 707-18740 1990 Boeing 707 FLt Dir, FMS, Airdata, Satphone 727-23-20095 1989 Boeing 727 EFIS 727-76OXY 1989 Boeing 727 EFIS 727-22362 1994 Boeing 727 EFIS 727-SN18998 1999 Boeing 727 Nav/Comm, FMS 727-SN19394 1998 Boeing 727 Airdata system 727-SN22362 2000 Boeing 727 TCAS 737-UJL 1992 Boeing 737 DMEs, Transponders, INS, No. 1&2 HF ALATHER 1997 Boeing 727-100 EFIS AMC727 1995 Boeing 727 EFIS B727-100-EGPWS 2001 Boeing 727 EGPWS B727-200_SN21474 2003 Boeing 727 ELT, ECS, IFE B737-200 2001 Boeing 737 EFIS, FMS B757 2003 Boeing 757 EGPWS B757 2005 Boeing 757 EGPWS B767 2002 Boeing 767 Interior, Emer Lts, PA B757 1992 Boeing 757 IFE FORBES727 1993 Boeing 727 EFIS LIMITED 1997 Undisclosed Autopilot Interface NASA-P3BN426NA 1991 Lockheed-Martin P3-B EFIS SPECIALCB 1990 Boeing 707 EFIS SPECIALEFIS 1990 Boeing 727 EFIS (EDZ-805)
    [Show full text]