ebook img

Loss of Pitch Control on Takeoff Emery Worldwide Airlines, Flight 17 McDonnell Douglas DC-8-71F PDF

124 Pages·2003·1.29 MB·English
by  
Save to my drive
Quick download
Download
Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.

Preview Loss of Pitch Control on Takeoff Emery Worldwide Airlines, Flight 17 McDonnell Douglas DC-8-71F

Loss of Pitch Control on Takeoff Emery Worldwide Airlines, Flight 17 McDonnell Douglas DC-8-71F, N8079U Rancho Cordova, California February 16, 2000 Aircraft Accident Report NTSB/AAR-03/02 PB2003-910402 Notation 7299A National Transportation Safety Board Washington, D.C. Aircraft Accident Report Loss of Pitch Control on Takeoff Emery Worldwide Airlines, Flight 17 McDonnell Douglas DC-8-71F, N8079U Rancho Cordova, California February 16, 2000 ATION AL TRE PLUARIBUNS UNUSM PORTATIO NTSB/AAR-03/02 NS AFETYBO AR DN PB2003-910402 National Transportation Safety Board Notation 7299A 490 L(cid:146)Enfant Plaza, S.W. Adopted August 5, 2003 Washington, D.C. 20594 National Transportation Safety Board. 2003. Loss of Pitch Control on Takeoff, Emery Worldwide Airlines, Flight 17, McDonnell Douglas DC-8-71F, N8079U, Rancho Cordova, California, February 16, 2000. Aircraft Accident Report NTSB/AAR-03/02. Washington, D.C. Abstract: This report explains the accident involving Emery Worldwide Airlines flight 17, a McDonnell Douglas DC-8-71F, which crashed in an automobile salvage yard shortly after takeoff, while attempting to return to Sacramento Mather Airport, Rancho Cordova, California, for an emergency landing. Safety issues discussed in this report include DC-8 elevator position indicator installation and usage, adequacy of DC-8 maintenance work cards (required inspection items), and DC-8 elevator control tab design. Safety recommendations are addressed to the Federal Aviation Administration. 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. Recent publications are available in their entirety on the Web at <http://www.ntsb.gov>. Other information about available publications also may be obtained from the Web site or by contacting: National Transportation Safety Board Public Inquiries Section, RE-51 490 L(cid:146)Enfant Plaza, S.W. Washington, D.C. 20594 (800) 877-6799 or (202) 314-6551 Safety Board publications may be purchased, by individual copy or by subscription, from the National Technical Information Service. To purchase this publication, order report number PB2003-910402 from: National Technical Information Service 5285 Port Royal Road Springfield, Virginia 22161 (800) 553-6847 or (703) 605-6000 The Independent Safety Board Act, as codified at 49 U.S.C. Section 1154(b), precludes the admission into evidence or use of Board reports related to an incident or accident in a civil action for damages resulting from a matter mentioned in the report. iii Aircraft Accident Report Contents Figures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v Abbreviations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vi Executive Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . viii 1.Factual Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1.1 History of Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1.2 Injuries to Persons. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 1.3 Damage to Aircraft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 1.4 Other Damage. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 1.5 Personnel Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 1.5.1 The Captain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 1.5.2 The First Officer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 1.5.3 The Flight Engineer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 1.6 Airplane Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 1.6.1 Cargo Load Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 1.6.2 DC-8 Longitudinal Flight Control System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 1.6.3 Maintenance Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 1.7 Meteorological Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 1.8 Aids to Navigation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 1.9 Communications. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 1.10 Airport Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 1.11 Flight Recorders. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28 1.11.1 Cockpit Voice Recorder. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28 1.11.2 Flight Data Recorder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28 1.12 Wreckage Recovery and Documentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38 1.12.1 Longitudinal Flight Control Surfaces . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39 1.13 Medical and Pathological Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41 1.13.1 Flight Crew Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41 1.13.2 Cargo Handlers(cid:151)Postaccident Drug and Alcohol Testing. . . . . . . . . . . . . . . . . . . 41 1.14 Fire/Explosion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42 1.15 Survival Aspects . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42 1.16 Tests and Research. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42 1.16.1 DC-8 Elevator Flight Control Tests. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42 1.16.2 Airplane Performance Studies. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 1.17 Operational and Management Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 50 1.17.1 Emery Worldwide Airlines, Inc. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 50 1.17.2 Tennessee Technical Services . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 57 1.17.3 FAA Oversight of Emery Worldwide Airlines(cid:146) Certificate. . . . . . . . . . . . . . . . . . . 59 1.18 Additional Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62 1.18.1 Design and Certification of DC-8 Elevator System. . . . . . . . . . . . . . . . . . . . . . . . . 62 1.18.2 Party Submissions Regarding Contact/Possible Contact with the Bolt. . . . . . . . . . 63 Contents iv Aircraft Accident Report 2. Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 2.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 2.2 The Accident Sequence . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 2.2.1 Disconnection of the Right Elevator Control Tab. . . . . . . . . . . . . . . . . . . . . . . . . . 66 2.3 Role of Aircraft Maintenance in the Accident . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68 2.4 Preflight Inspection and Flight Control/EPI Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . 69 2.4.1 Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 69 2.4.2 Elevator Checks/Use of the EPI Gauge. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 2.5 Elevator Design Issues . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 71 2.5.1 Elevator Geared Tab Crank Arm Fractures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73 2.6 Emery(cid:146)s DC-8 Maintenance Documents and Guidance. . . . . . . . . . . . . . . . . . . . . . . . . 73 2.6.1 Required Inspection Items. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73 2.6.2 Emery(cid:146)s B-2 Inspection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 74 2.6.3 DC-8 MM Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 2.7 FDR-Related Issues . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 76 2.8 Drug and Alcohol Testing of Ground Personnel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 79 3.Conclusions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 81 3.1 Findings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 81 3.2 Probable Cause. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 83 4.Recommendations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84 5.Appendixes A: Investigation and Hearing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 89 B: Cockpit Voice Recorder Transcript . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 90 v AircraftAccidentReport Figures 1. The airplane(cid:146)s ground track, with selected CVR comments, during the accident flight. . . . . . . . . . . . 7 2. A diagram of the elevator control tab installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 3. A photograph of an EPI gauge similar to the gauge installed on the accident airplane . . . . . . . . . . . 14 4. EPI installation on the lower left side of the first officer(cid:146)s instrument panel (shown by the yellow arrow), similar to that on the accident airplane. . . . . . . . . . . . . . . . . . . . . . . . 15 5. Photograph showing the elevator damper(cid:146)s location on the right elevator of a DC-8 . . . . . . . . . . . . 24 6. Elevator, pitch, and control column plots recorded by the accident airplane(cid:146)s FDR during ground operations before the accident flight. The first 20 seconds of data were recorded while the gust lock was engaged. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31 7. Pitch attitude, control column position, and (corrected) elevator position FDR data from the accident flight. About the first 20 seconds of data were recorded while the gust lock was engaged. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32 8. Pitch attitude, control column position, and (corrected) elevator position FDR data for the previous takeoff from RNO. About the first 1 minute 20 seconds of data were recorded while the gust lock was engaged. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32 9. A photograph of the accident airplane(cid:146)s right elevator control tab crank fitting. Note damage on forward face of control tab crank fitting lugs . . . . . . . . . . . . . . . . . . . . . . . 40 10. Photograph of the test airplane(cid:146)s right elevator control tab pushrod contacting the crank fitting. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43 11. Photograph of the test airplane(cid:146)s disconnected right elevator control tab pushrod centered between the lugs of the crank fitting with the control tab rotated 3” to 4” in the TEU direction after the attachment bolt was removed. . . . . . . . . . . . . . . . 45 12. The control column position required for the left elevator control tab to reach its TEU physical stop (for the recorded elevator position) and the actual recorded control column position for the accident flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 13. Plots of the control column and corrected elevator position recorded by the accident FDR during the accident takeoff roll and the previous takeoff roll (from RNO) . . . 50 vi AircraftAccidentReport Abbreviations AC advisory circular AD airworthiness directive ALPA Air Line Pilots Association AND airplane nose down ANU airplane nose up AOM aircraft operating manual ASB alert service bulletin ASOS automated surface observation system ATC air traffic control ATP airline transport pilot c.g. center of gravity CAR Civil Aviation Regulations CFR Code of Federal Regulations CVR cockpit voice recorder DAY James M. Cox Dayton International Airport DFR digital flight recorder EPI elevator position indicator FAA Federal Aviation Administration FAR Federal Aviation Regulations FCD fleet campaign directive FDR flight data recorder FOB flight operations bulletin FSB field service bulletins FSDO flight standards district office GPWS ground proximity warning system Abbreviations vii AircraftAccidentReport HBAW flight standards handbook bulletin for airworthiness IFR instrument flight rules IPC Illustrated Parts Catalog MAC mean aerodynamic chord MEL minimum equipment list MHR Sacramento Mather Airport MM maintenance manual MPPM maintenance policies and procedures manual msl mean sea level NASIP National Aviation Safety Inspection Program OHM overhaul manual P/N part number PMI principal maintenance inspector POI principal operations inspector PTC pitch trim compensator RASIP Regional Aviation Safety Inspection Program RNO Reno/Tahoe International Airport S/N serial number SB service bulletin SDR service difficulty reports STC supplemental type certificate TED trailing edge down TEU trailing edge up TRACON terminal radar approach control TTS Tennessee Technical Services ULD unit loading device viii AircraftAccidentReport Executive Summary On February 16, 2000, about 1951 Pacific standard time, Emery Worldwide Airlines, Inc., (Emery) flight 17, a McDonnell Douglas DC-8-71F (DC-8), N8079U, crashed in an automobile salvage yard shortly after takeoff, while attempting to return to Sacramento Mather Airport (MHR), Rancho Cordova, California, for an emergency landing. Emery flight 17 was operating under the provisions of 14 Code of Federal Regulations (CFR) Part 121 as a scheduled cargo flight from MHR to James M. Cox Dayton International Airport (DAY), Dayton, Ohio. The flight departed MHR about 1949, with two pilots and a flight engineer on board. The three flight crewmembers were killed, and the airplane was destroyed. Night visual meteorological conditions prevailed for the flight, which operated on an instrument flight rules flight plan. The National Transportation Safety Board determined that the probable cause of the accident was a loss of pitch control resulting from the disconnection of the right elevator control tab. The disconnection was caused by the failure to properly secure and inspect the attachment bolt. The safety issues discussed in this report include DC-8 elevator position indicator installation and usage, adequacy of DC-8 maintenance work cards (required inspection items), and DC-8 elevator control tab design. Safety recommendations are addressed to the Federal Aviation Administration.

Description:
2.6 Emery's DC-8 Maintenance Documents and Guidance . engineer nor the mechanics reported observing any significant airplane anomalies
See more

The list of books you might like

Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.