Proposal for the establishment of a database for civilian and military aircraft accident/incident due to spatial disorientation.

 

 

           

 

                                                                                    1 June 1994

 

 

 

                                                                                    Kaz Shimada

                                                                                    Aerospace Medicine

                                                                                                                Wright State University

 

 

                                                                                   

 

 

 

Introduction

 

            Spatial disorientation (including those terms such as Ôpilot vertigoÕ, spatial misorientation) has been attributed for a cause of aircraft accident.  It is frequently quoted in a crash investigation of high-performance military aircrafts [Gardetto].  But it could be a cause in a accident involving a large civilian jetliner.  In fact, there are some of the reports suggesting accidents happened due to spacial disorientation [NTSB].

            There have been not much attention paid on spatial disorientation in FAR Part 121/135 airline/commuter mishaps.  Especially in large jets incidents, factors from spatial disorientation were not clearly stated in accident reports [Veronneau].

            It is not easy to extract spatial disorientation issues from present accident reports, but efforts are being commenced by Federal Aviation Administration[Veronneau], US Navy[Patterson], US Air Force[Gardetto], and Army[Durnford].  To join these efforts and make a database available to researchers will be valuable for the further safety of air travel.  Today, we have to begin with constructing such database of civilian airliner accident cases.

Background

 

Spatial disorientation

 

            To an individual inside an aircraft, vestibular information can be misleading because the body no longer has a mixed reference with which to orient against, as the individual moves when the aircraft moves.  Further, steady aircraft motion, or an accelerating or decelerating aircraft, can produce vestibular sensations that are at odds with the reality of the bodyÕs orientation.  Generally, visual information in an aircraft can counter misleading vestibular information since either the horizon or aircraft instruments can tell the individual the aircraftÕs and thus the individualÕs orientation relative to the earth.  However, when such visual information is lacking or is not perceived, the individual can be misled by incorrect vestibular information.  That individual is spatially disoriented, or is perceiving an orientation in space that is incorrect.  A spatially disoriented pilot can believe that a straight and level aircraft is in a turn, or is climbing or descending [NTSB].

 

IFR/IMC flying

 

            Spatial disorientation is likely to occur when external visual cues are lost due to clouds (Instrument Meteological Condition, IMC) or at night.  Pilots are trained to rely on aircraft instruments which directly or indirectly indicates aircraftÕ attitude.  When they are flying under IMC by instrument flight method (Instrument Flight Rule, IFR), they are unable to rely on outside horizon when they lose spatial orientation. 

           

Autopilot

 

            Use of autopilot, not only to help the pilot recover from disorientation, but also to help the pilot recover from disorientation, but also to help prevent the disorientation in the first place, has a considerable potential for saving lives [Gillingham].

            Autopilots are always used in large aircrafts.  When it is disengaged forcedly by a turbulence, such as wake turbulence, pilots will have a hard time in transition from autopilot to his/her own instrument attitude orientation.  This could lead to a disorientation incident.

 

Flight data recorder

 

            Commuter airliners are not required to install a flight data recorder (FDR).  This makes post-accident analysis difficult.  For example,Beechcraft 1900C N811BE, operated by a commuter and crashed on 28 December 1991, was not equipped with a FDR [NTSB].  None is required by FAR135.  Its flight was analyzed with cockpit voice recording, air traffic control (ATC) communication recording, and ATC radar data.  Probable cause of the crash was that both instructor and trainee was disoriented by partial panel training low at night.

            It will be easier and less expensive to install a FDR onto a commuter aircraft with the use of GPS and connecting it to digitized flight control.  Then, number of cases of disorientation of commuters and general aviation aircraft might increase.

 

Current literature

 

            Because of absence of FDR in general aviation and commuter airline aircraft, and a less interest in disorientation factor in airline aircraft crash investigation, Some of the military accident case analysis are available [Gardetto] but not published as specialized regarding spatial disorientation.  Thus, spatial disorientation study in aircraft accidents is mostly observational and descriptive.

 

Objective

 

            To gather and organize civilian and military aircraft accident data and establish a database for spatial disorientation accident analysis.  Conduct cross-sectional study for spatial disorientation, and do case-control study if possible, then prepare for future historical cohort study.

 

Study design

 

This is a retrospective study.

1)         Extract civilian spatial disorientation cases from NTSB reports.  Search for keywords related to spatial disorientation in FAA database, and look up probable cases (might be several hundred), and assess the cause of the case.

2)         Coordinate with US Navy, US Air Force, and US Army and collect their cases of spatial disorientation.  Establish a standard report format if possible.  It is expected that about a thousand possible spatial disorientation cases and forty to fifty definite cases will be collected.

3)         Assess and standardize the quality of case description.  Basically all cases of probable cases will be included.  Exclusion of cases will be done concurrently with cross-sectional analysis using database.  The state of visual cues, the attitude and motion of the aircraft when pilot commence correction, etc. will be included.

4)         Organize the case description into computer database.

5)         Conduct a cross-sectional study.  Categorize described cases into VMC/IMC, single pilot/two pilot, type of aircraft, type of autopilot, the attitude/motion of aircraft when pilots commence control input, human factors such as previous wok hours, sleep, experience of pilots etc.  Possible experimental hypotheses are such as:

\There is a threshold for current actual IFR time and rate of accident.

\There is a significant number of reversal reading of attitude indicator.

\There is a difference in rate of accident in different types of autopilot.

etc.  Detail of an example study is to follow.

 

 

 

An example of a possible analysis after the establishment of this database

 

            Because the status of the knowledge regarding spatial disorientation in aircraft accedent is that there is no established database, numbers in this exapmle are all assumed (indicated with *).

 

Null hypothesis:      No difference in outcome (aircraft damage/personal injury) whether pilot began to input corrections to control, past 30 degrees* of roll or within 30 degrees* of roll.

 

Experimental hypothesis:               Significant outcome difference if pilot began correction before or after 30 degrees* of roll.

 

Subjects:        

            Inclusion criteria:     all pilots in a incident suspected of disorientation

                                                all category of aircraft in database

            Exlusion criteria:      no evidence of control input to the aircraft

 

Study duration:        all cases in database

 

Outcome criteria:     1) attained unusual attitude (either over 45 degrees* of roll, 30                                 degrees* of pitch up, 45 degrees* of pitch down, or stall)

                                    2) excess G of over 67 %* of design limit

                                    3) aircraft damage

                                    4) personal injury including total crash

 

Data analysis:           Assign a coefficient of 0.1, 0.3, 0.7, and 1.0 to each outcome criteria* (accumulative to a single case; 0 - 2.1) and make a score for a case (two cases if two pilots tried a control); compare the over-30 deg group to within-30 deg group for the difference in this score by a t-test.  Expect to have a necessary n =8* in each group, approximated by z test; a = 0.2, b = 0.5, m1 - m2 = 0.6, d = 0.6* (2[(1.28+0.7)0.6/0.4]**2).  If this does not do, a comparison for relative risk for personal injury will be compared.


 

 

 

 

 

 

 

 

 

 

                                                            References

 

 

 

 

1)         DeHart Rl, Beers KN. Arcraft accidents, survival, and rescue. In: DeHart RL                      ed. Fundamentals of aerospace medicine. Philadelphia, Lea & Febiger,                    1985: 862 - 887.

2)         Durnford SJ, Rosado NR, Crowley JS. Spatial disorientation - a review of U.S.                   Army accidents. Aviat Space Environ Med; 65, 1994: 442.

3)         Gardetto P. Fighter/bomber aircraft impacted ground during a formation                         rejoin loss of s/a, spacial misorientation.  Handout for WSU CMH721,                     1994.

4)         Gillingham KK, Wolfe JW. Spatial orientation in flight. In: DeHart RL ed.              Fundamentals of aerospace medicine. Philadelphia, Lea & Febiger,                    1985: 299 - 381.

5)         National Transportation Safety Board. Aircraft accident/incident summary                      report - loss of control business express, Inc., Beechcraft 1900C N811BE                  near  Block Island, Rhode Island December 28, 1991. PB93-910405, 1993.

6)         Patterson FR, Cacioppo AJ, Hinman GE, Nalepka JP. Aviation spatial                    orientation in relationship to head position and attitude interpretation.                  Aviat Space Environ Med; 65, 1994: 442.

7)         Veronneau S.  personal communication.

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