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|
Attributes | |
ACN | 516779 |
Time | |
Date | 200107 |
Day | Sun |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : riu.airport |
State Reference | CA |
Altitude | msl single value : 4000 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | general aviation : personal |
Make Model Name | Decathlon |
Operating Under FAR Part | Part 91 |
Flight Phase | cruise : level ground : maintenance |
Flight Plan | None |
Person 1 | |
Affiliation | other |
Function | flight crew : single pilot |
Qualification | pilot : commercial pilot : instrument pilot : multi engine |
Experience | flight time last 90 days : 20 flight time total : 540 flight time type : 10 |
ASRS Report | 516779 |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | none taken : detected after the fact |
Consequence | other other |
Supplementary | |
Problem Areas | Aircraft |
Primary Problem | Aircraft |
Narrative:
Door failure during the performance of a right snap roll at 4000 ft MSL. Door did not separate from aircraft, but remained attached at the rear handle lock mechanism and the lower forward hinge. Forward upper hinge separated from fiberglas door panel. A definite fold line noticeable from upper hinge to rear handle lock mechanism. This seemed to indicate that the upper forward latch and the top latch mechanisms released during the maneuver. Had performed 2 left snap rolls without incident and no loss of altitude prior to this right snap roll. 90 mph entry speed and throttle per poh. During door failure, upper portion of door went beyond door threshold to impact my right ear and jaw. Restraint mechanism extremely tight negating possibility of head movement beyond door threshold. No damage to door threshold or any other portion of aircraft. Aircraft was landed safely, without incident. Suggest that the latch mechanisms for the door be changed to provide more security, less chance of unplanned for release during maneuvers such as snap rolls, which are extremely violent.
Original NASA ASRS Text
Title: BL8 PLT HAD THE UPPER DOOR HINGE FAIL INFLT, WHILE DOING SNAP ROLLS.
Narrative: DOOR FAILURE DURING THE PERFORMANCE OF A R SNAP ROLL AT 4000 FT MSL. DOOR DID NOT SEPARATE FROM ACFT, BUT REMAINED ATTACHED AT THE REAR HANDLE LOCK MECHANISM AND THE LOWER FORWARD HINGE. FORWARD UPPER HINGE SEPARATED FROM FIBERGLAS DOOR PANEL. A DEFINITE FOLD LINE NOTICEABLE FROM UPPER HINGE TO REAR HANDLE LOCK MECHANISM. THIS SEEMED TO INDICATE THAT THE UPPER FORWARD LATCH AND THE TOP LATCH MECHANISMS RELEASED DURING THE MANEUVER. HAD PERFORMED 2 LEFT SNAP ROLLS WITHOUT INCIDENT AND NO LOSS OF ALT PRIOR TO THIS R SNAP ROLL. 90 MPH ENTRY SPD AND THROTTLE PER POH. DURING DOOR FAILURE, UPPER PORTION OF DOOR WENT BEYOND DOOR THRESHOLD TO IMPACT MY R EAR AND JAW. RESTRAINT MECHANISM EXTREMELY TIGHT NEGATING POSSIBILITY OF HEAD MOVEMENT BEYOND DOOR THRESHOLD. NO DAMAGE TO DOOR THRESHOLD OR ANY OTHER PORTION OF ACFT. ACFT WAS LANDED SAFELY, WITHOUT INCIDENT. SUGGEST THAT THE LATCH MECHANISMS FOR THE DOOR BE CHANGED TO PROVIDE MORE SECURITY, LESS CHANCE OF UNPLANNED FOR RELEASE DURING MANEUVERS SUCH AS SNAP ROLLS, WHICH ARE EXTREMELY VIOLENT.
Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.