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Attributes | |
ACN | 408107 |
Time | |
Date | 199807 |
Day | Sat |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | atc facility : t02 airport : t29 |
State Reference | TX |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Dusk |
Aircraft 1 | |
Operator | general aviation : personal |
Make Model Name | UH-12E/E4 |
Operating Under FAR Part | Part 91 |
Flight Phase | landing other |
Flight Plan | None |
Person 1 | |
Affiliation | Other |
Function | flight crew : single pilot |
Qualification | pilot : atp pilot : private |
Experience | flight time last 90 days : 120 flight time total : 9910 flight time type : 68 |
ASRS Report | 408107 |
Person 2 | |
Experience | flight time last 90 days : 120 flight time total : 9910 flight time type : 68 |
Events | |
Anomaly | conflict : ground critical other anomaly other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : regained aircraft control other |
Consequence | other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | Pilot Deviation |
Narrative:
Practicing precision automatic-rotations at clover field airport in gusty wind. The tail rotor of my helicopter contacted the ground as I was leveling the skids. The tailskid had been replaced with a non standard unit made out of aluminum, and bent back tail rotor. Struck ground causing damage to tail rotor gear box. Helicopter automatic-rotated to ground without further incident. Should not have been practicing precision automatic-rotations in gusty winds and should have stopped flare at higher level. Tailskid should have been original equipment.
Original NASA ASRS Text
Title: PLT OF A HILLER UH12 HELI HIT TAIL ROTOR DURING A PRACTICE AUTO-ROTATION LNDG, CAUSING DAMAGE TO THE TAILSKID, TAIL ROTOR AND TAIL ROTOR GEAR BOX.
Narrative: PRACTICING PRECISION AUTO-ROTATIONS AT CLOVER FIELD ARPT IN GUSTY WIND. THE TAIL ROTOR OF MY HELI CONTACTED THE GND AS I WAS LEVELING THE SKIDS. THE TAILSKID HAD BEEN REPLACED WITH A NON STANDARD UNIT MADE OUT OF ALUMINUM, AND BENT BACK TAIL ROTOR. STRUCK GND CAUSING DAMAGE TO TAIL ROTOR GEAR BOX. HELI AUTO-ROTATED TO GND WITHOUT FURTHER INCIDENT. SHOULD NOT HAVE BEEN PRACTICING PRECISION AUTO-ROTATIONS IN GUSTY WINDS AND SHOULD HAVE STOPPED FLARE AT HIGHER LEVEL. TAILSKID SHOULD HAVE BEEN ORIGINAL EQUIP.
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.