Free Memorandum - District Court of Arizona - Arizona


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Date: January 3, 2006
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State: Arizona
Category: District Court of Arizona
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APPENDIX "C" "
P
Case2:O2—cv-OO824—EHC Document 82-2 Filed O1/O4/2006 Page:1 0f4

Plaintiff’s Appendix "C"
SUBSTANTIAL SIMILARITY CHART
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I Arizona I I • Hydraulics of
I • Controls became very stm I
I • Controls remained stm I
I · Difficulty applying forward cyclic ,
I Im I · Started a slow turn to the left I
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I I Florida • Hydraulic warning light
` • Loss of cyclic control
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I New York I · Hydraulics off I I
I I I • Helicopter kept pitching up and left
I I I · Uncontrollable roll to the left I I
I • Pilots could not level the helicopter by using
I both hands to bring the cyclic to the neutralllevel I
I position I
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I California I • Loss of hydraulic pressure I I
I I • Helicopter began to spin I
I I • Pilot experienced control problems I I
I I I • One or more 360 degree turns I- I
Page C·l
Rocky Mntn Il-IW/WO Lg2368l/20060103 ‘
Case 2:O2—cv—OO824—EHC Document 82-2 Filed O1/O4/2006 Page 2 of 4

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I Hawaii I • Hydraulic accumulator test
I I I • Helicopter became airborne in a nose low attitude
I I I • Entered a figure 8 type of oscillation
I I I • Nose high then nose low position
‘ § • Extreme almost wing over attitudes
I I • Descended like a falling leaf I
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I Texas · "HYD" light illuminated I
I I `I • Helicopter's controls became very stiff I I
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I New Mexico • Hydraulic pump drive belt fractured
I • Cyclic would not move
• Pilot could not neutralize cyclic with both hands
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I Alaska • Hydraulic pressure warning horn
, • "HYD"warniug light I
I I • Loss of control
I I • Cyclic control became stiff and hard to move
I I • Cyclic frozen in full aft left position
I I • Aircraft became uncontrollable I
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I Georgia ' I I · Hydraulics off I
I I • Helicopter did not respond to control inputs
• Yaw rate became uncontrollable
I · Nose appeared to pitch up dramatically I
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Page C-2
Rocky Mum IHW/WO Lg2368l/20060I03
Case 2:O2—cv—OO824—EHC Document 82-2 Filed O1/O4/2006 Page 3 of 4

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I Nebraska · Binding in the right pedal
I I • Loss of control
I I • Began to spin with its nose angled down
I I • Started to descend rapidly, still spinning
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I Arizona I · Hydraulic warning light illuminated
I I I • Audio warning activated I
I I • Loss of control I
· I · Started to yaw to the left
I I • Pilot attempted to apply right pedal but was met I
I with more force than he was expecting to overcome I
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I Arizona I • Warning horn activated I
I I • Loss of control I I
I I I • Started to yaw to the left I
I · Pilot could not stop left yaw by applying right pedal
I I I · At least two full 360-degree turns I I
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I I New Mexico I • Pilot suspected loss of tail rotor effectiveness I
I I I • Nose began to go left I
I I • Cyclic seemed extremely stiff and/or stuck
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. Arizona I • Pilot suspected loss of tail rotor authority I I
I · Uncontrollable left yaw I
I I I • Unable to regain control of the helicopter I I
Page C-3
Rocky Mntn IHW/WO Lg2368l/20060103
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Case 2:02-cv-00824-EHC

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