20-4-1[speed decay at cruise]
TRANSCRIPT
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SPEED DECAY AT CRUISE
18thAIRBUS SAFETY CONFERENCE - BERLIN
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A330 SPEED DECAY EVENT
BOM to AMS FL380 over NW IRAN
Clear skies at dawn with a thin undercast
Airspeed 260 to 197 knots gradually
Autothrust ON / Autopilot maintained altitude
Maximum available thrust did not stop decay
Pilots received no warnings or messages
Pilots took over and flew manually
Descent to FL 340 and continued to AMS
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CREW INFORMATION
Captain on rest break
Right seat FO (Pilot Flying)
Left seat FO Pilot In Command (Pilot Monitoring)
Crew noticed speed at 240 knots
Autothrust commanded climb thrust
Speed continued to decrease
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CREW FEEDBACK
Assessed situation understanding
1. Normal law and flight protections
2. A330 will not stall in Normal law3. Alpha Protection would limit AOA below stall
Unsure why speed decay occurred
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RECOVERY
Crew disconnected AP at 198 knots and descent to FL360 initially,then FL340
Once they reached normal speed at FL340 the flight was routine
There was more thrust available at the lower altitude
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UPON ARRIVAL AMS
Investigation begins
Maintenance inspects aircraft
Flight data sent to Airbus and P&W
Performance Engineering, Tech OPS, Safety analyze FOQA data
Maintenance inspection results in no engine or aircraft malfunction
Potential atmospheric anomaly
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ATMOSPHERIC CONDITIONS
Proper altitude for weight and OAT
At FL380 for 21 minutes
Temperature increased slowly about 3 degrees (tropopause entry)
Horizontal wind change
Performance increasing wind created a high speed and low thrust state
Decreasing performance wind slowed the aircraft
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FLIGHT DATA
Blank
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THERE MUST BE MORE TO IT
The horizontal wind was manageable
Autothrust soft mode may have contributed, but was not the cause
There was some indication of a vertical wind component
When pitch exceeds AOA during level flight this indicates adowndraft
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TOULOUSE MEETING
Airbus calculated the vertical wind with performance modeling
It averaged 1000 fpm over four minutes
Why did it last so long
Delta meteorology theory
Perpendicular gravity wave encounter in the tropopause
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GRAVITY WAVE THEORY
Gravity waves are generated in the troposphere by frontal systemsor by airflow over mountains
The amplitude increases in the tropopause
Picture a surfer under a curl for a sustained period due to a
perpendicular direction of travel vs. the wave
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SIGNIFICANT VERTICAL WIND
Current weather forecasting tools cannot model or predict
New FOQA algorithm for vertical wind
Pitch > AOA in level flight = downdraft
FOQA study shows this vertical wind occurs on this route over
Turkey, Iran, and Pakistan in the winter/spring months
Winter/Spring months have higher seasonal winds
Winter/Spring trop heights are lower than Summer/Fall
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WAVE CLOUDS
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LIKE EVENT STUDY
All fleets checked for below Vls speed at cruise
1.4 million flights
This was only event
About a dozen flights had lost significant airspeed and some had todescend
AT soft speed mode saves 1% on fuel, but will cause a slight delay (up
to 30 seconds) in reaching full CLB thrust on A330
Checking 5 years of A330 flights showed about 2 per year wentbelow green dot at cruise altitude
Most of these where in moderate or greater turbulence Not as insidious as our subject event
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AMS-BOM-AMS 39 Events (Nov-May)
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CONCLUSIONS
This rare downdraft exceeded aircraft performance (All fleets)
Perpendicular direction
High winds over terrain
Tropopause height
No low speed warning exists at high altitude
High altitude speed awareness is key
Severe downdrafts
Windshear
Airspeed dropouts
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NEXT STEPS
Support industry change for a low speed warning on new aircraft
Current A330 design has a low energy warning below 2,000ft AGL
Assist meteorology to develop a model to predict and avoid gravitywave
Pilot training to manage this rare threat
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DOWNDRAFT STUDY RESULTS
Most were over IRAN
80 knots plus wind
Upwind high terrain
Only NOV-MAY over 3 year look back
Why only NOV-MAY?
Other times of year the tropopause altitude is above our normal
cruising altitudes Winter jet streams average twice the velocity of summer jet
streams
Avoidance strategies
Flying below the tropopause, stay below the wave FL340 max altitude will provide extra climb performance
Other events near mountainous regions and even oceanic areas
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PILOT EDUCATION
Rare Upper Air Downdrafts can cause;
Insidious speed decay even with full thrust applied
The Autopilot simply trades airspeed for altitude This downdraft lasted 4 minutes
Below green dot drag increases faster than lift
Descent to recover airspeed is only option
High thrust descent preferred - Not OPEN Descent
Proper recognition and recovery is key
It all starts with monitoring your speed at cruise
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QUESTIONS?
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