Threat and Error Management (TEM) and High Altitude ... - ASASI

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Stick Shaker Events 60 MILES BEFORE A T/STORM REQUESTED 15 DEGS RIGHT FROM ATC TO AVOID TO INCREASE SEPARATION TO APPROX 30 MILES. ATC GRANTED REQUEST. PASSED ABEAM T/STORM ABOUT 30 MILES TO EAST AT FL380. TAILWIND DROPPED AND SPEED RAPIDLY WASHED OFF. MCT APPLIED INTIALLY. WING AND ENG ANTI-ICE IMMEDIATLY SWITCHED ON AS ICE SEEN RAPIDLY FORMING ON WIPERS AND WINDSCREEN. TOLD ATC WE HAD TO DESCEND AND COULD NOT MAINTAIN 380 AND THEY CLEARED US TO DESCEND FL240. WHILE LEAVING FL380 STALL WARNING MOMENTARILY WENT OFF AND AERODYNAMIC BUFFET FELT WITH ACOMMPANYING SEVERE TURBULANCE. STOPPED ALMOST IMMEDIATLY WITH FURTHER PITCH DOWN AND THRUST. NORMAL FLIGHT PARAMATERS REGAINED BEFORE FL360. LEVELLED OFF AT FL360 AND FLIGHT CONTINUED NORMALLY. PIREP MADE TO ATC OF SEVERE ICING IN THE AREA AT FL380. OTHER PARAMETERS NOTED IMMEDIATLY AFTER THE EVENT: SAT -56DEGS. FMC CRZ PAGE OPT/MAX 375/398. WIND 180/50 IMMEDIATLY BEFORE INCIDENT. NOTED AT 220/22 IMMEDIATLY AFTER EVENT.
Stick Shaker Event DECAYING AIRSPEED MAX THRUST STICK SHAKER A/P REMAINS ENGAGED A/T DISCONNECTED
Page 1 and 2: A/NZSASI June 2007 Threat and Error
Page 7 and 8: West Caribbean MD-82 Maracaibo, Ven
Page 9: ISSUES: ‣ SPEED DECAY FOLLOWED BY
Page 16: HIGH ALTITUDE MANEUVERING PERFORMAN
Page 34 and 35: ‣ Aimed at Large Transport Catego
Page 36 and 37: ‣ Variable Situations and Outcome
Page 38 and 39: ‣ Basic Flaws in Knowledge and Tr
Page 40 and 41: Continued Accidents and ‣ Inciden
Page 42 and 43: Pilot-Commanded Sideslip ‣ Roll d
Page 44 and 45: Flight Control and Other Anomalies
Page 46 and 47: Directional Maneuvering ‣ Rudder
Page 48 and 49: Simulator Training ‣ Limitations
Page 50 and 51: STRATEGIES
Page 52: What is “Airplane Upset” 52
Page 55 and 56: Environmental Causes • Turbulence
Page 57 and 58: Pilot Induced Causes of Upsets •
Page 59 and 60: STRATEGIES
Page 61 and 62: B717 - TEST FLIGHT
Page 63 and 64: B717 - TEST FLIGHT
Page 65 and 66:
Use of Full Control Inputs 65
Page 67 and 68:
Stall Recovery 67
Page 69 and 70:
Recovery Techniques (cont) •Stall
Page 71 and 72:
Nose-High, Wings Level
Page 73 and 74:
Nose-high, Wings Level Recovery Tec
Page 75 and 76:
STRATEGIES
Page 77 and 78:
High Bank Angles • Lift vector
Page 79:
Conclusion ‣ Know the causes of a
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Threat and Error Management (TEM) and High Altitude ... - ASASI

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