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Right Engine Propeller Speed (%) 29. Eng2 Torque (%) Right Engine Torque (%) 30. Flap Asymmetry Flap Asymmetry (discrete) 31. Flaps (deg) Flap Position (degrees) 32. Gnd Speed ... According to ATR, in the event of a flap asymmetry, the recorded flap position should be considered an average position of the left and right

inner flapp while internal tube ends on asymmetry detector unit. Flap asymmetry protection activates (cid:132) for an asymmetry between 8 and 10° • Command ... SYSTEM – Asymmetry certification The flap system is designed to limit the flap asymmetry (8 to (cid:132) 10°), to prevent an unsafe condition to develop

degrees, and the captain's control input to counteract the flap asymmetry was no longer required. See the configuration change reflected in the shift ... considered two other potential sources for the uncommanded roll: a second flap asymmetry and a wing stall. Second Flap Asymmetry as Source of Roll

left and right trailing edge flaps. ' . ..,.: i..- 4 provides trailing edge flaps asymmetry protection. 4. Flaps Limit Placard (FLAPS UMIT) lists limit 'airspeed for each

Trailing Edge Flap Flap TE Asym T.E. FLAP ASYM Asymmetry Left FMC Fail (79) FMC Fail - L FMC FAIL - L Right FMC Fail

Safely operate” includes consideration of airplane (cid:52) handling qualities Asymmetric Flap Deployment Indication must be provided if needed to prevent or (cid:52) counteract ... handling qualities are not unsafe with asymmetry FAA Handling Qualities Requirements for Icing and Federal Aviation Asymmetric Flap Deployment 2 Administration September 23, 2009 [page

N810TA points 5–9 are flaps Up; points 10–11 are flaps 1. A/C ON means air conditioning on, A/I OFF means anti-ice off. AIRCRAFT ... retracted, unaccelerated flight, neutral control wheel, and that the engine inoperative thrust asymmetry is trimmed with rudder. NTSB and Boeing engineering staff performed independent consistency

Reynolds number predetermine the spanwise location of the initial stall. • The flaps and inboard wing “glove” stall at much higher angle of attack than ... wing typically (but not always) stalls before the other, causing a lift asymmetry and aircraft roll. • Large roll rates and roll angles can develop, depending

flaps 5 for the go-around flap setting for a flaps 20 approach or use flaps 20 as the go-around flap setting ... VREF + 80 Set “Flaps 5” → “Speed Check Flaps 5 Set” “Flaps 1” → “Speed Check Flaps 1 Set” “Flaps Up” → “Speed Check Flaps Up Set” “VNAV

Match # 5: Deceleration with Flaps UP (Figures: 11A, 11B, and 11C) Setup Notes Parameter Notes Flap Detent Flaps UP based on the paraphrased CVR transcript ... Match # 6: Deceleration with Flaps 1 (Figures: 12A, 12B, and 12C) Setup Notes Parameter Notes Flap Detent Flaps 1 was assumed based on the paraphrased

page 7] deflection, horizontal stabilizer pitch trim, flap handle position and left/right flap trailing edge position, and VHF L/R/C key status. The FDR parameters ... trim command status. Note that “apparent” FDR left and right parameter asymmetries (e.g., engine or flight control surface parameters) are affected by the limited parameter

landing weight of 112,500 lbs and flaps 40, the prior aircraft’s V was 124 kts. The accident flight’s weight ... section will discuss the possible contributions of the crosswind and reverse thrust asymmetry to the heading deviation. The McDonnell Douglas report used a yawing moment

factor, the aircraft began to rapidly roll to the left. Due to asymmetries in the aircraft including the shape of the wings, the control surfaces ... Flight 874 estimated landing weight was 29,327 lbs [Reference 4]. Flaps at the time of the upset were zero. According to Figure

tube, pitch trim compensator (PTC) motor and actuator, throttle quadrant, throttle handles, flap handle, spoiler handle, and thrust reverser levers, were located beneath a section ... flap handle was found with its lever latched in the third detent aft of its stowed position, which corresponded to 15º of flap extension

degrees lower than it would without the ice protection system on9. With flaps and landing gear down the stall warning initiates at a vane angle ... roll and potential loss of control. This is especially true of an asymmetry on the outboard sections of the wing in front of the ailerons

retract the landing gear (if extended), recover normal speed, and select the flaps as required. If one engine was inoperative, the pilot should “use with ... findings. A310 Airplanes 2/91 Operation 50 to 300 15º slats and 0º flaps Missed approach; three successive stalls; loss of control with repetitive rudder movements