23 results found (2940ms)
Airworthiness Directives; Cirrus Design Corporation Airplanes
Unsafe Condition: Cracks in the upper power lever, which could result in loss of engine thrust control and reduced control of the airplane.
Why matched: Airworthiness Directives; Cirrus Design Corporation Airplanes
Airworthiness Directives; Various Airplanes, Helicopters, and Engines
Unsafe Condition: Multiple failures of spot-welded, multi-segment v-band couplings at the tailpipe to the turbocharger exhaust housing flange.
Why matched: Airworthiness Directives; Various Airplanes, Helicopters, and Engines
Airworthiness Directives; Cirrus Design Corporation Airplanes
Unsafe Condition: uncommanded activation of the Cirrus Airframe Parachute System (CAPS) autopilot mode while in flight, which could cause the airplane to stall in a critical phase of flight if the autopilot is not d...
Why matched: Airworthiness Directives; Cirrus Design Corporation Airplanes
Airworthiness Directives; Various Airplanes
Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...
Why matched: Airworthiness Directives; Various Airplanes
Airworthiness Directives; Cirrus Design Corporation Airplanes
Unsafe Condition: A malfunction of the headset amplifier (part number (P/N) 38849-001) and the microphone interface (P/N 35809-001) circuit card assemblies for the 3.5 millimeter (mm) audio and microphone jacks can ...
Why matched: Airworthiness Directives; Cirrus Design Corporation Airplanes
Airworthiness Directives; Cirrus Design Corporation
Unsafe Condition: The SWPS or ESP systems may engage even when sufficient airspeed and proper angle of AOA exists for normal flight. The SWPS includes the stall warning alarm, stick shaker, and stick pusher. The ESP...
Why matched: Airworthiness Directives; Cirrus Design Corporation
Airworthiness Directives; Cirrus Design Corporation Airplanes
Unsafe Condition: Reports of partial loss of engine power due to a dislodged rubber gasket/seal being ingested into the turbocharger.
Why matched: Airworthiness Directives; Cirrus Design Corporation Airplanes
Airworthiness Directives; Cirrus Design Corporation Model SR22 Airplanes
Unsafe Condition: Anti-ice fluid distribution lines with improperly installed compression fittings, which could result in anti-ice fluid distribution line separation.
Why matched: Airworthiness Directives; Cirrus Design Corporation Model SR22 Airplanes
Airworthiness Directives; Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)
Unsafe Condition: PFDs may display incorrect attitude, altitude, and airspeed information, which could result in airspeed/altitude mismanagement, spatial disorientation of the pilot, loss of airplane control, inadeq...
Why matched: Airworthiness Directives; Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)
Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes
Unsafe Condition: The cabin door rod ends may fail, resulting in door separation from the airplane while in flight.
Why matched: Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Model SR20 Airplanes
Unsafe Condition: Engine exhaust fumes in the cabin due to leaks in the exhaust system, which could result in carbon monoxide entering the cabin heating system.
Why matched: Airworthiness Directives; Cirrus Design Corporation Model SR20 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: Jamming of the aileron and rudder controls, which resulted in loss of rudder and aileron flight controls.
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Model SR22 Airplanes
Unsafe Condition: Moisture enters through a gap at the interface of the left and right outboard wing tips and wing structure, travels along the aft wing shear web, accumulates below the aileron control pulley, and f...
Why matched: Airworthiness Directives; Cirrus Design Corporation Model SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: Premature separation of the pick-up collar support fasteners of the Cirrus Airplane Parachute System (CAPS), which could result in the parachute failing to successfully deploy (CAPS failure).
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: Overheating damage to the brake caliper piston O-ring seals, which could result in leakage of brake hydraulic fluid, leading to loss of braking with loss of airplane directional control or brake fire.
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: Crew seats folding forward during emergency landing dynamic loads, potentially causing occupant injury.
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: Reports of fuel line leaks resulting from wire chafing on the fuel lines.
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: The crew seats, under emergency landing dynamic loads, may fold forward at less than the 26 g required by 14 CFR Section 23.562(b)(2).
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders
Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...
Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: The rocket cone's internal diameter variance at the threaded end may cause the retaining nut to not be fully secured, leading to the CAPS activation cable not pulling the igniter pin free to releas...
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes
Unsafe Condition: Self-locking retaining nut on the roll and yaw trim cartridges could come off during flight, potentially jamming the corresponding flight control system and leading to loss of control of the airplane.
Why matched: Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: Certain Cirrus Aircraft Parachute System (CAPS) may not activate in an emergency situation, potentially resulting in occupant injury and/or loss of life and loss of aircraft.
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
Unsafe Condition: Understrength rivets on the elevator torque tube and rudder hinge, which could result in failure of the control surfaces.
Why matched: Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes