ex.catp

When are severe weather watch bulletins (ww) issued?. every 12 hours as required. every 24 hours as required. Unscheduled and issued as required.

SIGMETs (other than domestic convective SIGMETs) may be valid for not more than. 4 hours for the other phenomena and may be issued 2 hours before the valid time. 6 hours for other phenomena. 4 hours for other phenomena.

what time period is covered by the Outlook section of the convective Sigmet?. 24 hours after the valid time. 2 to 6 hours after the valid time. no more than 2 hours after the valid time.

when icing is detected, particulary while operating an aircraft without deicing equipment, the pilot should. fly to an área with liquid precipitation. fly to lower altitude. leave the aérea of precipitation or go to an altitude where the temperatura is above freezing.

taliplane icing can be detected by. a slow and steady decrease in altitude. Flaps falling to opérate. A sudden change in elevator force or uncommanded nose-down pitch.

If tailplane icing or tailplane Stall is detected, the pilot should. lower the Flaps to decrease airspeed. decrease power to Vfe. retract Flaps and increase power.

if icing is suspected on an airplane equipped with deicing equipment, the pilot should. first confirm ice with the ice light prior to deploying the pneumatic boots. Opérate the pneumatic deicing system several times to clear the ice. Operate the pneumatic deicing system once to allow time for the ice removal.

What happens when a tailplane ices?. the aircraft pitches up without configuration changes. the aircracft experience nosedown pitching momento. Flaps fail to opérate.

During icing conditions, a tailplane Stall may. begin as the Flaps are retracted. occur at a relativety high airspeed. slowly become evident as the nose pitches upward.

during icing conditions, a pilots response to tailplane Stall symptoms should incluide. retracting the landing gear. holding the Flaps at the current position by whatever means are necessary. applying sufficient power for the aircraft configuration.

the firts place ice is likely to formo n an aircraft is the. wings. tailplane. windshield.

A pretakeoff contamination check for snow, ice or frost is required by 14 CFR Part 135. This check is required to. be made within 2 minutes of staring the takeoff roll. Be completed within 5 minutes prior to beginning the taxi to the runway. See that the aircraft is clean, therefore, a safe takeoff can be made during the next 5 minutes.

Deicing procedures and equipment developed for large transport airplanes. will not be appropriate for the amaller aircraft, used under 14 CFR Part 135. Will be appropriate for all of the smaller aircraft, used under 14 CFR Part 153. May not be appropriate for some of the smaller aircraft, used under 14 CFR Part 135.

How can the pilot determine, for an ILS rumway equipped with MALSR, that there may be penetration of the obtacle identification surfaces (OIS), and care should be take in the visual segment to avoid any obtacles?. The runway has a visual approach slope indicator (VASI). The published visibility for the ILS is no lower than ¾ SM. The approach chart has a visual descent point (VDP) published.

What is the condition that may occur when gusts cause a sweptwing-type airplane to roll in one direction while yawing in the other?. Mach buffet. Wingover. Dutch roll.

Free directional oscilation (dutch roll) is. the result of three oscillations, pitch, roll, and yaw, about the respective axis. A coupled lateral/directional oscilation that is usually dynamically stable. A coupled lateral/vertical oscilation that is usually dynamically unstable.

An airplane located with the CG at the aft limit will. fly more efficiently. be very unbalanced in lateral control forces. feel heavy in the longitudinal axis.

(See Figure shown below) You see the indication in the figure on you PFD, but your standby indicator reads 120 knots and the power is set for 120-knot cruise in level flight. You decide the. Pitot tuve may be plugged with ice or a bug. Standby indicator is defective because there is no red “X” on the speed tape display. Airspeed means attitude is incorrect.

Automated flight decks or cockpits. enhance basic pilot flight skills. Decrease the workload in terminal áreas. Often créate much large pilot errors than traditional cockpits.

Automated flight decks or cockpits. improve basic flight skills. Decrease the workload in terminal áreas. Sometimes hide errors.

When flying an aircraft with electronic flight displays (EFDs), risk increases. if the pilot expects the electronics to enhance flight safety and remove pilot error. when the pilot expects the equipment to malfunction on occasion. if the pilot believes the EFD will compensate for lack of skill and knowledge.

Automation has been found to. créate higher workloads in terminal áreas. Improve crew situational awareness skills. Substitute for a lack of aviation experience.

When a pilot believes advanced avionics enable operations closer to personal or environmental limits,. greater utilization of the aircraft is achieved. risk is increased. risk is decreased.

Automation in aircraft has proven. to present new hazards in its limitations. that automation is basically flawless. effective in preventing accidents.

The lighter workloads associated with glass (digital) flight instrumentation. are useful in decreasing flightcrew fatigue. have proven to increase safety in operations. may lead to complacency by the flightcrew.

Humans are characteristically. dispoced to appreciate the workload imposed by automation. dispoced to expect automation to fail often. poor monitors of automated systems.