Most lateral and directional control difficulties are associated with _______, ________, ________, ________ or flight control malfunctions.
Answer: Engine, A/P, EFAS, YD.
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KC135
- Pilots shall be prepared to immediately disengage the autopilot, should any unscheduled ________ be evident. An autopilot lateral malfunction can result in bank angles of _____ deg within ____ sec even though recovery is started approximately ____ sec after the malfunction occurs. A pitch up malfunction could cause a stall within ___ seconds and is therefor considered the most serious autopilot malfunction.
- Since low outside air temperature causes a considerable increase in thrust, the ________________ limitations may be reached with somewhat lower throttle settings.
- During operation at low gross weight, and particularly at low ambient temperature, the airplane accelerates very rapidly; therefor care should be taken to not exceed the ______ during flap retraction.
- If the airplane fails to pressurize, ensure the cabin test valve handle is in the ______ position.
- (Cargo door opening after Takeoff) If conditions permit, maintain a flap setting of ______deg, this will retain the use of outboard ailerons for roll control
- Opening of the cargo door during or after takeoff will be noted by illumination of the _________ and will probably cause severe ________
- If during a climb all airspeed indicators are determined to be inaccurate, continue max climb thrust and maintain ____ deg of pitch on the ADI for gross weights up to 225K. Maintain ____ deg pitch for gross weights greater than 225K.
- To determine which airspeed indicator is most accurate, the aircraft should be flown with wings level so that the speed deviation pointer indicates _______ (0.6 AOA) and the airspeed reading at ).6 AOA should compare with the corresponding airspeed, for the aircraft weight and configuration obtained from the 1-1.
- If there is a disparity between airspeed indicators, the ____________ may be used to determine which indicators are most accurate
- For nose up trim, set the inboard spoiler switch to CUT-OUT. This configuration provides approx. ______ units of equivalent trim in takeoff configuration
- If a stabilizer trim runaway occurs at or below S1, simultaneously the pilot flying will ______ and the pilot not flying will ____________
- If the leading edge flaps fail to retract when the outboard flaps are raised above the 6 deg position and the outboard spoiler switch is in NORMAL, you should ___________
- Do not operate the _________ and the ________ simultaneously. Slow operation of the ______ and reduced climb performance will result.
- When the main flaps are retracted and one or both leading edge flaps remain extended, the airplane should be flown with caution at load factors in excess of 1.5 g's in the speed range between ____ and _____ kts.
- If all means of flap synchronization fail and conditions permit, institute ________(if required) and land as soon as possible.
- If the flap indicators or visual inspection reflect an asymmetric main flap condition and a rolling moment is present, the flap lever should be set to the ____________
- Takeoff should not be attempted if the oil pressure is more than ______ psi. Bearing failure die to plugged oil jets can result.
- Throttle reduction in response to a failed engine/engine flameout during takeoff or initial climb out after takeoff should not be made prior to ______________
- If a catastrophic engine failure occurs accompanied by a fire, take prompt action to pull fire switch and discharge extinguishing agent. Failure to accomplish these actions promptly can result in loss of _______ controls due to burned electrical wiring bundle.
- During actual or simulated engine loss, limit bank angle to ______ deg until as a minimum, the landing gear is up and maneuvering speed is reached.
- Charted ground min control speeds for a dry runway are based on the immediate use of _____ and corresponding _______
- On wet and icy runways, even with optimum technique, deviations up to ____ ft. from the takeoff path can be expected.
- Failure of an outboard engine necessitates _______ pilot response to prevent deviations from the takeoff path.
- During rotation to takeoff attitude, do not allow the airplane to bank beyond _____ deg due to the possibility of dragging an outboard engine nacelle.