![]() Extended crossbleeding of a failed engine traps feed tank fuel on that side if the _ light has not been pushed, and may result in a _. Put the landing gear handle down and do not cycle 46. Put the landing gear handle down and do not cycle.ĭ. Pull the landing gear control circuit breaker.Ĭ. (Multiple Choice) If the landing gear fails to retract you should perform the following:Ī. When making an arrested abort, allow time for the arresting hook to extend as a guide, lower the hook _ before the cable. (Multiple Choice) During flight brief consideration of takeoff abort possibilities, the following items should be considered:ĭ. True/False: A blown nose tire cannot FOD an engine. True/False: If you must land with the launch bar extended, you should request that the field arresting gear cables be removed. Aerobraking is authorized under the following conditions:ġ. Nosewheel steering low mode (may/may not) be momentarily engaged while the launch bar is down (circle correct answer). Anti-skid is effective down to approximately _ KGS. In such conditions, consider preheating the windshield by placing the DEFOG handle to _ and, if necessary, by placing the WINDSHIELD switch to either _ or _. The windshield may fog rapidly under conditions of very high aircraft descent rates and high humidity. On a section takeoff, turns into the wingman will not be made at altitudes less than _. True/False: Failure to route the restraint lines properly through the garters could cause serious injury during ejection/emergency egress. What two ways can you stop any BIT test in progress and return the equipment to normal operation? 1. The _ switch must be in the _ position to use the selective jettison system. If this is done inflight, the aircrew will be _. Pulling the manual override handle automatically rotates the ejection seat safe/armed handle to the _ position, releases the survival kit attachment lugs and leg restraint lines, and unlocks the inertia reel. True/False: The canopy can be jettisoned in the closed position only. Emergency jettison is performed by pushing the EMERG JETT button with either the _ or with _. True/False: High gain nosewheel steering should be used on takeoff roll up to 50 KIAS. True/False: Failure of both AOA probe heaters in icing conditions may cause a sharp uncommanded nose down attitude, uncontrollable by normal stick forces or paddle switch actuation. True/False: The hook light remains on except when the hook is up and latched. If the wings are commanded to unlock or fold during a catapult shot, bolter, or touch and go, the wings will unlock, the ailerons will fair, the wings may fold partially, and the aircraft will _. ![]() Ensure the WINGFOLD switch is lever-locked in the _ position during takeoff checks. True/False: With the wings spread and locked, pressing and holding the nosewheel steering button a second time will select the high mode (☗5°) and NWS HI is displayed on the HUD. ![]() The landing gear warning tone activates 25. What occurs with gear handle UP, airspeed below 175 KCAS, altitude less than 7,500 feet, and rate of descent greater than 250 feet per minute? a. Rudder toe-in is a function of FLAP switch position and _ with maximum toe-in being _. True/False: Once EMERG has been selected on FCS COOL switch, selection of NORM will switch FCC A and right TR cooling back to avionics air. On takeoff, accelerating with the FLAP switch in HALF, at what speed will the flaps begin AUTO scheduling? 240 KCAS 22. True/False: Selection of manual spin recovery mode (SPIN switch in RCVY) seriously degrades controllability, will prevent recovery from any departure or spin, and is prohibited. True/False: The FCS RESET button does not fix a detected failure it merely allows components to be restored and failure indications to be removed, if and only if the failure no longer exists. flight controls / arresting hook / APU / emergency brake accumulators 19. The right or HYD system 2 provides power to _ and _ and pressurizes both the _ and _. True/False: The exterior lights master switch must be on for operation of the position and formation lights, but not for the strobe lights. What is the cockpit warning of a single TR failure? There is no cockpit warning of a single TR failure 17. ![]() True/False: Fuel cannot be dumped with either a BINGO or FUEL LO caution displayed. Tanks 1 and 4 are empty and all available fuel from internal wing and external tanks has been depletedĤ. List four events which individually will cause fuel dump to stop. True/False: There is no voice alert associated with BINGO fuel. What fuel state illuminates the FUEL LO light, MASTER CAUTION light, and activates fuel low voice alert? 1125 lbs 13. True/False: The fuel low level indicating system is completely independent of the fuel quantity indicating system.
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