Questions taken from 16 October 2020 MSF 0% FE MSF FE MSF Quiz for E-3A 1 / 158 Sulfur hexafluoride (SF6) gas in the mission equipment is a colorless odorless gas which is heavier than air. To prevent inhaling SF6, open _____________, move away from door and allow compartment to ventilate for _____ minute(s) before entering airplane.NN1E-3A-1 Pg2-7 forward cargo door, two aft cargo door, one aft cargo door, two forward main door, one 2 / 158 Which of the following statement(s) is/are true regarding aircraft wing tip clearance procedures?FC FO 3.2-1 Pg 11 Do not taxi aircraft within 25 feet (8 meters) laterally of obstructions without wing walkers With wing walkers, do not taxi any aircraft closer than 10 feet (3 meters) laterally to any obstacles Aircraft will be towed, with engines shutdown, when closer than 10 feet (3 meters) to any obstacle that could potentially damage the aircraft. All of the above 3 / 158 Do not use FLT START position for more than ____________. Do not use GND START position in flight.NN1E-3A-1 Pg3-58 one and a half minutes 5 minutes 10 minutes 30 minutes 4 / 158 Replacement of tires, wheels, and brakes is required when brake energy exceeds ______ million foot-pounds.NN1E-3A(II)-1-1 PG:A8-5 10 24 28 40.3 5 / 158 _______ is the total length of runway required to accelerate on four engines to V1, experience an engine failure and then continue the takeoff or stop.NN1E-3A(II)-1-1 PG:A3-4 Critical field length Takeoff ground run Takeoff distance Takeoff run available 6 / 158 The flight crew UHF-ADF radio is powered by the UHF ADF AC and UHF ADF DC circuit breakers on the P5 panel and is cooled by the ____________ system.NN1E-3A-1 Pg1-861 fwd forced air cooling aft forced air cooling draw-through cooling cabin cooling 7 / 158 Takeoff with light coatings of ________ up to ___ – inch on lower wing surfaces is permissible.NN1E-3A-1 Pg7-13 frost, 1/8 frost, 1/4 frost, 1/2 ice, 1/4 8 / 158 When exiting through the pilots sliding window, ensure the strap is securely fastened and strap is extended fully (_______________ on the strap is at the _______________).NN1E-3A-1 Pg3-12 green lanyard, stowage box red lanyard, window sill red band, stowage box green band, window sill 9 / 158 When illuminating FASTEN SEAT BELT signs ___________, pilot or flight engineer will notify _______ by interphone.NN1E-3A-1 Pg1-1046 on the ground, TD in flight, SC on the ground or in-flight, TD in flight, TD 10 / 158 The normal operating range of the APU generator, as indicated by airplane instruments is _______ Hz. Under steady load, frequency may vary a maximum of ____ Hz about a mean value within the ______ Hz band.NN1E-3A-1 Pg5-30 400 ± 8, ± 4, 400 ± 8 400 ± 8, ± 2, 400 ± 8 400 ± 10, ± 2, 400 ± 10 400 ± 10, ± 4, 400 ± 10 11 / 158 The Flight Engineer’s seat does not provide maximum crash restraint, unless it is facing __________ or __________ degrees (first stop) outboard.NN1E-3A-1 Pg1-998 forward, 30 forward, 60 forward, 90 aft, 60 12 / 158 Ensure ______________ is powered down during fuel dump.NN1E-3A-1 Pg3-55 surveillance radar weather radar flight deck UHF radio Both A and B 13 / 158 If _____________ warning light illuminates continuously after flap retraction, at least one flap limit switch has malfunctioned. Autopilot pitch servo is in high torque mode and pitch trim is in ________ speed.NN1E-3A-1 Pg1-388 Rudder Boost; high Autopilot; low Flight Director; variable Autopilot; high 14 / 158 Use landing gear LOCK OVERRIDE __________________. Gear retracts whether in correct position or not. Gear could hit doors or structure, causing damage.NN1E-3A-1 Pg1-216 only in extreme emergencies when gear lever solenoid lock is inoperative when any gear fails to retract when main landing gear fails to retract 15 / 158 The climbout is divided into four segments; the second climbout segment continues from the end of the first, and is completed at the selected ______.NN1E-3A(II)-1-1 PG:A3-20 termination height acceleration height obstacle height screen height 16 / 158 Do not operate auxiliary rotodome drive at 6 RPM (XMIT) for__________________.NN1E-3A-1 Pg1-195 takeoff landing go-around All of the above 17 / 158 If aircraft purge is in progress, as indicated by the entry door closed and the shade down, the doors will remain closed, until cleared open by___________E-3A M 3.2-17 Pg 19 Only the FE The FE or ST Only the ST None of the Above 18 / 158 If the APU does not shutdown with the APU control switch, ____________, EGT should decrease immediately. After APU door caution light goes out, ______________ to prevent inadvertent discharge of APU fire bottle.NN1E-3A-1 Pg2-97 move the Manual Start switch to the MAN position, return switch to the NORM position place BATTERY switch to OFF, return switch to the ON position pull APU fire switch, push in APU fire switch none of the above 19 / 158 Flight suit sleeves are to be rolled down __________ with __________.FC FO 3.2-1 Pg 61 while on the aircraft, engines running while on the aircraft, the doors closed in-flight, simulated emergency procedures during pre-flight, engines running 20 / 158 During descent, approach and landing, all flight crewmembers will monitor their respective instruments and all radio transmissions by the controlling agency, and advise the pilot when noting any deviations from the clearance/procedures (± ___ knots of airspeed, ± ____ feet in altitude, or ± ___ degrees of heading/course).E-3A M 3.2-17 Pg 23 10, 200, 10 20, 100, 20 10, 100, 10 20, 200, 20 21 / 158 IFR departure procedures do not ensure clearance of ______ obstacles. Perform obstacle clearance calculations to ensure clearance of these obstacles.NN1E-3A(II)-1-1 PG:A3-22 AEO OEI low close-in mountain 22 / 158 Crewmember handling escape hatch in flight must wear _______________ .NN1E-3A-1 Pg3-15 nomex gloves restraint harness parachute firefighters gloves 23 / 158 The Takeoff Warning System receives power through the________________________________________ circuit breaker(s) on the P5 panel.NN1E-3A-1 Pg1-263 MACH WARN BELL LANDING GEAR WARN HORN MACH WARN BELL and LANDING GEAR WARN HORN NONE OF THE ABOVE 24 / 158 If starter shaft is sheared, indications are same as a normal start, except that __________________ do not increase. Release start selector switch immediately to prevent additional damage to starter.NN1E-3A-1 Pg2-38 N2 and fuel flow fuel flow and oil pressure N2 and oil pressure none of the above 25 / 158 Operation of the ground maintenance control panels is locked out by the landing gear safety (squat) switch and switches ___________ to the takeoff valve configuration at liftoff.NN1E-3A-1 Pg1-923 manually automatically abnormally after 40 seconds 26 / 158 Which of the following would increase or decrease Critical Field Length by approximately 100 feet:NN1E-3A(II)-1-1 PG:?? One degree Celsius of runway temperature 1,000 pounds gross weight 100 feet pressure altitude All of the above 27 / 158 Engine flameout can occur if airplane pitch attitude exceeds 8 degrees nose up or 10 degrees nose down when any outboard main tank contains less than ______ pounds or any inboard main tank contains less than ______ pounds.NN1E-3A-1 Pg6-16 2,000 / 6000 2,500 / 6,500 2,500 / 6,000 6,500 / 2,500 28 / 158 It can take up to _______ minutes after airflow stops for a NO FLOW caution light to illuminate.NN1E-3A-1 Pg1-940 Two Three Four Five 29 / 158 ______ is the highest speed from which the airplane can stop without exceeding the maximum energy absorption capability of the brakes.NN1E-3A(II)-1-1 PG:A3-4 Refusal speed Maximum braking speed (VB) Decision speed (V1) Rotation speed (VR) 30 / 158 The maximum takeoff rated thrust (TRT) EGT is ______.NN1E-3A-1 Pg5-16 565° C 555° C 455° C 490° C 31 / 158 When planning a takeoff, also check the maximum crosswind for ____. Under some conditions, landing crosswind limit is ________ takeoff crosswind limit, possibly preventing emergency return to departure airfield.NN1E-3A(II)-1-1 PG:A3-13 landing, equal to go-around, more than landing, more than landing, less than 32 / 158 In flight continued oil pressures below ___ psi or above ___ psi require engine shutdown or landing as soon as practicable, using the minimum thrust required.NN1E-3A-1 Pg5-3 35, 65 30, 65 35, 60 40, 60 33 / 158 The ______ can start no earlier than the time at which the crew member completes their duties from the previous flight or duty period and has departed their place of work.FC FO 3.2-1 Pg 37 crew duty day crew rest period showtime mission planning 34 / 158 Pilots are not to fly over the tops of thunderstorms or downwind under the anvil. Thunderstorms are to be avoided by ______ at or above _______, and _______ below _______.FC FO 3.2-1 Pg 43 20 NM, FL230; 10 NM, FL230 10 NM, FL230; 5 NM, FL230 15 NM, FL150; 5 NM, FL150 10 NM, FL150; 10 NM, FL150 35 / 158 If start valve fails to close when start selector is released (indicated by VALVE OPEN indicator illuminated, or no rise in duct pressure), call “____________” and terminate start by setting throttle to CUTOFF, closing wing ISOLATION valve(s), and shut off________________ to avoid damage to the starter.NN1E-3A-1 Pg1-69 stop start, APU bleed valve no cutout, APU bleed valve stop start, engine bleed air valve(s) no cutout, starter air source 36 / 158 Optimum outboard thrust is less than TRT if ______ is greater than ______ at takeoff rated thrust..NN1E-3A(II)-1-1 PG:A3-3 VMCG; VCEF runway available; critical field length VMCA; VR TODA; TORA 37 / 158 Flight engineer will select _______ on the Maintenance Interphone Selector Switch if personnel are in the lower deck in-flight or during ______________.NN1E-3A-1 Pg 1-10 BOTH, emergencies MISSION, emergencies requiring mission crew coordination AIRCRAFT, emergencies BOTH, emergencies requiring mission crew coordination 38 / 158 If IFF Master mode is selected to NORM the transponder transmits when interrogated, and when squitter is active. During transmission the minimum personnel safety distance is ______feet from either antenna. The minimum electro-explosive device distance is _____feet.NN1E-3A-1 Pg1-11 50, 100 10, 50 25, 50 10, 25 39 / 158 If a stop is attempted at a speed greater than ___, the airplane probably cannot be stopped in the available runway.NN1E-3A-1 Pg3-18 V1 VMCG Refusal VCEF 40 / 158 Operating air conditioning system manual mode with max cooling (pack bypass valve closed) can cause ice to form in the water separator. If any cabin altitude or pressure fluctuations are detected in the system, open bypass valve or switch air conditioning system to ______________.NN1E-3A-1 Pg1-910 MAN Ram air mode AUTO Heat exchanger only mode. 41 / 158 Which of the following statement(s) is/are true regarding bird strike actions?FC FO 3.2-1 Pg 44 If a bird strike causes visible damage to the aircraft or abnormal system indications, the flight is to be terminated and a landing is to be performed at the nearest suitable airfield as soon as practicable. If a minor bird strike has no impact on safety-of-flight, the mission may be continued at the discretion of the AC Confirmed bird strikes in an area not visible to the crew must be carefully treated and thoroughly analyzed. ACs are to determine what precautionary action, if any, is required. All of the above 42 / 158 Do not use the ________ position in flight, or attempt to re-engage starter on a rotating engine. Starter drive can be damaged.NN1E-3A-1 Pg1-56 BYPASS GND START FLT START None of the above 43 / 158 If Liquid Cooling System EGW leak or spill is found on preflight, do not accept airplane for flight until ____________ has determined whether the problem is a leak or spill and has removed as much of the liquid as possible.NN1E-3A-1 Pg2-8 The RT The Command Post Maintenance All of the Above 44 / 158 If engine was shut down as a precautionary measure and engine and flight conditions permit, the fuel system can be cooled if windmilling N2 RPM is at least ____; open CONTINUOUS IGNITION circuit breaker to prevent engine relight and set throttle to idle for __________________ to prevent excessive temperatures in the fuel control.NN1E-3A-1 Pg3-8 25%, 3 minutes each 30 minutes 35%, 2 minutes each 20 minutes 25%, 2 minutes each 20 minutes 15%, 3 minutes each 20 minutes 45 / 158 Aircrew duties are forbidden for at least ___ hours after a local anesthetic, including dental anesthetic.FC FO 3.2-1 Pg 68 6 24 48 72 46 / 158 When engine rpm and EGT have stabilized after starter cutout, N2 RPM should be between __________% and EGT below ________. N1 RPM below _____ at this time is a sign of possible internal engine malfunctions.NN1E-3A-1 Pg1-69 56 and 60, 400°C, 35% 54 and 60, 455°C, 25% 54 and 60, 340°C, 25% 40 and 60, 490°C, 35% 47 / 158 Crew bunks will not be occupied during takeoff, landing, or ______________. Additionally, bunks will not be used for _______________ at any time.NN1E-3A-1 Pg1-1006 in the orbit, eating in-flight refueling, cargo tiedown during cruise, cargo tiedown go-around, eating 48 / 158 The weather radar will not be operated at cabin pressure altitudes above _________ feet.NN1E-3A-1 Pg1-1090 15,000 18,000 20,000 25,000 49 / 158 The climbout is divided into four segments; For One Engine Inoperative, the first climbout segment begins at liftoff at the end of ______ and ends at ______.NN1E-3A(II)-1-1 PG:A3-20 takeoff ground run; screen height TORA; DER CFL; completion of landing gear retraction the clearway; termination height 50 / 158 Set APU control switch to STOP if EGT does not start to rise within _______ seconds of APU accumulator pressure stabilizing after drop for APU starter. Wait _______ minutes, then switch to other accumulator for second attempt.NN1E-3A-1 Pg2-11 two, five five, two ten, five thirty, five 51 / 158 Both ________ doors and the ________ door are equipped with safety straps. These straps will be fastened across door opening if door is open and _________________.NN1E-3A-1 Pg1-990 cargo, galley, ground refueling is in progress entry, galley, no stairs are in place cargo, radio access, ground refueling is in progress entry, radio access, no stairs are in place 52 / 158 With all engines operating, do not climb at a speed less than _____ because of degraded climb performance.NN1E-3A(II)-1-1 PG:A3-21 VMFR V2+10 V2 VMCA 53 / 158 Intersection take-offs are ______.FC FO 3.2-1 Pg 53 exciting prohibited a time saver allowed 54 / 158 For effective anti-ice protection, maintain a minimum of ___________ on each engine if anti-ice is on.NN1E-3A-1 Pg2-62 70% N1 2000 pph fuel flow 70% N2 55% N1 55 / 158 Excessive negative cabin pressure can cause personnel injury and/or damage to the __________ fanNN1E-3A-1 Pg2-13 AFT Forced Air Cooling FWD Forced Air Cooling Draw Through Cooling Power Feeder Duct 56 / 158 Take-offs, approaches and landings are not permitted at airfields where freezing ___ is falling, or ______ is present.FC FO 3.2-1 Pg 43 drizzle; freezing fog snow; sleet hail; standing water rain; freezing fog 57 / 158 If the EGT exceeds ______ at any time, shut down the engine, if thrust is not needed for safety of flight, or _______________________.NN1E-3A-1 Pg5-16 555° C, land as soon as practicable 555° C, land as soon as possible 565° C, land as soon as practicable 565° C, land as soon as possible 58 / 158 Which of the following statements is true regarding an inadvertent brute force disconnect?NN1E-3A-1 Pg8-11 Air refueling will be terminated except during fuel emergencies or when continuation of air refueling is dictated by operational necessity. Air refueling will be terminated immediately. Air refueling will be terminated except during fuel emergencies Air refueling may be continued during training sorties at the discretion of the aircraft commander. 59 / 158 When starting engines, the ENG OIL PRESS X caution message may remain displayed, or displayed intermittently, for up to _ minutes after the oil temperature reaches ____ at IDLE rpm.NN1E-3A-1 Pg1-57 4, 40°C 5, 40°C 5, 50°C 4, 50°C 60 / 158 Prior to entering, or at any time personnel are in wheel well, ensure manual door release handles are ________ and ___________.NN1E-3A-1 Pg1-229 down, latched down, engaged closed, latched closed, engaged 61 / 158 The radiation hazard to fuel handling operations does not extend beyond ___ feet from the radiating antenna. There are no personnel restrictions and it is not necessary to establish a restricted access zone in front of the antenna.NN1E-3A-1 Pg5-34 3.2 feet 32 feet 320 feet 322 feet 62 / 158 The maximum permitted crosswind component, gusts included, for take-off and landings is ______.FC FO 3.2-1 Pg 41 limited by FPS 15 knots 50 knots 25 knots 63 / 158 If DVRTR VALVE CLOSED light is not illuminated when airplane is on the ground with system in ENG-APU mode, diverter valve must be closed ____________ to assure adequate cooling airflow in selected racks.NN1E-3A-1 Pg1-944 prior to takeoff immediately electrically manually 64 / 158 The angle of attack system senses inboard flap position only. The indications are not correct when flying with _______________ flaps.NN1E-3A-1 Pg1-282 "split" asymmetric "split" or asymmetric emergency 65 / 158 If the indicated frequency of the isolated generator is outside the range of 400 + 8 Hz, fluctuates more than 4 Hz within the + 8 Hz range, or OHEAT light illuminates, or generator breaker does not remain closed, .NN1E-3A-1 Pg1-125 Check IDG oil temperature indicator and LOW RPM light. If indications are normal, shut down generator and disconnect IDG open bus tie breaker for the affected generator shut down generator Disconnect IDG 66 / 158 When performing a manual start, if the start valve does not close when released, notify pilot to ________________ to prevent starter damage.NN1E-3A-1 Pg1-70 have ground crew close valve manually motor engine for a minimum of 15 seconds pull fire switch immediately shut down engine 67 / 158 To prevent possible over-filling of tank and resulting structural damage, air refueling of wing tank with inoperative fuel gage will _________________.NN1E-3A-1 Pg3-112 never be attempted not be attempted except in an actual fuel emergency be attempted only when the gage in the same tank in the opposite wing is operable Both B and C 68 / 158 Terminate engine start if no oil pressure is observed within ___ seconds of start initiation.NN1E-3A-1 Pg2-40 15 20 30 60 69 / 158 Do not apply brakes with brake pedals while retracting landing gear. The forces generated by rapid stopping of wheels could damage ____________. If pedals are applied, record so maintenance can check the strut.NN1E-3A-1 Pg1-222 shock strut torsion link truck leveling mechanism trunnion 70 / 158 Flight crew UHF radio is available for communication as long as power is available on _____________. Limit transmission to five seconds and receiver operation to _____ minutes unless draw-through cooling is available.NN1E-3A-1 Pg2-94 emergency AC bus, ten emergency DC bus, five AVDC 2, ten battery bus, five 71 / 158 Maximum Refueling Altitude: The altitude (for a given gross weight and ambient temperature) at which the receiver has a climb capability of ______ feet per minute at normal rated thrust in the contact position at the normal refueling air speed.NN1E-3A(II)-1-1 PG:A10-1 200 zero 1,000 none of the above 72 / 158 What is the maximum engine oil temperature limit?NN1E-3A-1 Pg5-8 132° C 165° C 163 ± 5° C 163 ± 5° F 73 / 158 Do not operate the ____________ lights or the ____________ lights unless airplane is in motion, except for momentary checks to verify operation.NN1E-3A-1 Pg1-968 landing, wing runway turnoff, wing runway turnoff, strobe landing, runway turnoff 74 / 158 Do not pressurize airplane if APU DOOR caution light is illuminated, as damage to ________________ can occur.NN1E-3A-1 Pg3-60 APU doors APU door limit switches APU start box APU shroud 75 / 158 If possible, launch life rafts over ____________ of wing to avoid damage from flaps. Do not allow raft to contact ________________.NN1E-3A-1 Pg1-1036 leading edge, overwing fuel filler ports side, static dischargers leading edge, vortex generators trailing edge, static dischargers 76 / 158 Do not operate antiskid TEST switch while taxiing. If brakes are in use, TEST switch ____________ one set of brakes.NN1E-3A-1 Pg1-237 applies releases locks none of the above 77 / 158 Aircraft shall not exceed 0.75 Mach when aircraft gross weight is below __________ pounds and the CG is aft of ______ % MAC.NN1E-3A-1 Pg2-61 230,000, 32 230,000, 35 250,000, 35 250,000, 32 78 / 158 Do not operate nacelle anti-ice at power settings above 70% N1 when outside air temperature is above 10° C unless ____________________. Operation of nacelle anti-ice under these conditions for more than ___ seconds can cause damage to the engine. Anti-ice may be tested for up to ___ minute(s) at power settings below 70% N1 at temperatures above 10° C.NN1E-3A-1 Pg2-44 visible moisture is present, 10, one visible moisture is present, 30, two a nose cowl anti-icing valve does not open at idle thrust, 20, five none of the above 79 / 158 The DC load on any one-transformer rectifier (T/R) unit must never exceed ___ amperes for 1 minute; and ____ amperes continuous.NN1E-3A-1 Pg5-30 60, 170 65, 200 200, 75 170, 218 80 / 158 If refueling is in progress when crew members show up at the aircraft, they will not enter the refueling zone without permission from the ____________. The refueling zone can be identified by the _______________________.E-3A M 3.2-17 Pg 19 refueling supervisor, orange cones positioned around the aircraft maintenance supervisor, orange cones positioned around the aircraft refueling supervisor, refueling supervisor positioned at the nose of the aircraft maintenance supervisor, refueling supervisor positioned at the nose of the aircraft 81 / 158 If N2 sensing shaft fails on the ground, immediately _______________. If N2 sensing shaft fails during takeoff prior to ________ and the takeoff is aborted, immediately take the throttle to cutoff.NN1E-3A-1 Pg1-64 increase thrust on the symmetrical engine, V1 decrease thrust on the symmetrical engine, Refusal Speed pull fire switch for the malfunctioning engine, VB take the throttle to cutoff, V1 82 / 158 ______ is based on critical field length and is the lowest speed at which the upwind outboard engine can fail and the takeoff continue safely.NN1E-3A(II)-1-1 PG:A3-4 Ground minimum control speed (VMCG) Refusal speed Rotation speed (VR) Decision speed (V1) 83 / 158 The required AEO Climb Gradient (CG) for all departures is the greater of:FC FO 3.2-1 Pg13 200 ft/NM The CG required by ATC (unless unable and ATC is informed) The CG required for obstacle clearance All of the above 84 / 158 If torching is reported by the ground crew, _____________ with normal start procedures. If abnormal indications are observed, discontinue start immediately and announce “Stop Start”, and set throttle to CUTOFF and if N2 is below 35% hold the Start Selector switch to GND START for ____ seconds to clear fuel from engine.NN1E-3A-1 Pg2-38 discontinue, 15 continue, 15 discontinue, 30 continue, 30 85 / 158 Pack controller and zone temperature controllers are cooled by _________________.NN1E-3A-1 Pg2-108 forward forced air cooling aft forced air cooling draw-through cooling APU bleed air 86 / 158 Operating procedures, techniques, etc., which can result in personal injury and/or loss of life if not carefully followed is a _______________.NN1E-3A-1 Pg xix Note Caution Warning Local Operating Procedure 87 / 158 Equipment malfunction and damage can occur if indicated voltage drops to ______ volts or lower. If indicated voltage of isolated generator is outside the range of _______ volts, shut down generator.NN1E-3A-1 Pg1-178 110, 115 ± 2 95, 115 ± 4 110, 115 ± 4 95, 115 ± 2 88 / 158 ______ is the minimum airborne speed at which an outboard engine can fail, and with no change to the thrust of the remaining engines, the airplane can be kept on a straight flight path with rudder boost ON and no more than five degrees of bank away from the failed engine.NN1E-3A(II)-1-1 PG:A3-4 VMCA V1 VMCG VR 89 / 158 Which of the following starting malfunctions would require you to discontinue the start immediately by setting the throttle to cutoff?NN1E-3A-1 Pg2-37 EGT does not increase within 60 seconds after throttle is moved to idle. (Wet start.) N1 or N2 not increasing, or increasing slowly while EGT is rapidly increasing. (Hung start.) No indication of oil pressure 15 seconds after start initiation. N2 RPM 56% two minutes after fuel on (throttle advance). 90 / 158 During preflight, if air is not flowing from draw through fan outlet, open ________________ manually and check ______________.NN1E-3A-1 Pg2-24 overboard valve, fan circuit breakers heat exchanger valve, flow control valve hold open solenoid flow control valve, fan circuit breakers venturi exhaust, flow control valve hold open solenoid 91 / 158 If APU shuts down during power transfer, or from no apparent cause, have condition of APU _______________ checked before next start attempt.NN1E-3A-1 Pg2-12 start accumulators, battery bus generator, emergency lighting battery accessory drive shaft surge accumulator, hot battery bus 92 / 158 If changing drives with rotodome rotating, set SPEED switch to OFF and wait ___ seconds before selecting other system. SPEED switch must not remain OFF. Notify ___ when changing drives.NN1E-3A-1 Pg3-43 10, DT 10, TD 10, RT 15, RT 93 / 158 The rotodome must be rotating when any airplane engine(s) is operating. Failure to comply can cause damage to rotodome ________________.NN1E-3A-1 Pg1-195 system control shuttle valve hydraulic clutch turntable bearing drive motor 94 / 158 The FREQ. REF. UNIT (FRU) circuit breaker _________ be reset if it trips in flight.NN1E-3A-1 Pg3-93 will not should not may will 95 / 158 Operating procedures, techniques, etc., which can result in damage to equipment if not carefully followed is a ____________________.NN1E-3A-1 Pg xix Note Caution Warning Local Operating Procedure 96 / 158 ______ is the target speed after losing an engine during takeoff. For four engine operation, the airplane is accelerated to ______.NN1E-3A(II)-1-1 PG:A3-18 250; 280 V2; VMCA V2; V2+10 VMCG; VMCG +10 97 / 158 Landing or takeoff will not be attempted with over ___ – inch of _____________ on the runway.NN1E-3A-1 Pg7-8 1/2, water 1, standing water or slush 1, volcanic ash 1/2, standing water or slush 98 / 158 Minimum flap retraction speed VMFR is computed by adding __ knots to V2.NN1E-3A(II)-1-1 PG:A3-30 10 20 30 40 99 / 158 On preflight inspection, the main gear leveling cylinder reset handle must be in the green band if the system is pressurized. If the handle is in the _______________ band, replenish the fluid by pulling out on the handle. If the handle is in the _______________ band, the valve is defective.NN1E-3A-1 Pg1-229 outer red, inner red inner red, outer red silver, inner red silver, outer red 100 / 158 If any main landing gear down (green) light does not illuminate when gear is confirmed down and locked, and one or more REL indicators do not illuminate on preflight or during in-flight check, use _____________ data.NN1E-3A-1 Pg1-237 brakes released 6 brakes operating antiskid inoperative spoilers inoperative 101 / 158 For the first _____minutes after LAIRCM system power-up, the aircraft must remain stationary or a Signal Processor failure may occur.NN1E-3A-1 Pg2-46 Two One Three Four 102 / 158 Brake cooling procedures contained in section V of CSTO NN1E-3A-1 will be followed after any stop which yields a brake energy above ____ million foot-pounds per brake.NN1E-3A(II)-1-1 PG:A8-5 10 15 24 28 103 / 158 Do not use firefighter’s smoke mask with portable oxygen bottle above _________ feet cabin (pressure) altitudes.NN1E-3A-1 Pg1-1004 25,000 30,000 40,000 42,000 104 / 158 To prevent PFD reversion, close __________ circuit breakers prior to closing MFD circuit breakers. If PFDs are displayed on MFDs No.2 or No. 3, cycle applicable circuit breaker to reassign MFD as an IMFD (P61-4).NN1E-3A-1 Pg2-10 MFD NO. 2 & NO. 3 MFD NO. 2 & NO. 4 MFD NO. 1 & NO. 3 MFD NO. 1 & NO. 4 105 / 158 The takeoff phase is enabled when ground speed transitions to greater than 80 knots. The takeoff phase is terminated when which one of the following occurs?NN1E-3A-1 Pg 1-1045 Radio altitude transitions for above 400 feet 20 seconds after the aircraft transitions from ground to air Ground speed transitions from greater than 80 knots to less than 75 knots in the case of a rejected takeoff Any of the above 106 / 158 An extremely thin layer of frost on the upper wing surface and snow or ice on any surface _______________.NN1E-3A-1 Pg7-15 will have no appreciable effect on aircraft performance will have no appreciable effect on aircraft performance as long as the thickness is less than 1/8 inch can degrade performance seriously will blow off during takeoff roll 107 / 158 Re-compute applicable takeoff data if any weather or configuration change occurs greater than as follows: Runway Temperature_______ °C; Pressure Altitude _______ feet; Gross Weight _______ pounds; CG _______ %NN1E-3A-1 Pg2-3 2, 200, 2,000, 0.2 5, 500, 5,000, 0.5 5, 1,000, 500, 0.5 5, 500, 3,000, 1.0 108 / 158 When connecting external power, wait _____ seconds after the external power source is connected to the external receptacles or the BATTERY switch is set to ON, whichever occurs last, before pressing EXTERNAL POWER switch to ON.NN1E-3A-1 Pg1-157 four five six seven 109 / 158 ______ is the total length of hard surface, not including overruns.NN1E-3A(II)-1-1 PG:A3-4 Runway length Critical field length Takeoff distance available (TODA) Takeoff ground run 110 / 158 If internal engine damage is suspected, perform ________________ checklist.NN1E-3A-1 Pg3-54 ENGINE STALL RECOVERY ENGINE RELIGHT PRECAUTIONARY ENGINE SHUTDOWN ENGINE FAILURE OR FIRE 111 / 158 Which of the following statement(s) is/are true regarding touch-and-go landings?FC FO 3.2-1 Pg 52 Runway length and width must be a minimum of 8000 x 130 feet (7,800 x 130 feet if the runway is dry.) Minimum RCR is 07. Touchdown within the first 3,000 feet of runway available, otherwise a go-around is to be initiated Both A and C 112 / 158 ______ is the distance required to reach takeoff speed without loss of an engine.NN1E-3A(II)-1-1 PG:A3-4 TORA Runway available Critical field length Takeoff ground run 113 / 158 High pressure compressor (N2) RPM limit is _____ %.NN1E-3A-1 Pg5-7 100 101.1 101.5 104.5 114 / 158 If evacuating after aborted takeoff or heavyweight landing, depart directly _________ or _________ of airplane to avoid possible tire/wheel burst area if fuse plugs melt.NN1E-3A-1 Pg3-10 forward, aft left, right aft, side to the bus, left 115 / 158 If any combination of boost pump circuit breakers trip, set pump switch to OFF and open all breakers for that pump. In flight, unless required for safety of flight, leave circuit breakers open. Do not reset breakers until __________.NN1E-3A-1 Pg3-93 maintenance personnel inspect the system they have cooled for about five minutes maintenance personnel are reasonably sure that the circuit breaker is faulty maintenance personnel direct you to do so 116 / 158 The nose gear _________________ must be inserted manually before landing if the utility hydraulic system is depressurized.NN1E-3A-1 Pg1-230 ground lock handle maintenance downlock drag brace lock pin emergency lock pin 117 / 158 ______ is the speed at which rotation from three point-attitude to the takeoff attitude is initiated.NN1E-3A(II)-1-1 PG:A3-4 V1 Refusal VMCA Rotation speed (VR) 118 / 158 Allow _______ seconds for bypass valves to operate between turning emergency flap switch on and operating electric drive motors.NN1E-3A-1 Pg1-269 5 6 7 8 119 / 158 If LOW RPM light fails to go out during engine start __________________, shut down the engine and have maintenance make a visual check for structural integrity and verify IDG is reconnected before attempting restart.NN1E-3A-1 Pg1-179 do not attempt to close generator breaker and generator breaker does not close immediately disconnect the IDG Continue, parallel operation is not affected as long as the sync bus is energized 120 / 158 When operating unpressurized and the aft forced air cooling system RAM VALVE OPEN indicator is illuminated, control the temperature of the aft system manually at ___________.NN1E-3A-1 Pg2-110 40 ± 8° F 45 ± 5° F 40 ± 8° C 35 to 70° F 121 / 158 Best endurance airspeed will normally be used for the orbit (minimum airspeed = ______).E-3A M 3.2-17 Pg 25 220 KIAS 210 KIAS 200 KIAS 250 KIAS 122 / 158 _______________tank boost pumps must be OFF unless personnel are available in the flight deck to monitor low pressure lights. Each ______________tank boost pump must be positioned OFF without delay when the tank boost pump LOW pressure light illuminates.NN1E-3A-1 Pg5-19 Center wing, Main Center wing, Reserve Center wing, Center wing Main, Center wing 123 / 158 At any time if either the boom operator or the receiver pilot is unable to accomplish disconnect or if the blue READY indicator stays on or comes back on after contact has been established, the receiver engineer must set the SIG AMPL switch to ____ and the MNL TGL switch to ____ and the pilot must press the autopilot and boom disconnect button.NN1E-3A-1 Pg8-9 MAN, HOLD NORM, HOLD MAN, REL NORM, REL 124 / 158 For which of the following configuration(s) is no performance data available?NN1E-3A-1 Pg6-9 Go-around with two engines and rudder boost off. Flaps 25 with 2 engines inoperative Flaps 25, with 1 engine and rudder boost inoperative. All of the above 125 / 158 When setting RUDDER switch to ON in flight, ensure _________________. This is to prevent excessive structural loads caused by rapid increase in rudder deflection and to maintain aircraft control during the transition to powered rudder.NN1E-3A-1 Pg1-246 rudder is in neutral (centered) position rudder trim is in neutral (centered) position aircraft is straight and level both A and B 126 / 158 Training Missions will be terminated when any of the following occur.E-3A M 3.2-17 Pg 48 Engine shutdown Either hydraulic system failure Primary flight control malfunction. All of the above 127 / 158 Oxygen is required for personnel entering the aft lower lobe when pressurization is in ______________ operation.NN1E-3A-1 Pg1-10 automatic manual the takeoff mode of the landing mode of 128 / 158 Rolling takeoffs reduce available runway by a total of ______ feet which includes the lineup distance of ______ feet.NN1E-3A(II)-1-1 PG:A3-4 700; 200 600; 100 800; 300 400; 200 129 / 158 If external power is on the airplane bus and the AVAIL indicator is not illuminated, the _____________ switch must be off (ON indicator out) before connecting APU or airplane generators.NN1E-3A-1 Pg1-157 BUS TIE OPEN APU GENERATOR EXTERNAL POWER EMERGENCY POWER 130 / 158 To prevent crewmembers from being overcome by inadvertent leakage of SF6 gas in the lower aft compartment, crewmembers will ensure that flight engineer is ___________ the compartment before entering lower aft compartment. Crewmembers will don __________ before entering the aft lower compartment when investigating radar equipment malfunctions.NN1E-3A-1 Pg 1-10 venting, nomex gloves venting, fire fighter's gloves inspected, smoke goggles venting, oxygen 131 / 158 If brakes are applied above ___ knots, brake limits will be checked and recommended procedures followed for brake cooling.NN1E-3A-1 Pg3-18 70 80 90 100 132 / 158 When operating flaps electrically with utility hydraulic pressure available, set flap lever to a position ____________ desired flap setting in direction of motion to prevent damage to hydraulic drives.NN1E-3A-1 Pg1-268 corresponding to beyond at or beyond none of the above 133 / 158 Low pressure compressor (N1) RPM limit is _____ %.NN1E-3A-1 Pg5-6 100 101.1 101.5 104.5 134 / 158 Before initiating a high speed descent, check for structural damage which could be increased by high speed descent.NN1E-3A-1 Pg3-37 TRUE FALSE 135 / 158 ______ is the maximum speed to which the airplane can accelerate and then stop on the available runway.NN1E-3A(II)-1-1 PG:A3-4 V1 Refusal Speed Rotation speed (VR) VMCG 136 / 158 If draw through cooling NO FLOW caution light remains illuminated, _________________ and notify TD to shut down mission equipment cooled by draw through system.NN1E-3A-1 Pg3-117 open three flight deck UHF circuit breakers on P5 panel open UHF XCVR and UHF XCVR CPLR circuit breakers on P5 open four flight deck UHF circuit breakers on P6 panel open CSU 1 circuit breaker on P5 panel 137 / 158 Which statement is true concerning the Electrical Smoke Source Isolation procedure?NN1E-3A-1 Pg3-33 It will not be attempted on a bus which has been identified as the source of an electrical fire. It will not be attempted on a bus which has been identified as the source of fire, smoke or fumes. It will only be attempted at the direction of the pilot or flight engineer None of the above 138 / 158 Failure to hold engine start selector in GND START until _____ N2 RPM is reached can result in a “_____________”.NN1E-3A-1 Pg1-69 25%, Slow Start 35%, Wet or Hot Start 54%, Hung Start 25%, Wet Start 139 / 158 When opening entry or galley doors after emergency landing or ditching, stop when door handle is in vertical position and check _____________________.NN1E-3A-1 Pg3-9 for structural damage that unidentifiable odors are not present for possible entry of fire, smoke, or water that retaining bar passes through slide harness 140 / 158 Mission radar will remain in standby/dummy load until rotodome purge time is complete (______ minutes after closing slipway doors).NN1E-3A-1 Pg8-8 Two Five Seven Ten 141 / 158 To protect aileron control system from wind damage on the ground, flaps should be ___________ to lock out outboard aileron when airplane can be subjected to wind of ___ knots or more.NN1E-3A-1 Pg2-91 retracted, 35 extended, 35 retracted, 50 extended, 50 142 / 158 Prior to servicing or purging portable oxygen bottles, ensure __________ and oxygen _________ are free of oil or grease.NN1E-3A-1 Pg1-1027 supply lever, dust cap diluter lever, filler port filler port, recharger outlet release lever, recharger outlet 143 / 158 When transferring from external power or APU to the airplane generators, close only ______generator breaker. When bus tie breaker re-closes, the other generator breakers may be closed as rapidly as desired.NN1E-3A-1 Pg2-45 number 5 one number 6 number 2 144 / 158 When performing touch and go landings on a dry runway, use go-around thrust (instead of 90% N1) if above ____________ pressure altitude or ______ OAT.NN1E-3A-1 Pg2-86 1000 ft, 40° C 1500 ft, 50° C 1500 ft, 50° F 2000 ft, 50° C 145 / 158 Do not set rudder override switch to OVERRIDE above _________ KIAS. Structural damage could result from full or rapid rudder movement with full rudder pressure.NN1E-3A-1 Pg1-246 185 223 250 265 146 / 158 When parking, taxi the airplane a few feet with nose gear centered to _______.NN1E-3A-1 Pg1-233 ensure wheel chocks can be inserted properly prevent tire scrubbing relieve pressure in the centering cylinder relieve strut side loads 147 / 158 What is the normal pressure range for the auxiliary hydraulic system?NN1E-3A-1 Pg5-8 2600 – 3200 PSI 2400 – 3100 PSI 2400 – 3200 PSI 2600 – 3100 PSI 148 / 158 Do not operate radios until cabin temperature is below _____________.NN1E-3A-1 Pg1-855 110 F 105 F 100 F 95 F 149 / 158 The ____________ is unable to release the boom toggles during manual boom latching.NN1E-3A-1 Pg8-10 boom operator receiver pilot flight engineer all of the above 150 / 158 AAR is not to be conducted at gross weight less than ______ lbs and the aircraft center of gravity is to be forward of ______during AAR.FC FO 3.2-1 Pg 52 205,000; 32% 210,000; 31% 215,000; 31% 220,000; 32% 151 / 158 During engine start, if ground crew has not called “rotation”, and/or N1 RPM is not indicated by _____% N2, release start switch and investigate cause before attempting another start.NN1E-3A-1 Pg1-69 25 15 35 None of the above 152 / 158 Engine fuel line damage can result from IDG case separation. Possible indications of case separation are ______________.NN1E-3A-1 Pg3-94 generator failure illumination of LOW RPM light abnormally high or low IDG oil temperature indications All of the above 153 / 158 Do not retract fuel dump chutes until all fuel dump valves have indicated closed for ___ minutes to prevent fuel draining into wing (except as required to close valves).NN1E-3A-1 Pg3-56 1 2 3 4 154 / 158 Maintain fuel flow above 2000 pounds per hour when mission radar is operating at high power, except that thrust may be reduced to idle below ________ feet (________ feet with anti-ice on) if at least 6 generators are in parallel.NN1E-3A-1 Pg5-3 34,000, 29,000 35,000, 25,000 34,000, 28,000 35,000, 29,000 155 / 158 Interruption of electric power when changing from airplane generators to external power (or APU) or when changing to airplane generators from external power (or APU) can cause the forced air fan _____ to trip.NN1E-3A-1 Pg1-946 ELCU CB logic thermal sensor 156 / 158 The maximum load in the crew baggage tiedown area is _______ pounds or ______ pounds per square foot.NN1E-3A-1 Pg5-35 2598, 90 2600, 80 2598, 120 2500, 120 157 / 158 Do not restart an engine, which has been shut down for ____________ or ____________, unless a more serious emergency occurs which requires the thrust of that engine.NN1E-3A-1 Pg3-57 fire, abnormal vibration high oil pressure, fire low oil pressure, excessive vibration fire, excessive vibration 158 / 158 When loading baggage, do not obstruct access to __________________.NN1E-3A-1 Pg1-1019 first aid kits crash axes fire extinguishers emergency equipment Your score isThe average score is 90% LinkedIn Facebook VKontakte 0% Restart quiz FE 25 Question 1 / 25 Which of the following statement(s) is/are true regarding touch-and-go landings?FC FO 3.2-1 Pg 52 Runway length and width must be a minimum of 8000 x 130 feet (7,800 x 130 feet if the runway is dry.) Minimum RCR is 07. Touchdown within the first 3,000 feet of runway available, otherwise a go-around is to be initiated Both A and C 2 / 25 If internal engine damage is suspected, perform ________________ checklist.NN1E-3A-1 Pg3-54 ENGINE STALL RECOVERY ENGINE RELIGHT PRECAUTIONARY ENGINE SHUTDOWN ENGINE FAILURE OR FIRE 3 / 25 _______ is the total length of runway required to accelerate on four engines to V1, experience an engine failure and then continue the takeoff or stop.NN1E-3A(II)-1-1 PG:A3-4 Critical field length Takeoff ground run Takeoff distance Takeoff run available 4 / 25 When transferring from external power or APU to the airplane generators, close only ______generator breaker. When bus tie breaker re-closes, the other generator breakers may be closed as rapidly as desired.NN1E-3A-1 Pg2-45 number 5 one number 6 number 2 5 / 25 Prior to entering, or at any time personnel are in wheel well, ensure manual door release handles are ________ and ___________.NN1E-3A-1 Pg1-229 down, latched down, engaged closed, latched closed, engaged 6 / 25 Crew bunks will not be occupied during takeoff, landing, or ______________. Additionally, bunks will not be used for _______________ at any time.NN1E-3A-1 Pg1-1006 in the orbit, eating in-flight refueling, cargo tiedown during cruise, cargo tiedown go-around, eating 7 / 25 Pilots are not to fly over the tops of thunderstorms or downwind under the anvil. Thunderstorms are to be avoided by ______ at or above _______, and _______ below _______.FC FO 3.2-1 Pg 43 20 NM, FL230; 10 NM, FL230 10 NM, FL230; 5 NM, FL230 15 NM, FL150; 5 NM, FL150 10 NM, FL150; 10 NM, FL150 8 / 25 The flight crew UHF-ADF radio is powered by the UHF ADF AC and UHF ADF DC circuit breakers on the P5 panel and is cooled by the ____________ system.NN1E-3A-1 Pg1-861 fwd forced air cooling aft forced air cooling draw-through cooling cabin cooling 9 / 25 On preflight inspection, the main gear leveling cylinder reset handle must be in the green band if the system is pressurized. If the handle is in the _______________ band, replenish the fluid by pulling out on the handle. If the handle is in the _______________ band, the valve is defective.NN1E-3A-1 Pg1-229 outer red, inner red inner red, outer red silver, inner red silver, outer red 10 / 25 Use landing gear LOCK OVERRIDE __________________. Gear retracts whether in correct position or not. Gear could hit doors or structure, causing damage.NN1E-3A-1 Pg1-216 only in extreme emergencies when gear lever solenoid lock is inoperative when any gear fails to retract when main landing gear fails to retract 11 / 25 When operating unpressurized and the aft forced air cooling system RAM VALVE OPEN indicator is illuminated, control the temperature of the aft system manually at ___________.NN1E-3A-1 Pg2-110 40 ± 8° F 45 ± 5° F 40 ± 8° C 35 to 70° F 12 / 25 When operating flaps electrically with utility hydraulic pressure available, set flap lever to a position ____________ desired flap setting in direction of motion to prevent damage to hydraulic drives.NN1E-3A-1 Pg1-268 corresponding to beyond at or beyond none of the above 13 / 25 When opening entry or galley doors after emergency landing or ditching, stop when door handle is in vertical position and check _____________________.NN1E-3A-1 Pg3-9 for structural damage that unidentifiable odors are not present for possible entry of fire, smoke, or water that retaining bar passes through slide harness 14 / 25 During descent, approach and landing, all flight crewmembers will monitor their respective instruments and all radio transmissions by the controlling agency, and advise the pilot when noting any deviations from the clearance/procedures (± ___ knots of airspeed, ± ____ feet in altitude, or ± ___ degrees of heading/course).E-3A M 3.2-17 Pg 23 10, 200, 10 20, 100, 20 10, 100, 10 20, 200, 20 15 / 25 The ______ can start no earlier than the time at which the crew member completes their duties from the previous flight or duty period and has departed their place of work.FC FO 3.2-1 Pg 37 crew duty day crew rest period showtime mission planning 16 / 25 If external power is on the airplane bus and the AVAIL indicator is not illuminated, the _____________ switch must be off (ON indicator out) before connecting APU or airplane generators.NN1E-3A-1 Pg1-157 BUS TIE OPEN APU GENERATOR EXTERNAL POWER EMERGENCY POWER 17 / 25 Do not retract fuel dump chutes until all fuel dump valves have indicated closed for ___ minutes to prevent fuel draining into wing (except as required to close valves).NN1E-3A-1 Pg3-56 1 2 3 4 18 / 25 Aircraft shall not exceed 0.75 Mach when aircraft gross weight is below __________ pounds and the CG is aft of ______ % MAC.NN1E-3A-1 Pg2-61 230,000, 32 230,000, 35 250,000, 35 250,000, 32 19 / 25 The climbout is divided into four segments; For One Engine Inoperative, the first climbout segment begins at liftoff at the end of ______ and ends at ______.NN1E-3A(II)-1-1 PG:A3-20 takeoff ground run; screen height TORA; DER CFL; completion of landing gear retraction the clearway; termination height 20 / 25 Do not operate auxiliary rotodome drive at 6 RPM (XMIT) for__________________.NN1E-3A-1 Pg1-195 takeoff landing go-around All of the above 21 / 25 Allow _______ seconds for bypass valves to operate between turning emergency flap switch on and operating electric drive motors.NN1E-3A-1 Pg1-269 5 6 7 8 22 / 25 Landing or takeoff will not be attempted with over ___ – inch of _____________ on the runway.NN1E-3A-1 Pg7-8 1/2, water 1, standing water or slush 1, volcanic ash 1/2, standing water or slush 23 / 25 The Takeoff Warning System receives power through the________________________________________ circuit breaker(s) on the P5 panel.NN1E-3A-1 Pg1-263 MACH WARN BELL LANDING GEAR WARN HORN MACH WARN BELL and LANDING GEAR WARN HORN NONE OF THE ABOVE 24 / 25 During engine start, if ground crew has not called “rotation”, and/or N1 RPM is not indicated by _____% N2, release start switch and investigate cause before attempting another start.NN1E-3A-1 Pg1-69 25 15 35 None of the above 25 / 25 The maximum load in the crew baggage tiedown area is _______ pounds or ______ pounds per square foot.NN1E-3A-1 Pg5-35 2598, 90 2600, 80 2598, 120 2500, 120 Your score isThe average score is 91% LinkedIn Facebook VKontakte 0% Restart quiz FE 50 Question 1 / 50 During descent, approach and landing, all flight crewmembers will monitor their respective instruments and all radio transmissions by the controlling agency, and advise the pilot when noting any deviations from the clearance/procedures (± ___ knots of airspeed, ± ____ feet in altitude, or ± ___ degrees of heading/course).E-3A M 3.2-17 Pg 23 10, 200, 10 20, 100, 20 10, 100, 10 20, 200, 20 2 / 50 If LOW RPM light fails to go out during engine start __________________, shut down the engine and have maintenance make a visual check for structural integrity and verify IDG is reconnected before attempting restart.NN1E-3A-1 Pg1-179 do not attempt to close generator breaker and generator breaker does not close immediately disconnect the IDG Continue, parallel operation is not affected as long as the sync bus is energized 3 / 50 Replacement of tires, wheels, and brakes is required when brake energy exceeds ______ million foot-pounds.NN1E-3A(II)-1-1 PG:A8-5 10 24 28 40.3 4 / 50 Do not operate antiskid TEST switch while taxiing. If brakes are in use, TEST switch ____________ one set of brakes.NN1E-3A-1 Pg1-237 applies releases locks none of the above 5 / 50 If refueling is in progress when crew members show up at the aircraft, they will not enter the refueling zone without permission from the ____________. The refueling zone can be identified by the _______________________.E-3A M 3.2-17 Pg 19 refueling supervisor, orange cones positioned around the aircraft maintenance supervisor, orange cones positioned around the aircraft refueling supervisor, refueling supervisor positioned at the nose of the aircraft maintenance supervisor, refueling supervisor positioned at the nose of the aircraft 6 / 50 When illuminating FASTEN SEAT BELT signs ___________, pilot or flight engineer will notify _______ by interphone.NN1E-3A-1 Pg1-1046 on the ground, TD in flight, SC on the ground or in-flight, TD in flight, TD 7 / 50 The angle of attack system senses inboard flap position only. The indications are not correct when flying with _______________ flaps.NN1E-3A-1 Pg1-282 "split" asymmetric "split" or asymmetric emergency 8 / 50 If external power is on the airplane bus and the AVAIL indicator is not illuminated, the _____________ switch must be off (ON indicator out) before connecting APU or airplane generators.NN1E-3A-1 Pg1-157 BUS TIE OPEN APU GENERATOR EXTERNAL POWER EMERGENCY POWER 9 / 50 Sulfur hexafluoride (SF6) gas in the mission equipment is a colorless odorless gas which is heavier than air. To prevent inhaling SF6, open _____________, move away from door and allow compartment to ventilate for _____ minute(s) before entering airplane.NN1E-3A-1 Pg2-7 forward cargo door, two aft cargo door, one aft cargo door, two forward main door, one 10 / 50 If evacuating after aborted takeoff or heavyweight landing, depart directly _________ or _________ of airplane to avoid possible tire/wheel burst area if fuse plugs melt.NN1E-3A-1 Pg3-10 forward, aft left, right aft, side to the bus, left 11 / 50 The DC load on any one-transformer rectifier (T/R) unit must never exceed ___ amperes for 1 minute; and ____ amperes continuous.NN1E-3A-1 Pg5-30 60, 170 65, 200 200, 75 170, 218 12 / 50 The nose gear _________________ must be inserted manually before landing if the utility hydraulic system is depressurized.NN1E-3A-1 Pg1-230 ground lock handle maintenance downlock drag brace lock pin emergency lock pin 13 / 50 The required AEO Climb Gradient (CG) for all departures is the greater of:FC FO 3.2-1 Pg13 200 ft/NM The CG required by ATC (unless unable and ATC is informed) The CG required for obstacle clearance All of the above 14 / 50 High pressure compressor (N2) RPM limit is _____ %.NN1E-3A-1 Pg5-7 100 101.1 101.5 104.5 15 / 50 The takeoff phase is enabled when ground speed transitions to greater than 80 knots. The takeoff phase is terminated when which one of the following occurs?NN1E-3A-1 Pg 1-1045 Radio altitude transitions for above 400 feet 20 seconds after the aircraft transitions from ground to air Ground speed transitions from greater than 80 knots to less than 75 knots in the case of a rejected takeoff Any of the above 16 / 50 Take-offs, approaches and landings are not permitted at airfields where freezing ___ is falling, or ______ is present.FC FO 3.2-1 Pg 43 drizzle; freezing fog snow; sleet hail; standing water rain; freezing fog 17 / 50 The maximum permitted crosswind component, gusts included, for take-off and landings is ______.FC FO 3.2-1 Pg 41 limited by FPS 15 knots 50 knots 25 knots 18 / 50 ______ is the total length of hard surface, not including overruns.NN1E-3A(II)-1-1 PG:A3-4 Runway length Critical field length Takeoff distance available (TODA) Takeoff ground run 19 / 50 Use landing gear LOCK OVERRIDE __________________. Gear retracts whether in correct position or not. Gear could hit doors or structure, causing damage.NN1E-3A-1 Pg1-216 only in extreme emergencies when gear lever solenoid lock is inoperative when any gear fails to retract when main landing gear fails to retract 20 / 50 If aircraft purge is in progress, as indicated by the entry door closed and the shade down, the doors will remain closed, until cleared open by___________E-3A M 3.2-17 Pg 19 Only the FE The FE or ST Only the ST None of the Above 21 / 50 An extremely thin layer of frost on the upper wing surface and snow or ice on any surface _______________.NN1E-3A-1 Pg7-15 will have no appreciable effect on aircraft performance will have no appreciable effect on aircraft performance as long as the thickness is less than 1/8 inch can degrade performance seriously will blow off during takeoff roll 22 / 50 ______ is based on critical field length and is the lowest speed at which the upwind outboard engine can fail and the takeoff continue safely.NN1E-3A(II)-1-1 PG:A3-4 Ground minimum control speed (VMCG) Refusal speed Rotation speed (VR) Decision speed (V1) 23 / 50 If the indicated frequency of the isolated generator is outside the range of 400 + 8 Hz, fluctuates more than 4 Hz within the + 8 Hz range, or OHEAT light illuminates, or generator breaker does not remain closed, .NN1E-3A-1 Pg1-125 Check IDG oil temperature indicator and LOW RPM light. If indications are normal, shut down generator and disconnect IDG open bus tie breaker for the affected generator shut down generator Disconnect IDG 24 / 50 Brake cooling procedures contained in section V of CSTO NN1E-3A-1 will be followed after any stop which yields a brake energy above ____ million foot-pounds per brake.NN1E-3A(II)-1-1 PG:A8-5 10 15 24 28 25 / 50 The ____________ is unable to release the boom toggles during manual boom latching.NN1E-3A-1 Pg8-10 boom operator receiver pilot flight engineer all of the above 26 / 50 If engine was shut down as a precautionary measure and engine and flight conditions permit, the fuel system can be cooled if windmilling N2 RPM is at least ____; open CONTINUOUS IGNITION circuit breaker to prevent engine relight and set throttle to idle for __________________ to prevent excessive temperatures in the fuel control.NN1E-3A-1 Pg3-8 25%, 3 minutes each 30 minutes 35%, 2 minutes each 20 minutes 25%, 2 minutes each 20 minutes 15%, 3 minutes each 20 minutes 27 / 50 Do not pressurize airplane if APU DOOR caution light is illuminated, as damage to ________________ can occur.NN1E-3A-1 Pg3-60 APU doors APU door limit switches APU start box APU shroud 28 / 50 Which of the following statement(s) is/are true regarding aircraft wing tip clearance procedures?FC FO 3.2-1 Pg 11 Do not taxi aircraft within 25 feet (8 meters) laterally of obstructions without wing walkers With wing walkers, do not taxi any aircraft closer than 10 feet (3 meters) laterally to any obstacles Aircraft will be towed, with engines shutdown, when closer than 10 feet (3 meters) to any obstacle that could potentially damage the aircraft. All of the above 29 / 50 Flight suit sleeves are to be rolled down __________ with __________.FC FO 3.2-1 Pg 61 while on the aircraft, engines running while on the aircraft, the doors closed in-flight, simulated emergency procedures during pre-flight, engines running 30 / 50 Pilots are not to fly over the tops of thunderstorms or downwind under the anvil. Thunderstorms are to be avoided by ______ at or above _______, and _______ below _______.FC FO 3.2-1 Pg 43 20 NM, FL230; 10 NM, FL230 10 NM, FL230; 5 NM, FL230 15 NM, FL150; 5 NM, FL150 10 NM, FL150; 10 NM, FL150 31 / 50 Mission radar will remain in standby/dummy load until rotodome purge time is complete (______ minutes after closing slipway doors).NN1E-3A-1 Pg8-8 Two Five Seven Ten 32 / 50 Failure to hold engine start selector in GND START until _____ N2 RPM is reached can result in a “_____________”.NN1E-3A-1 Pg1-69 25%, Slow Start 35%, Wet or Hot Start 54%, Hung Start 25%, Wet Start 33 / 50 The ______ can start no earlier than the time at which the crew member completes their duties from the previous flight or duty period and has departed their place of work.FC FO 3.2-1 Pg 37 crew duty day crew rest period showtime mission planning 34 / 50 During engine start, if ground crew has not called “rotation”, and/or N1 RPM is not indicated by _____% N2, release start switch and investigate cause before attempting another start.NN1E-3A-1 Pg1-69 25 15 35 None of the above 35 / 50 For the first _____minutes after LAIRCM system power-up, the aircraft must remain stationary or a Signal Processor failure may occur.NN1E-3A-1 Pg2-46 Two One Three Four 36 / 50 The normal operating range of the APU generator, as indicated by airplane instruments is _______ Hz. Under steady load, frequency may vary a maximum of ____ Hz about a mean value within the ______ Hz band.NN1E-3A-1 Pg5-30 400 ± 8, ± 4, 400 ± 8 400 ± 8, ± 2, 400 ± 8 400 ± 10, ± 2, 400 ± 10 400 ± 10, ± 4, 400 ± 10 37 / 50 _______ is the total length of runway required to accelerate on four engines to V1, experience an engine failure and then continue the takeoff or stop.NN1E-3A(II)-1-1 PG:A3-4 Critical field length Takeoff ground run Takeoff distance Takeoff run available 38 / 50 When operating flaps electrically with utility hydraulic pressure available, set flap lever to a position ____________ desired flap setting in direction of motion to prevent damage to hydraulic drives.NN1E-3A-1 Pg1-268 corresponding to beyond at or beyond none of the above 39 / 50 Operating procedures, techniques, etc., which can result in damage to equipment if not carefully followed is a ____________________.NN1E-3A-1 Pg xix Note Caution Warning Local Operating Procedure 40 / 50 Allow _______ seconds for bypass valves to operate between turning emergency flap switch on and operating electric drive motors.NN1E-3A-1 Pg1-269 5 6 7 8 41 / 50 Do not use FLT START position for more than ____________. Do not use GND START position in flight.NN1E-3A-1 Pg3-58 one and a half minutes 5 minutes 10 minutes 30 minutes 42 / 50 If possible, launch life rafts over ____________ of wing to avoid damage from flaps. Do not allow raft to contact ________________.NN1E-3A-1 Pg1-1036 leading edge, overwing fuel filler ports side, static dischargers leading edge, vortex generators trailing edge, static dischargers 43 / 50 To prevent PFD reversion, close __________ circuit breakers prior to closing MFD circuit breakers. If PFDs are displayed on MFDs No.2 or No. 3, cycle applicable circuit breaker to reassign MFD as an IMFD (P61-4).NN1E-3A-1 Pg2-10 MFD NO. 2 & NO. 3 MFD NO. 2 & NO. 4 MFD NO. 1 & NO. 3 MFD NO. 1 & NO. 4 44 / 50 If APU shuts down during power transfer, or from no apparent cause, have condition of APU _______________ checked before next start attempt.NN1E-3A-1 Pg2-12 start accumulators, battery bus generator, emergency lighting battery accessory drive shaft surge accumulator, hot battery bus 45 / 50 Oxygen is required for personnel entering the aft lower lobe when pressurization is in ______________ operation.NN1E-3A-1 Pg1-10 automatic manual the takeoff mode of the landing mode of 46 / 50 The radiation hazard to fuel handling operations does not extend beyond ___ feet from the radiating antenna. There are no personnel restrictions and it is not necessary to establish a restricted access zone in front of the antenna.NN1E-3A-1 Pg5-34 3.2 feet 32 feet 320 feet 322 feet 47 / 50 Which statement is true concerning the Electrical Smoke Source Isolation procedure?NN1E-3A-1 Pg3-33 It will not be attempted on a bus which has been identified as the source of an electrical fire. It will not be attempted on a bus which has been identified as the source of fire, smoke or fumes. It will only be attempted at the direction of the pilot or flight engineer None of the above 48 / 50 On preflight inspection, the main gear leveling cylinder reset handle must be in the green band if the system is pressurized. If the handle is in the _______________ band, replenish the fluid by pulling out on the handle. If the handle is in the _______________ band, the valve is defective.NN1E-3A-1 Pg1-229 outer red, inner red inner red, outer red silver, inner red silver, outer red 49 / 50 The Takeoff Warning System receives power through the________________________________________ circuit breaker(s) on the P5 panel.NN1E-3A-1 Pg1-263 MACH WARN BELL LANDING GEAR WARN HORN MACH WARN BELL and LANDING GEAR WARN HORN NONE OF THE ABOVE 50 / 50 For effective anti-ice protection, maintain a minimum of ___________ on each engine if anti-ice is on.NN1E-3A-1 Pg2-62 70% N1 2000 pph fuel flow 70% N2 55% N1 Your score isThe average score is 96% 0% Restart quiz
