T-1A MQF June 2013 Flashcards
An Operating procedure or technique which is considered essential to emphasize is a ____?
Note
If either electronic fuel control fails, the synchronization system is still operative.
False
Once TCAS announces “clear of conflict”, the pilot should
return to his/her ATC clearance or as directed by ATC
Failure to properly set the decision height (DH) in the radio altimeter could result in
nuisance warnings from the GPWS
If the ARC format is selected on the DSP, the EHSI will present an expanded 70 degree (approximate) compass segment
True
The weather radar system detects ________ along the flight path ahead of the aircraft. The radar antenna sweeps _____ to paint a full screen radar picture of the precipitation pattern along the flight path
wet precipitation, +/- 60 degrees
Due to weather radar system limitations, _____
do not rely on the system as the only means to avoid adverse weather
If the left engine fails while the synchronization system is on, there will be a maximum of 1.5% rpm spool down of the right engine. For this reason, the engine synchronization system should be off during takeoff and landing.
True
Avoid finger lift actuation to preclude inadvertent engine shutdown when retarding the throttle toward IDLE
true
The weather radar system provides radar data for up to _______ NM
300
If the antenna on the WX radar is tilted down too far and GCS mode is selected, a GCS wedge may occur. The wedge is displayed as a black area located within ____ of aircraft heading
+/- 10 degrees
Binding throttles may indicate an impending throttle linkage cable break with subsequent loss of throttle authority. Throttle linkage cable failure usually results in an uncommanded ending shutdown, however, it is possible for the engine to remain at the power setting at the time of failure or retard to to idle. If the throttle linkage cable breaks and the engine flames out, or if necessary to control the aircraft due to an engine stuck at high power settings, shut down the engine using the Fuel/Hydraulic valve close switch, then accomplish the engine shutdown during flight checklist in section III
True
As oxygen cylinders become chill, the pressure is reduced. A temperature drop of 100 degrees F will reduce the pressure 20%. If the pressure begins to drop while the aircraft is in level flight or descending, ______
suspect an oxygen leak
In the event of a hung start, advance the throttle beyond IDLE. Increased Fuel Flow could result in engine cooling.
False
After flushing the lavatory, _____ to prevent contents from overflowing
leave the knife valve open at least a 1/4 inch
Resetting a popped circuit breaker in the fuel system is allowable.
False
During cross-side operations, pilots should cross-check ______ with other reliable instruments
All of the above (Position, attitude and altitude)
Asterisk (*) items in the checklist
need not be accomplished on subsequent flights by the same crew flying the same aircraft on the same day
While using the exterior inspection checklist, specific attentions hold be given to detect fluid leakage
true
The exterior door handle will stow by activation of the interior handle
False
Failure to stow the exterior door handle can result in damage to the door in flight
True
During the walk around, support the main landing gear door if releasing by the manual system
True
During the exterior inspection, how many circuit breaker panels are in the aft compartment that are required to be checked?
3
When the nose wheel mechanical disconnect pin is disconnected, nose wheel steering is still available.
False
With respect to the door locking pins, ______ or the door may open in flight
all eight must be white
If pilot valves are inoperative, single point pressure refueling should not be attempted and the aircraft should not be flown.
True
An improperly installed escape hatch can result in loss of cabin pressure in flight
True
Failure to remove the escape hatch lock pin will
All of the above (Make hatch inoperable from the outside, inside and delay emergency ground egress form the escape hatch)
Repeated tests of the AHRS battery are acceptable and will validate AHRS battery performance.
False
After pushing the battery feed test button and the battery switch is placed to “EMER”, check for operation of ___________
RTU #1
When the cabin pressure controller is set, set the altitude to _______ feet above the highest anticipated cruise altitude or according to mission requirements
1,000
Turning the manual pressure control knob past its normal range __________
could damage the threads or needle valve seat
When the battery fee test button is pushed with the battery switch ON, check for
A & B (FDR FAIL annunciator illuminated, STBY PWR ON annunciator illuminated)
Landing with brakes applied could result in
All of the above (Blown tires, potential runway departure, damage to the aircraft)
The H STAB DEICE TEST position will
B & C (Check de-ice timer in the fast advance mode through the 12 segment positions, allies power to the heater elements for 0.6 seconds in sequence with a pause after each six)
When checking the stall warning system ______
A & B (the master test switch must remain in the L or R STALL until stick shaker actuates twice, check hat the indexer on the glare shield follows AOA gauge indication)
When testing the indicator lights, the flowing lights do not illuminate
All of the Above (red landing gear unlocked indicator, starter DISENGAGE button, and ENG START buttons)
When doing the stall warning test on the left or right side, the stick shaker should activate
twice when the AOA pointer passes 0.4 to 0.5 and 0.7
After selecting the left tank during the fuel cross feed check, these lights will illuminate
Left boost pump light, right jet pump light, XFEED in-transit operation light
When running the pitch or roll trim switch for ______ seconds continuously, the trim arming horn will activate.
5
During flight control checks, after the pilot checks the controls, the copilot must also physicaly check the flight controls.
True
If starting engines with battery power only, do not start the seconds engine until the first engine’s load meter reads below ______ amps
150
For generator assisted starts on the second engine, the operating engine must be at idle
True
The stabilizer anti-ice fail annunciator will illuminate in _____ seconds once the anti-ice switch is set to the test position
3
While accomplishing the horizontal stabilizer de-ice test, if one of the 12 elements is open, the operation lights will remain off for 1-2 seconds during the test
True
Do not use the horizontal stabilizer anti-ice on the ground because a squat switch failure could cause damage to the ________
horizontal stabilizer
If not monitored properly, the VNAV function of the FMS may result in terrain impact
True
Do not operate entine anti-ice during ground operations (except for preflight test) at temperatures above ______ degrees Celsius OAT/SAT
10
An external power cart is required for engines tart at ambient temperatures below
5 degrees F
The throttles should be set at ____ to ensure that the anti-ice vale is open when checking wing and engine anti-ice
70 % N2
When taxiing for takeoff through ice and snow, leave the flaps ______ until approaching the runway to avoid accumulations of i.e. being cast off from the tires
retracted
An operating procedure or technique which could result in damage to equipment if not carefully followed is
Caution
During a wake turbulence takeoff, allow a minimum of ____ minutes behind a large type aircraft. With and effective crosswind over _____ knots, this interval may be reduced
2, 5
For a wake turbulence takeoff
a crosswind over 5 knots may reduce the required interval
After the gear is retracted on a a normal takeoff, with two engines operating, adjust the pitch to climb at a minimum of _____ until reaching _______ feet above field elevation
Vco + 10, 400
Flaps are retracted after takeoff passing _____ feet above field elevation and a minimum airspeed of _____
400, Vco + 10
During takeoff and landing, to avoid obscuring visibility, the visors must be in the stowed position
True
For extended high altitude cruise, the windshield heat should be set at
LOW
Ignition switches should be on
B and C (when flight is through turbulence and/or visible precipitation, for all takeoffs, approaches and landings)
During the cruise check a temperature drop of ______F will reduce the oxygen pressure by _____%
100, 20
Starting a descent at FL 200, maximum range descent is flown at ______, enroute descent is flown at ______ and rapid descent is flown at _______
230, 250, 330
Maximum range descent is _________.
Idle, clean, 0.70 IMN above 35,900 feet, 230 KIAS below 35,900 feet
During preflight inspection, a drop of fuel hanging on the sniffle valve _____
is acceptable
Steep idle power approaches, or approaches requiring late changes in pitch attitude during the landing flare are acceptable in the T-1A due to the stressed landing gear
False
Use of stabilizer trim for round out int he flare could induce strong pitch up tendency that would be difficult to control in the event that a go-around is attempted
True
In the event of a suspected hard landing:
A & B (Make an AFTO Form 781 write up with your gross weight, airspeed and RA/VSI, gear should remain down and the mission terminated
Touchdown will normally be made at approximately Vapp minus ________ KIAS
6
The wipers are functional at flight speeds up to __________ knots indicated airspeed. higher speeds can cause damage to the wiper motor and possible blade separation.
200
The takeoff trim setting mark is small and can be hard to see under many conditions. Avoid fixating on this gage while resetting trim to maintain aircraft control.
True
Failure to properly reset the trim can result in
All of the Above (Lower than normal yoke forces, over rotation and higher than normal yoke forces)
Crossfeed will supply fuel to a single engine from both wing tanks simultaneously
False
After landing on a snow or slush covered runway
do not retract flaps beyond 10 degrees
If the parking brake is set from the copilots side
A & C (binding could affect normal braking action from the pilot’s side at a later time., temporary binding in the mixing valve could occur)
During cross feed operation, the boost pump in the non-selected fuel feed chamber will not activate if the boost pump switch is in AUTO and the fuel feed line pressure drops below 5 psi
False
If any system emergency affecting safety of flight is experienced prior to S1 speed, the takeoff should be aborted.
True
If an emergency is experienced at or after S1 speed,
The takeoff should be continued
If the aircraft is decelerated and engages the barrier perpendicular to the middle half, no damage to the aircraft should be expected
False
Which statements(s) are true?
A & B (Taxi over cables lying on the runway is acceptable at slow speeds (less than 5 knots), Landing should be accomplished beyond arresting cables)
If engine shutdown or failure occurs in flight, consider the use of cross feed to balance the fuel load, unless fuel system contamination is suspected
True
The base of the emergency escape hatch is 4.5 feet above the ground with the landing gear extended. Use caution when using this exit
True
With dual Remote Tuning Unit (RTU) failure, how can VHF guard (121.5) be tuned?
Pulling and resetting the VHF circuit breaker
If UHF guard mode was on when the dual RTU failure occurred, guard reception is still available
True
Using the engine fire switch lights to close the fuel valve also closes the hydraulic valve
True
Pulling and resetting the UHF circuit breaker after dual RTU failure does what?
A & B (turns off the squelch, returns to the frequency tuned at the time of failure
NAV auto tuning is disabled when the RMT TUNE switch is in the DSABL position
True
In the event of a fuel quantity indicator failure, which of the following are true?
Both gauges’ dial pointers move off scale to below the zero mark to indicate an inoperative condition
Securing an engine after a failure/fire on takeoff should not be accomplished prior to ______
A & C (400 ft AGL (1500 optional), clear of obstructions)
If an engine fire occurs immediately after takeoff when using the ACM OFF procedure, the bleed air selector may be turned to NORM at any time
False
Do not attempt to restart an engine that has been shut down due to obvious mechanical difficulties
True
If a spin is entered:
simultaneously reduce power to idle, apply full rudder opposite spin direction, forward elevator control and neutral roll control
During a starter assisted airstart, a relight should normal be obtained within _____ seconds after the throttle is moved to idle
10
During a windmilling airstart, should the temperature rise indicate a hot start, place the throttle to CUTOF and windmill the engine for __________ seconds before attempting another start
30
The FMS does not recognize step-down fixes between the FAF and the MAP and will not try o comply with them. If a given approach has any step-down fixes between the FAF and arrival at MDA, VNAV should not be used for this portion of the approach
True
During the flight control check of the rudder, ensure that both the PF and the PM independently observe a proportional displacement of their left and right rudder pedals and a proportional rudder control surface movement
True
The switch light in the fire protection group on the shroud panel is used to close the _________ on the respective engine
A & B (main fuel line shutoff valve, hydraulic valve)
The autopilot is not capable of controlling the aircraft in the event of an engine failure.
False
Rudder boost is provided bye the rudder servo of the autopilot.
True
In the event of electrical system failure, excluding the aircraft artery, placing the battery switch to EMER causes the battery to power the
All of the above (emergency bus, standby battery, standby bus)
If smoke or fumes are emanating from the air-conditioning vents, select L ENG or R ENG in an attempt to isolate the source. Bleed air source selector must remain in each position approximately ______ seconds to allow adequate purging.
20
With oil pressure below ______, execute engine shutdown
40 psi
If high oil temperature is experienced, _______
increase affected engine throttle within N1 limits
While truing to eliminate smoke or fumes from the inside of the aircraft, turning the manual pressure controller fully counterclockwise will decrease the cabin pressure to the absolute pressure regulator setting of
12,500 +/- 1,500
Under high temperature, low altitude, high throttle setting conditions, entire oil temperature may exceed _______ when the throttles are reduced due to a reduction in cooling field through the fuel/oil heat exchanger. The maximum transient limit is _____ and _____ should not be exceeded for more than ____ minutes
121 degrees C, 135 degrees C, 121 degrees C, 15
If you have an EFC failure
matching the throttles using the engine with the EFC off may cause over boosting of the other engine
If the fuel filter bypass annunciator is illuminated, the bypass filters is purifying the fuel to the engine
False
Left or right fuel level low annunciator illumination indicates that approximately ____ pounds of fuel remains in the respective tank
200
If acceptable takeoff performance can only be achieved by selecting 0 degrees flaps and/or ACM off, takeoff in the presence of potential windshear is not recommended. Windshear conditions will quickly negate these minor performance enhancements.
True
If automatic starter dropout has not occurred by ______ % N2, press the starter disengage button.
45
Autopilot engagement is not possible with the pitch trim selector in the EMER position
True
An operating procedure or technique which could result in personal injury or loss of life is not carefully followed is a _____
Warning
What provides ground fault protection for external power?
Battery protection circuits
Air entering the cabin or pressurization during air conditioning emergency operation will not still be hot until the bleed air selector has been turned off.
True
In the event of a bleed air duct failure, if the wing anti-ice switch is turned OFF and the annunciator extinguishes, flight may be continued if icing conditions are avoided.
True
If the AIR COND FAIL annunciator illuminates, the system will switch from normal to emergency pressure mode automatically
True
