T-1A MQF 2017 - Top 40 Most Missed Questions Flashcards
The weather requirements for USAF aircraft flying VFR in FAA Class B airspace are
3 sm; clear of clouds
Simulated single-engine and no-flap approaches and patterns, as well as circling approaches may be flown at night if the ceiling and visibility is at least ___ feet and ___ statute miles or circling minimums, whichever is greater
2000; 3
When doing the stall warning test on the left or right side, the stick shaker should activate:
Twice, when the AOA pointer passes .4 to .5 and .7
When the anti-skid fail caution annunciator is illuminated, anti-skid is not available and braking will be in the power mode.
TRUE
During stall recoveries, placing the control column forward of neutral may
result in accelerations below 0G, exceeding the aircraft acceleration limit with flaps extended
During a starter assisted airstart, a relight should normally be obtained within ___ seconds after the throttle is moved to idle
10
When does the wingman maneuver to the stack level position for a formation tactical overhead pattern entry?
Initial
Alternate Air Refueling rendezvous procedures in order of precedence are primary ___, secondary ___, tertiary ___.
Use the computed backup timing; receiver calls miles from the ARCP (off FMS) every 2 NM; receiver calls DME off of the NAVAID defining the ARIP/ARCP line every 2 NM (if applicable).
After pushing the battery feed test button and the battery switch is placed to EMER,check for operation of___
RTU #1
Retractable gear aircraft will report gear down status to ATC or runway supervisory unit after extending the landing gear. This report shall be made during any approach prior to crossing the ___
runway threshold
After checking flight controls during cold weather operations, the speed brakes may not fully retract due to lack of airflow across the wing surfaces.
TRUE
As a technique, if the receiver is less than ____ of the computed turn range (half-way through the turn) or the bearing pointer is below the ___ degree index, an overrun can be expected.
1/3; 45
On a Sectional or TAC, Terminal Radar Service Areas (TRSA) are depicted by ____ indicating the various sectors within the area, with ceiling and floor altitudes of each sector shown in ___ indicating hundreds of feet
screened black lines, solid black numbers
If the aircraft is decelerated and engages the barrier perpendicular to the middle half, no damage to the aircraft should be expected.
FALSE
For unusual attitude recoveries, initiate recoveries above ___ KIAS, below ___ KIAS, and above ___ feet AGL.
130, 270, 5,000
During critical phases of flight, direct reference to the checklist is not required.
FALSE (per AFMAN 11-247)
The stabilizer anti-ice fail annunciator will illuminate in ___ seconds once the anti-ice switch is set to the test position.
3
Apply ___% of the tailwind component to CFL Vcef, Vr, Vb, and takeoff ground run and zero wind climbout factor.
150%
On a Sectional or TAC, Class C airspace is depicted by ___ indicating radials and arcs of the sectors, with MSL ceiling and floor altitudes of each sector shown in ___ indicating hundreds of feet.
Solid magenta lines; solid magenta lines
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
During crossfeed 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 line pressure drops below 5 psi.
FALSE
When cleared for a descent at the pilot’s discretion, you may temporarily level off at any intermediary altitude; however, once that altitude is vacated, you may not return to that altitude.
TRUE
When the battery feed test button is pushed with the battery switch ON, check for:
(A + B)
A. FDR FAIL annunciator illuminated
B. STBY PWR ON annunciator illuminated
Pulling and resetting the UHF CB after dual RTU failure does what?
(A + B)
A. Turns off the squelch
B. Returns to the frequency tuned at the time of the failure
(LAFBI 13-204 question)
When cancelling IFR, remain on the assigned frequency and squaw code until service is terminated by the RAPCON. When directed, change to RSU/Tower’s frequency and squawk:
222
VFR-on-top is
an ATC authorization for an aircraft on an IFR clearance to operate at VFR altitudes of their choice in VMC.
If the parking brake is set from the copilot’s side:
(A + C)
A. the binding could affect action from the pilot’s side at a later time
C. temporar binding in the mixing valve could occur
During crossfeed 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
Wing CC approval is the lowest approval authority required to perform practice instrument approaches under VFR.
FALSE
If the Manual Deice (Backup) switch for the horizontal stabilizer anti-ice system is held in the MANUAL position longer than momentarily, power to the gap heater elements will be maintained for more than ___ and overheating could result.
30 seconds
When reading a METAR, AUTO referes to an observation taken from
an unattended Automated Surface Observation System (ASOS)
Accumulations of 1/2 inch of ice can add ___ pounds or more to the aircraft gross weight.
500 pounds
The thermal fused screws are designed to soften and blow out, releasing air pressure in the tires when the temperature reaches approximately ____.
430 degrees Fahrenheit
Severe windshear is that which produces airspeed changes greater than ___ knots or vertical speed changes greater than ___ feet per minute.
15; 500
Left or right fuel level low annunciator illumination indicates that approximately ___ pounds of usable fuel remain in the affected wing tank.
200 pounds
While trying to eliminate smoke or fumes from inside the aircraft, turning the manual pressure controller fully counterclockwise will decrease the cabin pressure to the absolute pressure regulator setting of ___ feet.
12,500 +/- 1,500
The autopilot is not capable of controlling the aircraft in the event of an engine failure.
FALSE
On V-MDA type approaches, the FMS does not recognize step-down fixes between the FAF and the MAP and will not try to 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
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.
Which of the following is true concerning the stall characteristics of the T-1A?
The stick shaker activates at approximately 0.75 units on the AOA indicator below 20,000 feet and as los at 0.45 at high altitudes.
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