T-1A MQF 2017 - Top 40 Most Missed Questions

Question 1

The weather requirements for USAF aircraft flying VFR in FAA Class B airspace are

Answer 1

3 sm; clear of clouds

Question 2

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

Answer 2

2000; 3

Question 3

When doing the stall warning test on the left or right side, the stick shaker should activate:

Answer 3

Twice, when the AOA pointer passes .4 to .5 and .7

Question 4

When the anti-skid fail caution annunciator is illuminated, anti-skid is not available and braking will be in the power mode.

Answer 4

TRUE

Question 5

During stall recoveries, placing the control column forward of neutral may

Answer 5

result in accelerations below 0G, exceeding the aircraft acceleration limit with flaps extended

Question 6

During a starter assisted airstart, a relight should normally be obtained within ___ seconds after the throttle is moved to idle

Answer 6

10

Question 7

When does the wingman maneuver to the stack level position for a formation tactical overhead pattern entry?

Answer 7

Initial

Question 8

Alternate Air Refueling rendezvous procedures in order of precedence are primary ___, secondary ___, tertiary ___.

Answer 8

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).

Question 9

After pushing the battery feed test button and the battery switch is placed to EMER,check for operation of___

Answer 9

RTU #1

Question 10

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 ___

Answer 10

runway threshold

Question 11

After checking flight controls during cold weather operations, the speed brakes may not fully retract due to lack of airflow across the wing surfaces.

Answer 11

TRUE

Question 12

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.

Answer 12

1/3; 45

Question 13

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

Answer 13

screened black lines, solid black numbers

Question 14

If the aircraft is decelerated and engages the barrier perpendicular to the middle half, no damage to the aircraft should be expected.

Answer 14

FALSE

Question 15

For unusual attitude recoveries, initiate recoveries above ___ KIAS, below ___ KIAS, and above ___ feet AGL.

Answer 15

130, 270, 5,000

Question 16

During critical phases of flight, direct reference to the checklist is not required.

Answer 16

FALSE (per AFMAN 11-247)

Question 17

The stabilizer anti-ice fail annunciator will illuminate in ___ seconds once the anti-ice switch is set to the test position.

Answer 17

3

Question 18

Apply ___% of the tailwind component to CFL Vcef, Vr, Vb, and takeoff ground run and zero wind climbout factor.

Answer 18

150%

Question 19

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.

Answer 19

Solid magenta lines; solid magenta lines

Question 20

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.

Answer 20

wet precipitation, +/-60 degrees

Question 21

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.

Answer 21

FALSE

Question 22

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.

Answer 22

TRUE

Question 23

When the battery feed test button is pushed with the battery switch ON, check for:

Answer 23

(A + B)
A. FDR FAIL annunciator illuminated
B. STBY PWR ON annunciator illuminated

Question 24

Pulling and resetting the UHF CB after dual RTU failure does what?

Answer 24

(A + B)
A. Turns off the squelch
B. Returns to the frequency tuned at the time of the failure

Question 25

(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:

Answer 25

222

Question 26

VFR-on-top is

Answer 26

an ATC authorization for an aircraft on an IFR clearance to operate at VFR altitudes of their choice in VMC.

Question 27

If the parking brake is set from the copilot’s side:

Answer 27

(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

Question 28

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.

Answer 28

FALSE

Question 29

Wing CC approval is the lowest approval authority required to perform practice instrument approaches under VFR.

Answer 29

FALSE

Question 30

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.

Answer 30

30 seconds

Question 31

When reading a METAR, AUTO referes to an observation taken from

Answer 31

an unattended Automated Surface Observation System (ASOS)

Question 32

Accumulations of 1/2 inch of ice can add ___ pounds or more to the aircraft gross weight.

Answer 32

500 pounds

Question 33

The thermal fused screws are designed to soften and blow out, releasing air pressure in the tires when the temperature reaches approximately ____.

Answer 33

430 degrees Fahrenheit

Question 34

Severe windshear is that which produces airspeed changes greater than ___ knots or vertical speed changes greater than ___ feet per minute.

Answer 34

15; 500

Question 35

Left or right fuel level low annunciator illumination indicates that approximately ___ pounds of usable fuel remain in the affected wing tank.

Answer 35

200 pounds

Question 36

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.

Answer 36

12,500 +/- 1,500

Question 37

The autopilot is not capable of controlling the aircraft in the event of an engine failure.

Answer 37

FALSE

Question 38

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.

Answer 38

TRUE

Question 39

In the event of a fuel quantity indicator failure, which of the following are true?

Answer 39

Both gauges’ dial pointers move off scale to below the zero mark to indicate an inoperative condition.

Question 40

Which of the following is true concerning the stall characteristics of the T-1A?

Answer 40

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.

Question 41

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Answer 41

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