Malfunctions and Emergencies Ops Limits

Question 1

An engine being motored by the APU should reach _____ core RPM; below may indicate impending APU failure or insufficient engine-starting air.

Answer 1

24%-28%

Question 2

Minimum aerodynamic single-engine ground control speed is _____.

Answer 2

70 KIAS

Question 3

With left engine failure on takeoff, residual hydraulic pressure should retract landing gear if handle is raised within _____.

Answer 3

5 seconds

Question 4

The emergency jettison button will release all stores within _____.

Answer 4

1 second

Question 5

If an engine fails after takeoff, increase minimum climb speed _____ above best SERC with gear up, and another _____ after flaps retract.

Answer 5

10 KIAS; 10 KIAS

Question 6

If an engine fails after takeoff, delay flap retraction until _____.

Answer 6

150 KIAS

Question 7

With a loss of one hydraulic system, rudder pedal pressure will increase and SAS authority for yaw trim and turn coordination is reduced by _____.

Answer 7

50%

Question 8

After a total engine oil system failure, that engine will seize in _____.

Answer 8

1-3 minutes

Question 9

Rudder inputs needed to maintain coordinated flight are noticeably higher after failure of the _____ engine and may require up to _____.

Answer 9

Right; 100 pounds

Question 10

If one hydraulic system fails, engage only the operable _____ SAS.

Answer 10

Yaw

Question 11

If one hydraulic system fails, ensure both _____ SAS switches are off.

Answer 11

Pitch

Question 12

If an aileron or elevator is jammed, the appropriate jam light will illuminate for _____ after a force of _____ is applied to the control stick.

Answer 12

3-5 seconds; 50-65 pounds

Question 13

An engine oil pump driveshaft failure is indicated by simultaneous loss of oil pressure and engine _____.

Answer 13

Core speed (RPM)

Question 14

After a double-engine failure, the time required to restart the left engine may result in altitude loss of _____ prior to attaining usable power.

Answer 14

3700’

Question 15

Best glide speed in the A-10C is _____ plus 2 times each 1,000 pounds above basic aircraft weight (i.e. no-flap approach airspeed).

Answer 15

140 KIAS

Question 16

An erect spin is confirmed with the turn needle fully deflected, airspeed at or below _____ and AOA consistently above _____ units.

Answer 16

120 KIAS; 25

Question 17

Post-stall gyrations may require less than _____ to as much as _____ of altitude for recovery.

Answer 17

1000’; 8000’

Question 18

Spin recoveries require _____ to _____ of altitude for incipient half-turn spins, and _____ of altitude for 3-turn developed spins.

Answer 18

4000’; 6000’; 10,000’

Question 19

Do not delay controlled ejection below _____ AGL; during uncontrolled flight conditions, minimum ejection altitude is _____ AGL.

Answer 19

2000’; 4000’

Question 20

If a go around is required from a single-engine approach, best climb speed is _____ below approach speed; add _____ after gear is retracted.

Answer 20

10 KIAS; 10 KIAS

Question 21

Engine post-shutdown overtemp or fire is indicated by engine ITT above _____ as the core RPM drops below _____.

Answer 21

540°C; 5%

Question 22

If OBOGS stops producing oxygen-enriched air (e.g. loss of bleed air) and with the regulator in 100%, OBOGS will provide _____ of reserve.

Answer 22

2-3 minutes

Question 23

The REOS bottle on the ejection seat provides approximately _____ of regulated oxygen after activation.

Answer 23

12-15 minutes