Oil/Pneumatic/Misc

Question 1

What is the oil system capacity?

Answer 1

4 qts
1 qt expansion space

Question 2

What is the max consumption of oil?

Answer 2

6 ounces/hr

Question 3

What are the oil system limits?

Answer 3

10 sec of 0 G flight
30 sec of Neg G flight
5 Min in MIL power with oil pressure >55 psi
Cold weather - oil may exceed limits

Question 4

What powers all the pneumatic system controls?

Answer 4

AC power except for Defog

Question 5

Where does the air come from for the pneumatic system?

Answer 5

8th stage bleed air

Question 6

What is the cabin pressure schedule?

Answer 6

ambient up to 8K
8k to 23K: 8k +/- 1k
above 23k: half altitude - 3k +/- 2k

Question 7

How do you get rid of duct howl?

Answer 7

By matching air inlet valves in FCP/RCP

Question 8

When does anti-ice work?

Answer 8

Above 80% is recommended

Question 9

What is the thrust reduction using anti-ice?

Answer 9

8.5% in MIL
5.5% in MAX

Question 10

Is an EGT rise normal when using anti-ice?

Answer 10

Yes, using 94-98% a rise of 15C is normal

Question 11

At what percent RPM is the anti-ice valve open?

Answer 11

65%

Question 12

What is the pressure of the emergency oxygen bottle? and how long will it last?

Answer 12

1800-2500 PSI
lasts for 10 min

Question 13

What is the limit associated with adjusting your seat?

Answer 13

no more than 1 min adjustment in the span of 8 min

Question 14

When should you use the MOR handle?

Answer 14

if you want seat separation above 14K’

Question 15

What is the field of view of the HUD?

Answer 15

24 Deg

Question 16

When can you load an ICAO?

Answer 16

when degraded appears

Question 17

How long does the EGI require before shutdown?

Answer 17

10 Sec

Question 18

How long do landing and taxi lights take to retract?

Answer 18

10 sec

Question 19

What makes it difficult for directional control when its wet on the runway?

Answer 19

Rubber deposits on the opposite approach end when its wet and slow speed

Question 20

What is the thunderstorm penetration speed?

Answer 20

280 KCAS

Question 21

When does engine damage occur with ice?

Answer 21

more than 1/4 inch on inlet ducts

Question 22

What are the ejection altitudes?

Answer 22

2000 controlled
6000 uncontrolled

Question 23

What are the wake turb limits?

Answer 23

2 min behind large or copter
4 min behind heavy
times are reduced with >5kts crosswind

Question 24

What is the max landing VVI?

Answer 24

full fuel - 340 FPM
less than 1700 - 590 FPM

Question 25

What are the G tone limits?

Answer 25

medium tone - 1.0-.5 remaining high tone - .5-.2 remaining max tone - .2-0.0 remaining Over G - exceeded limits Negative warnings are half of positive warning

Question 26

Which instruments only receive static pressure?

Answer 26

stby altimeter and VVI

Question 27

What happens when the pitot heat is on longer than 30sec on the ground?

Answer 27

YSAS may disengage and stay off unless 25kts of cooling flow or the pitot heat is turned off ADC PFL and AOA lights may illuminate TAS not available

Question 28

What powers AOA Lights?

Answer 28

Left DC

Question 29

When is the low AOA indexer inop?

Answer 29

with gear and flaps up

Question 30

What do you get if either indexer fails?

Answer 30

ADC FAIL PFL

Question 31

What are the common AOAs?

Answer 31

Max Range - 0.18 Max Endurance - 0.3 Performance - 0.6 Stall - 1.0

Question 32

What is the max relative wind of the canopy?

Answer 32

50 kts don't open when relative wind is >30kts

Question 33

What are the bird strike limits of the canopy?

Answer 33

4lb bird at 125-400 kts

Question 34

What is L/D MAX and safe single engine speed?

Answer 34

230+gas Max endurance Best glide and best angle of climb

Question 35

What is the lock point?

Answer 35

min continuous level flight speed configured with 60 flaps is 160 kts

Question 36

What is the max airspeed?

Answer 36

710 kts

Question 37

What are the WSSP limits?

Answer 37

Turb/SB - 350 KCAS Max - 400 KCAS avoid abrupt maneuvers > 240 KCAS 140lb load 0-4.0 sym G 0-3.0 Asym G

Question 38

When does a reduction of directional stability occur?

Answer 38

above FL300 and .92 Mach