Limits

Question 1

max differential 1&4

Answer 1

on deck 1400, in flight 4389

Question 2

max differential 2&3

Answer 2

on deck 5025

Question 3

hydraulic pressure

Answer 3

2960 to 3200 psi

Question 4

emergency air brake reservoir

Answer 4

1800 to 3000 psi

Question 5

brake accumulator charge

Answer 5

800 psi of nitrogen

Question 6

min hydraulic quantity

Answer 6

sys 1-4.2gal sys 2-0.75gal

Question 7

battery

Answer 7

min voltage 22 volts

Question 8

safety pressure relief valve

Answer 8

13.9-14.5 in Hg

Question 9

max cabin differential

Answer 9

13.0-13.9 in Hg

Question 10

wing leading edge temp

Answer 10

110 degrees C

Question 11

oxygen

Answer 11

max-2000psi min for flight 1500

Question 12

SHP limits

Answer 12

warmup-min SHP until oil temp above 0 degrees C
oil temp 0-40 degrees C 1000 sHP max
aircraft limit- 4600 SHP
engine limit-5300 SHP for 3 seconds

Question 13

TIT before start limit

Answer 13

200 degrees C on deck
150 degrees C in flight
100 degrees C for prime

Question 14

TIT start limit

Answer 14

750-830 degrees C
above 830 record, above 850 stop, record and good for restart
965 overtemp inspection required

Question 15

normal rated TIT

Answer 15

1010 degrees C

Question 16

military power

Answer 16

1049 degrees C for 30 minutes

Question 17

max power

Answer 17

1077 degrees C for 5 minutes

Question 18

low rpm tit

Answer 18

410 to 730

Question 19

normal rpm TIT start position

Answer 19

445 to 645

Question 20

max reverse TIT

Answer 20

580 to 790

Question 21

flight idle TIT

Answer 21

430 to 705

Question 22

Low rpm limits %

Answer 22

71-73.8 %

Question 23

normal rpm start position

Answer 23

96.3-99.1%

Question 24

max reverse

Answer 24

96.7-104.9

Question 25

flight idle

Answer 25

94.5-98.4

Question 26

flight range RPM

Answer 26

99-101

Question 27

min oil temp for start up

Answer 27

-40

Question 28

min oil temperature during run up below 1000

Answer 28

0-40

Question 29

min oil for takeoff

Answer 29

40 and rising

Question 30

normal oil temp

Answer 30

60-90

Question 31

extremely cold

Answer 31

50-60

Question 32

max Oil temp

Answer 32

100 degrees c for 30 minutes on deck and 5 mins in flight

Question 33

power section oil psi

Answer 33

50-60 psi

Question 34

max except during warmup power section

Answer 34

60

Question 35

max during warmup power section

Answer 35

100 psi

Question 36

oil RGB normal rpm psi

Answer 36

130-250 psi

Question 37

oil RGB low rpm

Answer 37

50-250 psi

Question 38

engine starter duty cycle

Answer 38

60 secs on, 30 secs off. After 3 cycles, 30 mins off or 1 min on, 5 minutes off indefinitely

Question 39

Air starts speed limits

Answer 39

170-210, 345 @ sea level minus 6 knots per 1000 ft

Question 40

APU EGT limits

Answer 40

max peak-732 max peak continuous for 10 secs-710 max continuous- 649 max for shutdown-350

Question 41

APU rpm

Answer 41

in flight-98-103 | on deck-98-102

Question 42

Max APU airspeed

Answer 42

225 for doors

Question 43

max start altitude

Answer 43

25000 ft

Question 44

Flap limits

Answer 44

``` flap retraction after takeoff-140 man-275 to/appr-190 land-170 flap retraction to man with 2 engine-150 ```

Question 45

landing gear limits

Answer 45

extended-300 kias at more than 1 g extended-190 landing gear retraction-190

Question 46

landing lights

Answer 46

260

Question 47

over wing exit

Answer 47

170

Question 48

Fuel dump

Answer 48

140-220

Question 49

windshield unheated

Answer 49

240 below 10000

Question 50

turbulent air penetration

Answer 50

220 190 for crew comfort

Question 51

max xwind for landing

Answer 51

35

Question 52

weight limits

Answer 52

``` max gross takeoff 139760 max recommended takeoff 135000 max landing weight- 114000 max recommended landing-103880 max zero fuel weight-77200 ```

Question 53

Crosswind limits

Answer 53

``` Dry-35 knots Wet-25 knots Icy-10-15 knots Training-70% of max crosswind component Boost out-10 knots Tailwind-10 knots ```

Question 54

Math for airspeeds

Answer 54

``` Loiter-GW + 90 MRC-205 + 1/2GW - ALT MRC 2/3 ENG- MRC-10/MRC-20 MAX TAS- 405-Vne+IAS (+30%HW/-20%TW) MAX RANGE POWER-SHP=GW x 2 STALL BUFFET- 1/2GW+64 ```