Rob Forst

Question 1

Vmo (up to 8000 ft)

Answer 1

300 KIAS

Question 2

Vmo (8001 ft to 29,475 ft)

Answer 2

320 KIAS

Question 3

Mmo (above 29,475 ft)

Answer 3

.83 Mach Indicated

Question 4

Vra (rough air penetration speed)

Answer 4

265 KIAS/.75 MI

Question 5

Vlo (retract)

Answer 5

200 KIAS

Question 6

Vlo (extend)

Answer 6

250 KIAS

Question 7

Vle (extended)

Answer 7

250 KIAS

Question 8

Vfe (flaps 10)

Answer 8

210 KIAS

Question 9

Vfe (flaps 20)

Answer 9

210 KIAS

Question 10

Vfe (flaps 30)

Answer 10

175 KIAS

Question 11

Maximum tire speed (ground speed)

Answer 11

182 Kts

Question 12

Minimum operating speed

Answer 12

Intentional speed reduction below the onset of the stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for flight test or training ops.

Question 13

Maximum takeoff and landing pressure altitude

Answer 13

10,000 ft

Question 14

Maximum tailwind component

Answer 14

10 kts

Question 15

Takeoff and landing are limited to _________ runways

Answer 15

paved

Question 16

The maximum runway slopes approved for takeoff and landing are ___ % uphill and ___ % downhill

Answer 16

+2, -2%

Question 17

The maximum crosswind component for takeoff is ___ knots

Answer 17

28

Question 18

The maximum crosswind component for landing is ___ knots

Answer 18

24

Question 19

The maximum crosswind component for takeoff and landing on contaminated runway is ___ knots

Answer 19

10

Question 20

Operations on runways with a coefficient of less than __ is prohibited

Answer 20

0.3

Question 21

Maximum pressure altitude (enroute)

Answer 21

45,000 feet

Question 22

Takeoff (is/is not) permitted with frost adhering to the underside of the wing that is caused by cold soaked fuel

Answer 22

is (refer to FCM, Supplement 1 - Cold WX Ops)

Question 23

Maneuvering load factor, flaps up (+, - g)

Answer 23

+2.6 g to -1.0 g

Question 24

Maneuvering load factor, flaps extended (+, - g)

Answer 24

+2.0 g to 0.0 g

Question 25

If type III, III & IV anti-icing fluids have been applied

Answer 25

The wing anti-ice system must only be selected on, if required, just prior to thrust increase for takeoff

Question 26

Maximum operating temerature

Answer 26

50 deg C

Question 27

Minimum operating temperature

Answer 27

-45 deg C airframe limit, (see fuel temp limit)

Question 28

APU - maximum altitude for operation

Answer 28

37,000 feet

Question 29

APU - maximum altitude for generator operation

Answer 29

30,000 feet

Question 30

APU - maximum altitude for APU bleed air for engine start operation

Answer 30

20,000 feet

Question 31

APU - maximum altitide for ECS bleed air

Answer 31

20,000 feet for aircraft with SB 100-21-05 compliance

Question 32

APU - do not use the APU to start the ___ engine above ___ feet

Answer 32

left, 9000 feet

Question 33

APU - do not start the APU above ___ knots

Answer 33

300