Praetor Limitations (Red Items)

Question 1

Emergency Fuel

Answer 1

1300 LBS

Question 2

Max Crosswind (N) Dry or Wet Runway

Answer 2

Takeoff: 35 Knots (Above 25 Knots use Crosswind Takeoff Procedure)
Landing: 25 Knots

Question 3

Max Crosswind (N) Contaminated Runway Condition

Answer 3

> 150 Feet: 15 Knots
<150 Feet: 10 Knots

Question 4

Max Tailwind TO/LDG

Answer 4

10 Knots

Question 5

Max Ramp/Taxi Weight

Answer 5

37,699

Question 6

Max Takeoff Weight

Answer 6

37, 567

Question 7

Max Landing Weight

Answer 7

34,172

Question 8

Max Operating Altitude

Answer 8

45,000 Feet

Question 9

Flaps 1, 2, or FULL Extended Max Altitude

Answer 9

20,000

Question 10

Flaps 3 Extended Max Altitude

Answer 10

15,000

Question 11

Gear Extended Max Altitude

Answer 11

20,000

Question 12

Anti-ice Single Bleed Operation

Answer 12

20,000

Question 13

Takeoff and Landing Max Altitude

Answer 13

9,600

Question 14

Turbulent Air Penetration Speed

Answer 14

265/.77

Question 15

Max Gear Operating/Extended Speed

Answer 15

250

Question 16

Flaps 1 Max Speed

Answer 16

210

Question 17

Flaps 2 Max Speed

Answer 17

185

Question 18

Flaps 3 Max Speed

Answer 18

185

Question 19

Flaps FULL Max Speed

Answer 19

170

Question 20

Minimum Speed in Icing

Answer 20

180

Question 21

Unsuccessful APU Start

Answer 21

3 Consecutive Start attempts with 30 seconds between attempts

Question 22

Max Altitude for APU Start

Answer 22

31,000

Question 23

Minimum in-flight temp for start

Answer 23

-37C
(APU Start on ground prohibited with ambient temps below -40)

Question 24

APU Max operating altitude

Answer 24

31,000

Question 25

In-Flight APU assisted engine start max altitude

Answer 25

23,000

Question 26

Environmental Control System (ECS) Max Alt on APU

Answer 26

20,000

Question 27

Minimum Alt Autopilot Approach WITHOUT Vertical Path

Answer 27

180 FT AGL

Question 28

Minimum Alt Autopilot Approach WITH Vertical Path

Answer 28

80 FT AGL

Question 29

Minimum Autopilot Engagement Height

Answer 29

400 FT AGL

Question 30

Total Useable Fuel QTY

Answer 30

13,050

Question 31

Approach Category

Answer 31

Category B, if operational requirements dictate HIGHER than 120 THEN use CAT C

Question 32

All Engines Operating (AEO) TOGA Thrust Time Limit

Answer 32

5 Min

Question 33

One Engine Inoperative (OEI) TOGA Thrust Time Limit

Answer 33

10 Min

Question 34

Max ITT Initiating Start (N)

Answer 34

350 C