Limitations (remaining)

Question 1

Flight Maneuvering Load Acceleration Limits

Answer 1

Flaps up:

+2.5g to -1.0g

Flaps down:

+2.0g to 0.0g

Question 2

Takeoff / Landing Pressure Altitude

Answer 2

Maximum:

10,000 feet

Question 3

Runway Slope

Answer 3

Maximum:

+/- 2%

Question 4

Maximum Airspeed

Answer 4

Vmo:

Indicated by max airspeed pointer on airspeed indicator

Mmo:

.82 Mach

Question 5

Miximum Gear retration speed

Answer 5

235 knots

Question 6

Maximum gear extension speed

Answer 6

270 knots / .82 Mach

Question 7

Maximum Gear Operating / Extended Speed

Answer 7

320 knots / .82 Mach

Question 8

Maximum Cabin pressure differential

Answer 8

9.1 PSI

Question 9

Maximum differential pressure for takeoff and landing

Answer 9

.125 PSI

Question 10

Engine Anti-ice operation

Answer 10

• Must be ON during all ground operations, including after landing, when icing conditions exist or are anticipated
• Must be ON during all flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temp is below -40 degreess SAT
• Must be ON prior to and during descent in all icing conditions, including temps below -40 degrees C SAT
• Engine ignition must be selected to CONT prior to and during engine anti-ice operation

Question 11

Wing Anti-ice operation

Answer 11

• Use Wing anti-ice during all ground operations between engine start and takeoff when icing conditions exist or are anticipated, unless the aircraft is or will be protected by the application of Type II or Type IV fluid
• Do not operate Wing Anti-ice on the ground when the OAT is above 10 degrees C / 50 degrees F
• Do not use wing anti-ice as a substitute for ground deicing / anti-icing

Question 12

Windshield wiper use

Answer 12

Do not operate windshield wiper on a dry windshield

Question 13

Window Heat

Answer 13

Window heat must be on 10 minutes before takeoff

Question 14

Probe Heat

Answer 14

Probe heat must be on prior to takeoff

Question 15

Wing Anti-Ice

Answer 15

During takeoff, do not use wing anti-ice unitl after the first thrust reduction

Question 16

Autopilot use at high altitude airports

Answer 16

Autopilot use prohibited below 100 feet radio altitude at airport pressure altitudes above 8400 feet

Question 17

Single Engine Drive Generator Load

Answer 17

Maximum:

75 KVA - 215 amps (ground operations)

Question 18

Battery Voltage for APU Start

Answer 18

Minimum:

23 volts

Question 19

Engine Ignition must be on:

Answer 19

HELT

Heavy Rain

Engine anti-ice operation

Landing

Takeoff

Question 20

Minimum Oil Pressure

Answer 20

13 PSI

Question 21

Maximum oil temp

Answer 21

155 degrees C

Question 22

Maximum Oil temp (max continuous)

Answer 22

140 degrees C

Question 23

Max Oil Temp (max allowable)

Answer 23

140 degrees C - 155 degrees C (45 minutes)

Question 24

Max EGT Takeoff (5 minutes)

Answer 24

950 degrees C

Question 25

Max EGT (max continuous)

Answer 25

925 degrees C

Question 26

Max EGT (start)

Answer 26

725 degrees C

Question 27

Engine Start Duty Cycle

Answer 27

• Multiple consecutive start attempts are permitted. Each start attempt is limited to 2 minutes or starter usage
• A minimum of 10 seconds is needed between start attempts

Question 28

RPM Maximum

Answer 28

N1:

104.0%

N2:

105.0%

Question 29

Reduced thrust takeoffs restrictions

Answer 29

• Operation with assumed temperature reduced takeoff thrust is not permitted with antiskid inoperative
• Use of assumed temperature reduced takeoff thrust is not permitted when the runway is contaminated with standing water, ice, slush, or snow

Question 30

Max Altitude APU bleed and electrical

Answer 30

10,000 feet

Question 31

Max Altitude APU Bleed

Answer 31

17,000 feet

Question 32

Max altitude APU Electrical Load

Answer 32

41,000 feet

Question 33

Engine Oil Minimum QTY prior to engine start

Answer 33

60%

Question 34

Engine Starter Engagement

Answer 34

Do not engage starter above 20% N2

Question 35

Engine starts in ambient temp below -35 degrees C

Answer 35

• Idle engine 2 minutes before changing thrust lever position

Question 36

APU starter duty cycle

Answer 36

For both ground and in-flight starts, 15 minute cooling is required after third start attempt