200 Limitations, POH Rev 25

Question 1

-200 Max Operating Altitude

Answer 1

36,000 ft.

Question 2

-200 Max Taxi and Ramp Weight

Answer 2

53,250 lbs

Question 3

-200 Max T/O Weight

Answer 3

53,000 lbs

Question 4

-200 Max Landing Weight

Answer 4

47,000 lbs

Question 5

-200 Max Zero Fuel Weight

Answer 5

44,000 lbs

Question 6

-200 Engine Starter Limits:

Answer 6

• 1 min on, 10 sec off
• 1 min on, 10 sec off
• 1 min on, 5 min off

Question 7

-200 APU Starter Limits - Battery

Answer 7

• 30 sec on, 2 min off
• 30 sec on, 20 min off
• 30 sec on, 2 min off
• 30 sec on, 40 min off

Question 8

-200 APU Starter Limits - DC Ground Power

Answer 8

• 15 sec on, 2 min off
• 15 sec on, 20 min off
• 15 sec on, 2 min off
• 15 sec on, 40 min off

Question 9

-200 Structural Limits

Answer 9

• Max Taxi/Ramp Weight: 53,250
• MTOW: 53,000
• MLW: 47,000
• MZFW: 44,000

Question 10

-200 Max APU Bleed Air Extraction Altitude for Air Conditioning:

Answer 10

15,000 ft

Question 11

-200 APU Door Limits:

Answer 11

When door is not closed or door position is unknown:

Limited to 300 kts or APU must be running.

Question 12

-200 Max Altitude for Single Pack Operations:

Answer 12

25,000 ft.

Question 13

-200 Max ITT during Eng Start:

Answer 13

900 C

Question 14

-200 Max N2 Ground Power Idle Split

Answer 14

Not greater than 2% N2

Question 15

-200 If N2 is 57% or less with OAT of -20C or warmer:

Answer 15

Do not accelerate above idle.

Question 16

-200 Max Fuel Imbalance:

Answer 16

800 lbs for all phases of flight.

Question 17

-200 Both Engine APU Start Limit:

Answer 17

If both engines are to be started using the APU, the Operating Engine’s Thrust must not exceed 70% N2 while starting the second engine.

Question 18

-200 Stab Trim Runaway

Answer 18

1. Control wheel
   * Assume manual control and override runaway
2. Both STAB TRIM DISCs
   * Push, hold, and release
3. Captain assumes PF duties
4. STAB CH1 cb (2F5)
   * Open
5. STAB CH2 cb (4A1)
   * Open

Question 19

-200 Wing Anti Ice:

Answer 19

Must be selected ON during the final two minutes prior to takeoff during all ground operations at temperaturees of 5C or below unless Type IV anti-icing fluid has been applied.

Question 20

-200 Anti Ice Bleeds

Answer 20

The tenth stage engine bleeds must be CLOSED for takeoff and landing when the cowl and/or wing anti-ice systems are in use.

Question 21

Max Flap Operating Speed (-200 only):

Answer 21

200 KIAS

Question 22

-200 Max Taxi and Ramp Weight

Answer 22

53,250 lbs

Question 23

-200 Max T/O Weight

Answer 23

53,000 lbs

Question 24

-200 Max Landing Weight

Answer 24

47,000 lbs

Question 25

-200 Max Zero Fuel Weight

Answer 25

44,000 lbs

Question 26

-200 Structural Limits

Answer 26

• Max Taxi/Ramp Weight: 53,250
• MTOW: 53,000
• MLW: 47,000
• MZFW: 44,000

Question 27

-200 Max Operating Altitude

Answer 27

36,000 ft.

Question 28

-200 APU Starter Limits - Battery

Answer 28

• 30 sec on, 2 min off
• 30 sec on, 20 min off
• 30 sec on, 2 min off
• 30 sec on, 40 min off

Question 29

-200 APU Starter Limits - DC Ground Power

Answer 29

• 15 sec on, 2 min off
• 15 sec on, 20 min off
• 15 sec on, 2 min off
• 15 sec on, 40 min off

Question 30

-200 Max APU Bleed Air Extraction Altitude for Air Conditioning:

Answer 30

15,000 ft

Question 31

-200 Both Engine APU Start Limit:

Answer 31

Operating Engine Thrust must not exceed 70% N2 while starting 2nd engine.

Question 32

-200 Max Altitude for Single Pack Operations:

Answer 32

25,000 ft.

Question 33

-200 APU Door Limits:

Answer 33

When door is not closed or door position is unknown:

Limited to 300 kts or APU must be running.