Limitations 700

Question 0

Engine Type

Thrust Rating

Answer 0

GE CF34-3C1
• 8,729 lbs per engine
• 9,220 lbs per engine

Question 1

Fuel imbalance

Answer 1

Takeoff…..300 lbs.

Flight……..800 lbs.

Question 2

Pressure refueling

Answer 2

19,594 lbs.

Question 3

Maximum airspeed for windshield wiper operation failed in the non-parked position

Answer 3

250 KIAS

Question 4

Cargo in cargo compartment

Answer 4

Flight must be within 60 min of suitable airport

Question 5

Maximum Weight in Cargo Compartment

Answer 5

1,000 lbs. (for)

3,300 lbs. (aft)

Question 6

Ramp Weight

Answer 6

75,250 lbs.

Question 7

• Max altitude for single pack operation

* Max differential

Answer 7

• 31,000’

* 8.7 psi

Question 8

Maximum Takeoff Weight

Answer 8

75,000

Question 9

Maximum Landing Weight

Answer 9

67,000

Question 10

APU Door not closed or position unknown

Answer 10

220 KIAS

or APU must remain in operation

Question 11

Maximum Zero Fuel Weight

Answer 11

62,300 lbs.

Question 12

Bleed air extraction from APU

NOT permitted above

Answer 12

25,000’

Question 13

Starter cranking limits

Answer 13

90 secs……..10 secs off
90 secs……..10 secs off
90 secs……..5 minutes off
The starter must not be engaged if indicated N2 RPM exceeds 45%

Question 14

Flaps Vfo

Answer 14

1 - 230
8 - 230 KIAS
20 - 220 KIAS
30 - 185 KIAS
45 - 170 KIAS

Question 15

Flaps Vfe

Answer 15

1 - 230
8 - 230 KIAS
20 - 220 KIAS
30 -185 KIAS
45 -170 KIAS

Question 16

Oil Pressure Limits

Answer 16

Idle……………..25psi
Takeoff……….45psi
Max cont……95psi
Transient…….156psi when oil temp is <60°C
Max transient after cold start (10 min)
182 psi or amber dashes
After cold start, engine must remain at idle until oil pressure returns to normal range.

Question 17

Max load on TRU

Answer 17

120 amps

Question 18

Engine Operating Limits Due to Wind Direction.

Answer 18

Within 30° on either direction of the airplane
nose-no windspeed limit

>30° in either direction of the airplane
nose- 30° in either direction of the airplane
nose-between 5 and 30 knots windspeed
Apply maximum of 75% N1 before brake
release, then TOGA thrust.

> 30° in either direction of the airplane
nose- >30 knots windspeed
Apply maximum of idle/taxi thrust before
brake release, then TOGA thrust

Question 19

Engine Operating Limits Due to Wind Direction.

Answer 19

Within 30° on either direction of the airplane
nose-no windspeed limit
>30° in either direction of the airplane
nose- 0 to 30° between 5 and 30 kts
max 75% N1 before brake
release, then TOGA thrust.
>30° and >30 knots
max of idle/taxi thrust before
brake release, then TOGA thrust

Question 20

APU Starting

Answer 20

(3) starts/start attempts in one (1) hour with a two

(2) minute delay between cranking attempts.

Question 22

Airplane Cold Soak (700)

Answer 22

• -30 for more than 8 hrs before first flight
• The engines must be motored for 60 seconds and fan rotation must be verified before an engine start is initiated
• Thrust reversers must be actuated until the deploy and stow cycles are less than 2 seconds

Question 23

Maximum operating altitude

Answer 23

• 41,000 ft

Question 24

Max Starting Altitude for APU

Max Operating Altitude for APU

Answer 24

• 37,000 ft.

* 41,000 ft.

Question 25

AC Gen Loading Values

Answer 25

Main GEN - 40 kVA up to FL 410

APU GEN - 40 kVA up to FL 410

Question 26

Minimum Operating Weight Empty

Answer 26

42,000 lbs.

Question 27

Takeoff on contaminated runways is prohibited when:

Answer 27

• Standing water >0.5 inch in depth
• Slush >0.59 inch in depth
• Wet snow >0.59 inch in depth
• Dry snow > 3.0 inches in depth
• Crosswind or tailwind component exceeds the guidelines for braking action in 3.7 Braking Action Takeoff & Landing
Wind Component Guidelines
All contaminated performance data will be for ROLLING takeoffs due to AFM limitations.

Question 28

Landing on contaminated runways is prohibited when:

Answer 28

• Standing water is more than 0.75 inch in depth
• Slush is more than 0.88 inch in depth
• Wet snow is more than 0.88 inch in depth
• Dry snow is more than 3.75 inches in depth
• Crosswind or tailwind component exceeds the guidelines for braking action in 3.7 Braking Action Takeoff & Landing
Wind Component Guidelines

Question 29

Maximum N1

Answer 29

99.5%

Question 30

Max altitude for main engine start with APU Bleed

Answer 30

21,000 ft