Limitations 700 Flashcards
This deck is a copy of a Quizlet deck
Engine Type
Thrust Rating
GE CF34-3C1
• 8,729 lbs per engine
• 9,220 lbs per engine
Fuel imbalance
Takeoff…..300 lbs.
Flight……..800 lbs.
Pressure refueling
19,594 lbs.
Maximum airspeed for windshield wiper operation failed in the non-parked position
250 KIAS
Cargo in cargo compartment
Flight must be within 60 min of suitable airport
Maximum Weight in Cargo Compartment
1,000 lbs. (for)
3,300 lbs. (aft)
Ramp Weight
75,250 lbs.
- Max altitude for single pack operation
* Max differential
- 31,000’
* 8.7 psi
Maximum Takeoff Weight
75,000
Maximum Landing Weight
67,000
APU Door not closed or position unknown
220 KIAS
or APU must remain in operation
Maximum Zero Fuel Weight
62,300 lbs.
Bleed air extraction from APU
NOT permitted above
25,000’
Starter cranking limits
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%
Flaps Vfo
1 - 230 8 - 230 KIAS 20 - 220 KIAS 30 - 185 KIAS 45 - 170 KIAS
Flaps Vfe
1 - 230 8 - 230 KIAS 20 - 220 KIAS 30 -185 KIAS 45 -170 KIAS
Oil Pressure Limits
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.
Max load on TRU
120 amps
Engine Operating Limits Due to Wind Direction.
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
Engine Operating Limits Due to Wind Direction.
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
APU Starting
(3) starts/start attempts in one (1) hour with a two
(2) minute delay between cranking attempts.
Airplane Cold Soak (700)
- -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
Maximum operating altitude
• 41,000 ft
Max Starting Altitude for APU
Max Operating Altitude for APU
- 37,000 ft.
* 41,000 ft.
AC Gen Loading Values
Main GEN - 40 kVA up to FL 410
APU GEN - 40 kVA up to FL 410
Minimum Operating Weight Empty
42,000 lbs.
Takeoff on contaminated runways is prohibited when:
• 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.
Landing on contaminated runways is prohibited when:
• 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
Maximum N1
99.5%
Max altitude for main engine start with APU Bleed
21,000 ft
