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71 Cards in this Set
- Front
- Back
Min Flight Crew and Max Pax
|
2 Pilots
375 Pax |
|
Max Taxi Weight
|
515.7 lbs
|
|
Max Take Off Weight
(Brake Release) |
513.7 lbs
|
|
Max Landing Weight
|
401.2 lbs
|
|
Max Zero Fuel Weight
|
374.8
|
|
Min Weight
|
255.7
|
|
Flight Maneuvering Load Limits:
Clean Config Other Config |
Clean -1 to 2.5g
Other 0 to 2g |
|
Runway Slope
|
+/- 2%
|
|
Max Runway Altitude
|
12,500 ft
|
|
Max Crosswind for Take off
|
32 kts (includes gust)
|
|
Max Tailwind for Takeoff
|
15 kts
|
|
Max Landing crosswind
|
45 kts
|
|
Max Tailwind for Landing
|
10 kts
|
|
Max wind for Pax door operation
|
40 kts
50 kts with nose pointed into wind |
|
Max wind for cargo door operation
|
40 kts
50 kts with nose pointed into wind |
|
Pax and Cargo doors must be closed before wind exceeds
_____ kts? |
60 kts
|
|
Max Altitude with Slats/Flaps extended?
|
20,000 ft.
|
|
Max speed Flaps 1?
|
240 kts
|
|
Max speed flaps 1+F?
|
215 kts
|
|
Max Speed flaps 2?
|
196 kts
|
|
Max Speed flaps 3?
|
186 kts
|
|
Max Speed flaps Full?
|
180 kts
|
|
Max Speed Landing Gear extended?
|
250 kts/ .55 mach
|
|
Max speed landing gear operation?
|
250 kts/ .55 mach
|
|
Max speed landing gear gravity extension?
|
200 kts
|
|
Max altitude landing gear may be extended?
|
21,000 ft
|
|
Max tire speed?
|
204 kts ground speed
|
|
Max windshield wiper speed?
|
230 kts
|
|
Max speed cockpit window open?
|
230 kts
|
|
Speedbrakes max speed?
|
none
|
|
Max cabin diff pressure?
|
9.25 psi
|
|
Max Neg. diff pressure?
|
-0.73 psi
|
|
Cabin pressure safety relief valve settings? (- to +)
|
-.26 / 8.85 psi
|
|
Ram air inlet opens only if diff pressure less than ____?
|
1 psi
|
|
Can you use the packs and LP ground air simultaneously?
|
No
|
|
Air flow supplied by two carts should not exceed ____?
|
2 x 3.53 lbs/sec
|
|
Can the APU supply bleed air with an HP ground unit hooked up?
|
No
|
|
Minimum weight for use of auto land?
|
271.1 lbs
|
|
Min height for use of autopilot on T/O with SRS mode?
|
100 Ft AGL
|
|
Min height for autopilot use, straight in non precision approach?
|
MDA/MDH
|
|
Min Autopilot height, straight in LNAV/VNAV Approach?
|
Applicable DA
|
|
Use of autopilot or flight director in open descent or Descent mode is not permitted in App, unless FCU Altitude is set to or above?
|
MDA/MDH or 500 ft, whichever is higher
|
|
Use of Autothrust is approved with or without AP/FD in selected or managed mode, true or false?
|
True
|
|
Minimum Fuel for takeoff?
|
11,460 lbs.
(wing tank low level warning must not be displayed for take off) |
|
You cannot use the electrical outlets during ____ & _____
|
Takeoff and Landing
|
|
Min Autopilot use circling approach?
|
MDA/MDH -100ft
|
|
Min autopilot use ILS Approach Cat 1?
|
160 AGL
|
|
Min height for engagement of autopilot during go around?
|
100 AGL
|
|
Min autopilot height all other uses?
|
500 AGL
|
|
Normal hydraulic operating pressure?
|
3000 psi +/- 200
|
|
Max Brake Temp for Takeoff?
|
300 C
|
|
Max nose wheel steering angle?
For pushback? |
72
65 pushback |
|
ISIS bug function should not be used when?
|
Both PFD's are lost
|
|
How long can you use the APU without maintenance action if the Low oil level message is displayed?
|
15 hrs
|
|
APU starter limits
|
3 start attempts, no cool down, then 60 minutes cool down
|
|
APU max N speed?
|
107%
|
|
APU max EGT?
|
650 C
|
|
APU max EGT for start?
|
1250 C
|
|
Engine TOGA limits:
Time Limit/EGT Limit |
20 sec @ 920 C
5 min @ 900 C (10 min with engine failure) |
|
Engine MCT
Time/EGT Limit |
Unlimited @ 850 C
|
|
Engine Starting EGT limits?
|
700 C
850 C (air start only) |
|
Oil Temp:
Max Temp? |
190 C
|
|
Oil Temp:
Min for Takeoff? |
20 C
|
|
Min Oil Press?
|
25 psi
|
|
Engine Max N1?
|
99%
(possibly lower based on ambient conditions and bleed config) |
|
Engine Max N2?
|
103.3%
|
|
Engine Max N3?
|
100%
|
|
Engine Starter Limits?
|
One continuous 5 min cycle
or (2) 3 min cycles + (1) 1 min cycle with N3 rundown to 0 between cycles 30 minutes cool down after either |
|
No running engagement of starter when N3 is above?
|
10% on ground
30% in flight |
|
Max reverse thrust off by?
|
70 kts
|
|
Requirements for reduced thrust take offs? (5 things)
|
-Meets performance requirements at planned t/o weight
-Flex temp not higher than ISA+60 -AT must not be lower than the flat rating temp or actual OAT -Not permitted on contaminated runways -Performance penalties must be accounted for and still meet min requirements |