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63 Cards in this Set
- Front
- Back
Max tailwind |
10 knots |
|
Max take off and landing altitude |
10,000’ |
|
Max operating altitude |
41,000’ |
|
Max tire speed |
182 knots ground speed |
|
Max temp for takeoff and landing |
ISA + 35 degrees Celsius |
|
Minimum temp for takeoff |
-40 degrees Celsius |
|
Max cross wind |
27 knots |
|
If cargo carried |
45 minutes of suitable airport |
|
Max pax |
50 |
|
Minimum go around altitude |
100 feet |
|
Max crosswind dry runway |
27 kts |
|
Max crosswind contaminated runway |
10 kts |
|
Max wind during ground operations |
40 kts |
|
Max taxi weight |
53,250 lbs |
|
Max takeoff weight |
53,000 lbs |
|
Max landing weight |
47,000 pounds |
|
Max ZFW |
44,000 lbs |
|
Minimum flight weight |
30,000 lbs |
|
Flaps 8 |
200 KIAS |
|
Flaps 20 |
200 KIAS |
|
Flaps 30 |
185 KIAS |
|
Flaps 45 |
170 KIAS |
|
Gear extension |
250 KIAS |
|
Gear retraction |
200 KIAS |
|
Max tire speed |
182 KIAS |
|
Turbulence speed |
280 KIAS/.75 Mach |
|
Wiper speed |
220 KIAS |
|
Cowl anti-ice |
Ground: OAT 10 degrees C or below Air: (ICE annunciator) TAT 10 degrees C to SAT -40 degrees Celsius, visible moisture |
|
Wing anti ice |
Ground: OAT 5 degrees C or below Air: (ICE annunciator) 230 KIAS or below in icing conditions; TAT 10 degrees Celsius to SAT -40 degrees Celsius, visible moisture |
|
Takeoff and landing with anti-ice on |
10th stage valves closed |
|
Max ITT engine start |
900 degrees Celsius |
|
Airplane cold soaked (-30 degrees Celsius for 8 hours) |
-engines must be monitored for 60 seconds and fan rotation before start -thrust reversers actuated until deploy and stow cycles less than 5 seconds |
|
Continuous ignition |
-takeoff and landing with a contaminated runway -takeoff in high crosswind -moderate or heavier rain -moderate or heavy turbulence -vicinity or thunderstorms |
|
Starter cranking |
-no starter use if N2 above 55% 1: 1 minute ON; 10 seconds OFF 2: 1 minute ON; 10 seconds OFF 3: 1 minute ON; 5 minutes OFF 4: 1 minute ON; 5 minutes OFF |
|
Thrust lever SHUT OFF to IDLE |
Ground start: ITT 120 degrees Celsius or less Air start: ITT 90 degrees Celsius or less |
|
Dry monitoring |
1: 90 seconds on; 5 minutes OFF 2&up: 30 seconds on; 5 minutes OFF |
|
Fuel: left main |
Pressure refueling: 4,760 lbs Gravity refueling: 4,488 lbs |
|
Fuel: right main |
Pressure refueling: 4,760 lbs Gravity refueling: 4,488 lbs |
|
Fuel: center |
Pressure refueling: 4,998 Gravity refueling: 4,930 |
|
Fuel: total |
Pressure refueling: 14,518 lbs Gravity refueling: 13,906 lbs |
|
Minimum fuel for a go around |
450 lbs per wing |
|
Minimum takeoff fuel temp |
5 degrees Celsius |
|
Minimum takeoff bulk fuel temp |
-30 degrees Celsius |
|
Engine oil level checked |
3 minutes to 2 hours after shutdown |
|
Oil replenishment system |
15 minutes to 2 hours after shutdown |
|
Max oil refill without dry motor |
2 quarts |
|
Minimum temp for starting APU |
-40 degrees Celsius |
|
APU start cycle batteries |
1: 30 seconds ON; - 2: 30 seconds ON; 20 minutes OFF 3: 30 seconds ON; - 4: 30 seconds ON; 40 minutes off |
|
Max altitude for APU bleed for air conditioning |
15,000 feet |
|
Max altitude for APU bleed to start engine |
13,000 feet |
|
Max load APU generator |
30 kVA |
|
Max pressure differential |
8.7 psi |
|
Max negative pressure differential |
-0.5 psi |
|
Max pressure differential taxi, takeoff, and land |
0.1 psi |
|
Max altitude for autopilot engagement |
600’ AGL |
|
Minimum altitude for autopilot: non-precision |
400’ AGL |
|
Minimum altitude for autopilot: precision |
80’ AGL |
|
AC generator load limit |
0-35,000’: main generator (30); APU (30) 35,001’-37,000’: main generator (25); APU (30) 37,001,&above: main generator (25); APU (0) |
|
Max TRU load |
100 amps |
|
Max time of DC power only |
5 minutes |
|
Minimum altitude: flight spoilers extended |
300’ AGL |
|
Minimum airspeed: flight spoilers |
Approach speed +17 KIAS |
|
Max speed: thrust reverse above idle |
60 KIAS |