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73 Cards in this Set
- Front
- Back
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Maximum operating altitude |
41,000 |
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Maximum altitude takeoff and landing |
8,000 |
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Minimum altitude takeoff and landing |
-1,000 |
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Max allowable load factors Flaps up |
+2.5 -1 |
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Flaps Down |
+2 0 |
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Maximum runway slope |
+-2 |
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Approved runway surface |
Paved |
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Max tailwind T/O and LDG |
10 knots |
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Max crosswind Dry runway |
28G38 |
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Max cross Wet |
28 knots |
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Maxx cross compacted snow |
20 knots |
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Max cross standing water/slush |
18 knots |
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Max cross ice |
12 knots |
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Max wind for Cat II head/tail/cross |
25/10/12 |
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Max/min temp for T/O |
+35 -40 |
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Max taxi dry/wet Contaminated |
30 15 |
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Min flight speed |
Except as described in normal/abnormal/emergency procedures, the airplane may never be operated below the green dot speed |
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Max Operating Speeds VmO MmO |
320 .82 |
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Max Turbulent Airspeed Less 10,000 Greater than 10,000 |
250 270/.76 (whichever is less) |
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Min RAT speed |
130 |
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Oxygen quantity Green Cyan Amber |
Normal operating range (min for dispatch with three crew members on the flight deck) Normal operating range (min for dispatch with two crew members on the flight deck) Cautionary operating range (dispatch is not allowed) |
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Cabin Pressurization limits up to 37,000 |
7.8 |
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Above 37,000 |
8.3 |
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Maximum differential overpressure |
8.7 psi |
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Maximum differential negative pressure |
-.5 psi |
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Maximum differential pressure for T/O and LDG |
.2 psi |
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Pneumatics Maximum altitude for single pack operation |
FL310 |
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Minimum height to engage AP on TO |
Acceleration altitude |
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Minimum height to engage AP on go Around |
400'AGL |
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Minimum height to engage AP enroute |
500' AGL |
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Minimum height to engage APnon precision approach |
MDA |
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Minimum height to engage AP precision approach |
70' AGL |
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Special instrument approach |
As specified in the procedure |
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Maintenance is required if the battery voltage is less than |
21Volts |
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Minimum battery temperature for an APU start |
-20 degrees C |
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When airplane is stopped, taxi and LDG lights must be |
Off |
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for takeoff and in flight |
taxi nose light must be off |
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To avoid power transfer interruptions when connecting/disconnecting and electrical source |
Confirm power transfer on the electrical synoptic page or wait 10 seconds |
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Maximum altitude for flap extended |
20,000 ft |
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Flap speed limits Flaps 1 2 3 4 5 Full |
1-230 2-215 3-200 4-180 5-180 Full-165 |
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Max useable fuel |
20,785 lbs |
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Max fuel imbalance |
794 lbs |
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Min fuel tank temp |
-40 C |
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Crossfeed During TO and LDG the cross feed selector knob must be |
OFF |
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A hydraulic system warm-up must be accomplished before starting the engines if the reservoir temperatures are below |
-18 C |
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Freezing Rain and Drizzle |
If abnormal ice formation is observed on areas of the airplane that do not usually accrete ice, the flight is operating in an SLD condition. Exit the SLD condition as soon as possible. |
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Icing on the ground The MCDU TO DATASET MENU must be set to ENG when SAT is 5°C to 10°C and: |
1. If there is any possibility of encountering visible moisture up to 1700 ft. AFE or, 2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines nacelles, or engine sensor probes. |
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The MCDU TO DATASET MENU must be set to ALL when SAT is less than 5°C and: |
1. If there is any possibility of encountering visible moisture up to 1700 ft. AFE or, 2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines nacelles, or engine sensor probes. |
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Icing in flight |
Icing conditions exist in flight whenever the Static Air Temperature (SAT) on the ground or for takeoff, or Total Air Temperature (TAT) in flight, is 10°C or below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals). |
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If either or both ice detectors are failed |
the crew must set the mode selector to ON when icing conditions exist or are anticipated below 10°C TAT with visible moisture. |
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Max windshield wiper speed |
250 |
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VLO for LDG gr extension and retraction |
250 |
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Tire Max ground speed |
195 knots |
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Min runway/taxiway width for 180 turn 170 |
54' 8" |
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Min runway/taxiway width for 180 turn 175 |
59'2" |
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Avionics Cat I |
Baro altimeter minimums must be used for all Cat I approaches. |
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The VOR flight director mode is prohibited. |
This VOR flight director mode is inhibited. VOR navigation using the flight director must be predicated on HDG mode and VHF (green) needles or LNAV mode (magenta). |
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IESS limitations |
Back course approaches using the IESS are prohibited. |
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Min APU start temp |
-54 C |
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Max APU start |
30,000 ft |
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Max altitude for APU Gen |
33,000 ft |
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Max alt APU Bleed air |
15,000 ft |
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Max alt for APU assisted start |
21,000 ft |
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Min battery voltage to start APU |
21 volts |
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APU starter duty cycle limits |
1 and 2-- Max 60 Cool--60 3--60 and 5 min |
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Before starting the APU after an engine shut down |
Wait for engine to go below 30% N2 |
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ITT Max start |
815 C |
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ATTCS |
For takeoff the ATTCS must be on |
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Engine warm up.cool down period |
2 min |
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Engine starter limits |
1 and 2 -90 sec ground 120 flight, cool down-10 sec 3-5 90 G 120 F, cool down- 5 minutes |
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Powerback operations |
Prohibited |
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Reverse thrust idle by out of reverse by |
60 30 |
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An assumed temperature (FLEX) takeoff is not allowed if any of the following conditions exist: |
1. The runway is contaminated. Refer to “Takeoff on wet, slippery or contaminated runways” on page 7.3.13. 2. The antiskid system is inoperative. 3. The Takeoff performance section of the takeoff report does not include FLEX takeoff data. 4. Compass airport information pages (10-7s) prohibit an assumed temperature takeoff. 5. The PIC determines the conditions for an assumed temperature takeoff are unsafe. |
