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85 Cards in this Set
- Front
- Back
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Fuel quantity of the main wing tanks |
4760 lbs Gravity refueling 4488 lbs |
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Fuel quantity of the auxiliary tank (center) |
4998 lbs Gravity refueling 4930 lbs |
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Total fuel |
14 518 lbs Gravity refueling 13 906 lbs |
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Max Ramp and Taxi weight |
53 250lb |
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MTOW |
53 000 lb |
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Max Landing Weight |
47 000 lb |
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Max Zero Fuel weight |
44 000 lb |
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Minimum Flight weight |
30 000 lb |
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Max Cargo Weight |
3500 lb |
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Time to a suitable airport when cargo is carried |
45 minutes |
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Max turbulent air speed |
280 KIAS - 0.75 MACH |
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Max Operating Speed (Vmo) |
335 KIAS - 0.85 MACH |
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Pressurization Max defferential pressure |
8.7 PSI |
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Pressurization Max negative deffirential pressure |
-0.5 PSI |
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Pressurization Diff. Pressure for taxi, takeoff and landing |
0.1 PSI |
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Pressurization Minimum cabin alt on manual mode |
-1500 ft |
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Max altitude for single PACK operation |
25 000 ft |
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Minimum altitude with the autopilot engaged And exceptions |
600 ft AGL 400 ft AGL Non precisions approaches 80 ft AGL PAR and ILS |
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Packs pressure 2 packs 1 packs ops |
2 packs ops - 32±4 PSI 1 pack ops - 44±4 PSI |
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O2 tank level Full And Low |
1850 PSI 1410 PSI Variable with T° |
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APU max altitude |
37 000ft |
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APU max starting altitude |
30 000 ft |
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APU max altitude for engine start |
13 000 ft |
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APU max altitude for bleed air ability |
15 000 ft |
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Max continuous load on each TRU |
100 AMPS |
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Max time on DC Power only (battery) |
5 min |
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Altitude for knots to mach# change |
31 600 ft |
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AC gen limitation |
0 yo 35 000 ft --- 30 KVA Above 35 000 ft --- 25 KVA |
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Flaps Speed |
8° --- VFo 200 kt - VFe 230 kt 20 --- VFo 200 kt - VFe 230 kt 30 --- 185 kt 45 --- 170 kt to be determined |
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Min altitude for flight spoilers operations |
300 ft AGL |
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Minimum spoiler speed |
Vref of the flaps setting + 17 KIAS |
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Center tank max permitted fuel without retrictions |
500 lbs |
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Center tank fuel exception |
Wings tanks above 4400 lbs Or Wings tanks above 2000 lbs and ZFW is reduce by the excess of 500 lbs in the center tank And CG in the envelope |
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Max fuel imbalance between main tanks |
800 lbs caution message Pump turns on ar 200lbs |
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Minimum fuel in each main tanks for go-around |
450 lbs |
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Wipers max speed |
220 KIAS |
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Hydraulics pressure normal range |
2800 to 3200 PSI |
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Hydraulics normal quantity range |
45%* to 85% * could be lower if the pressure is low |
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ADG max speed |
Vmo 335kt |
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Flaps Maximum flap operation altitude |
15 000ft |
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Minimum engine fuel temp. |
5° c |
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When the bleed misconfig message may be display during initial approach |
- ceiling at arrival is at or above 3000 ft AGL - no icing conditions - wing and cowl is selected off prior to landing |
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Max gear operating speed |
Extension --- 250 KIAS down and locked --- 250 KIAS Retraction --- 200 KIAS |
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Tire max speed |
182kt ground speed |
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Brake cooling Between landing stop or rejected takeoff And subsequent takeoff |
15 min |
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Max brake temp prior to takeoff |
05 or less And stable or decreasing |
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Max N1 RPM |
98.6% |
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Max ITT |
Normal takeoff 900° first 2 min 884° next 3 min Go around or APR trust 928° first 2 min 900° next 3 min MCT 900° |
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N2 max RPM |
99.3 % Amber arc appears if wing anti-ice ON 0 to 77.9 % |
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Max oil temp° |
163° |
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Oil press range |
0 to 25 red 26 to 115 green 116 to 156 amber |
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Starter cranking limits |
60 sec ON 10 sec OFF 60 sec ON 10 sec OFF 60 sec ON 5 min OFF 60 sec ON 5 min OFF Same time for any subsequent |
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ITT max temp for start |
120° ground 90° airborne |
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Minimum Oil pressure |
Idle 25 PSI Takeoff power 45 PSI |
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When do we use continuous engine ignition |
- Takeoff and landing on contaminated runway - takeoff with high crosswind (15 kts) - flight trough moderate or heavier intensity rain - flight in vicinity of thunderstorm - flight trough moderate or heavier intensity turbulence - takeoff after de-icing/anti-icing |
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Trust reversers idle range |
25% to 30% N1 |
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Minimum N1 RPM when flexing |
85.0% |
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When flex is not permitted |
- rated trust is below 85% - anti skid is inoperative - wing or cowl system is ON - runway is contaminated (with exceptions) - with windshear and down draft forcasted - wet runway (exception with wet perf data above 10°) - aerodata specified |
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Max APU EGT |
743° |
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Max APU RPM |
107% |
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Max speed when APU door position unknown |
300 KIAS APU must remain operative |
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Max pressure altitude for Takeoff and landing |
10 000 ft |
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Range of temperature for takeoff and landing |
-40°c to 50°c |
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Takeoff runway contamination |
More than 0.5 inch standing water 0.5 inch slush 1 inch wet snow 3 inch dry snow |
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Landing runway contamination |
More than .75 inch standing water .88 inch slush 1.5 inch wet snow 3.75 inch of dry snow |
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If anti skid is inoperative What restriction apply |
Prohibited on contaminated runway |
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If nose wheel steering is inoperative What restrictions apply |
Prohibited on wet or contaminated runway |
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If 1 trust reversers is inoperative What restrictions apply |
Prohibited on runway contamination with ice |
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If Automatic power reserve (APR) is inoperative What restriction apply |
Prihibited on contaminated runway |
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If electric hydraulic pump 2 (ACMP 2B) Is inoperative What restriction apply |
Prohibited on contaminated runway |
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When is a tactile inspectition for frost contaminants required |
- OAT is 10°c or less - the bulk fuel temp° is 0°c or less - atmospheric conditions ihave been conducive to frost formation |
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Maximum frost permited |
- ⅛ inch under the wind due to cold soaked fuel - light hoar frost on the upper fuselage If all vents and ports are clean (Thin enough to distinguish surface features lines lettreing marking ) |
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Max runway slope |
± 2% ± 1% for cat II/III Approach |
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Minimum runway widht Takeoff or landing |
100 ft (minimum for a U turn) |
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Max cabin altitude |
13 250 ±750 ft |
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Pax oxygen auto deploy altitude |
14 000 ft |
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If pass signs is set on auto At what altitude do the seat belts come ON |
8500 ft |
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Altitude of the CABIN ALT warning message |
10 000 ft cabin altitude |
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Max crosswind Dry and wet |
27 dry 22 wet |
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Max continuous Oil pressure |
115 PSI |
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Apu max EGT |
974 °c |
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Max head wind Cat 2 and 3 |
19 kts |
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Max crosswind Cat 2 and 3 |
15 kts on cat 2 13 kts on cat 3 |
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Max tailwind |
10 kts |
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When vib does not desapear after start |
2% split between engines
57% or less And OAT is -20°c or above Dont not Accelerate above idle |
