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65 Cards in this Set
- Front
- Back
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Max 90° xw for takeoff/landing
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27 kts
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Cat II Max xw
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15 kts
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Cat II Max hw
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17 kts
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Max 90° crosswind for reduced landing minima (RVR below 2400) to runways without/inop TDZL and/or CL
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15 kts
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Max tailwind for takeoff/landing
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10 kts
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Max operating altitude
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36,000 ft
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Max taxi/ramp weight
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53,250 lbs
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Max takeoff weight
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53,000 lbs
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Max landing weight
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47,000 lbs
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Max zero fuel weight
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44,000 lbs
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Max weight in cargo compartment
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3,500 lbs
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Turbulence penetration speed
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280 KIAS/ .75 M whichever is lower
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V le
V lo (up) V lo (down) |
220 KIAS
200 KIAS 220 KIAS |
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Max speed for windshield wiper operation
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220 KIAS
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V fe
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8-230 KIAS
20-220 KIAS 30-185 KIAS 45-170 KIAS |
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V fo / V fe
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8 - 200 KIAS / 230 KIAS
20 - 200 KIAS / 220 KIAS 30 - 185 KIAS / 185 KIAS 45 - 170 KIAS / 170 KIAS |
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Max engine start temp
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900°C
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Engine to engine N2 split at ground idle power
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Not greater than 2% N2
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If N2 is 57% or less and OAT
- 20°C or warmer, thrust lever... |
Do not accelerate above idle
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Continuous ignition
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-TO/LDG contaminated runways
-TO w XW +15 kts -Flight through MOD+ rain or turbulence -Invof TS |
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Engine starter cranking limits
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1-1 min on, 10 sec off
2-1 min on, 10 sec off 3+-1 min on, 5 min off |
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Thrust lever advanced from SHUTOFF to IDLE if ... (temp) |
ITT 120°C or less for all ground starts |
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Max fuel imbalance between L and R
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All phases of flight =800 lbs
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Fuel qty (pressure fueling)
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14,518 lbs total
L,R=4,760 lbs C= 4,998 lbs |
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C fuel tank takeoff limit
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500 lbs if each wing tank is below 4,400 lbs
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Fuel XFLOW TO setting
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Powered and gravity
XFLOW = off for takeoff |
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APU starter limits (on battery)
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1-30 sec on, 2 min off
2-30 sec on, 20 min off 3-30 sec on, 2 min off 4-30 sec on, 40 min off |
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APU starter limits (DC ground power)
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1- 15 sec on, 2 min off
2- 15 sec on, 20 min off 3- 15 sec on, 2 min off 4-15 sec on, 40 min off |
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APU 2 min starting delay for :
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Cooling of starter and start contractor and APU fuel drainage
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APU max starting altitude
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30,000 ft
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APU max operating altitude
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36,000 ft
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APU bleed air for A/C (max altitude)
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Not above 15,000 ft
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Slats/flaps max altitude
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15,000 ft
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RVSM req. Equip.
Must be operational prior to entering |
Autopilot
Altitude alert system (1) altitude reporting xpdr (2) ADC s |
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AFCS use of SPEED MODE (DES or IAS)
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FD or AP coupled, during app not permitted
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Min Altitude flight spoilers
Min Speed |
1,000 ft agl
App speed + 17 KIAS |
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Taxi lights time
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OFF if stationary over 10 min
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APU bleed air for engine start on ground
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If starting both with APU bleed air: operating engine thrust must not exceed 70% N2
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Wing Anti-Ice ON
(takeoff and flight) |
-when ICE annunciated by IDS or
-when icing conditions exist and speed less than 230 KIAS except when inflight SAT is -40°C or below |
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WING ICING conditions
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OAT 5°C/TAT 10°C or below and visible moisture in flight or below 400' agl for takeoff or surfaces wet/contaminated
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COWL ICING conditions
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OAT/TAT = 10°C or below and visible moisture in flight or below 400'agl for ground ops or surfaces wet/contaminated
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Cowl Anti-Ice ON
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-when ICE annunciated by IDS or
-All ground and flight ops when icing conditions exist except when inflight SAT is -40°C or below |
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Wing Anti-Ice ON
(prior to takeoff) |
For final 2 min prior to takeoff for all ground ops OAT 5°C or below unless Type III or IV anti-icing fluid has been applied
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Engine Indications
Red Amber Green |
Max/min
Caution range Normal operating range |
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Min brake cooling time
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15 min + all BTMS green and not increasing
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Thrust reversers
(%N1,speed) |
+60% N1 = not below 75 KIAS
Below 60 KIAS = idle (below 30% N1) |
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Permissible DC electrical system loads
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Max time DC ground power only = 5 min (to protect CRT displays)
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AFCS below 600' agl
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Not permitted except:
1 - visual/non-precision = 400' agl 2 - precision app = 80' agl 3 - Cat II app = engaged |
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RVSM max cruise speed
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.82 M
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APU door open/unknown speed
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Max 300 KIAS or APU must stay on
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Braking Loss / Asymmetry
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1- brakes - release momentarily
2- PM - select ANTI-SKID to OFF 3- brakes - re-apply 4- reverse thrust - apply max |
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Cabin ALT msg/Emergency Descent
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1- oxygen masks - don and 100%
2- crew comm. - establish 3- captain assumes PF 4- PASS SIGNS - ON 5- ATC - declare emrg/advise descent 6- autopilot - recommended 7- altitude preselector - 10,000 or lowest safe altitude 8- SPEED mode - select 9- thrust lever - idle 10- Flight spoiler - max deploy *Imm Action Items complete - go to page 5-1 |
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Double Engine Failure
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1-CONT IGNITION - ON
2- airspeed - 240 KIAS min 3- engine instruments - monitor N1,N2,ITT 4- thrust reversers (both) - confirm and SHUTOFF 5- ADG manual deploy handle - Pull 6- STAB TRIM CH2 - engage *maintain speed until ready to restart engines. Increase speed to maintain at least 4% N2 for successful relight. Imm Action Items complete - go to page 2-1 |
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Smoke / fumes
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1- oxygen masks - don and 100%
2- crew comm - establish Imm Action Items complete - go to page 1-1 |
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STAB TRIM RUNAWAY
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1- control wheel - assume manual control and override runaway
2- both STAB TRIM DISCs - push, hold, and release 3- captain assumes PF 4- STAB CH1 - open 5- STAB CH2 - open Imm Action Items complete - go to page 9-1 |
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Max Pressure Altitude for takeoff and landing
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8,000'
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Min ambient Temp for Takeoff
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-40°C
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Do not hold in icing conditions with
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Slats and/or flaps extended
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Continued operations in areas where SLD icing conditions exist
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Is prohibited
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All contaminated performance data...
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will be for STATIC takeoffs
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Max ITT for air start =
Max ITT for ground start = |
90°C
120°C |
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Tactile check - when, why, how
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-OAT 5°C or less, wing fuel temp 0°C or less, or atmospheric conditions conducive to frost.
-determine the wing is free from frost, ice, snow, or slush -touching the surfaces |
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With cargo; must be within__minutes of suitable airport
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45 min
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Oil pressure - steady state idle =
. . . . . . . - takeoff power = |
25 psi
45 psi |
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Minimum oil temp for engine starting
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-40°C
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