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61 Cards in this Set
- Front
- Back
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Max TO/Landing Altitude
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10,000 Ft
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Min TO/Landing Altitude
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-1,000Ft
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Takeoff Min Temp
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-40 deg C
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Takeoff Max Temp (-1,000 to sea level)
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+50 deg C
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Takeoff Max (sea level to 10,000ft)
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ISA +35 deg C
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Enroute Max Temp (sea level to 10,000 ft)
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ISA +35 deg C
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Enroute Max Temp (above 10,000 to 41,000 ft)
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ISA +30 deg C
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Flaps 8
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200/230
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Flaps 20
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200/230
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Flaps 30
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185/185
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Flaps 45
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170/170
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Landing gear extension/retraction max speeds
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Ext 250
Ret 200 |
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Turbulence Penetration Speed
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280 KIAS or .75 mach
Whichever is most restrictive |
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Tire limit speed
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182 kts
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Max windshield wiper speed
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220 kias
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Crosswind Limits
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Dry.................................27
Wet................................24 Snow/ice.........................15 |
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Max Depths for Contaminated Runway
TO and Landing |
TO LAND
water .5 .75 slush .5 .88 wet snow 1.0 1.5 dry snow 3.0 |
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Flap Failure AD
Take off alternate criteria |
>Terrain and wx must allow a min flight alt not to exceed 15000 feet.
>Fuel to land with 1000 lbs >At least 6000 ft runway >IFR approach (if wx there will be IFR) |
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Cargo Limitation
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Flight must be within 45 minutes of a suitable airport, if cargo carried in cargo compartment
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Tactile check during preflight required when?
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OAT 5 deg C or less
or Wing fuel temp 0 deg C or less or Atmosphere conducive to frost |
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Max/Min differential pressure
During taxi, TO and landing? |
8.7 psi
-0.5 0.1 |
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Auto Pilot Engagement Altitudes
TO Visual App Nonprecision Precision (ILS) |
TO.....................600
Vis App..............400 Nonprec..............400 Precision.............50 feet below DH |
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APU EGT TEMP LIMIT
APU RPM % LIMIT APU EGT START LIMIT |
743
107 974 |
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Bleed air extraction from the APU is not permitted above?
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15000 ft MSL
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APU bleed air for double engine failure start max altitude
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13000 ft MSL
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Maximum load on APU generator in flight
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30kVA
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Max altitude for starting APU
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FL300
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MINIMUM TEMP FOR STARTING COLD SOAKED APU ON GROUND
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-40 DEG C
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APU START CYCLES (GPU/BATT)
1 2 3 4 |
GPU/BATT
15SEC/30SEC 2MIN OFF 15/30 20 MIN OFF 15/30 2 MIN OFF 15/30 AT LEAST 40 MIN |
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BLEED AIR RESCTRICTIONS FOR T/O AND LANDING WITH ANTI ICE ON
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10TH STAGE BLEED MUST BE CLOSED FOR T/O AND LANDING
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LOAD LIMITATION FOR GEN
0-FL350 FL350-FL370 ABOVE FL370 |
30
25 25 |
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MAXIMUM CONTINUOUS LOAD ON EACH TRU
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100 AMPS
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MAX TIME FOR GROUND OPERATIONS WITH DC POWER ONLY
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5 MINUTES
(CRT COOLING) |
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FLIGHT WITH FLAPS EXTENDED AT ALTITUDES ABOVE __________ IS PROHIBITED
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15000 FT
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FLIGHT SPOILERS MUST NOT BE EXTENDED IN FLIGHT BELOW...
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1000 FT AGL
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FLIGHT SPOILERS MIN AIRSPEED FOR USE
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Vref +5
Vref +10 +17 |
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STALL PROTECTION TEST AND SWITCHES
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TEST BEFORE 1ST FLIGHT EACH DAY
SWITCHES MUST BE ON FOR ALL PHASES OF FLIGHT |
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FUEL QUANTITIES
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L C R
4760 4998 4760 |
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CENTER FUEL TANK LIMITATION
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T/O WITH >500 LBS CENTER TANK NOT PERMITTED UNLESS EACH MAIN WING TANK IS ABOVE 4400 LBS
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MINIMUM FUEL FOR GO AROUND
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450 LBS PER WING
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MAX FUEL IMBALANCE
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800 LBS
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T/O WITH ENGINE FULE TEMP BELOW ____ IS PROHIBITED
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5 DEG C
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MIN BULK FUEL TEMP
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-40 DEG C
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AUTO AND GRAVITY CROSSFLOW MUST BE _____ FOR T/O
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OFF
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INFLIGHT ICING CONDITONS EXIST WHEN?
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TAT OF 10 DEG C TO -39 DEG C
WITH VISIBLE MOISTURE |
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ICING CONDITIONS EXIST ON THE GROUND WHEN?
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>OAT 5 DEG C OR BELOW
>MOISTURE BELOW 400 FT AGL >WET/CONTAMINATED RUNWAY >ANY PRECIP |
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WING ANTI ICE MUST BE ON FOR TAKE OFF WHEN?
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>OAT 5 DEG C OR BELOW
>VIS MOISTURE >MOISTURE BELOW 400 FT AGL >ANY PRECIP |
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GROUND ANTI ICE MUST BE ON WHEN?
GROUND? FLIGHT? |
OAT 10 DEG C OR BELOW
VIS MOISTURE CONTAMINATED SURFACES WHEN IN ICE COND OR ICE ANNUNCIATED |
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WING ANTI ICE MUST BE ON IN FLIGHT WHEN ICE ANNUN ON AND AIRSPEED IS LESS THAN _____
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230KTS
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ITT AND ANTI ICE ON: WHEN SELECTING ANTI ICE ON, THRUST SHOULD BE REDUCED TO BRING ITT BELOW ______
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840 DEG C
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MAX OIL CONSUMPTION ON EACH ENGINE:
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.05 GAL PER HOUR
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ENGINE TYPE
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GENERAL ELECTRIC
CF34-3B1 |
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MAX CONT THRUST ITT
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RED 874-900 (>874 FOR 30 SEC)
AMBER 874-900 GREEN 0-874 |
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MAX TRANSIENT OIL PRESSURE AFTER COLD START
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156 PSI
130 PSI AT IDLE FOR 10 MIN MAXIMUM *engine must remain at idle until oil pressure returns to normal |
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MAX N2 SPLIT
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ON GROUND, IDLE THRUST
NOT GREATER THAN 2% *If N2 is 57% or less with an OAT of -20C or greater, remain at idle thrust |
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COLD SOAKED ENGINE START
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Before 1st flight of day, with temp -30C or below for MORE than 8 hours
>N1 rotation must be verified before introducing fuel >T/R must be cycled until deploy & stow cycles less than 5 seconds |
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CONTINUOUS IGNITION
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TO AND LAND ON CONTAMINATED RUNWAYS
TO WITH XWIND OVER 15 KTS HEAVY RAIN TURBULENCE VICINITY OF THUNDERSTORMS |
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HYD PUMP SWITCH AD
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PUMP 3B MUST BE SELECTED ON NO AUTO FOR ALL PHASES OF FLIGHT
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START CYCLE
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TBD
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DRY MOTOR CRANKING LIMITS
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TBD
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T/L MOVEMENT FROM SHUT OFF TO DIEL FOR START (ITT)
GROUND AIR |
120C OR LESS
90C OR LESS |
