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93 Cards in this Set
- Front
- Back
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Max number of PAX
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19
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Definition of a contaminated runway
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25 percent of the runway has to be covered by 0.125 of rain, snow or sleet
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Max runway slopes
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Plus 2 percent uphill and minus 2 percent downhill
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Max tailwind for takeoff and landing
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10 kts
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Take off min RVR
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2000ft or 600 meters
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Approach dh or da shall not be lower than
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300ft above touchdown zone elevation—unless equipped with HUD
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Types of operation permitted
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Land, Instrument, night, Cat 1, known Icing, /E /G ops, extended overwater, RNP 10,
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Max Operating Altitude
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45000 feet
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Max Op Alt yaw damper inop and failed Mach trim
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41000 feet
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Max Vlo and Vle Altitude
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20000 feet
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Max Alt for Landing flaps 39 degrees
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20000 feet
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Max Alt for 10 or 20 degrees flaps
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25000 feet
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Vmca
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106 kts
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Vmcl
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99 kts
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Vmcg
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109 kts
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Va
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206kts
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Flaps Extended Speeds
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10 deg 250 kts, 20 deg 220 kts, 39 deg 180 kts
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Vle
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250 kts doors opened or closed
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Vlo
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225 kts
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Vlo Alternate Extension
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175 kts
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Vmo
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Check Altitude/Mach Envelope Chart 28000-.84 43500-.88 45000-.874
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Min Yaw Damper Inop Speed
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Above 20000-210kts Below 20000-Check Chart depends on amount of fuel
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Max Mach Trim/Elec Trim Inop Speed
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.75 Mach
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Turbulence Penetration Speed
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Above 10000-270kts or .75 whichever is less below 10000-240kts
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Max Tire Speed
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195kts
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Max Emergency Stabilizer Speed
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With the Emer Stab Trim armed, autopilot engaged and jammed elevator 270kts/.75
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Max Flight load Acceleration Flaps Up
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-1 to 2.5Gs for all weights up to Max Takeoff Wt
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Max Flight Load Acceleration Flaps 10 or 20 degrees
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0 to 2.0Gs for all weights up to Max Takeoff Wt
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Max Flight Load Acceleration Flaps 39 degrees
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up to Max Landing Wt-0 to 2.0Gs Above Max Landing Wt-0 to 1.5Gs
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Max Zero Fuel Wt
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49000lbs
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Max Ramp Wt
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74300lbs
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Max Takeoff Wt
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73900lbs
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Max Landing Wt
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66000lbs
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Max Fuel Imbalance
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Check Chart Between 400 and 2000lbs depending on Airplane Gross Wt
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Fuel Balancing CAUTION
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Eng will only run on suction fuel below 20000, above 20000 the eng wil run eraratically and flame out if the crossflow is not open with one boost pump on
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Balancing fuel with intertank valve
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Sideslip, adjusting the rudder trim in the direction of the heavy tank will create a wing down condition and allow fuel to flow to light tank
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Hydraulic Fluid
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Skydrol LD-4 Preferred, Alternates Skydrol 500b-4 Hyjet IV-A
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Engine Fuel Grades
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Jet A, Jet A-1, JP-8
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Anti Icing additive
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EGME Max .15 volume conforming to the following standards MIL-I-85470, S-1745, AIR 3652, AL-41
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Static Dissapator Type
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Shell ASA 3, 2mg/liter
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Anti-Microbiological Additive
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Biobor JF 270 parts per million non-continuous basis, 135 parts per million continuous only pre-mixed in storage
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Engine and APU Oil Grades
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Aeroshell Turbine Oil
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Mach Trim must be on during
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All operations except as provided for in Section 05-02-40, Mach Trim Failure
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Max Mach Trim Inop Mach
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.75
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Is single engine coupled Go-Around approved
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NO
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Min Autopilot Engaged Altitude
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200ft
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Min Autopilot Disengage Altitude
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60ft on Ils/mls, 50ft below mda/da from an lnav/vnav approach
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Max demonstrated Alt loss Coupled go-around
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60ft
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Category limitation for coupled, flight dir app
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CAT 1
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Is use of autothrottle during SE Approaches
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NO
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Do you need both stall warning/barrier working
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No, not if you have an MEL that allows dispatch with one inop
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Must stall warning/barrier be on at all times
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Yes, unless required to be selected off for procedural reasons
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Speed Brakes with flaps full or landing gear
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NO
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Automatic Ground Spoilers Inop
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TO is permitted provided anti-skid is operative, 20 deg flaps are used, and the cowl and wing anti-ice systems are not used, only per MEL
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Max Usable Fuel
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left and right tank 14750 or 2185 gallons each, totals 29500 or 4370 gallons for both
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Do all boost pumps need to be on
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YES, unless balancing fuel
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Fuel Tank Temps
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Max +54C or greater will cause a red Fuel Tank Temp msg, Min -35C to -36C Cause amber msg, -37C Red msg
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Icing Conditions Exists When
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SAT is 8C or less and visible moisture
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When is Wing Anti-Ice activated
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If icing conditions are imminent or immediately upon detection of ice formation
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When is Cowl Anti-ice used on ground and TO
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SAT is +8c or less and visible moisture, taxi or holding on grnd at low power at less than +1 engine ops of 85% for two secs not more than 60 secs
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When is Cowl Anti-ice used inflight
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When temp range chart indicates use, or visible moisture and less than +8 degrees
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When is Automatic Anti-Ice inhibited
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Above 35000ft
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Is Electronic Checklist approved
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Yes
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Is T.O. allowed with Anti-Skid Inop
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YES, if runway is dry, Ground Spoilers are operative, Flaps 20 and the cowl and wing anti-ice systems are not used. Dispatch with ref to MMEL
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Can Airborne wx be on during fueling
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NO, and not within 300ft of other fueling ops
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Can Airborne wx be operated on ground
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Not within 49ft of ground personnel
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When is FMS Navigation approved
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Above 89 degrees north or south
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FMS approaches approved
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RNAV(GPS), RNAV(RNP), VOR, VOR/DME, VOR/DME RNAV, NDB, GPS AND TACAN with SAAR, see 01-34-30
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What are Amber CAS Messages
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Do Not Dispatch, See MEL for dispatch instructions
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What are Blue CAS Messages
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Allow dispatch as the systems that generate these messages are fault tolerant. To dispatch with amber or blue msg, see MEL
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When can the APU be operated
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On the ground, during takeoff, inflight and during landing
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APU Max EGT during Start
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973c
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APU Max EGT while running
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746c
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APU Max Continuous
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655c
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APU Max Rotor Speed
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107c
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How many APU starts on Batteries
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3 consecutive starts, after that you have to wait 1 hour before trying again
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How many APU starts on GPU
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3 consecutive starts, with 15 minutes between start attempts, then you have to wait 1hour
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Max APU operating Altitude
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37000 feet
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Can APU deliver 100% of ship power
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Yes up to 37000 feet
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What APU limitation Between 30000 to 37000
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APU cannot be loaded more than 85%
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Max Engine TGT for Start
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700c
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Max Engine TGT for Inflight Start
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780c
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Max Powerplant Takeoff Limitations
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LP 95.5%, HP 100.6%, Max TGT 800c, Max 5 minutes
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Max Continuous Powerplant limits
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LP 95.5%, HP 97.5%, Max TGT 715c, No Time Limit
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Max Powerplant Overspeed
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LP 96.5%, HP 101.6%, 20 Second Time Limit
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Max Powerplant Overtemperature
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Max TGT 820c, 20 Second Time Limit
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Max Powerplant Reverse Thrust
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LP 65.0%, 30 Second Time Limit
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Max crosswind for ground start
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25 knots
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Max tailwind for ground start
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25 knots
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Max Powerplant fuel Temp
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-40c
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Min Powerplant fuel Temp
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+95c
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Max Transient Temp and Time Limit
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+130c, 15minutes
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Max Fuel Tank Temp
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+54c
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