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124 Cards in this Set
- Front
- Back
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Max pressure alt for t/o and landing
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10000ft
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Max operating alt
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41000ft / company 37000ft
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max operating alt with 1/inop pack
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25000ft
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max ambient air temp for t/o landing
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ISA +35 C
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Min temp for t/o
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-40 C
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Max taxi/ramp weight
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53,250 lb
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MTOW
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53,000 lb
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MLW
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47,000 lb
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MZFW
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44,000 lb
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min flight weight
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30,000 lb
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max runway slope
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+/- 2% gradient
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Max tailwind
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10kt
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max x-wind comp on wet runway
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27kt
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max x-wind comp on contaminated runway
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15kt
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max demonstrated x-wind component landing/to?
Is is regulatory or limiting? |
27kt
No |
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What is visible moisture (defined as?)
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clouds
fog w/ vis <1 mile rain snow sleet ice crystals |
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When must cowl anti-ice be used on the ground?
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OAT below 10C and:
visible moisture runway has snow, ice, water, slush |
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When must wing anti-ice be used on the ground for takeoff?
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OAT below 5C and:
visible moisture runway has snow, ice, water, slush |
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Can SAT or TAT be used before takeoff?
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No, because the probes may give inaccurate readings on the ground or at low speed.
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When must anti-ice be used when type 2/4 anti-icing fluids have been applied?
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just prior to thrust increase for take-off.
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Define icing conditions in flight:
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TAT 10C or below and visible moisture, unless the temp is -40C or below.
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When must Engine cowl anti-ice must be used in flight?
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Icing conditions
ICE is annunciated |
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When must wing anti-ice be used in flight?
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ICE is annunciated
Icing conditions below 230kt |
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Vle
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250kt
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Vlo (retract gear)
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200kt
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Vlo (gear extended)
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250kt
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Vfe 8*
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215kt
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Vfe 20*
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215kt
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Vfe 30*
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185kt
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Vfe 45*
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170kt
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Max windshield wiper speed
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220 kt
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Max tire speed/ground speed
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182kt
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Target turb air penetration speed
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280kt or mach .75 (Whichever is lower)
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max speed with STAB or MACH trim INOP
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250kt or mach .7 (unless autopilot is engaged)
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If you are above 10,000ft, what is the minimum climb speed?
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250kt/.7 Mach
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What should you do if you cannot maintain 250kt/.7 and 350ft/min climb above 10,000ft?
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Immediately level off and advise ATC
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Minimum enroute cruise speed above 10,000ft
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.7 Mach or Long Range Cruise Speed (whichever is lower)
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Describe the three main gauge colors:
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Red = max/min limitations(fuck!)
Amber = Caution Green = Normal |
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Engine operating limits for start:
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N2% 20
ITT*C 900 degrees |
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Engine operating limits for idle:
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N2% do not accelerate above idle if below 57% N2
N2 split no greater than 2% |
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Max ITT's
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Accelerating: 900*C
Max continuous: 874*C |
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Normal Takeoff ITT max temps:
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884 for 5 mins
900 for 2 mins/5mins |
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Go-around or APR thrust max ITT temps:
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900 for 5 mins
928 for 2 mins/5mins |
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What must you do for the first flight of the day if the plane is cold-soaked at a temp -30 or below for +8 hours?
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motor engines for 60 secs, verify fan rotation
Reverse thrusters must be actuated until the deploy and stow cycles are less than 5 secs |
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Max oil temp continuous
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+155*C
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Max oil temp permissible
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+163*C (15 min max)
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min oil temp for starting
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-40*C
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oil pres minimum: steady state idle
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25 PSI
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oil pres minimum: take off
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45 PSI
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Max cont oil pres
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115 PSI
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oil pres: max transient after cold start
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156 PSI
130 PSI at idle, 10 min max |
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when is continuous ignition required?
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t/o & landing on contaminated runways
t/o x-wind +10kt flight thru moderate/heavy rain flight thru moderate/heavy turb flight in vicinity of thunderstorms flight at or near shaker and pusher settings |
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When must APR be verified?
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When takeoff performance is predicated on its use
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How long must engines run prior to takeoff or landing?
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2 mins
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What should you do if ITT rises above 350*C following engine shut-down?
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carry out an engine motoring cycle to reduce ITT
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Starter limits
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on ground or in-flight - cannot be used if N2 >55%
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engine start cycle times
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1st try = Max time on 1 min, followed by 10 second off
2nd try = Max time on 1 min, followed by 10 second off 3rd try = Max time on 1 min, followed by 5 min off |
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ITT limits at the initiation of thrust lever movements from SHUT-OFF to IDLE?
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ITT < 120*C for ground starts
ITT < 90*C for air starts |
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max fuel imblance?
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800lb
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Takeoff with fuel in excess of ??? pounds in the center is not allowed unless each wing tank has ???? pounds
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no more than 500lb center unless the wings are above 4400lb.
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Min fuel for go-around
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450lb per wing
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Minimum engine fuel temp for takeoff?
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5C
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Min bulk fuel temp prior to flight?
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-30C
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Fuel Cross-flow - what must be off prior to t/o?
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powered crossflow
gravity crossflow |
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Minimum temp for starting a cold-soaked APU?
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-40*C
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APU start times on bat
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1: max 30 secs on
2: max 30 secs on, wait 20 min 3: max 30 secs on 4: max 30 sec on, wait 40 mins |
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APU start times using DC ground power
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1: max 15 secs on
2: max 15 secs on, wait 20 min 3: max 15 secs on 4: max 15 sec on, wait 40 mins |
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Bleed air limits:
AC in-flight |
bleed air from APU not permitted above 15000ft
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Bleed air limits:
engine start - ground |
no bleed air extraction limit
each engine may be started using APU bleed If both engines are started via APU, the operating engine cannot exceed 70% N2 |
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Bleed air limits:
engine start during flight |
during single engine ops, APU bleed air for engine start not permitted
during double engine failure, APU bleed permitted at/below 13000ft |
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If the APU door is open you must:
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Limit to 300kt
APU must remain in operation |
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Aircon/Pressurization:
max positive dif presure |
8.7 psi
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Aircon/Pressurization:
max negative presure |
-.5 psi
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Aircon/Pressurization:
during taxi/to/landing |
.1 psi
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AC and Pres.. Max differential presures:
Max Positive Pres? |
8.7PSI
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AC and Pres.. Max differential presures:
Max negative pres? |
-.5PSI
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AC and Pres.. Max differential presures:
During takeoff and landing |
.1PSI
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Permissible loads on the AC system (Load limitation in kVA:
ALT = 0-FL350 |
Main Gens = 30kVA
APU Gen = 30 kVA |
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Permissible loads on the AC system (Load limitation in kVA:
ALT = FL350-FL370 |
Main Gens = 25kVA
APU Gen = 30 kVA |
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Permissible loads on the AC system (Load limitation in kVA:
ALT = above FL370 |
Main Gens = 25kVA
APU Gen = NA |
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Max permissible continuous load on each TRU
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100 amps
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Flaps above XXXXX feet prohibited
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15,000FT
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Flight spoilers may not be extended beyond ??? ft AGL
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300 ft AGL
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Flight spoilers may not be extended at airspeeds below the recommended approach/maneuvering speeds plus ?? KIAS:
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+ 17 KIAS
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Use of spoilers with flaps greater than ?? degrees prohibited:
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N/A with flaps greater than 30 degrees
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Upon departure from a wet or contaminated runway:
At 10,000 ft, or when SAT falls below 0*C, the ailerons must be operated manually every ???? feet until the top of climb: |
every 5000 feet
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Are both stall protection systems required for flight?
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YES
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Are thrust reversers approved for ground use only?
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YES
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Can you attempt a go-around when thrust reversers have been used during landing?
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NO, TR's only intended for full-stop landings
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Can take-off occur with any of the following error messages?
TRUST REVERSER UNLK Light REV icon N1 L/R REV UNLOCK |
only if you are suicidal
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Max reverse thrust must stop at what airspeed on the ground?
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60 KIAS, TR must be at idle
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Taxi lights must be switched off if the plane is stationary for longer than ?? minutes
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10 minutes
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Normally, the auto pilot use is prohibited at altitudes below ??? ft:
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600 FT
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Normally, the auto pilot use is prohibited at altitudes below 600 ft AGL, except under what conditions?
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visual approaches: 400ft AGL
precision approaches: 80ft AGL |
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If your DH/MDA is 92ft, what number would you dial in with the DH/MDA knob?
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100 ft. Knob works in 10' increments
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If you receive a TCAS RA, should you deviate from an ATC clearance to comply?
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YES
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If you receive a EGPWS warning, should you deviate from an ATC clearance to comply?
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YES
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What does the FIRE PUSH button do?
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Arms the following:
Squibs fuel feed SOV bleed air SOV HYD SOV EDG off |
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What is the total fuel for pressure refueling, and total usable fuel?
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14,518 lbs
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Describe the fuel capacities in each tank:
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Wings can hold 4,760 lbs each
Center tank 4998 lbs |
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When does the XFO/APU pump come on?
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+200 lb fuel imbalance
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When does the center fuel tank automatically begin transferring fuel to the wing tanks?
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Anytime the wing tanks are below 94% full
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What does the 10th stage bleed air provide?
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AC Packs
Pressurization Main engine start |
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What does the 14th stage bleed air provide?
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wing/cowl anti-ice
thrust reverse |
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What are the pressure limits for the Packs?
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30PSI if both in use
41PSI if 1 inop |
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What causes a PACK FAULT caution?
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over pressure
over temp |
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Cabin pressure controllers (CPC) are spring loaded XXXX and modulated XXXX with XXXX pressure from XXXX
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Cabin pressure controllers (CPC) are spring loaded SHUT and modulated OPEN with VACUUM pressure from 10TH STAGE BLEED
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Describe what happens when you press the PRES CONT button:
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Press 1: manual mode
Press 2: PRES CONT 2 Press 3: manual mode Press 4: PRES CONT 1 |
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What would cause a PRES CONT FAULT to appear?
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failure of both CPCs
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What happens to the CPC's 3 minutes after landing?
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The active/inactive CPC's switch
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If the aircraft is above 14250ft +/- 750 feet, the plane will maintain what pressure?
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14250ft +/- 750 feet
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Describe CPAM CABIN ALT messages, and when they occur:
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***Cabin Alt *master caution* between 8,500 and 9,999 ft. and master warning *CABIN ALT > 10,000 ft., illumination of fasten seat belts, and no smoking signs automatic when switch is selected to auto. Passenger O2 masks drop automatically at 14,000 ft.***
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What happens if an APU XFLO pump fails?
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Negative gravity relief valve supplies fuel from the right tank
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How does the APU shutdown?
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From a simulated overspeed signal
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What are the critical altitudes to know concerning the APU?
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FL370 max opp alt
FL300 max alt to start APU 13000 engine start with bleed 15000 ECS operation |
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Are both batteries required to start the APU? What is the battery minimum voltage?
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Yes. 22V
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What causes an APU shutdown in the air?
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Fire
Loss of speed signal ECU failure DC power loss overspeed |
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BITE stands for?
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Built in test equipment
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Describe the AC power system:
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115V
400 HZ 30 kVA BUS 1/2 UTIL BUS 1/2 SERV BUS ESSENTIAL BUS |
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What is the voltage of the DC power system?
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28V via the TRU's
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What would cause an IDG fault?
What would cause an IDG DISC message? |
Low oil pres
High oil temp overtemp, over torque |
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Describe the APU Battery
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43 Amp
24 Volt Powers ADG Deploy and APU start Charged by AC UTIL BUS 2 |
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Describe the main Battery
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17 Amp
24 Volt Charged by AC UTIL BUS 1 Powers 4 busses: L/R bat busses main bat bus APU bat bus DC emergency bus |
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Describe the ADG power
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AC POWER
115 V 400 HZ 15 KVA Powers: AC ESS BUS HYD PUMP 3B |
