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126 Cards in this Set
- Front
- Back
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static engine thrust
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43000 lbs
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N1 Max
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106%
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N1 idle
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17-29%
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N2 Max
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102%
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N2 Idle
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61-67%
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N1/N1 vibration range
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75-85%
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n1 icing vibration range
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67-87%
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Use anti-ice when temp C is below ___ in visible moisture.
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8
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On the ground with noted or suspected ice build ups, momentarily advance engines to ____% N__ every __ minutes.
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90, 1, 5
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Avoid prolonged flight in icing conditions below ___% N1. If required, momentarily advance each engine, individually, to at least ___ % N__ every ___ minutes above ____ ft or every ___ minutes below _____ ft.
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90, 1, 5, 15000, 6, 15000
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TRT -- TIT and max time
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940, 5 min
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MRT -- TIT and max time
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930, 30 min
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NRT -- TIT and max time
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915, continuous
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engine idle TIT guide
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370-525
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Starting TIT limits
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800-860 for 25s
> 860 for 2s |
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transient TIT limits
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940-960 for 2 min
960-970 for 30 sec |
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max reverse TIT and time
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960 for 30 sec
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Starter duty cycle
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1 min on--30 s off
1 min on--30 s off 1 min on--30 min off --- or --- 2 min on 5 min off continuous |
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max stable fuel flow prior to light off
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900 PPH
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TIT rise w/in ___ (time) of "run"
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30 sec
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N1 RPM indication by ___ (time)
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idle N2 + 5 min
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N2 RPM for air start without starter assist below 10000ft
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10%
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min oil pressure
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10 psi
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idle oil pressure guide
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10-22 psi
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80% N2 oil pressure guide
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20-30 psi
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outboard engine suction feed limits during climb
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12600 ft
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inboard engine suction feed limits during climb
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20000 ft
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outboard engine suction feed limits level
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32000 ft
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inboard engine suction feed limits level
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40000 ft
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static O2 pressure
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275-450 psi
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stabilized O2 pressure
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275-400 psi
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CG limits
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19-41%
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home station oil consumption limit
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1.1 qt/hr
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enroute mission oil consumption limit
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2.2 qt/hr
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normal hydraulic pressure
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3000 +/- 150 PSI
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hydraulic overpressure
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3400 psi
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min hydraulic pressure for NLG extension
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2500 psi
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min hydraulic pressure for 1 brake application
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1000 psi
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max pitch on rotation
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13 deg
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normal pitch on rotation
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8-10 deg
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max pitch after takeoff
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15 deg
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pitch attitude for windshear
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15-18 deg
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max pitch for rapid descent
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15 deg
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max pitch below 200 ft
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10 deg
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max bank below 200 ft
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15 deg
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max bank below 50 ft
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5 deg
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holding AOA
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3 deg
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40/100% flap approach, no slats AOA
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5 deg
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40/100% flap approach AOA
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7.2 deg
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no flap approach AOA
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7.8 deg
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flaps up stall AOA
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15 deg
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flaps down stall AOA
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18 deg
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clean max airspeed
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350 KCAS/.825M
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rapid descent max airspeed
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350 KCAS/.825M
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max taxi up to EWP weights
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30kts
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max taxi at EWP weights
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15kts
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landing lights extended max airspeed
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300KCAS/.825M
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do not operate landing lights > ___ (time) when less than fully extended
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25 min
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windshield wiper max airspeed/adequate rain clearing speed
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175 KCAS
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windshield wipers provide good rain clearing up to, but start to float above this airspeed
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150 KCAS
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max airspeed with inboard T/R extended
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350KCAS/.825M
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min airspeed with inboard T/R extended
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210KCAS
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T/R above reverse idle on ground airspeed range
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150-60 KCAS
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T/R above reverse idle on ground below ___ KCAS requires ________
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60, fan blade inspection
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max airspeed with landing gear extended
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250KCAS/.6M
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max airspeed for landing gear operation
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250KCAS/.6M
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landing gear recommended max airspeed
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200 KCAS
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NLG may not retract at airspeeds greater than ______
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225 KCAS
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(normal hydraulic pressure available) MLG may not rotate at airspeeds greater than ______
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185 KCAS
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(APU accumulator pressure only) MLG will not rotate at airspeeds greater than ______
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170 KCAS
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accel check speed tolerance
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3 kts
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rudder effective for directional control above ~ _____
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60KCAS
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elevator effective for directional control above ~ _______
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80 KCAS
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Vapp increase for ice on wing or tail
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5 KCAS
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min touchdown speed
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Vapp - 10 KCAS
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min airspeed above 10000' for air start without starter assist
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210
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RAT extension max airspeed
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350KCAS/.825M
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RAT retraction max airspeed
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180 KCAS/.45M
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RAT operation above 15000' (airspeed)
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190
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RAT operation below 15000' (airspeed)
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175
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max airspeed w/ main tank low (due to fuel mismanagement)
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280KCAS/.825M
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Main sump low max airspeed
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280KCAS/.825M
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three engine enroute climb airspeed above 650k lbs
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250KCAS/.6M
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three engine enroute climb airspeed 650k - 550k lbs
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230KCAS/.6M
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three engine enroute climb airspeed 550k - 450k lbs
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210KCAS/.6M
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three engine enroute climb airspeed below 450k lbs
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190KCAS/.6M
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two engine climb airspeed
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190KCAS/.45M
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driftdown airspeed (2/3 engines at NRT)
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250KCAS/.6M
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clean severe turbulence penetration max airspeed
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280KCAS/.825M
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recommended turbulence penetration airspeed
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240KCAS/.74
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ALDCS inop moderate/severe turbulence max airspeed
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240KCAS/.825M
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ALDCS inop light turbulence max airspeed
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300KCAS/.825M
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Yaw Aug inop airspeed range (M)
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.70-.75M
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Yaw Aug inop max altitude
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31000'
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40% flaps max airspeed
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215 KCAS
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62.5% flaps max airspeed
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195KCAS
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62.5% flaps, no slats max airspeed
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185 KCAS
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landing flaps max airspeed
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180 KCAS
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landing flaps, no slats max airspeed
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175 KCAS
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slats extended, no flaps max airspeed
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215 KCAS
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max ramp weight (non-ewp)
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772k lbs
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max takeoff weight (non-ewp)
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769k lbs
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max fuel weight (non-ewp)
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332.5k lbs
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max zero fuel weight (non-ewp)
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665k lbs
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max inflight weight (non-ewp)
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769k lbs
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max landing weight (non-ewp)
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769k lbs
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normal ramp weight (non-ewp)
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732.5k lbs
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max normal landing weight (non-ewp)
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635,850 lbs
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max VVI at touchdown below normal landing weight/fuel
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540 fpm
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max normal landing fuel weight (non-ewp)
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159,250 lbs
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max VVI at touchdown, above normal landing weight/fuel
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360 fpm
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A/R door open max airspeed
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350KCAS/.825M
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normal rendezvous airspeed
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300KCAS/.72M
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rendezvous airspeed outside 3 NM
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325 KCAS
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A/R @ 1 NM
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300KCAS/.72M
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AR KC-135 @ 1/2 NM
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270KCAS/.65M
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AR KC-135 contact
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252KCAS/.62M
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AR KC-10 @ 1/2 NM
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290KCAS/.7M
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AR KC-10 contact
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275KCAS/.66M
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Taxi NLG limit
(GW above normal ramp) ____fixed _____ castored symmetric thrust, symmetric braking |
60, 60
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Taxi NLG limit
(GW above normal ramp) ____fixed _____ castored asymmetric thrust, symmetric braking |
45, 60
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Taxi NLG limit
(GW above normal ramp) ____fixed _____ castored symmetric thrust, asymmetric braking |
45, 60
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Taxi NLG limit
(GW above normal ramp) ____fixed _____ castored asymmetric thrust, asymmetric braking |
30, 45
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max rudder deflection, airspeed below 153KCAS
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35 deg
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max rudder deflection, airspeed 153-238 KCAS
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12 deg
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max rudder deflection, airspeed above 238 KCAS
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4
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