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100 Cards in this Set
- Front
- Back
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SPEEDBRAKES
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DO NOT USE WITH GEAR EXT OR FLAPS FULL
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APU ELEC. LOAD
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100% SEA LEVEL TO 45,000FT
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FLIGHT LOADS
FLAPS O |
-1 TO 2.5G
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APU MAY BE USED FOR STARTER ASSISTED
ENG AIRSTART BELOW |
30000FT, HOWEVER ENG ONLY STARTS AT
25000FT AND BELOW |
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MAX OIL TEMP
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+160C
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MIN OIL PRESS T/O PWR
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35 PSI BELOW 72.3 HP
45 PSI ABOVE 90 HP |
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MIN OIL TEMP FOR START
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-30C
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MIN OIL PRESS CONT. FLIGHT
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25 PSI BELOW 72.3 HP
35 PSI ABOVE 90 HP |
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MIN OIL TEMP T/O PWR
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+20C
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MAX ENG FUEL TEMP 15 MIN
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+165C
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MAX ENG FUEL TEMP UNRESTR
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+140C
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MIN ENG FUEL TEMP
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-40C
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MAX FUEL TANK TEMP
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+54C
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MIN FUEL TANK TEMP
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-37C
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MAX CROSSWIND FOR START
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30 KTS
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MAX TAILWIND FOR START
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20 KTS
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MAX TGT FOR START
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700C GRN/ 850C AIRSTART
150C INITATION. |
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WHEN FUEL TANK TEMP IS AT OR BELOW
- 30C WITH LESS THAN 5000LBS REMAINNG |
THE A/C SHOULD DESCEND TO AN ALT.WHERE
TEMP IS A SAT. -60C OR WARMER AND MAINTAIN AN AIRSPEED MIN M.80 |
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MAX CONTINUOUS
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N1 101 N2 98.9 TGT 860C TIME N/A
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MAX TAKE OFF ENG PRAMITERS
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N1 101.1 N2 99.6 TGT 900C TIME 5 MIN
2ENGS 10 MIN 1 ENG |
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MAX OVERSPEED ENG
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N1 101.5 N2 99.8 TGT 905C TIME 20 SEC.
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MAX REVERSE ENG
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N1 70% TIME 30 SEC
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ENG START DUTY CYCLES
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3 CYCLES, MAX 3 MINS PER CYCLE,15 SEC BETWEEN CYCLES, AFTER 3 CYCLES, DELAY USE OF STARTER 15 MINS
STARTER RE-ENG.UP T0 42%HP RPM |
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COWL ANTI ICE ON IF
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SAT +8 OR BELOW & VISIBLE MOSISTURE
AND OR WET RUNWAY |
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max airport alt
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15000ft
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max oper alt
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51000ft
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max single pack alt
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48000ft
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internal bag door open, alt& time
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above,40000 ft for 5 min,
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int bag door open, single pack
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max 45000ft
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max yaw damper inop alt
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45000ft
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mmo
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fl 290-310 0.85m
fl320-440 0.885m fl440-510 0.86m |
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vmo below 8000ft
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300 kcas
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vmo above 8000ft
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340 kcas
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vmca
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112 kcas
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vmcg
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103 kcas at sea level
84 kcas at 15000ft 1kn per 1000ft decrease from sl to 15000ft |
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va
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206 kcas
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vb/ turb pen sp
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240 kcas below 10000ft
270 kcas/.80m above 10000ft |
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holding in ice, min speed
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160 kcas
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mach trim inop speed
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.80m
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tire speed
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195.5 kts
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max demo xwind
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28 kts
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yaw damper inop speeds
below 10000ft |
250 kcas
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yd inop above 10000ft
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260 kcas
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yd inop above 20000ft
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210 kcas min
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yd inop speed below 20000ft
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see chart aom volume 1
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max diff
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10.48
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max diff t/o & landing
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0.3 psid
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fms- min alt for autopilot coupled
imc vnav operations is |
300agl or 50ft below mda whichever is
higher |
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zero fuel
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54,500lbs
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ramp weight
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90,900lbs
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max t/o weight
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90,500lbs
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max landing weight
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75,300lbs
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max fuel inbalance
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1000lbs t/o
2000lbs flight |
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max fuel weight
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41,300lbs, heavier loads ok,if within
other limits |
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max speed 10 deg. flaps
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250kcas/.60m
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max speed 20deg. flaps
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220kcas/.60m
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max speed 39deg. flaps
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170kcas/.60m
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use of speedbrakes not allowed with
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gear down and or full flaps
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use of flaps in icing conditions limit
to |
takeoff, app ,landing
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flap setting for holding in icing cond.
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0 only
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APU MAX START TGT
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1050C
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For take-off, once on center line . .
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Use of tiller not recommended above 60 KCAS.
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Max slopes for T/O and landing?
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+2% uphill, -2% downhill.
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Stall Barrier, Stall Warning?
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Both must be operative for T/O.
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max alt flaps 39deg.and or gear
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20000ft
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max alt flaps 10 or 20 deg.
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25000ft msl
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vlo
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225 kcas/.70m
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FLIGHT LOADS
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FLAPS 10 TO 20
0 TO 2.0G UP TO MAX T/O WEIGHT |
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APU MAX RUNNING TGT
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732C
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When fuel tank temp. is less than O C all pumps must remain on. Balancing is performed?
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Through intertank valve.
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VLE
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250KCAS/.70M
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FLIGHT LOADS
FLAPS 39 |
0 TO 2.0G BELOW 75,300LBS
0 T0 1.5G ABOVE 75,300 |
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APU MAX ROTOR SPEED
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106%
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The engine will only run on suction feed, at or below?
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20,000 feet
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VLO BLOWDOWN
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175KCAS/.70M ONCE GEAR EXT 250KCAS/.70M
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MACH TRIM INOP
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.80M MAX
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apu start duty cycles a/c batterys
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3 consecutive starts,1 hour cooldown
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Above 20,000 feet, the engine will run erractic and flame out if?
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Crossfeed is not open, with at least one boost pump on.
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AUTO PILOT
T/O L/D |
200FT T/O ENGAGE
50FT DISENGAGE L/D |
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apu start,ext pwr
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3 start attempts, 15 min cooldown
between attempts ,then 1 hour cooldown |
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Takeoff
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Takeoff in Alt Control Mode prohibited
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Coupled go-around?
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Single-engine not approved.
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EICAS messages?
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Amber=do not dispatch
Blue=allows dispatch Check MEL |
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WEATHER RADAR
FROM REFULING FROM PERSONAL 21" ant from personal 18" ant |
300 FT
49 FT 33 FT |
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AUTOTHROTTLES
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AVAILABLE FROM T/O TO L/D
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Crosswind Take-off Limitations
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For Take-off with crosswinds above 20 kts., the fan speed is limited to less than 66% LP until 20 kts. has been reached. Above 20 kts. forward speed, a slam acceleration to take-off power is required. Add 600 ft to required field length when using this procedure
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Minimum flight crew?
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Pilot, co-pilot
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Max number of occupants?
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22
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Coupled go-around max alt. loss?
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60 feet
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Thrust Reversers?
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Power back is not approved.
Cancellation of Thrust Reverse to be at idle by 60KCAS. Thrust Reverse shall be deployed at least once every 100 hours. Thrust Reverese for taxi purposes is without time limited. In an emergency, T/R to stop A/C must be reported for maintenance action. |
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APU MAX ALT
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45000FT
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apu starts,consecutive
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6 starts at ten min intervals
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Single engine inop and TCAS
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Select TA only, as operating mode
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APU GUARANTEED START ALT
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39000FT
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If touch & go's are to be performed, ground spoiler switch must be?
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Off and manual spoiler landing distances must be taken into account.
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Static ground run?
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Engine operation in the band between 66% and 80% LP is prohibited.
(10 second limit-only applies to forward thrust) |
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Max number of passengers?
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19
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When HMG is used?
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Speed brakes may be used, operation is slow 3 seconds for full range.
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Continous Air-Start Ignition?
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No time limitation.
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windshield wiper speed
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max 200 kcas
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