-
Rejected take-off
- Simultaneously
- Thrust Levers...................................................... Idle
- Wheel Brakes.............................. Max until safe stop
- Thrust Reverser(s)........................ Max Consistent w/
- directional control
-
Double Engine Failure
- ignition, cont. ........................................................ON
- airspeed............................................... 240 KIAS min
-
L(R) Rev. Unlocked
Affected Thrust Lever................................ Confirm & Idle
-
Uncommanded Acceleration or Engine Overspeed Msg.
- Gnd.
- Affected Thrust Lever............................ Idle then shut off
- Flt.
- Affected Thrust Lever.............................Confirm & Idle,
- Check Engine Response
-
Stall Recovery
- Autopilot...........................................Disengage, if required
- Pitch attitude...........................Lower nose to reduce A O A
- Thrust levers.....................................Advance to Max PWR
- Roll attitude......................................................Wings Level
- Flt. Spoiler lever.........................................Select to Retract
-
Cabin Alt. or
Emergency Descent procedure
- Oxygen masks................................................DON, 100%
- Crew communication........................................ establish
-
Loss of all AC power
ADG manual deploy handle.................................... PULL
-
STAB TRIM runaway
- Control Column............. assume man. control & override
- runaway
- BOTH STAB TRIM Disc................ press, hold & release
- Airplane control........................transfer to pilot (CA) side
- STAB CH1, CH2, HSTCU cbs(2F5 & 4A1)..........OPEN
-
Loss of Braking or Excessive Assymmetry
- Wheel Brakes...................................... Release momentarily
- Anti-skid....... ...................................................................off
- Wheel brakes..................................... Re-apply as Required
-
Config. Warning
T/O ............................................. Discontinue immediately
-
Reduced Thrust T/O limits
reduced Engine "flex' Thrust T/O must
not be used:
- * if normal T/O fan speed is less than 85% N1
- * if reduced"flex" thrust value is less than 85% N1
- * Crew Confirm Availability of full thrust, checked
- once every 100 flight hours.
- * if Wing and/or Cowl Anti-icing Bleeds are on.
- * Contaminated runways w/ water, slush or snow
- * when Warnings of Windshear or Downdrafts have been forcasted.
-
FMS limits
- * FMS calculated thrust setting must not be used if the
- pressure alt. is > than 36,000/ FL 360
- * FMS approved for: en route, terminal and non-pre
- cision approach phases of flt.
-
Taxi & Ramp Weight NA
53,250
-
Structural weight limits NA
T/O
53,000
-
Structural weight limits
landing
47,000
-
Structural weight limits NA
zero fuel
44,000
-
Cowl Anti-Ice
Gnd. Operations
- * OAT is 10' c (50' F) or < and visible moisture is present
- (1 mile or <).
- * OAT is 10'c(50'f) or < when on runways, ramps &
- Taxiways with snow, ice, water or slush is present.
-
Cowl Anti-Ice
Flight ops
- * TAT of 10'C (50'F) or < and visible moisture
- (except SAT of -40'C(-40'F) and <).
- * when in icing conditions OR
- * when ICE is annunciated by IDS system.
-
Max Rotation Rate
3' per second
-
Wing Anti-Ice System
Gnd. Operations
- * must be selected ON for final taxi prior to T/O if OAT
- is 5'c(41'f) or below, unless Type II, III, or IV.
- * must be selected and confirmed ON for T/O when OAT
- is 5'c(41'f) or below and: visible moisture 400' AGL or,
- RNWY is wet or contaminated or presence of
- precipitation.
- * turn system ON prior to T.L > when Type II, III or IV
- have been applied.
-
Wing Anti-Ice System
Flight Ops
TAT of 10'C (50'F) or below w/ visible moisture (except SAT -40'C & <)
- Wing A.I.SYST ON
- *ICE annunciated by I.D.S. or
- *icing conditions below 230 KIAS
-
Thrust Reverser
MAX reverse thrust airspeed
- * During landing, max reverse is NOT permitted below
- 60 KIAS. < 60 KIAS, Thrust must be reduced to idle.
-
Tire limit speed
gnd. tire limit speed
182 KIAS gnd. speed
-
Taxi lights
taxi lights off
A/C stationary in excess of 10 minutes
-
FLAPS
Flaps prohibited
- *enroute
- *altitudes above 15,000 feet
-
Winshield wiper
V wipe
not above 220 KIAS
-
Turbulence Penetration Speed
max speed for turb. penetration
280 KIAS or .75 MACH
-
Maximum Landing Gear Operating Speeds
Extend..............250 KIAS
Retract..............200 KIAS
-
Max gear extended speed
max airspeed w/ gear down & locked
250 KIAS
-
Oil Temps
Min start
-40'C
-
Oil Temps
Max continuous
+ 155'C
-
Oil Temps
Max permissable
+ 163'C (max 15 min)
-
Fuel
Max imbalance between L/R main tanks
800 lbs inflight
-
APU door open (EICAS MSG. DOOR___)
airplane limited to 300 KIAS or
APU must remain in operation
-
OIL PRESSURE
T/O power
45 PSI min.
-
Oil pressure
max transient after cold start
156 PSI (max 130 PSI for 10 Mins)
NOTE: Engine must remain @ idle until oil pressure returns to normal range.
-
FUEL
Min Quantity for go-around
450 lbs. PER WING (A/C level) and max pitch of 10' nose up
-
BLEED AIR SYSTEMS 10th stage;
valves must be closed for T/O & Landing if:
Engine Cowl and/or Wing Anti-Ice Systems are ON.
-
Flight Spoilers
minimum altitude
300 fl. AGL
-
Flight Spoilers
@ or < FL 250
Safe Speed or V ref + 20 KIAS
-
Flight spoilers
above FL. 250
Safe Speed or Holding-Safe speed + 25 KIAS
-
Automatic Flight Control System
- prohibited below altitudes of 600 feet AGL
- (T/O)
-
Automatic Flight Control System
visual and non-precision approaches
400 feet AGL
-
Automatic Flight Control System
precision approaches
80 feet AGL
-
Max Airspeed for ADG deployment
250 KIAS (7002-7304)
Vmo/M/mo (7305 or >)
-
Flap Speeds
Vfo
0 -8'
200 KIAS
-
Flap Speeds
Vfo
8-20
200 KIAS
-
Flap Speeds
Vfo
20-30
185 KIAS
-
Flap Speeds
Vfo
30-45
170 KIAS
-
Flap Speeds
Vfe and Vfo(retraction)
8/ 8-0
230 KIAS
-
Flap Speeds
Vfe and Vfo(retraction)
20/20-8
230 KIAS
-
Flap Speeds
Vfe and Vfo(retraction)
30/30-20
185 KIAS
-
Flap Speeds
Vfe and Vfo(retraction)
45/45-30
170 KIAS
-
Fuel Loading
T/O with > than 500 lbs in Center Tank not permitted:
unless Normal Fuel Loading and each Main Tank is above 4,400 lbs.
-
Continuous Engine Ignition
- * T/O and Landings on contaminated runways.
- * T/O with high crosswind components.
- * FLT through Mod. or > rain.
- * FLT through Mod or > turbulence.
- * FLT in vicinity of thunderstorms w/lightning.
-
CF 34-3A1 Limitations
START
N2%..............................................................................20
-
CF 34-3A1 Limitations
IDLE
N2%...............................................56.5 to 68.0
engine N2 split at gnd idle pwr, not to be greater than 2% N2. If N2 is 57% or < with OAT of -20'C or colder, do not accelerate above idle.
-
CF 34-3B1 Limitations
START
N2%......................................................................20
-
CF 34-3B1 Limitations
IDLE
N2%......................................................56.5 to 68.0
- engine N2 split at gnd idle pwr, not to be greater than 2% N2. If N2 is
- 57% or < with OAT of -20'C or colder, do not accelerate above idle.
|
|
