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max ramp wt
75,250
max to wt
75,000
max landing wt
67,000
max zfw
62,300
min flt wt
42,000
min operating empty wt
39,835
max airport pressure altitude for to and landing
8000 ft
max operating alt
41,000 ft
max ambience air temp for to and landing
isa + 35
min ambient temp for to
-40
cowl anti ice ground ops
system must be on when oat is 10c or below and visible moisture is present or operating on contaminated surfaces.
cowl anti ice flight ops
in icing conditions or ICE annunciation by ice detection system.
wing anti ice ground ops
on for to when oat is 5c and below and visible moisture is present or contaminated surface. when type 4 is used, turn on just prior to thrust increase for to.
wing anti ice flight ops
on in flight when oat is 10c and below except below -40c when visible moisture is present below 230 kts or ICE annunciation. note- do not hold in icing conditions with slats/flaps extended.
to with frost adhering to:
-upper surface of the fuselage if it is possible to distinguish surface features.
-max 1/8\" layer on underside of wing caused by cold soaked fuel.
max runway slope
+/- 2%
max tailwind component
10 kts
min flight crew
one pilot and one copilot
cargo
flight must be within 60 minutes of suitable airport if cargo is carried in the cargo compartment.
engines
cf34-8c5b1
engine warm up
-must remain at idle until oil pressure reaches normal range.
-during all starts, do not exceed 75% N1 for 2 minutes after start or until all operating indications are in the normal range, whichever is longer.
thrust mgmt data
with engines running and bleeds configured for to, crew must verify Target N1 values correspond to the data presented in the charts +/- 1%
airplane cold soak
before ffod when a/c is cold soaked at an ambient temp of -30c or less for more than 8 hrs:
engines must be motored 60 seconds and fan rotation verified before start is initiated.
-thrust reversers must be actuated until deploy and stow cycles are 2 seconds or less.
continuous ignition
must be used during:
-to and landings on contaminated runways
-moderate or heavier rain
-moderate or greater turbulence
-flight in vicinity of thunderstorms
starter must not be used above _____N2
45%
initiation of thrust lever movement from shut off to idle (ITT)
120c or less on ground
90c or less in flight
engine starter limits ground.
start 1&2 90 on 10 off
starts 3-5 90 on 5 min off
engine start or motoring in flight
start 1 120 on 10 off
starts 2-5 60 on 5 min off
starter motoring on ground
motor 1 90 on 5 min off
motor 2-5 30 on 5 min off
fuel imbalance
300 for to
800 all other phases of flight
fuel qty
pressure
l and r, 7492 each
center 4610
total 19,594

gravity
l and r 7290 each
total 14580
min fuel for go around
600 each wing tank
center tank limitation
max 500 in center tank unless each wing rank art is above 4400 of consult AFM for additional requirements
min fuel temps
to engine fuel temp min 5c
to bulk fuel temp min -30c
in flight -40c
fuel crossflow
powered and gravity crossflow must be off for to
oil consumption
max .05 gal/hr
engine oil checks
-max duration without servicing is 36 operating hrs.
-in excess of 36 hrs without oil tank servicing, level must be checked within 3 mins to 2 hrs after shutdown.
oil replenishment
-if req\'d, should be replenished within 15 mins to 2 hrs after shutdown.
-max 2 qts refill without dry motoring
-engine must be dry motored if serviced outside replenishment period.
APU
allied signal RE 220
APU start min temp cold soaked
-40c
APU starter limits
-3 start cycles per hour
-2 minute delay between cranking attempts to allow for cooling of starter, starter contactor and APU fuel drainage
APU operating range limits
max rpm 106%
max egt 1038c
APU bleed air
-max 25,000 feet for extraction
max 21000 for engine start
APU generator
max load 40kva
max altitude for APU start
37,000
max APU operating altitude
41,000
max cruise mach in rvsm
.83
Vfe flaps 1,8,20
230
Vfe flaps 30
185
Vfe flaps 45
170
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