Limits and immediate action items test Flashcards
Max takeoff weight
53000
maximum taxi and ramp weight
53250
Max landing weight
47000
Max zero fuel weight
44000
Max pressure alt for takeoff and landing
8,000
Max operating altitude
36000
Min ambient temp for takeoff
-40c
Definition of icing conditions for COWL
cowl icing conditions exist when:
OAT on the ground and for takeoff or the TAT inflight is 10C or below and visible moisture is present in flight
below 400 feet AGL for ground ops
when operating on surface that are wet or contaminated
Cowl A\I must be on when
Cowl A/I Must be on for:
all ground and flight ops when icing conditions exist
when ice is annunciated by the ICE detect system
except when the inflight SAT is -40 or below
Wing Anti Ice conditions
wing Icing conditions exist when:
OAT is 5C or less or tat in flight is 10 C or below and visible moisture is preset
in flight or below 400ft AGL for takeoff
the runway is wet or contaminated
Wing A/I must be on:
Wing anti-ice must be on:
>takeoff and flight operations when ice is annunciated
>when icing conditions exist at less than 230 kias unless inflight SAT is >-40c or below.
>Must be ON during final 2 mins before takeoff unless type 4 anti ice fluid has been applied.
Tactile Check when why and how
Tactile check is needed when
OAT is 5c or less or wing fuel temp is 0C or less
atmospheric conditions have been conducive to frost formation.
Ice and frost may continue to adhere to wing surfaces for some time even at air temps above 5c
Check leading edge, wing forward upper surface, and wing rear/upper surface during external walk around inspection
Do not hold in icing conditions with ____ and or ____ extended
slats /flaps
Continued operation in areas where SLD icing conditions exist is _____
Prohibited
All contaminated performance data will be for ______ takeoffs
Static
Maximum tailwind for takeoff and landing ___
10kts
Maximum crosswind for takeoff and landing___
27kts
Max 90 degree xwind for landing from a cat II approach ___
15 kts
Max headwind for cat II approach ___
17kts
Max weight in cargo compartment ___
3500
flights must be within__minutes of a suitable airport with cargo in the cargo compartment
45 minutes
Eicas limit markings
RED- min and max limits
Amber- Caution range
Green- normal operating range
Max itt for start
900C
Max n2 split at idle
2%
Max itt allowed to advance the thrust levers to idle for all ground starts
120
Oil pressure steady state idle
25 psi
Oil pressure takeoff power
45 psi
Min oil temp for engine starting
-40C
during all starts do not exceed ___N1 for ___minutes after start or until all operating indications are in the normal range whichever is ___
75% 2min Longer
operate engines at or near idle for ____ minutes prior to shutdown
2
Airplane cold soak Defined
Before first flight of the day has set out in -30C or below for more than 8 hours
Cold soak operation requirements
Motor engines for 60 seconds and fan rotation must be verified thrust reversers must be actuated until the deploy and stow cycles are 5 seconds or less
Continuous ignition must be used during: (5 things)
1- takeoff and landing on contaminated runways
2- takeoff with high crosswind components 15kts or greater
3- flight through moderate or heavier intensity rain
4- flight through moderate or heavier intensity turbulence
5- flight in the vicinity of thunderstorms
Starter Cranking limits
Start Max time on time off
1 1 min 10s
2 1 min 10s
3+ 1 min 5min off
Dry motoring cycle for engines
Start Max time on followed by
1 90 seconds 5 min off
2+ 30 seconds 5 min off
Max fuel imbalance between the left and right wing tank ______
450
Max total fuel for Pressure refueling
14518 lbs
Takeoff with fuel load in excess of _____ in the center tank is not permitted unless each wing tank is above ____
500lbs, 4400 lbs
Powered crossflow and gravity crossflow must be____ _____ for takeoff
selected off
Takeoff with the engine fuel temperature indications below ____ is prohibited
5C
Minimum fuel quantity for a go around per wing tank assuming 10 degrees pitch up
450
APU start on battery
Start Max time on Off
1 30s 2 min
2 30s 20 min
3 30s 2 min
4 30s 40 min
APU start on DC ground power
Start Max time on followed by
1 15s 2 min
2 15s 20 min
3 15s 2 min
4 15s 40 min
APU max starting altitude
30,000
APU Max operating altitude
36,000
Max apu RPM
107%
With the APU door not closed or the door position unknown, the airplane must be limited to _______ or _______
300 kias or apu remain operational
Max bleed air extraction for air conditioning from the APU is ____
15,000ft
Max engine start altitude with APU bleed air
13,000 ft
Min engine oil pressure for takeoff
45PSI
Flaps 8 VFE/VFO
230/200
Flaps 20 VFE/VFO
220/200
Flaps 30
185
Flaps 45
170
VLE
220
landing gear down and locked
220
Gear Up
200
Max tire speed
182
Max airspeed for windshield wiper operation failed in the non parked position
220
Max turbulence penetration speed
280/.75
Max cruise mach in RVSM airspace
.82M
RVSM equipment List
Autopilot- must be operational
Altitude alerting system- must be operational
Altitude reporting transponder (2) -one must be operational
Air data computers (2) - two must be operational
Minimum autopilot engagement altitude_____ except when performing non precision approach_______ or precision approach
600/400/80 AGL
Max slats/ flaps extension altitude _____
15,000
Max permissible time on the ground with only DC power
5Min
Min alt for flight spoiler deployment
1000ft
Min airspeed for flight spoiler use
Reft +17kts
Min brake cooling time
15 min and all BTMS green and not increasing
During landing application of thrust reverse above_____ is not permitted at airspeeds below _____. Below _____ reverse thrust must be reduced to idle not above____.
60%N1
75kts
60kts
30%N1
use of the EMER DEPRESS switch above ______ is prohibited
15000
Max altitude for singe pack ops
25000
Max differential pressure for taxi takeoff and landing
0.1
Max relief diff pressure
8.7
Braking loss/asymmetry
Wheel brakes….. release momentarily
PM will select anti-skid to off
Wheel brakes…. re-apply as required
Reverse thrust…. apply maximum until stopping assured
Cabin alt
oxygen masks…… Don and 100%
Crew communication…… establish
Captain assumes PF duties
Double Engine Failure
Cont ignition …. on
Airspeed 240 kias minimum
Smoke/fumes
oxygen masks Don and 100%
Crew Communication Establish
Stab Trim Runaway
Control wheel assume manual control and override runaway
Both stab trim discs… push hold and release
Captain assumes pf duties
Stab ch1 cb 2f5 … open
stab ch2 cb 4a1… open
