Limitations and Immediate Action Items Test Flashcards
Maximum Taxi and Ramp Weight
53,250 lbs
Maximum Takeoff Weight
53,000 lbs
Maximum Landing Weight
47,000 lbs
Maximum Zero Fuel Weight
44,000 lbs
Minimum Operating Weight Empty
25,480 lbs
Maximum Pressure Altitude for takeoff and landing
8,000 ft
Maximum Operating Altitude
36,000 ft
Minimum Ambient Temperature for Takeoff
-40°C
Definition of Icing Conditions COWL
Icing Conditions exist when the OAT (on the ground and for takeoff) or TAT (inflight) is 10°C or
below, and:
• Visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet, or ice crystals), is present in flight, or below
400 feet AGL for ground operations, or
• When operating on surfaces that are wet or contaminated.
When must COWL anti-ice be on
Cowl Anti-Ice must be ON for all ground and flight operations when icing conditions exist except when the inflight SAT
is -40°C or below, or ICE is annunciated by the ice detection system.
Definition of Icing Conditions WING
Icing conditions exist when the OAT (takeoff) is 5°C or TAT (inflight) is 10°C or below, and:
• Visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet or ice crystals) is present in flight, or below
400 feet AGL for takeoff, or
• The runway is wet or contaminated.
When must WING anti-ice be on
Wing Anti-Ice must be ON for takeoff and flight operations when ICE is annunciated by the ice detection system, or
when icing conditions exist and the airspeed is less than 230 KIAS except when the inflight SAT is -40°C or below. In addition, Wing Anti-Ice must be ON for the final two minutes prior to takeoff during all ground operations 5°C
OAT or below unless Type III or IV anti-icing fluid has been applied.
Tactile Check - When-Why-How
OAT is 5°C or less or wing fuel temperature is 0°C or less or the atmospheric conditions have been conducive to frost formation.
Ice and frost may continue to adhere to wing surfaces for some time at OAT above 5°C
Tactile check wing leading edge, wing forward upper surface, wing rear upper surface
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
10 kts
Maximum Crosswind for takeoff and landing
27 kts
Maximum 90 degree Crosswind for landing from a Category II approach
15 kts
Maximum headwind for landing from a Category II Approach
17 kts
Maximum weight in the cargo compartment
3,500 lbs
Flights must be within _______ minutes of a suitable airport with cargo in the cargo compartment
45
EICAS Limit Markings Red/Amber/Green
Maximum and Minimum Limitations/Caution Range/Normal Operating Range
Maximum ITT for start
900°C
Maximum N2 split at idle
2%N2
Maximum ITT for all air starts
90°C
Maximum ITT allowed to advance the thrust levers to idle for all ground starts
120°C
Oil pressure Steady-state idle
25 PSI minimum
Oil pressure Takeoff Power
45 PSI minimum
Minimum oil temperature for engine starting
-40°C
During ALL starts, do not exceed ________N1 for _______ minutes after start, or until all operating indications are in the normal range, whichever is _________
75%/2/longer
Operate engines at or near idle for ______ minutes prior to shutdown
2
Airplane Cold Soak Define:
Before the first flight of the day, when the airplane is cold soaked at an ambient temperature of -30°C or below for more than 8 hours
Airplane Cold Soak Operational
The engines must be dry motored for 60 seconds and fan rotation must be verified before an engine start is initiated.
Thrust revers must be actuated until deploy and stow cycles are less than 5 seconds
Continues ignition must be used during:
Takeoff and landing on contaminated runways
Takeoffs with high crosswinds (15 kts or greater)
Flight through moderate or heavier precipitation
Flight through moderate or heavier turbulence
Flight in the vicinity of thunderstorms
Starter cranking limits
1 min/10 sec, 1 min/10 sec, 1 min/5 min
Dry Motor Cycle for engines
90 sec/5 min, 30 sec/5 min
Maximum fuel imbalance between the left and right wing tank
800 lbs
Maximum total fuel for pressure refueling
14,518 lbs
Takeoff with a fuel load in excess of ______ in the center tank is not permitted unless each wing tank is above ________
500 lbs / 4,400 lbs
Powered Crossflow and gravity crossflow must be ______ for takeoff
Off
Takeoff with engine fuel temperature indications below ______ is prohibited
5°C
Minimum Fuel Quantity for a go-around per wing tank, assuming 10 degrees pitch up _________
450 lbs
APU start (on battery)
30 sec/2 min, 30 sec/20 min, 30 sec/2 min, 30 sec/40 min
APU start (on DC ground power)
15 sec/2min, 15 sec/20 min, 15 sec/2 min, 15 sec/40 min
APU maximum starting altitude
30,000 ft
APU maximum operating altitude
36,000 ft
Maximum APU RPM
107%
With the APU door not closed, or the door position is unknown: The airplane must be limited to _____, or _________
300 KIAS/The APU must remain in operation
Maximum bleed air extraction for air conditioning from the APU is______
15,000 ft
Maximum engine start altitude with APU bleed air______
13,000 ft
Minimum Engine Oil Pressure for takeoff ________
45 psi
Flap position 8 Vfe / Vfo
230 KIAS / 200 KIAS
Flap position 20 Vfe / Vfo
220 KIAS / 200 KIAS
Flap position 30 Vfe / Vfo
185 KIAS
Flap position 45 Vfe / Vfo
170 KIAS
Gear extension maximum operating airspeed
220 KIAS
Gear down and locked maximum operating airspeed
220 KIAS
Gear retraction maximum operating airspeed
200 KIAS
Maximum Tire Speed ________
182 kts
Maximum airspeed for windshield wiper operation failed in the non-parked position__________
220 KIAS
Maximum Turbulence Penetration Speed______
280 KIAS or .75M whichever is lower
Maximum cruise mach in RVSM airspace
.82 M
RVSM Required Equipment List
Autopilot (1) / Must be operational
Altitude Alerting System (1) / Must be operational
Altitude Reporting Transponder (2) / (1) Must be operaitonal
ADC (2) / (2) Must be operational
Minimum Auto Pilot engagement altitude ______ except when performing Non-precision approach_________, Precision approach________
600 ft AGL / 400 ft AGL / 80 ft AGL
Maximum slats/flaps extension altitude
15,000 ft
Maximum permissible time on the ground with only DC power
5 min
Minimum altitude for light spoiler deployment
1000 ft AGL
Minimum airspeed for flight spoiler use
Vref + 17 KIAS
Minimum brake cooling time
15 minutes and all BTMS indicators are green and not increasing
During ladning application of thrust reverse above ______ is not permitted at air speeds below _____. Below _____, reverse thrust must be reduced to idle, not above _______
60%N1 / 75 KIAS / 60 KIAS / 30%N1
Use of the EMER DEPRESS switch above ______ is prohibited
15,000 ft
Max altitude for single pack operations
25,000 ft
Max differential pressure for taxi, takeoff, and landing
0.1 psi
Maximum relief differential pressure
8.7 psi
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
Airpspeed…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, release
Captain assumes PF duties
STAB CH1 cb (2f5)….open
STAB CH2 cb (4a1)….open
