Memory Items Flashcards
Max. Ramp weight
85,000 lbs.
Max. Landing weight
75,100 lbs.
Max. Zero fuel weight
70,750 lbs.
Min. Flight weight
45,000 lbs.
When conducting instrument approaches what category is CRJ900
Category D
Flight deck door must be:
Kept closed and locked except per FOM & CFM
Challenge and response when opened.
Must always have 2 crew members in flight deck.
Baggage compartment aft.
3,650 lbs.
Baggage compartment forward.
1,700 lbs.
Max. RVSM Mach speed.
.82 M
Flaps 1
230 KIAS
Flaps 8
230 KIAS
Flaps 20
220 KIAS
Flaps 30
185 KIAS
Flaps 45
170 KIAS
Max. Landing gear extension.
220 KIAS
Max. Landing gear retraction
200 KIAS
Max. Speed w/ landing gear extended.
220 KIAS
Max. Turbulent air speed.
280 KIAS or .75 M
Whichever is less
Max. Windshield wiper speed.
250 KIAS
Max. Windshield wiper speed when failed in non parking position.
250 KIAS
Max. Tire speed.
195 KIAS
Max. Airspeed for ADG operation.
VMO / MMO
Max tailwind for TO & lndg
10 kts.
Max. Crosswind for Takeoff dry runway
PIC 35 kts.
SIC 35 kts.
Max. Crosswind for landing dry runway.
PIC 32 kts.
SIC 32 kts.
Max. Crosswind for takeoff and landing ; wet runway
PIC 27 kts.
SIC 27 kts
Max. Crosswind for takeoff and landing; slippery runway braking action fair
PIC 20 kts.
SIC 20 kts
Max. Crosswind for takeoff and landing; slippery runway braking action poor
PIC 15 kts.
SIC 15 kts
Max. Crosswind for takeoff and landing; high mins
PIC 25 kts.
SIC 15 kts
Max pressure altitude for takeoff and landing
9600’
Max. Operating altitude
41,000’
Max. Ambient air temperate for takeoff and landing
ISA +35C
Min. Ambient air temperature for takeoff
-40C
Cargo: flight must be within ___ min. of a suitable airport if cargo is carried within either cargo compartment.
60 min.
Taxi lights must be switched off when stationary in excess of ___ min.
10 min.
Wheel brake cooling limits ____ __ ________ between landing or low energy rejected takeoff and subsequent takeoff.
must be observed
Max. Differential pressure
8.7 PSI
Max. Negative differential pressure
-0.5 PSI
Max. Differential pressure during taxi, takeoff, and landing
0.1 PSI
Max. Altitude for single pack operation
25,000’
Max. Take off weight
84,500 lbs.
To preclude possible ear damage use of emergency depress switch above ____ is prohibited
15,000’
Autopilot operation below 600’ AGL is prohibited except when performing a visual or non precision approach
400’
Autopilot operation below 600’ AGL is prohibited except when performing a precision approach (ILS) all engines operating.
80’
Autopilot operation below 600’ AGL is prohibited except when performing a precision approach (ILS) one engine inoperative.
110’
RVSM flight; The ADC source coupled to the active Autopilot must be:
Same as that coupled to the ATC transponder during flight in RVSM airspace.
Max. TRU load in flight
120 Amps
Max. Time for DC only power to CRT displays is:
5 min
Max. Differential pressure before opening any doors
0 PSI
Circuit breaker reset in flight is prohibited unless:
Directed by written procedure or in the judgement of the PIC it is necessary for the safe completion of the flight.
Setting the MDA must rounded to the next higher
10’
Pilots are authorized to deviate from ATC instructions when:
Necessary to comply with TCAS or RA command.
Icing condition definition in flight is defined as:
TAT less than or equal to 10 C and in visible moisture (clouds, rain, snow, sleet, or ice crystals) except when SAT is less than or equal to -40 C.
SLD Definition
Ice accretion on flight compartment side windows
1) Wing anti-icing must be ON
2) Cowl anti-icing must be ON
3) Leave icing condition
(Contamination)
Takeoff with
Frost, ice, snow or slush on adhering to any critical surface (wings,winglets, horizontal & vertical stabilizers, control surfaces, and engine inlets)
Fuel Imbalance TO
300 lbs.
Fuel Imbalance Flight
800 lbs.
Fuel remaining in tanks when indicator reads zero is:
Not usable
Takeoff with more than _____ lbs. of fuel in center tank is prohibited unless each wing has more than ____ lbs.
500 lbs.
4,400 lbs.
Minimum go-around fuel is ____ lbs. and limited to a pitch angle of ___ degrees.
600 lbs. per tank
10 degrees nose up
Min. Engine fuel temperature for TO is
5 C
Powered and Gravity fuel cross flow must be ___ for TO and Landing
OFF
Minimum ambient temperature for APU start is
-40 C
APU Starter motor duty cycle
No more than 3 start/start attempts within 1 hr. with a minimum of 2 min. between cranking attempts for starter and starter contactor cooling and APU drainage.
Max. APU Generator load. 0 - FL410
40 kVA
Engine Warm-up
Must remain at IDLE until oil pressure reaches normal range.
During all starts do not exceed 75% N1 until 2 min. after start or until all operating indications are in normal range, whichever is longer.
Cold Soaked Aircraft
Less than or equal to -30C for more than 8 hours
Motor engines for 60 sec. and verify Fan rotation.
Thrust reversers must be actuated until deploy and stow cycles are less than or equal to 5 sec.
Continuous ignition must be used when.
Takeoff and Landing on a contaminated runway.
Moderate or greater rain
Moderate or greater turbulence
Flight in the vicinity of thunder storms.
If cowl anti-ice and continuous ignition are simultaneously required
Aalways select cowl anti-ice before continuous ignition. (Endeavor)
Reduced (Flex) thrust takeoff is prohibited when:
If wing or cowl anti-ice is in use.
Contaminated runway.
Windshear or downdrafts have been forecast.
Anti-skid is inoperative.
Flexing is acceptable provided wet runway data are used.
Engine Starter Cranking limitations
Cannot be used if N2 > 45%
Engine Start (Ground)
Attempt - Max. Time on - Cool down
1&2 90 sec. - 10 sec.
3-5 90 sec. - 5 min.
Engine Start or Motoring (Flight)
Attempt - Max. Time on - Cool down
1 120 sec. - 10 sec.
2-5 60 sec. - 5 min.
Motoring (Ground)
Attempt - Max. Time on - Cool down
1 90 sec. - 5 min.
2-5 30 sec. - 5 min.
Do not move thrust lever from SHUT OFF to IDLE unless: (Ground)
ITT 120C or below
Do not move thrust lever from SHUT OFF to IDLE unless: (Flight)
ITT is 90C or below
Thrust Reverser is approved for:
1) Ground use only
2) Full stop landing
3) Do not attempt go around after deployment
4) TO w/ EICAS Caution/Warning is prohibited
Max. Reverse Thrust is:
Prohibited below 75 KIAS,
REV idle below 60 KIAS
Thrust Reverser preflight check is
Limited to reverse idle only.
Reverse taxi ops is
Prohibited
Slats and flaps use are
Prohibited enroute
Prohibited above 15,000’
Flight Spoiler in flight must
Not be extended below 1000’ AGL (Company)
Not be extended in flight at airspeed below Vref +10
Both stall protection switches must
Be ON for all phases of flight
Operation with ILS glidepath angles greater than __ is prohibited
3.5 degrees
Rejected Takeoff Memory Items:
CA
Idle, brakes, spoilers, thrust reversers A/R.
Abort, I have an aircraft.
This is the Captain. We have discontinued the takeoff. Please remain seated.
FO You have the aircraft. Verify IDLE Brakes Maximum. Spoilers Green Thrust reverser A/R. ATC Notify
