Memory Items Flashcards
(85 cards)
1
Q
Max. Ramp weight
A
85,000 lbs.
2
Q
Max. Landing weight
A
75,100 lbs.
3
Q
Max. Zero fuel weight
A
70,750 lbs.
4
Q
Min. Flight weight
A
45,000 lbs.
5
Q
When conducting instrument approaches what category is CRJ900
A
Category D
6
Q
Flight deck door must be:
A
Kept closed and locked except per FOM & CFM
Challenge and response when opened.
Must always have 2 crew members in flight deck.
7
Q
Baggage compartment aft.
A
3,650 lbs.
8
Q
Baggage compartment forward.
A
1,700 lbs.
9
Q
Max. RVSM Mach speed.
A
.82 M
10
Q
Flaps 1
A
230 KIAS
11
Q
Flaps 8
A
230 KIAS
12
Q
Flaps 20
A
220 KIAS
13
Q
Flaps 30
A
185 KIAS
14
Q
Flaps 45
A
170 KIAS
15
Q
Max. Landing gear extension.
A
220 KIAS
16
Q
Max. Landing gear retraction
A
200 KIAS
17
Q
Max. Speed w/ landing gear extended.
A
220 KIAS
18
Q
Max. Turbulent air speed.
A
280 KIAS or .75 M
Whichever is less
19
Q
Max. Windshield wiper speed.
A
250 KIAS
20
Q
Max. Windshield wiper speed when failed in non parking position.
A
250 KIAS
21
Q
Max. Tire speed.
A
195 KIAS
22
Q
Max. Airspeed for ADG operation.
A
VMO / MMO
23
Q
Max tailwind for TO & lndg
A
10 kts.
24
Q
Max. Crosswind for Takeoff dry runway
A
PIC 35 kts.
SIC 35 kts.
25
Max. Crosswind for landing dry runway.
PIC 32 kts.
| SIC 32 kts.
26
Max. Crosswind for takeoff and landing ; wet runway
PIC 27 kts.
| SIC 27 kts
27
Max. Crosswind for takeoff and landing; slippery runway braking action fair
PIC 20 kts.
| SIC 20 kts
28
Max. Crosswind for takeoff and landing; slippery runway braking action poor
PIC 15 kts.
| SIC 15 kts
29
Max. Crosswind for takeoff and landing; high mins
PIC 25 kts.
| SIC 15 kts
30
Max pressure altitude for takeoff and landing
9600'
31
Max. Operating altitude
41,000'
32
Max. Ambient air temperate for takeoff and landing
ISA +35C
33
Min. Ambient air temperature for takeoff
-40C
34
Cargo: flight must be within ___ min. of a suitable airport if cargo is carried within either cargo compartment.
60 min.
35
Taxi lights must be switched off when stationary in excess of ___ min.
10 min.
36
Wheel brake cooling limits ____ __ ________ between landing or low energy rejected takeoff and subsequent takeoff.
must be observed
37
Max. Differential pressure
8.7 PSI
38
Max. Negative differential pressure
-0.5 PSI
39
Max. Differential pressure during taxi, takeoff, and landing
0.1 PSI
40
Max. Altitude for single pack operation
25,000'
41
Max. Take off weight
84,500 lbs.
42
To preclude possible ear damage use of emergency depress switch above ____ is prohibited
15,000'
43
Autopilot operation below 600' AGL is prohibited except when performing a visual or non precision approach
400'
44
Autopilot operation below 600' AGL is prohibited except when performing a precision approach (ILS) all engines operating.
80'
45
Autopilot operation below 600' AGL is prohibited except when performing a precision approach (ILS) one engine inoperative.
110'
46
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.
47
Max. TRU load in flight
120 Amps
48
Max. Time for DC only power to CRT displays is:
5 min
49
Max. Differential pressure before opening any doors
0 PSI
50
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.
51
Setting the MDA must rounded to the next higher
10'
52
Pilots are authorized to deviate from ATC instructions when:
Necessary to comply with TCAS or RA command.
53
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.
54
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
55
(Contamination)
Takeoff with
Frost, ice, snow or slush on adhering to any critical surface (wings,winglets, horizontal & vertical stabilizers, control surfaces, and engine inlets)
56
Fuel Imbalance TO
300 lbs.
57
Fuel Imbalance Flight
800 lbs.
58
Fuel remaining in tanks when indicator reads zero is:
Not usable
59
Takeoff with more than _____ lbs. of fuel in center tank is prohibited unless each wing has more than ____ lbs.
500 lbs.
4,400 lbs.
60
Minimum go-around fuel is ____ lbs. and limited to a pitch angle of ___ degrees.
600 lbs. per tank
10 degrees nose up
61
Min. Engine fuel temperature for TO is
5 C
62
Powered and Gravity fuel cross flow must be ___ for TO and Landing
OFF
63
Minimum ambient temperature for APU start is
-40 C
64
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.
65
Max. APU Generator load. 0 - FL410
40 kVA
66
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.
67
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.
68
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.
69
If cowl anti-ice and continuous ignition are simultaneously required
Aalways select cowl anti-ice before continuous ignition. (Endeavor)
70
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.
71
Engine Starter Cranking limitations
Cannot be used if N2 > 45%
72
Engine Start (Ground)
Attempt - Max. Time on - Cool down
1&2 90 sec. - 10 sec.
3-5 90 sec. - 5 min.
73
Engine Start or Motoring (Flight)
Attempt - Max. Time on - Cool down
1 120 sec. - 10 sec.
2-5 60 sec. - 5 min.
74
Motoring (Ground)
Attempt - Max. Time on - Cool down
1 90 sec. - 5 min.
2-5 30 sec. - 5 min.
75
Do not move thrust lever from SHUT OFF to IDLE unless: (Ground)
ITT 120C or below
76
Do not move thrust lever from SHUT OFF to IDLE unless: (Flight)
ITT is 90C or below
77
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
78
Max. Reverse Thrust is:
Prohibited below 75 KIAS,
| REV idle below 60 KIAS
79
Thrust Reverser preflight check is
Limited to reverse idle only.
80
Reverse taxi ops is
Prohibited
81
Slats and flaps use are
Prohibited enroute
Prohibited above 15,000'
82
Flight Spoiler in flight must
Not be extended below 1000' AGL (Company)
Not be extended in flight at airspeed below Vref +10
83
Both stall protection switches must
Be ON for all phases of flight
86
Operation with ILS glidepath angles greater than __ is prohibited
3.5 degrees
87
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
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