Proficiency items Flashcards
(60 cards)
1
Q
Aircraft type versus tail number
COM 3.1.7
A
A319 502NK to 536NK
A320 601NK to 656 NK
A320 NEO 901NK to 905NK
A320 690NK to 694NK
A321 657NK to 687NK
2
Q
Wingspans
COM 3.1.8
A
Not sharklets 111 feet 10 inches
Sharklets 117 feet 5 inches
3
Q
Tailstrikes Pitch attitudes
COM 3.1.8
A
A310-320 Pitch 10’
A321 Pitch 7.5’
Compress. A319 13.9 A320 11.7 A320 NEO 11.7 A321 9.7
4
Q
Max Certified Alt
COM 3.1.9
A
FL 398
5
Q
Minimum runway width
COM 3.1.12
A
148 feet (45 meters)
98 feet reduced ops
6
Q
Maximum Runway alt
COM 3.1.12
A
9200 feet
7
Q
Runway Slope
Com 3.1.12
A
+2 /-2 %
8
Q
Maximum X-wind
COM 3.1.12
A
For To and Lnd
38 kts
9
Q
Max tailwind for TO
COM 3.1.12
A
15kts
10
Q
Max Tailwind for Lnd
COM 3.1.12
A
10kts
11
Q
Max wind for Passengers door operations
A
65 kts
12
Q
Max Speed with gear extended
COM 3.1.16
A
280 kts or .67M
13
Q
Max speed for gear extension
COM 3.1.16
A
250kts or .60M
14
Q
Max speed gear retraction
COM 3.1.16
A
220 kts .54M
15
Q
Max altitude for gear
COM 3.1.16
A
25.000 feet
16
Q
Max Tire speed
COM 3.1.16
A
195 kts
17
Q
Max speed for cockpit window
A
200 kts
18
Q
Taxi Speed
COM 3.1.17
A
10 kts if making a 90’ or more turn
30 kts straight
20 kts in turn if weight <167.550 pounds
19
Q
max windshield wipers speed
COM 3.1.17
A
230kts
20
Q
Max landing weight
A
A319 137.788
A320 145.505
A320 NEO 148.591
A321 171.519
21
Q
APU Bleed Use with Air Start unit
A
The Flight Crew must not use bleed air from the APU BLEED and from
the HP Air Start Unit at the same time, to prevent any adverse effect
on the Bleed Air System.
22
Q
Cabin Pressure
A
- Max positive differential pressure. . . . . . . . . . . . . . . . . . 9.0 PSI
- Max negative differential pressure . . . . . . . . . . . . . . . . . -1.0 PSI
- Safety relief valve setting . . . . . . . . . . . . . . . . . . . . . . . . . . 8.6 PS
23
Q
Packs Use With LP Air Conditioning Unit
A
The Flight Crew must not use conditioned air from the packs and
from the LP Air Conditioning Unit at the same time, to prevent any
adverse effect on the Air Conditioning system.
24
Q
Autopilot
Minimum Height For Use Of Autopilot
Take Off with SRS mode
A
100 ft AGL
Note: Takeoff with SRS mode - An internal FMGS logic prevents the
autopilot from engaging during the 5 seconds after liftoff.
25
Autopilot
Straight in non precision app
COM 3.1.44
Applicable minimum
26
Autopilot
ILS app when CAT2 or CAT3 not display
COM 3.1.44
160 ft AGL
27
Autopilot
Go Around
COM 3.1.44
AP or FD engagement 100 Ft AGL
28
Autopilot
All other phase
COM 3.1.44
500 feet AGL (A319-A320)
| 900 feet AGL (A321)
29
Autopilot
Use of AP or FD in OPEN DES or DES mode is not permitted in APP unless the FCO is set at or above
COM 3.1.44
Highest of:
Minimum or 500 ft AGL (319-320)
Minimum or 900 ft AGL (321)
30
FD must be selected off when
Reaching MDA
Or
300 ft AGL on a RNAV visual
31
Nag Mode may be used in terminal area provided that:
- GPS Primary is available, or
- The appropriate RNP is checked or entered on the MCDU, and
HIGH accuracy is displayed, or
- FMS navigation is crosschecked with navaid raw data.
32
One Engine Inop approach Limitations:
A319 &A321
If one engine is inoperative, it is not permitted to use the autopilot to
perform NPAs in the following modes: FINAL APP, NAV V/S, NAV/
FPA.
Only FD use is permitted
33
APU Start Limitations:
COM 3.1.57
After three consecutive APU start attempts, the Flight Crew must wait
60 min before a new start attempt.
34
ENGINE ITT limits:
A319 & A320 - 635 TO/GA (5 min/10 min), 610 MCT, 635 start.
A321 - 650 TO/GA (5 min/10min0,610 MCT, 635 Start.
A320 NEO - 1083 TO/GA (5 min/10 min), 1043 MCT, 1083 Start.
35
Oil Temperature
-40 Start
-10 Idle
+50 To
+155 max
+165 Transiant (15min)
36
Oil Pressure
COM 3.1.69 & 3.1.70
60 Psi Classic
65 Psi NEO
37
Starter engagement
- A standard automatic start that includes only one start attempt, is considered one cycle
- For ground starts (automatic or manual), a 15 s pause is required
between successive cycles
- A 30 min cooling period is required, subsequent to three failed
cycles or 5 min of continuous crank
- For manual start, observe a two-minute maximum cycle time
- For crank, observe a 5 min maximum cycle time
- The starter must not be run when N2 is above 10 % on-ground and
18 % in-flight
38
Starter engagement NEO
- A standard automatic start that includes up to three start
attempts, is considered one cycle
- For ground starts (automatic or manual), a 35 s pause is required
between successive cycles
- A 15 min cooling period is required, subsequent to three failed
cycles, or 15 min of continuous or cumulated crank
- The starter must not be run when N2 is above 20%.
39
Reverse Thrust
Maximum reverse should not be used below 70 kt. Idle reverse is
permitted down to aircraft stop
40
Flex To not permitted:
On contaminated runway.
More than 25% derated
Temp is within 10’c of Flex
APG says so
41
Max X-wind for engine start
35kts
42
Max altitude for flaps
20.000 ft
43
Fuel temperature
COM 3.1.76
For JET A only, if TAT reaches -34 °C, monitor on FUEL SD page
that fuel temperature remains higher than -36 °C
44
Max fuel imbalance at TO
COM 3.1.80 & 3.1.81
882 (A321) or 1102
45
Max fuel imbalance at LND
COM 3.1.80 & 3.1.81
2910 (A321) or 3306
46
Brake Temp
Maximum brake temperature for takeoff . . 300 °C
| 150 if brake fan ON
47
Takeoff at reduced thrust is not permitted:
- On contaminated runways.
- For known windshear conditions.
- When a Special Departure Procedure specifies
full thrust for takeoff.
- When a deferred maintenance item per the MEL
requires full thrust for takeoff.
- When the flex temp is within 10 0C of actual OAT.
48
AOM 2.121.26
| Takeoff Performance Data Validity
- If there is a tailwind component, takeoff performance data must
indicate tailwind data.
- Actual QNH is no less than takeoff data QNH minus 0.10”.
- Actual OAT is no less than takeoff data OAT minus 10°C.
- Actual takeoff weight is less than or equal to MTOW.
49
Emergency Descent
MEMORY ITEMS
1. CREW OXY MASKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .USE
2. SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
3. EMER DESCENT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE
4. THR LEVERS (if A/THR not engaged). . . . . . . . . . . . . . . . . . . . IDLE
5. SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL
6 min to descend to 18.000 then 12min @ 18000 then 30 min at 14.000
50
EGPWS WARNING
Simultaneously:
- Pull to full backstick and maintain in that position.
- Aircraft achieve the best climb performance when the wings
are as level as possible.
- If the "TERRAIN TERRAIN PULL UP" or "TERRAIN AHEAD
PULL UP" or "OBSTACLE OBSTACLE PULL UP" or
"OBSTACLE AHEAD PULL UP" aural alert triggers, a turning
maneuver can be initiated if the Flight Crew concludes that
turning is the safest action. The PULL UP maneuver must be
performed before the turn toward the safe direction, as climbing
increases the terrain clearance.
Apr 16, 2018MEMORY & PROFICIENCY ITEMS
A320 Series 3.2.4
MEMORY ITEMS
• AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• PITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL UP
(Pull to full backstick and maintain in that position.)
• THRUST LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TOGA
• SPEED BRAKES lever . . . . . . . . . . . . . . . CHECK RETRACTED
• BANK . . . . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL or ADJUST
51
Loss of Braking
• REV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX
• BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
• A/SKID & N/W STRG. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
• MAX BRK PR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,000 PSI
• PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . .SHORT AND SUCCESSIVE APPLICATIONS
52
TCAS RA
• AP (if engaged) . . . . . . . . . . . . . . . . .. . . . . . .OFF
• BOTH FDs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . .OFF
• ATC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
Note: Respect stall, GPWS, or windshear warning
53
Unreliable Speed Indication/ADR Check Procedure
If the safe conduct of the flight is impacted:
• AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• PITCH/THRUST:
- Below THRUST RED ALT . . . . . . . . . . . . . . . . . . . . . . . .15°/TOGA
- Above THRUST RED ALT and Below FL 100. . . . . . . . .10°/CLB
- Above THRUST RED ALT and Above FL 100. . . . . . . . . . 5°/CLB
• FLAPS (if CONF 0(1)(2)(3)). . . . . . MAINTAIN CURRENT CONF
• FLAPS (if CONF FULL) . . . . . SELECT CONF 3 AND MAINTAIN
• SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED
• L/G . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
54
Windshear Ahead
Before TO & TO roll: Delay/reject
When airborne: Thrust Lever ... TOGA
AP (if engaged) ... Keep On
SRS orders ... Follow
Landing: Go Around ... Initiate
AP (if engaged) ... Keep On
Note: - Autopilot disengages if the angle of attack value goes
above α prot.
- If the FD bars are not displayed, move toward an initial
pitch attitude of 17.5°. Then, if necessary, to prevent a
loss in altitude, increase the pitch attitude
55
WINDSHEAR
RED “windshear, windshear,windshear”
If before V1: Reject
After V1: Thrust levers ... TOGA
At Vr ... Rotate
SRS orders ... Follow
Airborne, Initial climb or landing:
Thrust Levers ... TOGA
AP (if engaged) ... Keep On
SRS orders ... Follow
Note: - Autopilot disengages if the angle of attack value goes
above α prot.
- If the FD bars are not displayed, move toward an initial
pitch attitude of 17.5°. Then, if necessary, to prevent a
loss in altitude, increase the pitch attitude
56
STALL WARNING AT LIFT OFF
1. THRUST. . . . . . . . . . . . . . . . . . . . . . . . . . TOGA
2. PITCH ATTITUDE . . . . . . . . . . . . . . . . . . .15°
3. BANK . . . . . . . . . . .. . . . . . . . . . . . . WINGS LEVEL
57
Stall recovery
1. Nose Down Pitch Control ... Apply
2. Bank ... Wings Level
when out of Stall:
Thrust Increase Smoothly as needed
Speed brakes ... Check Retracted
Flight Path ... Recover Smoothly
if below 20.000 feet: Flaps 1 ... Select
58
Severe Turbulence
1. SIGNS . . . . . . . . . . . . . . . . . . . . . . .. . . . . . ON
2. AUTO PILOT. . . . . . . . . . . .. . . . ... . . KEEP ON
3. A/THR (when thrust changes become excessive) . . DISCONNECT
4. TURBULENCE SPEED. (275 .76)..SET
Do Not Chase
6. Descent..............................................Consider
7. For Approach.........AT keep on (in manage speed)
8. For Landing.
Flaps 3 less drag more energy, Flaps full better protection
59
Crew Incapacitation
Call lead FA
60
One engine INOP Obstacle / STD
1. Thrust set MCT
2. Auto Thrust disconnect
3. ATC notify
4. Decelerate/ Descent: Green Dot / 300 .78M
5. Engine out cruise altitude figure out.
6. Start ECAM actions.
