Limitations
Question 1
Maximum Operating
Altitude
Answer 1
-323, -200
41,100 feet
-302, -900
41,450 feet
Limitations
Question 2
Maximum Takeoff and
Landing Tailwind
Component
Answer 2
-200, -323, -302
10 knots, or as permitted by Company Pages
-900
15 knots, or as permitted by Company Pages
Limitations
Question 3
Maximum Crosswind Component
Answer 3
-200, -323, -302
Crosswind limit is 40 knots for takeoff or landing, including gusts.
-900
Crosswind limit is 30 knots for takeoff, including gust. Landing is 35 knots,
including gusts.
Limitations
Question 4
Autopilot Minimum Altitudes
Answer 4
The minimum altitude for autopilot engagement during takeoff and manual go-around is 100 feet AGL and at least 5 seconds after liftoff.
Limitations
Question 5
Automatic Landing Wind Limits
Answer 5
-200, -323, -302
| Headwind | 35 knots |
| Tailwind | 10 knots |
| Crosswind | 20 knots (15 knots when operating below CAT I minimums) |
-900
| Headwind | 20 knots |
| Tailwind | 10 knots |
| Crosswind | 15 knots |
Limitations
Question 6
Soft Go-Arund
Answer 6
The use of soft go-around is prohibited with one engine inoperative.
Limitations
Question 7
Max flap or slat altitude.
Answer 7
Do not extend flaps or slats above 20,000 feet.
Maneuvers
Question 8
Engine out
Answer 8
-Rotate
- "Positive Rate" (PM) - "Gear Up" (PF)
-SRS speed (V2 or current airspeed)
-Rudder to center Beta target
-When Safely Airborne
-Set rudder trim
-Engage autopilot if desired
-At acceleration height (normally 1000 ft.)
-Press ALT
-Retract flaps on schedule
-Accelerate to Green Dot
-After Takeoff chedklist
-At Green Dot
-select OP CLB
-Set MCT Thrust
-PM begin ECAM
Maneuvers
Question 9
Missed Approach
Answer 9
- "Go Around, Flaps" (PF)
- Select TOGA
If above TRA use TOGA bump and back to CLB
- "SRS Verified" "Positive Rate" (PM)
- "Gear Up" (PF)
- 400 ft verify or call for lateral mode
- Thrust Reduction Altitude (normally 1000 ft)
FMA should indicate with LVR CLB
- Thrust levers to CLB
- Follow FD
- Retract flaps on schedule
- After Takeoff checklist
Memory Items
Question 10
Driftdown
Answer 10
Condition:Engine failure or shutdown during cruise.
1 Max continuous thrust (MCT)...............Set
2 A/THR.....................................Disconnect
3 Select HDG or NAV as appropriate.
4 FCU SPD/MACH..............................Set
Set Green Dot SPD (not MACH).
5 FCU Altitude..............................Set
Memory Items
Question 11
CAB PR EXCESS CAB ALT or Rapid Depressurization
Answer 11
CREW OXY MASKS . . . . . . . . . . . . . . . . . . . . ON
Memory Items
Question 12
Loss of Brakeing
Answer 12
1 Thrust Levers........................Maximum reverse (as reqd)
2 Brake Pedals.........................Release
3 A/SKID & NWS switch..................OFF
4 Brake Pedals.........................Press (Max 1000 psi)
5 If required, apply parking brake with short,
successive applications.
Memory Items
Question 13
Unreliable Airspeed Indication
Answer 13
If the safe conduct of the flight is impacted:
1. A/P....................................OFF
2. A/THR..................................OFF
3. FD.....................................OFF
4. PITCH/THRUST
• BELOW THR RED ALT.................15°/TOGA
• ABOVE THR RED & Below FL 100......10°/CL
• ABOVE THR RED & Above FL 100.......5°/CL
5. FLAPS
(If CONF 0(1)(2)(3))....MAINTAIN CURRENT CONF
6. FLAPS
(If CONF) FULL..........SELECT CONF 3 & MAINTAIN
7. SPEED BRAKES.........................CHECK RETRACTED
8. L/G..................................UP
9. When at or above MSA or Pattern altitude:
• Level off for troubleshooting.
Non-memory Limits
Question 14
Brake temperature for takeoff
Answer 14
275° C (from Vol1 Landing Gear Supp Procedures)
Non-memory Limits
Question 15
Gear Speed
Answer 15
240 kts (250 Airbus limited to 240 by Delta)
Non-memory Limits
Question 16
Severe Turbulence speeds
Answer 16
-323, -302
240 KIAS below 20,000 ft.
260 KIAS or .78 (whichever is lower) above 20,000 ft.
-200, -900
240 KIAS below 20,000 ft.
260 KIAS or .80 (whichever is lower) above 20,000 ft.
Non-memory Limits
Question 17
Flap Speeds
Answer 17
<pre>
1 240 kts
1+F 215 kts
2 196 kts
3 180 kts
Full 180 kts
</pre>
Non-memory Limits
Question 18
Turn Radius for 180 turn
Answer 18
-200 142 ft.
-300 157 ft.
-900 158 ft.B31
Non-memory Limits
Question 19
Wing span
Answer 19
197' 10" (60m)
209'12"(64m) - 900
Non-memory Limits
Question 20
Fuel Capacity
Answer 20
323: 172,000
-200, -302, -900 245,000
Non-memory Limits
Question 21
Ignition
Answer 21
-moderate rain
-moderate turbulence
-standing water or slush on the runway
Vocab / ACRONYMS
Question 22
IR (on ADIRS panel)
Answer 22
Inertial Reference
Vocab / ACRONYMS
Question 23
ADR (on ADIRS panel)
Answer 23
Air Data Inertial Reference System
Vocab / ACRONYMS
Question 24
FMGEC
Answer 24
Flight Management Guidance and Envelope Computer
Vocab / ACRONYMS
Question 25
LGCIU
Answer 25
Landing Gear Control and Interface Unit
Vocab / ACRONYMS
Question 26
BSCU
Answer 26
Brake and Steering Control Unit
Vocab / ACRONYMS
Question 27
SRS
Answer 27
Speed Reference System
Vocab / ACRONYMS
Question 28
DMC
Answer 28
Display Management Computer
Vocab / ACRONYMS
Question 29
ISIS
Answer 29
Integrated Standby Instrument System
Vocab / ACRONYMS
Question 30
CIDS
Answer 30
Cabin Intercommunication Data System
Vocab / ACRONYMS
Question 31
BSCU
Answer 31
Brake and Steering Control Unit
Vocab / ACRONYMS
Question 32
ECAM
Answer 32
Electronic Centralized Aircraft Monitor
Vocab / ACRONYMS
Question 33
DMC
Answer 33
Display Management Computer
Non-memory Limits
Question 34
Minimum and Emergency Fuel
Answer 34
Min 7800
Emergency 6000
Maneuvers
Question 35
ECAM
Answer 35
First to recognize: Call out ECAM item. Example "Eng 1 Fail"
Stabilize the aircraft.
Decide time or no time
Captain assigns duties
PF: "ECAM actions"
PM: Call out ECAM item. Example "Eng 1 Fail"
-Confirm no OEB.
-Execute ECAM Actions
-PNF: "Clear <underlined label> ?"
-PF "Clear <underlined label>"
At status: "Stop ECAM":
Normal Checklist
System reset
Additional procedures such as engine start