CH16 A330 LIMITS & RECALLS Flashcards
Maximum Operating Altitude
- 200, -323
- *• _________ feet**
-302, -900
• _________ feet
Maximum Operating Altitude
- 200 PW, -323 PW
41,100 feet
-302 GE, -900 RR
• 41,450 feet
Maximum Operating Altitude
- ____, -____
- *• 41,100 feet**
-____, -____
•41,450 feet
Maximum Operating Altitude
- 200 PW, -323 PW
41,100 feet
PW are 41,100
The 200 and 323 are PW
-900 RR -302 GE
• 41,450 feet
RR & GE are 41,450
900 & 302 are GE
Maximum Takeoff and Landing Tailwind Component
-200, -302, -323
____ knots, or as ___________________
-900
___ knots, or as ___________________
Maximum Takeoff and Landing Tailwind Component
-200, -302, -323
10 knots, or as permitted by Company Pages
- 900
15 knots, or as permitted by Company Pages
Maximum Takeoff and Landing Tailwind Component
-____ , -____ , -____
10 knots, or as permitted by Company Pages
- _____
15 knots, or as permitted by Company Pages
Maximum Takeoff and Landing Tailwind Component
-200, -302, -323
10 knots, or as permitted by Company Pages
-900
15 knots, or as permitted by Company Pages
Maximum Crosswind Component:
-200, -302, -323:
Takeoff or Landing Crosswind limit ______________ including _____________
-900
Takeoff Crosswind: ______________ including _____________
Landing Crosswind: ______________ including _____________
Maximum Crosswind Component:
-200, -302, -323:
Takeoff or Landing:
Crosswind limit is 40 knots including gusts.
-900
Takeoff Crosswind limit is 30 knots including gust.
Landing is 35 knots, including gusts.
Maximum Crosswind Component:
-_______,__-______, -______:
Takeoff or Landing Crosswind limit is 40 knots including gusts.
-______
Takeoff Crosswind limit is 30 knots including gust.
Landing is 35 knots, including gusts
Maximum Crosswind Component:
-200, -302, -323:
Takeoff or Landing Crosswind limit is 40 knots including gusts.
-900
Takeoff Crosswind limit is 30 knots including gust.
Landing is 35 knots, including gusts.
Autopilot Minimum Altitudes
The minimum altitude for autopilot engagement during takeoff and manual go-around:
The minimum altitude for autopilot engagement during takeoff and manual go-around is:
100 feet AGL and at
least 5 seconds after liftoff.
Automatic Landing –200, -302, -323
For autoland operations the following wind limits apply:
Headwind
Crosswind
Tailwind
Automatic Landing -200, -323, -302
For autoland operations the following wind limits apply:
Headwind 35 knots
Crosswind 20 knots (15 knots when operating below CAT I minimums)
Tailwind 10 knots
Automatic Landing -_____, -_____, -_____
For autoland operations the following wind limits apply:
Headwind 35 knots
Crosswind 20 knots (15 knots when operating below CAT I minimums)
Tailwind 10 knots
Automatic Landing -200, -302, -323
For autoland operations the following wind limits apply:
Headwind 35 knots
Crosswind 20 knots (15 knots when operating below CAT I minimums)
Tailwind 10 knots
Automatic Landing
-900
For autoland operations the following wind limits apply:
Headwind.
Crosswind
Tailwind.
Automatic Landing
-900
For autoland operations the following wind limits apply:
Headwind. 20 knots
Crosswind 15 knots
Tailwind. 10 knots
Engines and APU
Soft Go-Around
-900:
Engines and APU
Soft Go-Around
-900
The use of soft go-around is prohibited with one engine inoperative.
Flight Controls
Do not extend flaps or slats above _________ feet
Flight Controls
Do not extend flaps or slats above 20,000 feet
Recall item for Driftdown
Recall item for Driftdown
Condition: Engine failure or shutdown during cruise.
- Max continuous thrust (MCT)……………………..SET
- A/THR………………….DISCONNECT
- SELECT HDG OR NAV AS APPROPRIATE
* FLT PLN:
L1
L2 OFFSET then
L1 enter R05 – INSERT - FCU SPD/MACH……..SET GRN DOT SPEED (not Mach)
- FCU ALT…………………..SET** To Maintain MAX ALT for ICING COND or TERRAIN clearance**
1. ALT…..Set DRIFTDOWN TO Altitude from **PERF** pg into FCU ALT
- At Green Dot Speed: Open Descent
When Offset 5 NM or when DD is no longer required <28.5FL : FCTM 4.2.11
1. SET LRC E/O REC MAX ALTITUDE from MCDU **PROG** page in FCU… SET/VERIFY
2. PULL OPEN DES
3. MSPD…ACTIVATE
3A. Planned ETOPS Divert Speed: 320
Enter on PERF pg or Spd SEL then PERF pg
4. A/TH…ON
To Maintain MAX ALT for ICING COND or TERRAIN clearance:
1. ALT…..Set DRIFTDOWN TO Altitude from PERF pg into FCU ALT
1A. — PULL for OP DES —
2. SPD…MNTN GREEN DOT
3. THRUST…MNTN MCT
—FP “ECAM ACTIONS”
QRH 0.14 DRIFTDOWN
ODM 4.7 ONE ENG INOP: LRC ALT
CAB PR EXCESS CAB ALT or Rapid Depressurization
CAB PR EXCESS CAB ALT or Rapid Depressurization
- CREW OXYGEN MASKS ……. ON
Q 2.25
Loss of Braking
Loss of Braking
- Thrust Levers …………..Maximum Reverse (as reqd )
- Brake Pedals …………………. Release
- A/SKID & N/W STRG switch ……….OFF
- Brake Pedals ………….APPLY (max 1000 psi)
- Parking Brake (if required) ………USE
Note: Use short successive parking brake applications to stop the aircraft.
Q. 14.29
A330-900 ROW WARNING - “RUNWAY TOO SHORT”
A330-900 ROW WARNING - “RUNWAY TOO SHORT”
- GO-AROUND………………. PERFORM
Unreliable Airspeed Indication
PF “My airspeed is ______, what do you show?”
- MAP 10
- PROG. 2/2 for HDG info. Request RV while sorting this problem
A330 Ebrief notes:
C: “Looks like we have unreliable airspeed, let’s apply the memory items”
► If the safe conduct of the flight is impacted:
- AP …………………………………….. OFF
- A/THR …………………………………OFF
- FD ………………………….…………. OFF
- PITCH/THRUST
— Below THR RED ALT ….. 15°/TOGA
— Above THR RED ALT & Below FL100 …. 10°/CLB
— Above THR RED ALT & Above FL100 …. 5°/CLB - FLAPS
{If CONF 0(1)(2)(3)} … MAINTAIN CURRENT CONFIG. - FLAPS
{If CONF FULL} ……. SELECT CONF 3 & MAINTAIN - SPEEDBRAKES ……… CHECK RETRACTED
- L/G ……..UP
- When at/above MSA or Pattern altitude: Level off for troubleshooting
Cruise Setting:
Think 3/4:
3-4° pitch and
75% thrust
PITCH: +2°
POWER: 85% N1
DESCENT Setting:
PITCH: -2°
POWER: IDLE stop
APCH: +4°
APCH: 55% N1
Emergency Evacuation Flow/Philosophy
Emergency Evacuation Flow/Philosophy
QRH Back Cover.2:
STOP – CONFIGURE – SHUTDOWN – EVACUATE
STOP
1. Set parking brake. 2. Notify Tower or Ground Control (VHF 1). 3. Notify the flight attendants “EASY VICTOR” three times.
CONFIGURE
4. ∆P(only if MAN CAB PR has been used)
4A. **CHECK ZERO**
4B. **>> IF ∆P is not zero:**
* CAB PRESS MODE SEL...............MAN
* MAN V/S CTL ............................Full UP
SHUTDOWN
5. ALL ENG MASTERS .........................…………..OFF 6. ALL FIRE pb (ENGs & APU).............…………..PUSH 7. ALL AGENTS (ENGs & APU) as required….PUSH
- EMER EXT LTS. . . . . . . . . . . . . . . . . . . . . . ON
EVACUATE
9. Notify the flight attendants:
“THIS IS THE CAPTAIN (special instructions) EVACUATE, EVACUATE.”
10. ALL BATs.............................OFF
11. Perform assigned crew evacuation duties.
The First Officer and Relief Pilot (if installed) will exit from a forward exit and assist from outside. Lead passengers off the surface to grass at 45° off the nose or tail.
The Captain will exit from a rear exit after all passengers are off, if possible.
If smoke is present, the Captain should take a PBE and fire extinguisher as he proceeds to the rear of the aircraft.
Move all passengers away from fire equipment, away from any possible fire or explosion and off paved surfaces. Preferably in front of the aircraft at a 45° angle
Recall the turbulent air penetration speed below FL200:
–200
–300
Recall the turbulent air penetration speed below FL200:
–200: 240 kts
–300: 240 kts
Recall the turbulent air penetration speed at and above FL200:
–200
–300
Recall the turbulent air penetration speed at and above FL200:
–200 260/.80 whichever is lower
–300 260/.78 whichever is lower
Recall the turbulent air penetration speed below 10,000
900: _________
Recall the turbulent air penetration speed below 10,000
900: 250 kts
Recall the turbulent air penetration speed AT & ABOVE 10,000’
900: ___/_____
Recall the turbulent air penetration speed AT & ABOVE 10,000’
900: 270/.80
- Thrust Mode: A330 V2 22.2.7.4
Thrust Climb / Descent : THCLB THDES
-indicates a FIXED thrust setting
-SPEED is controlled by _______
—-Column 1:
THR _____ /_______
THR _____
—-Column 2:
OPEN ____ or
OPEN _____
or MAN ____ or
MAN _____
Fixed Thrust setting
FIXED THRUST: ______ controls SPEED.
________ controls PATH
- Speed mode
-indicates a ________ thrust setting
—Airspeed is being controlled by _______
—Column 1:
_______ or _______ modes
SPEED is controlled by ________
PATH is controlled by ________
VARIABLE THRUST: THRUST controls ________
Column 2:
ALT
ALT CRZ
VS
FPA
G/S
APPROACH
Thrust Mode:
Thrust Climb / Descent :
—Indicates a FIXED thrust setting
SPEED is controlled by PITCH
—Column 1:
THR CLB / DES
THR IDLE
NOTES
**A330 VOL 1 5.4.2 Operations with Autothrust Off **
Operations in FIXED THRUST mode
Indicated by FMA COL 1:
THR CLB or
THR IDLE or
THR DES
FIXED THRUST: PITCH controls AIRSPEED
FMA COL 2: CLB, OP CLB, OP DES, DES, FLARE
May use the CL detent or IDLE position of the thrust levers.
C2 VERTICAL MODE: C1 THRUST MODE CLB THR CLB OP CLB THR CLB OP DES THR IDLE DES THR IDLE or THR DES (idle path and when above the path) FLARE (autoland only) THR IDLE
MAN FLEX and MAN TOGA are actually manual thrust settings and not autothrust modes.
They only occur when the thrust levers are placed outside the active range.
—Column 2:
OPEN CLB or OPEN DES
or
MAN CLB or MAN DES
FIXED THRUST MODE:
—FIXED THRUST:
PITCH controls SPEED.
THRUST controls PATH
V2 22.2.7.4 Active Autothrust Modes
In fixed thrust modes, the autothrust sets and maintains a constant thrust setting.
The fixed thrust settings include: (MCI)
MCT
CL (climb), or
Idle, .
When a fixed thrust mode is in use, the FMS uses pitch to control speed.
-
SPEED MODE
—Indicates a VARIABLE thrust setting
—Airspeed is being controlled by THRUST
—Column 1: SPEED MODE
SPEED or
MACH modes
SPEED is controlled by THRUST
PATH is controlled by PITCH
VARIABLE THRUST: THRUST controls SPEED—Column 2: SPEED MODE ALT ALT CRZ VS FPA G/S APPROACH
V2 22.2.7.4 Active Autothrust Modes
In variable thrust modes, the autothrust varies the thrust within its authority range to maintain the selected or managed target speed.
When variable thrust is in use, the FMS uses:
thrust to control speed and pitch to control vertical flight path.
detent.
V2 22.2.8.3 Variable Thrust Modes
When the autothrust is operating in a variable thrust mode, FMA column 1 displays SPEED or MACH in green.
FMA Indication Meaning:
Speed:
Autothrust is maintaining the target speed
Mach:
Autothrust is maintaining the target mach
The target speed may be either selected on the FCU or managed by the FMS.
When in SPEED or MACH, the autothrust will not command thrust that causes the speed to exceed the following limits, regardless of the speed selected:
Selected speed
Lowest: VLS
Highest: VMAX (VMO/MMO, VFE, or VLE as appropriate)
Managed speed
Lowest: Maneuvering speed (Green Dot, S, F as appropriate for flap configuration)
Highest: 320 Knots/.84 Mach, VFE, or VLE (whichever is lowest)
In descent phase: 315 Knots/.83 Mach, VFE, or VLE (whichever is lowest)
A330 V2 22.2.7.4 Active Autothrust Modes
When the autothrust is active it can operate in one of two basic modes:
1. _______ thrust
2. _______ thrust
A330 V2 22.2.7.4
A330 V2 2.2.7.4 Active Autothrust Modes
When the autothrust is active it can operate in one of two basic modes:
1. FIXED thrust
2. VARIABLE thrust
In FIXED thrust modes, the autothrust sets and maintains a constant ______ setting.
The fixed thrust settings include:
_______,
_______,
or ______.
When a FIXED thrust mode is in use, the FMS uses ________ to control speed.
FIXED THRUST: _______ controls SPEED.
A330 V2 22.2.7.4
V2 22.2.8.2 FIXED THRUST MODES
In fixed thrust modes, the autothrust sets and maintains a constant THRUST setting.
The FIXED thrust settings include:
MCT
CL or
IDLE
When a FIXED thrust mode is in use, the FMS uses :
PITCH to control speed.
FIXED THRUST: PITCH controls SPEED.
V2 22.2.7.4 Active Autothrust Modes
In fixed thrust modes, the autothrust sets and maintains a constant thrust setting.
The fixed thrust settings include: (MCI)
MCT
CL (climb), or
Idle, .
When a fixed thrust mode is in use, the FMS uses pitch to control speed.
V2 22.2.8.2 Fixed Thrust Modes
When the autothrust is operating in a fixed thrust mode, FMA column 1 displays THR combined with the appropriate commanded thrust setting in green:
FMA Indication
Meaning
THR MCT
The most forward thrust lever is in the MCT detent (engine-out).
THR CLB
The most forward thrust lever is in the CL detent.
THR LVR
Both thrust levers are below the CL (or MCT detent with one engine) or,
one thrust lever is in CL and the other is above the CL detent.
THR IDLE
Both engines are at idle thrust.
THR DCLB 1(2)
The most forward thrust lever is in the CL detent, and a derated climb has been selected in the MCDU.
THR DES
Minimum thrust in a managed descent
Note:
During takeoff or go around, when autothrust is armed, the FMA will display MAN TOGA, MAN FLX, or MAN DTO to indicate that the thrust levers are positioned properly. However, since these thrust settings are not commanded by the autothrust system, they are not considered autothrust modes.
In VARIABLE thrust modes, the autothrust varies the ______ within its authority range to maintain the selected or managed _____ ______.
When VARIABLE thrust is in use, the FMS uses:
________ to control speed and
________ to control vertical flight path.
VARIABLE THRUST: ________ controls SPEED
A330 V2 22.2.7.4
V2 22.2.8.3 VARIABLE THRUST MODES
In VARIABLE thrust modes, the autothrust varies the thrust within its authority range to maintain the selected or managed target speed.
When VARIABLE thrust is in use, the FMS uses:
THRUST to control speed and
PITCH to control vertical flight path.
VARIABLE THRUST: THRUST controls SPEED
22.2.8.3 Variable Thrust Modes
When the autothrust is operating in a variable thrust mode, FMA column 1 displays SPEED or MACH in green.
FMA Indication
Meaning
Speed
Autothrust is maintaining the target speed
Mach
Autothrust is maintaining the target mach
The target speed may be either selected on the FCU or managed by the FMS.
When in SPEED or MACH, the autothrust will not command thrust that causes the speed to exceed the following limits, regardless of the speed selected:
Selected speed
Lowest: VLS
Highest: VMAX (VMO/MMO, VFE, or VLE as appropriate)
Managed speed
Lowest: Maneuvering speed (Green Dot, S, F as appropriate for flap configuration)
Highest: 320 Knots/.84 Mach, VFE, or VLE (whichever is lowest)
In descent phase: 315 Knots/.83 Mach, VFE, or VLE (whichever is lowest)
What is the Engine Run Up during Icing Conditions?
200 PW
323 PW
302 GE
900 TRNT
Icing conditions exist when ____ (on the ground) or ____ (in flight) is _____°C or below and any of the following exist:
visible moisture (clouds, fog with visibility of ______ statute mile (______m) or less, rain, snow, sleet, ice crystals, etc.) is present; or ice, snow, slush or standing water is present on the ramps, taxiways, or runways.
What is the Engine Run Up during Icing Conditions?
200: PW 15 MIN: 50% N1 for 01 SEC
323: PW 15 MIN: 50% N1 for 01 SEC
302: GE 30 MIN: 60% N1 for 30 SEC
900: TRNT Standing TO: HOLD BRAKES 50% N1 for 02 SECs RELEASE BRAKES
5.16.2 Cold Weather Operation
Considerations associated with cold weather operation are primarily concerned with low temperatures and with ice, snow, slush, and standing water on the airplane, ramps, taxiways, and runways.
Icing conditions exist when OAT (on the ground) or TAT (in flight) is 10°C or below and any of the following exist:
visible moisture (clouds, fog with visibility of one statute mile (1600m) or less, rain, snow, sleet, ice crystals, etc.) is present; or ice, snow, slush or standing water is present on the ramps, taxiways, or runways.
T/OFF with
T/WIND OR
XW > 20 KTS
________ FWD STICK
200 PW
323 PW
302GE
900 TRENT
T/OFF with
T/WIND or
XW > 20 KTS
FULL FWD STICK
NO SPOILER DEFLECTION
OUT BY 100 KTS
200: PW 1.1—>1.3—>FLX/TOGA
323: PW 1.1—>1.3—>FLX/TOGA
302: GE 50%—>70%—>FLX/TOGA
900: RR 50%—>60%—> ”30 KTS” GS —>FLX/TOGA
200 PW L/W
LENGTH
WINGSPAN
PVMNT WIDTH 180
200 PW
LENGTH: 192 (59M)
This is the shortest A/C Model
WINGSPAN: 198 (60M)
Note: All A/C are 198 (60M) except 900
PVMNT WIDTH 180: 142 (44M) Same as 323 PW
302 GE
LENGTH
WINGSPAN
PVMNT WIDTH 180
302 GE
LENGTH: 209 (64M)
Note: The 300 series are the same
WINGSPAN: 198 (60M)
Note: All A/C are 198 (60M) except 900
PVMNT WIDTH 180: 157 (48M)
323 PW L/W
LENGTH
WINGSPAN
PVMNT WIDTH 180
323 PW
LENGTH: 209 (64M) same as 302
WINGSPAN: 198 (60M) all wingspans except 900
PVMNT WIDTH 180: 142 (44 M)
Same as 200 PW
- L/W
LENGTH:
WINGSPAN
PVMNT WIDTH 180
900
LENGTH: 209 (64M)
WINGSPAN: 210 (64M)
PVMNT WIDTH 180: 158 (49 M)
- Speed mode
-indicates a ________ thrust setting
—Airspeed is being controlled by _______
—Column 1:
_______ or _______ modes
SPEED is controlled by ________
PATH is controlled by ________
VARIABLE THRUST: THRUST controls ________
Column 2:
ALT
ALT CRZ
VS
FPA
G/S
APPROACH
-
SPEED MODE
—Indicates a VARIABLE thrust setting
—Airspeed is being controlled by THRUST
—Column 1: SPEED MODE
SPEED or
MACH modes
SPEED is controlled by THRUST
PATH is controlled by PITCH
VARIABLE THRUST: THRUST controls SPEED—Column 2: SPEED MODE ALT ALT CRZ VS FPA G/S APPROACH
Note from A330 VOL 1 5.4.2 Operations with Autothrust Off :
VARIABLE THRUSTt: Indicated by SPEED or MACH in Column 1 FMA
Phase of flight:
V/S, FPA
ALT, ALT, ALT CRZ, ALT CRZ ALT CSTR, ALT CSTR G/S, G/S
FINAL
DES
All APs and FDs off
What is Vls
It’s the speed represented by the hook
Lowest speed A/TH will maintain in SPD SEL
Margin above stall varies with weight and configuration
Min. Speed for normal ops
What is AProt:
Speed represented by the top of the ________ & ______ stripe
Active during _______ Law
-Limits _______ of _______
-Allows pilot to command _______ angle of _______ without _______ (w/s or GPWS Event)
Speed represented by the top of the BLACK & AMBER stripe
Active during Normal Law
-Limits Angle of Attack
-Allows pilot to command max angle of attack without stalling (w/s or GPWS Event)
What is Amax
Max safe angle of attack without stalling.
FOM 14.4.1.4 Fueling Tolerances
The flight release is legal if the fuel quantity gauges/display reflect the BLOCK FUEL within:
+_______/-_____ pounds for widebody aircraft.
difference between the flight deck indications vary from the EFSR/FSR by more than ____ (widebody), contact the fueler to have the wing panel fuel quantity validated. If the wing panel fuel quantity cannot be validated, contact MCC.
FOM 14.4.1.6 Pre-Servicing Wing Imbalances
A330: ________
See FOM 14.4.1.4 fueling TOLERANCES
FOM 14.4.1.4 Fueling Tolerances
The flight release is legal if the fuel quantity gauges/display reflect the BLOCK FUEL within:
+1,500/-500 pounds for widebody aircraft.
difference between the flight deck indications vary from the EFSR/FSR by more than 500 pounds (widebody), contact the fueler to have the wing panel fuel quantity validated. If the wing panel fuel quantity cannot be validated, contact MCC.
FOM 14.4.1.6 Pre-Servicing Wing Imbalances
A330 3200
See FOM 14.4.1.4 fueling TOLERANCES
