VX Limitations & Memory Items - REV. 24 Flashcards

(51 cards)

1
Q

Max Crosswind - Takeoff

A

A319/320

38 kts

A321

35 kts

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2
Q

Max Crosswind - Landing

A

A319/320/321

38 kts

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3
Q

Max Crosswind Engine Start

A

A321 only

45 kts

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4
Q

Max Tailwind (Takeoff and Landing)

A

10 kts

* For the A319, at elevations greater than 5,750 or CONF 3, AUTOLAND tailwind limit is 5 knots

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5
Q

Max Wind for Passenger Door Operations

A

65 kts

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6
Q

Max Wind Cargo Door Operation

A

40 kts

(50 kts if aircraft is positioned into the wind or door is on the leeward side)

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7
Q

Cargo Doors must be closed before wind exceeds

A

65 kts

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8
Q

VLE

A

280 kts / M 0.67

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9
Q

VLO - Extension

A

250 kts

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10
Q

VLO - Retraction

A

220 kts

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11
Q

Max Tire Ground Speed

A

195 kts

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12
Q

Max Brake Temp for Takeoff

A

300°C

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13
Q

Max Operating Altitude with Slats and Flaps Retracted

A

FL 390

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14
Q

Severe Turbulence Penetration Speed

A

275 kts / M0.76

(250 kts below FL 200)

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15
Q

Max Speed with Windshield Wipers in Use

A

230 kts

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16
Q

Max Speed with the Flight Deck Window Open

A

200 kts

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17
Q

Do Not Use LP Ground Conditioned Air While

A

Packs Operating

(Avoids valve chatter)

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18
Q

REMOVED

Do not use Pack Flow High in combination with Wing Anti-Ice above

(A321 only)

A

FL 250

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19
Q

Min Height for AP Engagement on Takeoff With

SRS Mode *

A

100 ft AGL

* An internal FMGS logic prevents the AP from engaging during the first 5 seconds after liftoff

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20
Q

Min Height for AP Use on Straight-In Non-Precision Approach

A

Applicable MDA (DA)

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21
Q

Min Height for AP Use on a Circling Maneuver**

A

1,000 ft AGL or Circling MDA(H), whichever is higher

** Virgin America only conducts circling maneuvers (not circling approaches) and must be in VMC weather conditions. The flight crew must conduct the maneuver within the circling area, while maintaining required visual reference at all times.

22
Q

Min Height for AP Use during a CAT I ILS WITHOUT CAT II or CAT III DUAL/SINGLE Displayed

A

160 ft AGL

Note: All approaches to weather minimums below Category I, i.e. CAT II/III approaches require the use of AUTOLAND per Virgin America’s GM Operation Specifications; and the Captain shall be the Pilot Flying

23
Q

Min Height for AP Use during a CAT I ILS WITH CAT II or CAT III DUAL/SINGLE Displayed

A

80 ft AGL

Note: All approaches to weather minimums below Category I, i.e. CAT II/III approaches require the use of AUTOLAND per Virgin America’s GM Operation Specifications; and the Captain shall be the Pilot Flying

24
Q

Min Height for AP Engagement on Go Around

25
Min Height for AP Use in All Other Phases
**A319/320** 500 ft AGL **A321** 900 ft AGL
26
If One Engine Inoperative, DO NOT use AP to Perform Non-Precision Approaches in the Following Modes
FINAL APP, NAV V/S, NAV FPA (FD use is permitted) Only applicable to **A319** aircraft (N521VA through N530VA)
27
Max Operating Altitude With Slats and/or Flaps Extended
FL 200
28
Max Fuel Imbalance for Takeoff
800 lbs\* \* The above limitations are the most restrictive Virgin America fuel imbalance values fleet wide. Anytime either of these values is reached or is about to be reached, refer to FCOM LIM-28 for actual values for your specific fuel configuration and phase of flight. The above fuel management limitation numbers are rounded. Below is for **A319/320** only: Do not use center tank fuel for takeoff\*\* Center Tanks must be emptied first, then wing tanks\*\* \*\*These limitations only apply to the aircraft not equipped with center tank jet pumps (N200 series and N900 series)
29
Max Fuel Imbalance Inflight or Landing
1,500 lbs \*The above limitations are the most restrictive Virgin America fuel imbalance values fleet wide. Anytime either of these values is reached or is about to be reached, refer to FCOM LIM-28 for actual values for your specific fuel configuration and phase of flight. The above fuel management limitation numbers are rounded.
30
Max Altitude for Dual Pack Operations | (Both packs on APU)
15,000 ft
31
Max Altitude for Single Pack Operations (one pack on APU)
FL 225
32
Max Altitude for Engine Start Assist Using APU Bleed Air
FL 200
33
After 3 APU Starter Motor Duty Cycles
Wait 60 min before attempting another start
34
Max Altitude to Start the APU during EMER ELEC CONFIG
FL250
35
Min Oil Quantity for Departure
**A319/A320** 9.5 Quarts + 0.5 Quarts per Hour of Flight **A321** 11 Quarts + 0.5 Quarts per Hour of Flight
36
Min Oil Temperature for Takeoff
**A319/320** - 10°C **A321** 19°C
37
Max Number of Consecutive Start Cycles
**A319/320** 4\* **A321** 3\* \* A standard auto-start cycle for the Leap 1A and CFM56-5B engine may consist of up to 3 start attempts
38
Min Cooling Period After Max Engine Cycles
15 min
39
Min Pause Between Start Cycles (Ground Start)
**A319/320** 20 sec **A321** 60 sec
40
Max N2 for Running Re-Engagement of Starter
**A319/320** 20% **A321** 63%
41
Speed Below Which Max Reverse Thrust SHOULD Not be Used
70 KIAS
42
EGPWS ALERTS ## Footnote FOR ANY EGPWS WARNING OR FOR EGPWS CAUTIONS DURING NIGHT OR IMC CONDITIONS
**Simultaneously:** AP...................................................................................OFF PITCH....................................................................PULL UP THRUST LEVERS....................................................TOGA SPEEDBRAKES LEVER................CHECK RETRACTED BANK.....................................WINGS LEVEL or ADJUST GO TO FCOM PRO-ABN-SURV FOR EGPWS WARNINGS PROCEDURE GO TO FCOM PRO-ABN-SURV FOR EGPWS CAUTIONS PROCEDURE
43
EMERGENCY DESCENT
CREW OXY MASKS.........................................................ON CREW COMMUNICATIONS...........................ESTABLISH SIGNS..................................................................................ON ALT......................................................................SET & PULL HDG.....................................................................SET & PULL SPD/MACH...................................................................ADJUST THRUST LEVERS (IF A/THR off)................................IDLE SPD BRK......................................FULL (RESPECTING VLS) GO TO QRH ABN 25.02A FOR EMER DESCENT PROCEDURE
44
LOSS OF BRAKING
**IF AUTOBRAKE IS SELECTED:** \*BRAKE PEDALS........................................................PRESS **IF NO BRAKING AVAILABLE:** \*REV.................................................................................MAX BRAKE PEDALS ...................................................RELEASE A/SKID & N/W STRG ....................................................OFF BRAKE PEDALS ........................................................PRESS MAX BRK PR ..........................................................1000 PSI **IF STILL NO BRAKING:** \*PARKING BRAKE...................SHORT AND SUCCESSIVE APPLICATIONS
45
STALL RECOVERY
NOSE DOWN PITCH CONTROL................................................APPLY BANK...................................................................................WINGS LEVEL **When Out of Stall** (no longer stall indications): \*THRUST.....................................INCREASE SMOOTHLY AS NEEDED SPEEDBRAKES......................................................CHECK RETRACTED FLIGHT PATH....................................................RECOVER SMOOTHLY **In Clean Configuration and Below 20,000':** \*FLAP 1.............................................................................................SELECT GO TO FCOM PRO-ABN-MISC FOR STALL RECOVERY PROCEDURE
46
STALL WARNING AT LIFTOFF
THRUST.................................................................TOGA PITCH ATTITUDE......................................................15° BANK.......................................................WINGS LEVEL GO TO FCOM PRO-ABN-MISC FOR STALL WARNING AT LIFTOFF PROCEDURE
47
TCAS WARNINGS
AP (If engaged)...................................................................................... OFF BOTH FDs...............................................................................................OFF V/S .........................ADJUST PITCH - MAINTAIN GREEN, AVOID RED ATC....................................................................................................NOTIFY GO TO FCOM PRO-ABN-SURV FOR TCAS WARNINGS PROCEDURE
48
UNABLE TO MAINTAIN ALTITUDE – ENGINE FAILURE DRIFTDOWN
THR LEVERS........................................................MCT A/THR.....................................................................OFF SPD/MACH....................................SET M.78 & PULL HDG............................................................SET & PULL ALT...............................................SET FL200 & PULL GO TO QRH ABN 25.11A FOR UNABLE TO MAINTAIN ALTITUDE - ENGINE FAILURE DRIFTDOWN PROCEDURE
49
UNRELIABLE SPEED INDICATION IF THE SAFE CONDUCT OF THE FLIGHT IS IMPACTED
AP/FD........................................................................................................OFF A/THR.......................................................................................................OFF **PITCH/THRUST:** \*Below THRUST RED ALT.........................................................15°/TOGA \*Above THRUST RED ALT and Below FL100 .........................10°/CLB \*Above THRUST RED ALT and Above FL100 ..........................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 When at, or above MSA or Circuit Altitude Level off for trouble shooting GO TO QRH ABN 26.02A FOR UNRELIABLE SPEED INDICATION PROCEDURE
50
WINDSHEAR
**At Takeoff:** **If Before V1:** \*TAKEOFF....................................................................REJECT The takeoff should be rejected only if significant airspeed variations occur below indicated V1 and the pilot decides that there is sufficient runway remaining to stop the airplane **If After V1:** \*THR LEVERS................................................................................................TOGA \*REACHING VR.........................................................................................ROTATE \*SRS ORDERS...........................................................................................FOLLOW **Airborne, Initial Climb or Landing:** THR LEVERS AT TOGA............................................................SET or CONFIRM AP (If engaged)..........................................................................................KEEP ON SRS ORDERS..............................................................................................FOLLOW DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR CLOSELY MONITOR FLIGHT PATH AND SPEED RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR GO TO FCOM PRO-ABN-SURV FOR WINDSHEAR PROCEDURE
51
WINDSHEAR AHEAD (RED)
**During the Takeoff Run** \*TAKEOFF............................................................REJECT **When Airborne:** \*THR LEVERS...............................................................TOGA AP (If engaged)......................................................KEEP ON SRS ORDERS..........................................................FOLLOW **Landing:** \*GO AROUND........................................................PERFORM AP (If engaged)......................................................KEEP ON GO TO FCOM PRO-ABN-SURV FOR WINDSHEAR AHEAD (RED) PROCEDURE