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F9 > F9 > Flashcards

F9 Flashcards

0
Q

Weights

A

A319 155,200 154,320 134,480 125,660
A319 IGW 167,320 166,440 137,780 128,960
A320 170,630 169,750 142,190 134,480
A320 IGW 170,630 169,750 145,500 137,780
A320 NEO 170,630 169,750 148,590 141,750
A321 207,010 206,130 171,520 162,700

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1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS
Clean configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Slats and/or flaps extended . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A

Clean -1 to 2.5

Flaps n slats 0 to 2

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2
Q

Slope
Runway alt
Min runway width

A

+- 2

9200

100ft / 30 m

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3
Q

Maximum crosswind demonstrated for takeoff . . . . . . . . . . . . . . . . . . . . . . . . .

Maximum crosswind demonstrated for landing. . . . . . . . . . . . . . . . . . . . . . . . .

Maximum tailwind for takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Maximum tailwind for landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A

Maximum crosswind(1)
Takeoff Landing.
35kts 38kts
Maximum tailwind(1).
A319 &A320s A321s
Takeoff Landing Takeoff Landing
15kts 10kts 10kts. 10kts

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4
Q

– A normal runway is any runway at least ……wide.

– A narrow runway is any runway less than ……wide.

A

150 ft / 45 m

100 ft/ 33 m

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5
Q

Diversion to a normal runway is recommended in case of:

A 
• Autoland is not authorized
• Diversion to normal width runway is recommended 
in case of:
– Rudder jam
– Rudder pedal jam
– Yaw damper fault
– No nosewheel steering
– Any wheel brake inoperative
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6
Q

PASSENGER & CARGO DOOR LIMITATIONS

A

MAXIMUM WIND FOR PASSENGER DOOR OPERATION 65kts
MAXIMUM WIND FOR CARGO DOOR OPERATIONS 40kts/50kts(1)
(1) If the aircraft nose is oriented into the wind, or if the cargo door is on the leeward side of the aircraft, operation of the cargo door

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7
Q

SPEED LIMITATIONS

Maximum VMO/MMO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt/…..mach

A

350 / .82

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8
Q

Turbulence speed
FL200 and below. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt
Above FL200 through FL310 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt
Above FL310 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . mach

A

250
275
.76

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9
Q

Flap slat speed

A

Flap 319/320. A321 Flt Phase
1 18 0/0/0 1 230 235 Holding
1 18 10/10/10 1 + F 215 225 Takeoff
2 22 15/15/14 2 200 215 TO / App
3 22 20/20/21 3 185 195 TOAppLdg
FULL 27 40/35/25 FULL 177 190 Landing

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10
Q

Gear

Maximum speed with landing gear extended (VLE) . . . . . . . . . . . . . . . …..kt/….mach
Maximum speed at which the landing gear may be extended . . . . . . . . . . . . . . . kt
(VLO extension)
Maximum speed at which the landing gear may be retracted . . . . . . . . . . . . . . . kt
(VLO retraction)

A

280/.67
250
220

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11
Q

Maximum altitude at which the landing gear may be extended . . . . . . . . . ft

A

25000

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12
Q

Maximum Tire Speed (ground speed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt

A

195

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13
Q

Maximum speed for use of windshield wipers . . . . . . . . . . . . . . . . . . . . . . . . . . kt

A

230

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14
Q

Maximum speed for opening cockpit window . . . . . . . . . . . . . . . . . . . . . . . . . . kt

A

200

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15
Q

Max taxi speed Weight Greater than 167,550 lbs

A

20knts

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16
Q

Max operating altitude with slats and/or flaps extended is ……..feet.

A

20000

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17
Q

Cabin pressure
Maximum positive differential pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . psi
Maximum negative differential pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . psi
Safety relief valve setting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . psi

A
  1. 0
    - 1
  2. 6
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18
Q

Ram air inlet
If change in P is greater than …..psi, the check valve located downstream will not open even if
the ram air door has been selected open.

A

1

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19
Q

Air conditioning
WITH LP GROUND UNIT
Do not use conditioned air simultaneously from …..and …..ground unit (to avoid
chattering of the non return valves).

A

Packs, LP

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20
Q

WITH HP GROUND UNIT
An external ….. source may be used for air conditioning, provided the air supply is
confirmed to be free from ….. contamination. Do not use …. ground unit when ….. supplies bleed air to avoid bleed system damage.

A

HP, oil, HP, APU

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21
Q

Avionics ventilation
The airplane electrical system should not be powered for more than …. hours without
a cooling system when the outside air temperature is above ….C.

A

2, 49

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22
Q

Reporting sheet
Airframe vibrations shall be recorded in the aircraft …….and on the ………….. (Form 31048), which contains detailed
information used by maintenance to isolate and resolve airframe vibration issues.
Whenever possible this form should be filled out in …… and as soon as practical after
experiencing airframe vibration. Completed forms shall be left in the ………… .

A

Logbook, airframe vibration reporting sheet, flight, aircraft logbook

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23
Q

APU
The APU may be started and operated even if the …………….. advisory is
displayed. Maintenance action is required within the next …… hours of APU operation.
NOTE: A logbook entry is not required after receiving this advisory message.
Contact …… to determine the status of required maintenance action.

A

Low oil level exam,10 , mcc

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24
Q

APU
After ….. starter motor duty cycles, each separated by a …. minute cool down, wait
….. minutes before attempting three more cycles.

A

3, 1, 60

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25
Q

APU
Maximum N . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . %
NOTE: The APU automatically shuts down at % N speed (ECAM display).
Maximum EGT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C
Maximum EGT for start (below 35,000 feet) . . . . . . . . . . . . . . . . . . . . . . . . . . . . C
Maximum EGT for start (above 35,000 feet) . . . . . . . . . . . . . . . . . . . . . . . . . . . . C

A 
107
107
675
1090
1120
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26
Q

Maximum altitude for APU electrical and start . . . . . . . . . . . . . . . . . . . . . . . . . ft

A

39000

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27
Q

Maximum altitude for APU battery start . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ft

A

25000

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28
Q

Maximum altitude for APU pneumatics (1 pack w/electrical) . . . . . . . . . . . . .ft

A

22500

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29
Q

Maximum altitude for APU assisted engine start . . . . . . . . . . . . . . . . . . . . . . . Ft

A

20000

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30
Q

Maximum altitude for APU pneumatics (2 packs w/electrical) . . . . . . . . . . . . Ft

A

15000

31
Q

Autopilot After Takeoff/Go-Around (If SRS is indicated) …AGL

A

100

32
Q

Autopilot enroute

A

500

33
Q

Autopilot Non-Precision Approaches

A

DDA/DA

34
Q

Autopilot Non-Autoland ILS Approach with CAT 1 displayed on FMA

A

160

35
Q

Autopilot Non-Autoland ILS Approach with CAT 2/3 displayed on FMA

A

80

36
Q

Autopilot Autoland ILS Approach (one or two autopilots)

A

Rollout/taxi

37
Q

Autopilot
When visibility is less than …..RVR or ….,the approach must be flown with the
autopilot(s) engaged if operable.

A

4000 / 3/4

38
Q

Autopilot
The use of AP or FD in OPEN DES or DES mode is not permitted inside the ……or
below …….ft AGL on a visual approach.

A

FAF

1000

39
Q

The use of autothrust is approved with or without ……in selected or managed
mode.

A

AP/FD

40
Q

NON PRECISION APPROACHES WITH ENGINE-OUT
If one engine is inoperative, it is ………..to use the autopilot to perform non
precision approaches in the following modes: FINAL APP, NAV V/S, NAV/FPA (not
applicable on A/C 205 - 216, 220, 223 & 227).
Only…..use is authorized.

A

Not permitted,

Fad

41
Q

FLIGHT MANAGEMENT FUNCTION
FMGS lateral and vertical navigation has been certified for takeoff, departure, en
route, arrival (terminal area operations), instrument approach procedures (except ….,
…. and ….) and missed approach/go around procedures.

A

ILS, LOC, LDA

42
Q 
RNP accuracy with GPS PRIMARY, or radio updating, has been demonstrated to be:
With AP ON in NAV With AP OFF and FD 
on in NAV
With AP OFF and FD 
OFF
En route ...nm ....nm ....nm
Terminal area ....nm .....nm ....nm
Approach ....nm ....nm ......
A

1 1 1.1
.5. .51. .51
.3. .3. Not authorized

43
Q

Without ………… (GPS deselected or inoperative), …..accuracy has been
demonstrated provided the appropriate RNP value is checked or entered on the MCDU
and …….accuracy is displayed.

A

GPS Primary, NAV, HIGH

44
Q

RNP 0.3 has been demonstrated in normal and non-normal conditions as follows for
the following modes.
–
–
–
–
NOTE: Use of AP for RNP AR operations is recommended.

A

– Departure in NAV mode,
– Initial approach in NAV or APP NAV modes,
– Final approach in FINAL APP mode,
– Missed approach in NAV mode.

45
Q

Autoland approaches may be conducted when the following conditions are satisfied:

A

CAT II/III runway, CAT II/III aircraft, crews CAT II/III trained, appropriate ground facilities
are operational, wind within limits, braking action medium or better.

46
Q

toland Required: If the requirements for an autoland are satisfied and the ATIS
reported RVR/visibility is at or below …….RVR or ……mile, the approach must be
briefed and flown as a CAT II or CAT III autoland except as noted below.
NOTE: If any of the CAT II/III requirements are not met, and CAT I or better
weather conditions prevail upon arrival at the airport, the crew may brief
and fly the approach to current CAT I minimums as stated in FOM I, Chapter
20, with a manual landing

A

2400, 1/2

47
Q

Autolands are prohibited if braking action is reported less than

A

Medium

48
Q

Autolands are not authorized on runways less than …..feet wide

A

150

49
Q

Automatic landing is not allowed below ……ft pressure altitude.

A

-1000

50
Q

Autobrakes (if available) are required for all CAT III approaches.
– Runways less than 8000 ft – …….
– Runways 8000 ft or longer – ……..

A

Medium

Low or medium

51
Q

“PULL UP” - “OBSTACLE AHEAD PULL UP” - “TERRAIN AHEAD PULL UP”

A

– AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
– PITCH. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL UP
Pull to full backstick and maintain in that position.
– THRUST LEVERS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TOGA

52
Q

Emergency decent

A

CREW OXY MASKS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE
– SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
– EMER DESCENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE)
– THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .IDLE
– SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL

53
Q

Loss of braking

A

– 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

54
Q

SMOKE / FUMES / AVNCS SMOKE

A

– OXY MASK/GOGGLE . . . . . . . . . . . . . . . . .USE/100%/EMERG

55
Q

Stall recovery

A

– NOSE DOWN PITCH CONTROL . . . . . . . . . . . . . . . . . . . .APPLY
– BANK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL
– THRUST . . . . . . . . . . . . . . .INCREASE SMOOTHLY AS NEEDED
– SPEEDBRAKES. . . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED
– FLIGHT PATH. . . . . . . . . . . . . . . . . . . . . .RECOVER SMOOTHLY
– FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT

56
Q

Stall warning at lift off

A

– THRUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TOGA
– PITCH ATTITUDE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .15°
– BANK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL

57
Q

Tcas warning

A

AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
– BOTH FDs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
– Respond promptly and smoothly to an RA by adjusting or maintaining the vertical
speed, as required, to reach the green area and/or avoid the red area of the
vertical speed scale.

58
Q

UNRELIABLE SPEED INDICATION/ADR CHECK PROCEDURE

A/C 201 - 204, 218, 219, 221, 223 AND ALL A319

A

– AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
– A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
– THRUST/PITCH
– Below THR RED ALT. . . . . . . . . . . . . . . . . . . . . . . . .15TOGA
– Above THR RED ALT and Below FL 100 . . . . . . . . 10CL
– Above THR RED ALT and Above FL 100 . . . . . . . . .5CL
– FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN CURRENT CONFIG
– FLAPS (if CONF FULL). . . . . . . . . . SELECT CONF 3 AND MAINTAIN
– SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED
– L/G . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UP

59
Q

UNRELIABLE SPEED INDICATION/ADR CHECK PROCEDURE

A/C 205 - 216, 220, 227

A

– AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
– A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
– THRUST/PITCH
– Below THR RED ALT . . . . . . . . . . . . . . . . . . . . . . . . .15TOGA
– Above THR RED ALT and Below FL 100 . . . . . . . . .10CL
– Above THR RED ALT and Above FL 100 . . . . . . . . . 5CL
– FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN CURRENT CONFIG
– FLAPS (if CONF FULL) . . . . . . . . . . SELECT CONF 3 AND MAINTAIN
– SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . . . . . .CHECK RETRACTED
– L/G. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

60
Q

Wind shear

A

WINDSHEAR
Refer to ABN-80 WINDSHEAR or FOM Vol II 4.10
 If after V1
 AIRBORNE, INITIAL CLIMB or LANDING
– THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TOGA
– REACHING VR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ROTATE
– SRS ORDERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FOLLOW
This includes the use of full back stick, if demanded.
– THR LEVERS AT TOGA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET OR CONFIRM
– AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .KEEP ON
– SRS ORDERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FOLLOW

61
Q

Winds hear ahead

A

WINDSHEAR AHEAD
Refer to ABN-80 WINDSHEAR or FOM Vol II 4.10
 When airborne
As usual, the slat/flap configuration can be changed, provided the windshear is not entered.
 During landing
– THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TOGA
– AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .KEEP ON
– SRS ORDERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FOLLOW
– GO AROUND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PERFORM
– AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . KEEP ON

62
Q

321 weights

A

Max taxi wt 207010
Max to wt 206130
Max ld wt 171520
Zero fuel wt 162700

63
Q

Max tail wind for take off. 319, 320, 321

A

15,15,10

64
Q

Flap slats 321

1,
1 +f,
2,
3,
4,
A 
235
225
215
195
190
65
Q

Taxi when over 167550 don’t go faster than?

A

20 knots in turn

66
Q

Max altitude with flap/slats extended

A

20000

67
Q

Only open ram air inlet when pressure diff is?

A

Lower than 1psi

68
Q

AUTOLAND PERFORMANCE LIMITS (BELOW 500 FT)

A 
– Glideslope Deviation < one dot
– Localizer Deviation < 1/4 dot
– Airspeed ±5 knots of target
– Max Rate of Descent 1000 fpm
– Airspeed not below VLS
– Bank not to exceed 7°
– -2.5° < Pitch < 10°
69
Q

GENERATOR LOAD – MAXIMUM

A

Continuous load per generator100% (90 kVA)

70
Q

TR LOAD – MAXIMUM

A

Continuous load per TR200 amps

71
Q

ENGINE EGT AND THRUST - MAXIMUM

A

OPERATING CONDITION TIME LIMIT (1) EGT LIMIT NOTE
TAKEOFF and GO-AROUND
5 min. 950°C
10 min. Only in case of engine failure

MCT Unlimited 915°C
STARTING. 725°C

72
Q

ENGINE OIL QUANTITY

A

11 Quarts plus .5 quart for every hour of estimated flight time

73
Q

Minimum oil temperature for takeoff

A

19° C

74
Q

Takeoff at reduced thrust is prohibited:

A

• on slippery or contaminated runways;
• when suspected, reported or known wind shear is present (e.g., predictive wind shear alerts, or ATC-
issued wind shear alerts for the departure runway or departure path);
• when a Special Departure Procedure specifies full thrust for takeoff.

75
Q

AVIONICS VENTILATION

A

The aircraft electrical system should not be powered for more than 2 hours without a cooling system when the
outside air temperature is above 49°C

75
Q

Auto land max wind

A

Include gusts when applying these wind limits.
A320 & A321 A320NEO & A319
Headwind. 30 knots 20 knots
Crosswind. 15 knots 15 knots
Tailwind. 10 knots 5 knots
Wind Correction: Vls + wind correction(2)
5 to 15 knots 5 to 15 knots

F9 (1 decks)

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