Limitations Flashcards by W H

Nominal Runway Width

148 ft

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Minimal Runway Width

100 ft

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Max demonstrated crosswind (dry runway)

38 kt (gust included)

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Max demonstrated crosswind

wet runway

33 kt (gust included)

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Max demonstrated crosswind

contaminated runway

10 kt (gust included)

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Max tailwind for takeoff/landing

10 kt

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Max wind for pax door door operation

65 kt

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Max wind for FWD and AFT cargo door operation

40 kt (or 50 kt if the aircraft nose is into the wind, or if the doors are on the leeward side).

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FWD and AFT cargo doors must be closed before the wind speed exceeds….

65 kt

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Max flap/slat speeds:

Config 1

230 kt

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Max flap/slat speed:

Config 1+F

215 kt

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Max flap/slat speed:

Config 2

200 kt

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Max flap/slat speed:

Config 3

185

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Max flap/slat speed:

Config Full

177

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Max speed with gear extended- VLE

280 kt/M 0.67

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Max speed gear may be extended- VLO Extension

250 kt/M 0.60

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Max speed gear may be retracted- VLO Retraction

220 kt/M 0.54

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Max tire speed

195 kt

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Max speed for windshield wipers

230 kt

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Max speed cockpit window

200 kt

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Min height for use of autopilot on takeoff with SRS mode

100 ft AGL or 5 seconds after takeoff

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Min height for use of the autopilot on an ILS approach with CAT3 SINGLE/DUAL displayed on the FMA

50 ft below DA

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Min height for use of the autopilot during:

-straight in non-precision approach

250 ft AGL

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Min height for use of the autopilot on an ILS approach with CAT1 displayed on the FMA

160 ft AGL

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Min height for use of the autopilot during: | -circling approach

500 AGL

Min height for use of the autopilot during: | -Go-around (AP or FD engagement)

100 ft AGL

Min height for use of the autopilot during: | -All other phases

500 ft AGL

What must the FCU altitude be set to when in OPEN DES or DES mode on approach?

At or above MDA, or 500 ft, whichever is highest

What approaches cannot be used in NAV or NAV and APP NAV and FINAL APP mode

ILS, LOC, LOC B/C, LDA

A navaids approach may be performed in NAV, APP NAV, or FINAL APP provided that:

- AP or FD is used and, - if GPS PRIMARY is available: Reference navaid may be unserviceable, or the airborne radio equipment may be inoperative, or not installed, with operational approval -if GPS PRIMARY is not available: Reference navaid and corresponding airborne equipment are serviceable, tuned and monitored

RNAV (GNSS) approaches may be preformed provided that...

-GPS PRIMARY is available

NAV mode may be used in the terminal area provided...

- GPS PRIMARY is available, or - HIGH accuracy is displayed, and appropriate RNP is checked or entered on MCDU, or - FMS navigation is cross-checked with navaid raw data

Max operating altitude for use of flaps/slats

20,000 ft

While engine-out, it is prohibited to use the autopilot to preform non-precision apps in what modes? (319 aircraft only)

FINAL APP, NAV V/S, or NAV/FPA

Fuel: Min fuel quantity for takeoff

3,307 lbs

Fuel: Prior to takeoff, if WING TK LO LVL warning is displayed on ECAM...

Takeoff is prohibited

Fuel: What order of tanks do we burn fuel

Center tank then wing tanks

Fuel: Takeoff on center tank is...

Prohibited

Hydraulic: Normal operating pressure

3000 psi +/- 200

Max brake temp for takeoff (brake fans, if installed, off)

300 *C

May the APU be started and operated if the LOW OIL LEVEL ECAM advisory is displayed?

Yes, maintenance action is required within next 10h of APU operation

APU: Starter duty cycle

3 starter duty cycles, wait 60 mins before attempting 3 more cycles

Can we use APU bleed air for wing anti-icing?

Engines: Max EGT for takeoff and go-around

950 *C for 5 mins | 10 mins only in case of engine failure

Engines: Max EGT for MCT

915 *C

Engines: Max EGT for starting

725 *C

Engines: Max continuous oil temp

140 *C

Engines: Max transient oil temp (15 mins)

155 *C

Engines: Min oil temp for starting

-40 *C

Engines: Min Oil Quantity

9.5 qt + 0.5 qt/hr

What is T MAX FLEX?

ISA +53 °C -the max allowable flex temperature so that thrust reduction does not exceed 25% of the full rated takeoff thrust

During Flex takeoffs, the assumed temp must not be lower than...

The flat rating temp or the current OAT

Can we takeoff at reduced thrust on a contaminated runway?

Can we takeoff at reduced thrust with any inoperative item that affects performance?

Yes, as long as we still meet all performance requirements after the penalty has been applied.

Engines: Starter duty cycle

A standard auto start includes up to 3 start attempts, is considered 1 cycle 4 consecutive cycles with 20 sec pause between each, 15 min cooling period after 4th cycle -no running engagement of the starter when N2 is above 20%

Engines: When is reverse thrust not permitted?

- In flight - To back up the aircraft - Max reverse should not be used below 70 kt (idle reverse is permitted to aircraft stop)

Flight Maneuvering Load Limits: | Clean Configuration

-1g to +2.5g

Flight Maneuvering Load Limits: | Slats or Flaps extended

0g to +2g

Max Runway Slope

+/- 2%

Max Takeoff Altitude

9,200 ft

What 3 contaminated runway conditions is takeoff not recommended?

- wet ice - water on top of compacted snow - dry snow or wet snow over ice

Vmo/Mmo

350 kts / 0.82 Mach

Max Cabin Differential Pressure

9 psi

Max Negative differential pressure

-1 psi

Safety relief valve setting

8.6 psi

Max continuous load per TR

200 A

Max degrees with handwheel?

75*

Max degrees during pushback?

95*

At what N speed will the APU automatically shut down?

107% (ECAM display)

APU Bleed: Max altitude to assist engine start

20,000 ft

APU Bleed: Max altitude for air conditioning and pressurization (single pack)

20,000 ft

Engines: Min oil temp for takeoff

-10 *C

APU Bleed: Max altitude for air conditioning and pressurization (dual pack)

15,000 ft

When is dispatch to/from narrow runways not allowed?

- nose wheel steering inop | - one or more brake inop

Limitation on speed for a turn during taxi when taxi weight is above what weight?

Do not exceed 20kts during turn when above 167,550 lbs

Narrow Runway Ops- Diversion to a 148ft wide runway is recommended in case of:

- Rudder jam - Rudder pedal jam - Yaw damper system fault - Rudder travel limit system fault - All failures leading to loss of the nose wheel steering