BCSX Limitations

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Über diese Lernkartei

Diese Karteikarten bieten eine grundlegende Einführung in die technischen Grenzen und Betriebsbedingungen von Flugzeugen, insbesondere im Hinblick auf Wind, Temperatur und Runway-Bedingungen. Sie behandeln wichtige Begrenzungen wie maximale Geschwindigkeiten, Höhenrestriktionen und spezifische Verfahren für den Start und die Landung unter verschiedenen Wetterbedingungen. Piloten und Flugpersonal profitieren von diesen Informationen, um sichere und effiziente Flugoperationen zu gewährleisten, insbesondere in herausfordernden Umgebungen wie starkem Wind oder vereisten Pisten.

Karten

195

Lernende

Sprache

Deutsch

Kategorie

Elektrotechnik

Stufe

Grundschule

Erstellt / Aktualisiert

26.01.2023 / 16.05.2024

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APPR 2 (no autoland) min Runway width

Land 2 (autoland) min Runway width

ASA displays highest capability between ____(ft) and ____(ft)

1500 800

Retard armed (ft)

400

ALIGN arm, FLARE arm from ____ ft to ____ ft

350 250

ALIGN active from ____ to _____

200 150

FLARE active, Rollout arm at ____ ft

RETARD active at ft

ROLLOUT active WW + ___ seconds

Rollout is removed at ___ kts

Thrust Limitation at Low Speed (TLLS) limits the thrust of the engines to approximately ___% of the takeoff power. As the aircraft accelerates in the takeoff run, thrust increases with airspeed and reaches full power at ____ kt.

60 80

APPROACH IDLE is avtive when:

aircraft descends below _____ ft RA

when F___ is selected

when the_____ is down

400 4 gear

Minimum oxygen dispatch pressure with 2 crew members in cockpit (whilst flying over mountainous terrain)

950

Minimum oxygen dispatch pressure with 3 crew members in cockpit (whilst flying over mountainous terrain)

1300

Minimum height with flight spoilers manually extended is ____ft AGL.

300

Minimum speed with flight spoilers manually extended is VREF + ____ KIAS.

BTMS range green? format: XX-XX

00-06

BTMS range white? format: XX-XX

07-14

BTMS range red? format: XX-XX

15-20

Takeoff allowed with BTMS in _____ ranging from which values?

format: (colour) XX-XX

white 07-09

Certified max. altitude in icing conditions (ft)

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

35000

General certification for landings with approach path angles no greater than ??.? degrees

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

3.5

BCS1 MTOW (kg)

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

58000

BCS1 MLW (kg) approx on hundreds

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

52400

BCS3 MTOW (kg)

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

65000

BCS3 MLW (kg) approx on hundreds

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

58700

VMO (kt) > FL100

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

330

VMO (kt) < FL80

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

300

MMO (M)

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

0.82

BCS1+BSC3 VA (design manoevering speed) in direct mode (M)

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

0.8

BCS1 VA (design manoevering speed) in direct mode (KIAS)

format: XXX-XXX

285-300

BCS3 VA (design manoevering speed) in direct mode (KIAS)

300

VFE FLAP 1 (KIAS)

230

VFE FLAP 2 (KIAS)

210

VFE FLAP 3 (KIAS)

210

VFE FLAP 4 (KIAS)

190

VFE FLAP 5 (KIAS)

170

VLO extension (KIAS)

250

VLO retraction (KIAS)

220

VLE (KIAS) The maximum speed with landing gear extended is

250

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Cartes-fiches

T/O RCAM Crosswind Limit

Dry

T/O RCAM Crosswind Limit

Damp, wet, water, slush, sry or wet snow <= 3mm

T/O RCAM Crosswind Limit

Compacted Snow <= -15°C

T/O RCAM Crosswind Limit

Compacted Snow > -15°C

Slippery Wet

Ice treated,

Dry Snow

Wet Snow

T/O RCAM Crosswind Limit

Slush, Standin Water, Ice

T/O RCAM Crosswind Limit

Wet Ice

Water on top of Comp Snow

Dry Snow or Wet Snow on top of ice

no takeoff

LDG RCAM Crosswind Limit BCS1

BA 6

LDG RCAM Crosswind Limit BCS3

BA 6

LDG RCAM Crosswind Limit BCS1

BA 5

LDG RCAM Crosswind Limit BCS3

BA 5

LDG RCAM Crosswind Limit BCS1 + BCS3

BA 4

LDG RCAM Crosswind Limit BCS1 + BCS3

BA 3

LDG RCAM Crosswind Limit BCS1 + BCS3

BA 2

LDG RCAM Crosswind Limit BCS1 + BCS3

BA 1

maximum runway slope positive limit (%)

maximum runway slope negative limit (%)

-2

BCS1 maximum number of cabin occupants

129

BCS3 maximum number of cabin occupants

149

minimum runway width (m)

maximum distance from adequate airport (NM)

360

maximum positive pressure differential in psi delta

8.8

maximum negative pressure differential in psi delta

-0.5

maximum pressure differential in psi delta during inital touch down (Landing)

minimum height for autopilot engagement (ft) AGL

400

minimum height for autopilot disengagement (ft) AGL if a manual landing is planned

During approach and landing with autothrottle, approach speed must be increased by ___ kts

If the autothrotte incremet is not made, the autothrottle must be switched off before descending below ____ ft AAE or when reducing to VRef earlier

1000

minimum oil temperature for an APU start is ___°C

-40

how many APU start attempts maximum per hour?

How much delay must be ovserved between start attempts? (min)

altitude limit for APU bleed air extraction (FL)

FL230

When ever using APU Bleed as source, check tables in FCOM

yes

maximum AC generator lad must not exceed ____ kVA continuous

The maximum permissible continuous load on TRU 1 and 2 is ___ amp

350

The maximum permissible continous load on TRU 3 is ___ amp

225

maximum altitude with slats/flaps extended (FL)

FL200

maximum height with flight spoilers extended (ft AGL)

300

minimum speed with flight spoilers extended vRef + ____ KIAS

maximum permissible fuel imbalance between contents of left and right tank is (kg)

454

BCS1 maximum usable fuel load (kg) left/right main

3080

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