CJ1+

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Matthias Telgmann

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Matthias Telgmann

À propos de ce fichier

Diese Lernkarten bieten eine umfassende Übersicht über die technischen Spezifikationen und Betriebsgrenzen von Flugzeugen, insbesondere im Hinblick auf Gewicht, Geschwindigkeit und Systemdesign. Sie decken Aspekte wie maximale Start- und Landungsgewichte, Fluggeschwindigkeiten, Systeme wie TAWS und EGPWS sowie die Positionierung von Flugkontrollen ab. Piloten und Flugtechniker profitieren von diesen Informationen, um sichere und effiziente Flugoperationen zu gewährleisten, indem sie die Betriebsgrenzen und Systemfunktionen verstehen.

Cartes-fiches

Utilisateurs

Langue

Allemand

Catégorie

Technique

Niveau

Autres

Créé / Mis à jour

12.05.2014 / 19.12.2019

Fichiers de cartes similaires

Cartes-fiches

V(FE)

Maximum Speed With Flaps Failed to GROUND FLAPS Position (60°)

140 KIAS

190 KIAS

200 KIAS

213 KIAS

The maximum operating limit speeds must not be deliberately exceeded in any regime of flight (climb, cruise or descent) unless a higher speed is authorized for flight test or pilot training.

V(FE)

LAND Position (35°)

161 KIAS

200 KIAS

120 KIAS

136 KIAS

The maximum operating limit speeds must not be deliberately exceeded in any regime of flight (climb, cruise or descent) unless a higher speed is authorized for flight test or pilot training.

V(FE)

LAND Position (35°)

120 KIAS

200 KIAS

162 KIAS

165 KIAS

161 KIAS

VMO / MMO

MMO (Above 30,500 Feet)

0,691 MACH

0,710 MACH

0,590 MACH

0,810 MACH

0,900 MACH

VMO / MMO

VMO (Between Sea Level and 30,500 Feet)

259 KIAS

263 KIAS

251 KIAS

273 KIAS

264 KIAS

Weight Limitations

Maximum Design Ramp Weight

10,800 lbs

9,900 lbs

10,700 LBS

8,400 lbs

5,400 lbs

Maximum Design Takeoff Weight

10,800 lbs

9,900 lbs

10,700 lbs

8,800 lbs

there is no limit

Maximum Design Landing Weight

8,400 lbs

there is no limit

10,900

9,950 lbs

9,900 lbs

Maximum Design Zero Fuel Weight

10,300 lbs

9,500 lbs

8,400 lbs

12,100 lbs

Takeoff weight is limited by the most restrictive of the following requirements:

Maximum Certified Takeoff Weight 10,700 lbs

Maximum Design Zero Fuel Weight

Maximum Takeoff Weight, permitted by Climb Requirements

Takeoff Field Length

Brake Energy Limits

Landing weight is limited by the most restrictive of the following requirements:

Maximum Design Ramp Weight

Maximum Certified Landing Weight 9,900 lbs

Maximum Landing Weight Permitted by Climb Requirements or Brake Energy Limits

Maximum Design Takeoff Weight

Landing Distance

Abbrevations:

ADC

Air Data Computer (same as DADC)

Abbrevations:

AHRS

Attitude Heading Reference System

Abbrevations:

CDI

course deviation indicator

Abbrevations:

CDU

Control display unit (interface to FMS)

Abbrevations:

Dead Reckoning

Abbrevations:

FLC

Flight Level Change (airspeed mode)

Abbrevations:

IAPS

Integrated avionics processing system

Abbrevations:

MFD

Multifunction Display

Abbrevations:

EGPWS

Enhanced Ground Proximity Warning System

Abbrevations:

TAWS

Terrain alert and warning system

Abbrevations:

Yaw Damper

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