Lernkarten

Karten 37 Karten
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Erstellt / Aktualisiert 02.04.2020 / 18.06.2020
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3 Exakte Antworten 13 Text Antworten 21 Multiple Choice Antworten

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Fenster schliessen

Turbulent air penetration speed

Below 25.000 ft

250

260

270

280

Fenster schliessen

Turbulent air penetration speed

above 25,000 ft? ......whichever is lower.

260 kts or 0.80

270 kts or 0.81

280 kts or 0.82

290 kts or 0.83

Fenster schliessen

Turbulent air penetration speed

Maintain how many kts above minimum Maneuvering speed at all altitudes when airspeed

is below 0.82 Mach?

5 kts

10 kts

15 kts

20 kts

Fenster schliessen

Autopilot/Flight Director System

Do no use Autopilot below ..... ft RA at airport elev. above .... ft

50 ft RA and 8300 ft

100 ft RA and 8500 ft

150 ft RA and 8700 ft

200 ft RA and 8900 ft

Fenster schliessen

Autopilot/Flight Director System

Autopilot must not be engaged below a minimum engage altitude of ...... after take off.

100 ft AGL

100 ft MSL

200 ft AGL

200 ft MSL

Fenster schliessen

Do NOT use FLCH on final approach below which altitude?

500 ft AFE

500 ft AGL

1000 ft AFE

1000 ft AGL

Fenster schliessen

Without LAND 2 or Land 3 Announciated, the autopilot must be

disengaged below how many feet?

100 ft AGL

100 ft AFE

200 ft AGL

200 ft AFE

Fenster schliessen

Reverse Thrust

Inentional selection of reverse thrust in flight is allowed?

YES

NO

Fenster schliessen

Reverse Thrust

Inentional selection of reverse thrust in flight is prohibited?

YES

NO

Fenster schliessen

Reverse Thrust

Backing the airplane with use of reverse thrust is prohibited?

YES

NO

Fenster schliessen

Reverse Thrust

Backing the airplane with use of reverse thrust is allowed?

YES

NO

Fenster schliessen

Flight Controls

The maximum altitude with flaps extended is?

18.000 ft

19.000 ft

20.000 ft

20.200 ft

22.000 ft

Fenster schliessen

Flight Controls

Large alternating control inputs (changes in pitch, yaw, roll) result in? 

structural failure

phugoid

pilot induced oscillation

upset of the aircraft

Fenster schliessen

Flight Controls 

At which speed can structural failure occure due to large alternating flight control inputs?

max 250 kts

max 310 kts / .84

Vmo/Mmo

any speed

Fenster schliessen

Name indications of ICE CRYSTAL ICING! (5)

1. Flying above amber/red weather radar indications

2. TAT ~ 0° (EICAS)

3. Liquid water on the windshield at temperatures too cold for rain

4. A/T Disconnects

5. Abnormal Engine vibrations/indications

-----------------

6. Smell of ozon/sulfur

7. Light/moderate turbulence

8. Static discharge on windshield

9. Humidity increase

Fenster schliessen

Aborted Engines Start L,R Memory Items

FUEL CONTROL Switch .........CUT OFF
Fenster schliessen

Aborted Engine Start L,R Condition (2)?

Manual Start: All abort conditions

Autostart: EGT rise but NO Oil pressure rise

Fenster schliessen

Unreliable airspeed Memory Items

1. Autopilot disengage switch ......... Push

2. A/T Arm switches (both)     .......... OFF

3. F/D Switches (both) ..................... OFF

4. Set the following gear up pitch attitude and thrust:

                 Flaps extended: 85% N1 and 10° pitch

                 Flaps retracted: 70% N1 and 4° pitch

                 In cruise: 82.5 N1 und 2.5° pitch

Fenster schliessen

[ ] Cabin Altitude (Memory Items)

1. Don oxygen masks

2. Establish crew communication

3. Monitor cabin altitude and rate

IF cabin altitude is uncontrollable:

PF: "Emergency descend!"

PM: Suppernumary oxygenswitch.....push and hold for 1 sec. 

Without delay descend to 10.000 ft or minimum safe altitude whichever is higher.

To descend: 

1. Altitude window

2. HDG Select (90° of Track)

3. FLCH

4. Extend Speedbrakes

5. Thrustlever IDLE

 

Fenster schliessen

Dual Engine Fail/Stall (Memory items)

Engine Speed of both engines is below idle

1. Fuel Control Switches (both) ........ CUTOFF, then RUN

2. RAM AIR TURBINE switch ............ Push and Hold for 1 sec. 

Fenster schliessen

Engine Lim/Surge/Stall L,R

1. A/T ARM switch .............. OFF

2. Thrust lever .......... RETARD until engine indications stay within limits or thrust lever is at idle

Fenster schliessen

ENG/LIM/SURGE/STALL L, R (Conditions)

Engine indications are abnormal

Engine indications are quickly nearing or show an exceedence

Abnormal engine noises are heard, possibly with engine virbrations

There is no response to thrustlever movement or the response is abnormal

Flames in the Engine inletor exhaust are reported

Fenster schliessen

[ ] ENG AUTOSTART L, R (Memory Items)

1. FUEL CONTROL switch ........ CUT OFF
Fenster schliessen

[ ] AUTOSTART L, R (Conditions)

During Ground Start one of these occurs:

1. Airframe vibration with abnormal engine indication

2. Fuel control switch is in RUN at low engine RPM with

Autostart switch OFF

Fenster schliessen

ENG Svr Damage/Sep L, R (Memory Items)

1. A/T arm switch ........ OFF

2. Thrust lever .............. IDLE

3. FUEL CONTROL switch .... CUT OFF

4. Engine Fire switch ............ PULL

Fenster schliessen

ENG Svr Damage/Sep L, R (Conditions)

Airframe vibration with abnormal engine indication

Engine seperation

Fenster schliessen

[ ] FIRE ENG L, R

1. A/T ARM switch  ...... OFF

2. Thrust lever .............. Idle

3. FUEL CONTROL switch ...... CUT OFF

4. Engine fire switch ............... Pull

5. IF engine fire message stays shown:

engine fire switch ........... Rotate to the stop and hold for 1 sec.

IF after 30 sec. The FIRE ENG message stays shown:

Engine fire switch ...... rotate to the other stop and hold for 1 sec.

Fenster schliessen

[ ] Stabilizer 

1. STAB cutout switches (both) ......... CUTOUT

2. Do not exceed the current airspeed

Fenster schliessen

[ ] Stabilizer  (Condition)

One of these Occurs:

Stabilizer movement without a signal to trim

The stabilizer is failed

Fenster schliessen

Operational Limitations

Maximum Takeoff and Landing Tailwind Component 

10 kts

15 kts

20 kts

25 kts