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Flying > F100 > Flashcards

F100 Flashcards

1
Q

Max operating altitude

A

35000ft

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2
Q

Max take off and landing altitude

A

8000ft

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3
Q

Max operating temperature

A

ISA + 35˚

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4
Q

Max temperature on the ground with avionics cooling inop

A

44˚

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5
Q

Max ramp weight F100

A

44680kg
(230kg above MTOW)

UQD - 46040kg (extra 1360kg)

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6
Q

Max take off weight F100

A

44450kg

UQD - 45810kg (extra 1360kg)

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7
Q

Max landing weight F100

A

39915kg

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8
Q

Max zero fuel weight F100

A

36740kg

UQW - 37420kg (extra 680kg payload)

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9
Q

Max flap extension altitude

A

FL200

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10
Q

Max gear extension altitude

A

FL250

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11
Q

Vmo/Mmo

A

320/.77

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12
Q

Vra

A

250/.65

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13
Q

Vfe8

A

250kt

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14
Q

Vfe15

A

220kt

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15
Q

Vfe25

A

220kt

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16
Q

Vfe42

A

180kt

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17
Q

Vlo/Vle

A

200kt

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18
Q

Max lift dumper extend speed

A

170kt

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19
Q

Max speed for side window operation (demonstrated)

A

160kt

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20
Q

Max XWC

A

35kt

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21
Q

Max XWC wet

A

30kt

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22
Q

Max TWC

A

10kt

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23
Q

Max TGT - start

A

F100 - 740˚ (2 seconds)

F70 - 700˚ (2 seconds)

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24
Q

Max TGT - takeoff

A

F100 - 850˚ (5 minutes, 10 minutes OEI)

F70 - 800˚ (5 minutes, 10 minutes OEI)

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25
Q

Max TGT - continuous

A

F100 - 795˚

F70 - 735˚

26
Q

Minimum idle (N2 should not fall below)

A

47.9%

27
Q

Max fuel asymmetry in flight

A

1000kg

If >350kg, max XWC 20kt

28
Q

Minimum height for autopilot use - takeoff

A

35ft AGL

29
Q

Minimum height for autopilot use - level flight/cruise

A

700ft AGL

30
Q

Minimum height for autopilot use - NPA

A

250ft

31
Q

Max XWC ILS Cat II

A

25kt

32
Q

Max XWC AUTOLAND Flap42

A

25kt

33
Q

Max XWC AUTOLAND Flap25

A

15kt

34
Q

Max TWC ILS Cat II

A

10kt

35
Q

Max TWC AUTOLAND

A

10kt

36
Q

Max total wind ILS Cat II

A

30kt

37
Q

Max wind AUTOLAND Flap42

A

25kt

38
Q

Max wind AUTOLAND Flap25

A

15kt

39
Q

ENGINE START FAULT

A

START PB … OFF
If alert persists:
- BLEED … ALL OFF
- FUEL LEVER … SHUT

40
Q

EMERGENCY DESCENT

A

ATS … DISCONNECT
THRUST LEVERS … IDLE
SPEED BRAKE … OUT
FLIGHT MODE PANEL … 10,000FT(/MEA) + LVLCH + MMO/VMO

41
Q

ON GROUND EMERGENCY EVACUATION

A 
PARK BRAKE ... SET
FLAPS ... FULLY DOWN
REVERSE THRUST LEVERS ... FULLY DOWN
LIFT DUMPERS ... DISARM
BOTH FUEL LEVERS ... SHUT
42
Q

BOTH ENGINES FLAME OUT

A

IGNITION … RELIGHT

43
Q

JET-PIPE FIRE

A 
FUEL LEVER ... SHUT
BLEED AIR PRESS ... ESTABLISH
START PB ... ON
ENGINE SELECTOR ... AS REQD
Motor engine until fire extinguished or TGT decreases
START PB ... OFF
44
Q

HOT START

A

If it is anticipated that the TGT start limit (740c) will be exceeded:
- FUEL LEVER … SHUT
After approx. 30 sec:
- START PB … OFF

45
Q

N2 STAGNATION

A

If during or after starting, N2 stagnates in combination with a rising TGT:

  • FUEL LEVER … SHUT
  • START PB … CHECK OFF
46
Q

LOW IDLING N2

A

If N2 RPM stabilises below minimum idling (47.9%) advance the thrust lever slowly until minimum idling RPM is reached.
Monitor TGT.

47
Q

INTERRUPTED START

A

If a start is interrupted before the fuel lever is selected to OPEN:
- START PB … OFF

48
Q

NO LIGHT UP

A

If an engine fails to light up within approx. 20 sec from selecting the fuel lever to OPEN:
- FUEL LEVER … SHUT
After approx. 30 sec:
- START PB … OFF

49
Q

When shall you not use Flex for take-off?

A 
Contaminated runway
Icing conditions (TAT +6˚-25˚ + visible moisture)
Windshear
Lift dumpers/anti-skid INOP
Wind/tail icing ON
50
Q

Best angle of climb speed

A

Green dot

51
Q

Best rate of climb speed

A

250/.65

52
Q

Max FOB

A

10256kg

UQD & F70 - 10692 (extra 430kg fuel)

53
Q

Max ramp weight F70

A

41955kg

54
Q

Max take off weight F70

A

41730kg

55
Q

Max landing weight F70

A

36740kg (same as F100 MZFW)

56
Q

Max zero fuel weight F70

A

33565kg

57
Q

Max TGT - relight

A

780˚

58
Q

Max TGT - reverse thrust

A

F100 - 850˚

F70 - 800˚

59
Q

Max fuel asymmetry on the ground

A

500kg for manoeuvring if >39000kg

1000kg for manoeuvring if <39000kg

60
Q

Minimum height for autopilot use - GS/LOC (no autoland)

A

80ft

61
Q

RVSM - notify ATC if:

A

A primary altimetry system fails
Crosscheck between primary altimetry systems >200ft
Failure of AP alt hold function
Loss of thrust necessitating descent
Any equipment failure resulting in an inability to maintain altitude

Flying (5 decks)

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