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Fokker F100 AOM Book 2 (02 Oct 20) > Limitations > Flashcards

Limitations Flashcards

1
Q

What is the maximum certified number of passenger seats?

A

109

Note - Compliance with emergency evacuation requirements were demonstrated with 3 CC for pax seating capacity above 100 and 2 cc for a pax seating capacity of 100 and below

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2
Q

F100 Maximum Operating Pressure Altitude?

A

35,000 ft

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3
Q

What is the Maximum Operating Temperature on the ground with the avionics cooling operative and the air conditioning inoperative ?

A

44ºC

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4
Q

What are the Runway slope limitations?

  1. Normal
  2. Autoland
A
  1. 2% UP and 2% DOWN
  2. 0.8% UP and 0.8% DOWN
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5
Q

What is the F100 maximum take-off and landing pressure altitude?

A

8,000ft

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6
Q

What is the Maximum Operating Temperature for take Off, Flight and Landing with Air Conditioning operative ?

A

ISA +35ºC

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7
Q

What are the weight limitations for the VARA HGW F100 aircraft?

  1. Registrations
  2. Max Taxi Weight (MBRW)
  3. Max Takeoff Weight (MTOW)
  4. Max Landing Weight (MLW)
  5. Max Zero Fuel Weight (MZFW)
A
  1. FNJ, FNR, FNY, FSQ
  2. 46,040 kg
  3. 45,810 kg
  4. 39,915 kg
  5. 36,740 kg
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8
Q

What are the weight limitations for the VARA LGW F100 aircraft?

  1. Registrations
  2. Max Taxi Weight (MBRW)
  3. Max Takeoff Weight (MTOW)
  4. Max Landing Weight (MLW)
  5. Max Zero Fuel Weight (MZFW)
A
  1. FNC, FNN, FNU, FNT, FSW, FWH, FWI, FZH, FZI, FZO
  2. 44,680 kg
  3. 44,450 kg
  4. 39,915 kg
  5. 36740 kg
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9
Q

What are the F100 maneuvering load limits?

  1. Flap Up
  2. Flap Down
A
  1. +2.5G to -1.0G
  2. +2.0G to 0.0G
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10
Q

What is the maximum operating limit speed?

A

320 kt / M0.77

Note - VH-FZH - Before exceeding a speed of 300kt IAS below 10 000ft both pilots must ensure proper windshield heating by feeling that the windshield is not cold when touched.

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11
Q

What is the F100 maneurvering speed (VA) speed?

A

215 kts at S.L (MTOW)

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12
Q

What is F100 Turbulence Penetration Speed (Rough Air = VRA/MRA) maximum speed?

A

250 kts / M0.65

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13
Q

What are the F100 maximum flap extension speeds ?

  1. F8
  2. F15
  3. F25
  4. F42
A
  1. F8 = 250 kt / M0.50
  2. F15 = 220 kt/ M0.45
  3. F25 = 220 kt /M0.45
  4. F42 = 180 kt / M0.36
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14
Q

What is the maximum altitude for flap extension ?

A

20,000 ft

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15
Q

What is the maximum landing gear extended (VLE) and operating speed (VLO) ?

A

200 kt

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16
Q

What is the maximum altitude for landing gear extension ?

A

25,000 ft

17
Q

What is the maximum lift dumper extension speed ?

A

170 kt

18
Q

What is the maximum demonstrated speed for flight with an open sliding window ?

A

160 kt

19
Q

Maximum crosswind component for take-off and landing ?

A

35 kt

20
Q

What is the maximum tailwind component for take-off and landing ?

A

10 kt

21
Q

To avoid structural damage a take-off with 0 degrees flap-setting is not allowed on a runway if ?

HINT - Comtaminated Runway

A

More than 25% of the runway surface area within the required runway length and width is covered by either:

  1. Standing water (s.g. 1.0) with a depth of more than 3 mm
  2. Slush (s.g. 0.85) with a depth of more than 3.5 mm
  3. Wet loose snow (s.g. 0.5) with a depth of more than 6 mm
  4. Dry loose snow (s.g. 0.2) with a depth of more than 15.0 mm
22
Q

To avoid structural damage a take-off with 8 or 15 degrees flap-setting is not allowed on a runway if ?

HINT - Comtaminated Runway

A

More than 25% of the runway surface area within the required runway length and width is covered by either:

  1. Standing water (s.g. 1.0) with a depth of more than 12.7 mm
  2. Slush (s.g. 0.85) with a depth of more than 15.0 mm
  3. Wet loose snow (s.g. 0.5) with a depth of more than 25.4 mm
  4. Dry loose snow (s.g. 0.2) with a depth of more than 63.5 mm
23
Q

Take Off is PROHIBITED unless the flight crew has ensured that the wings, tail, control surfaces, engine inlets and other critical surfaces of the airplane are free of ?

A

Ice, frost and snow

24
Q

Dispatch with only frost at the underside of the wing is allowed, provided that the frost layer does not extend outside the fuel tank area and its thickness does not exceed ?

A

3mm

25
Q

Can the crew use on ground wing leading edge heating system instead of undertaking de-icing treatment ? T

A

No

ADDITIONAL INFORMATION - The on ground wing leading edge heating system is intended to be used in addition to approved de-/anti-icing procedures and adherence to applicable hold over times as required by national operational regulations.

26
Q

What are the engine limitations during start?

A

740 ºC Momentary

(not exceeding 2 seconds)

27
Q

What are the engine limitations during a relight?

A

780 ºC Momentary

(not exceeding 2 seconds)

28
Q

What are the maximum engine parameters for Take Off?

A

N1 = 95.5%

N2 = 103.5%

Max TGT = 850 ºC

Time Limit = 5 mins (2 Engine)

10 Mins (1 Engine)

29
Q

What are the maximum continuous engine parameters ?

A

N1 = 95.5%

N2 = 100.5%

Max TGT = 795 ºC

Time Limit = Unrestricted

30
Q

What are the maximum overspeed engine parameters ?

A

N1 = 98.3%

N2 = 106.6%

Time Limit = 20 seconds

31
Q

What is the maximum over temperature limitation ?

A

870 ºC for 20 seconds

32
Q

What is the minimum Low Idle N2 permited ?

A

47.9 % Unrestricted

33
Q

What are the parameters for Maximum Reverse Thrust ?

A

N1 = 95.5%

N2 = 99.2%

Max TGT = 850 ºC

Time Limit = 60 seconds

ADDITIONAL - To avoid high fan blade stresses, stabilized operation in the speed range of 57% to 75% N1 is not permitted in reverse thrust.

Fokker F100 AOM Book 2 (02 Oct 20) (1 decks)

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