Limitations

Question 1

What is the maximum certified number of passenger seats?

Answer 1

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

Question 2

F100 Maximum Operating Pressure Altitude?

Answer 2

35,000 ft

Question 3

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

Answer 3

44ºC

Question 4

What are the Runway slope limitations?

1. Normal
2. Autoland

Answer 4

1. 2% UP and 2% DOWN
2. 0.8% UP and 0.8% DOWN

Question 5

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

Answer 5

8,000ft

Question 6

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

Answer 6

ISA +35ºC

Question 7

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)

Answer 7

1. FNJ, FNR, FNY, FSQ
2. 46,040 kg
3. 45,810 kg
4. 39,915 kg
5. 36,740 kg

Question 8

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)

Answer 8

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

Question 9

What are the F100 maneuvering load limits?

1. Flap Up
2. Flap Down

Answer 9

1. +2.5G to -1.0G
2. +2.0G to 0.0G

Question 10

What is the maximum operating limit speed?

Answer 10

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.

Question 11

What is the F100 maneurvering speed (V_A) speed?

Answer 11

215 kts at S.L (MTOW)

Question 12

What is F100 Turbulence Penetration Speed (Rough Air = V_RA/M_RA) maximum speed?

Answer 12

250 kts / M0.65

Question 13

What are the F100 maximum flap extension speeds ?

1. F₈
2. F₁₅
3. F₂₅
4. F₄₂

Answer 13

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

Question 14

What is the maximum altitude for flap extension ?

Answer 14

20,000 ft

Question 15

What is the maximum landing gear extended (V_LE) and operating speed (V_LO) ?

Answer 15

200 kt

Question 16

What is the maximum altitude for landing gear extension ?

Answer 16

25,000 ft

Question 17

What is the maximum lift dumper extension speed ?

Answer 17

170 kt

Question 18

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

Answer 18

160 kt

Question 19

Maximum crosswind component for take-off and landing ?

Answer 19

35 kt

Question 20

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

Answer 20

10 kt

Question 21

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

HINT - Comtaminated Runway

Answer 21

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

Question 22

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

HINT - Comtaminated Runway

Answer 22

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

Question 23

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 ?

Answer 23

Ice, frost and snow

Question 24

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 ?

Answer 24

3mm

Question 25

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

Answer 25

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.

Question 26

What are the engine limitations during start?

Answer 26

740 ºC Momentary ## Footnote (not exceeding 2 seconds)

Question 27

What are the engine limitations during a relight?

Answer 27

780 ºC Momentary ## Footnote (not exceeding 2 seconds)

Question 28

What are the maximum engine parameters for Take Off?

Answer 28

N1 = 95.5% N2 = 103.5% Max TGT = 850 ºC Time Limit = 5 mins (2 Engine) 10 Mins (1 Engine)

Question 29

What are the maximum continuous engine parameters ?

Answer 29

N1 = 95.5% N2 = 100.5% Max TGT = 795 ºC Time Limit = Unrestricted

Question 30

What are the maximum overspeed engine parameters ?

Answer 30

N1 = 98.3% N2 = 106.6% Time Limit = 20 seconds

Question 31

What is the maximum over temperature limitation ?

Answer 31

870 ºC for 20 seconds

Question 32

What is the minimum Low Idle N2 permited ?

Answer 32

47.9 % Unrestricted

Question 33

What are the parameters for Maximum Reverse Thrust ?

Answer 33

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.