Operational Relevant Knowledge and Limitations Flashcards

1
Q

Manoeuvre load (G) limits ?

A

Flaps up + 2.5g to - 1.0g

Flaps down +2.0g to 0.0g

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2
Q

Max OAT takeoff, flight and landing with A/C operative ?

A

ISA + 35
(50 deg C at sea level)

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3
Q

Opening and closing window / doors

A

40 knots / 60 knots once opened
L1 / L2 operations not to be operated above 64 knots

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4
Q

Aircraft weights for A and T variant ?

(MZFW, MRW, MTOW, MLW)

A

MZFW = 36 740 kg
MRW = 46 040 kg
MTOW = 45 810kg
MLW = 39 915 kg

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5
Q

Aircraft weights for G type variant ?

A

MZFW = 36 740 kg
MRW = 44 680 kg
MTOW = 44 450g
MLW = 39 915 kg

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6
Q

What are the following aircraft speed limitations:
1. Vmo / Mmo
2. Normal climb rate
3. Max rate of climb
4. Max angle of climb
5. Turbulence Penetration
6. Maneurvering Speed (Va)Aircraft Speed Limitations ?

((Vmo/Mmo, Turbulence, Va (maneurvering))

A

320 kts / M 0.77
250 kts / 280 KIAS / M0.7
250 kts / M0.65
Green Dot
250 kts / M0.65
215 kts (SL @ MTOW)

Vmo Note - 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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7
Q

Aircraft Gear Limitations

A

Vlo / Vle = 200 kts

Max Alt = 25,000 ft

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8
Q

Aircraft Flap Limitations

A

Vfe 8 = 250 kts
Vfe 15 = 220 kts
Vfe 25 = 220 kts
Vfe 42 = 180 kts

Max Alt = 20,000 ft

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9
Q

What is the maximum sliding window opening speed ?

A

160kt

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10
Q

What is the maximum lift dumper extension speed ?

A

170 kt

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11
Q

What is the maximum wind limitations for takeoff and landing ?

A

Max crosswind = 35 kts
Max crosswind Double aileron fault = 15 kts
Max crosswind Total hydraulic failure = 10 kts
Max crosswind Fuel asymmetry = 20 kts
Maxi crosswind limit for non-grooved, wet runways operations = 30 kts

Tailwind = 10 kts

Maximum crosswind for CAT 1 where the visibility is less than 1200m = 30 kts

If a fuel asymmetry exceeds 350 kg = 20 kts

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12
Q

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

A

44ºC

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13
Q

Take-off with flap setting 0 is not allowed if more than 25% of the runway is covered with….?

A

3 mm standing water

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14
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

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15
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

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16
Q

What consittutes a contaminated runway ?

A

Standing water more than 3mm deep covering more that 25% of the runway surface to be used.

Assessed by flight crew after lining up on takeoff runway.

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17
Q

What is the earliest point after takeoff that tail anti ice can be selected ?

A

After climb thrust is set

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18
Q

When exiting icing conditions with only engine anti ice on, wait how long before turning off ?

A

1 minute, or in any case, after the MFDU icing alert has ceased

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19
Q

What is the maximum TGT for
1. Engine Start
2. Take-off
3. Maximum Continuous
4. Engine Relight?
5. Reverse Thrust
6. Maximum Over temperature

A
  1. 740 deg C (max 2 sec)
  2. 850 deg C (5 mins 2E, 10 mins SE)
  3. 795 deg C
  4. 780 deg C (max 2 sec)
  5. 850 deg C (60 secs max)
  6. 870 ºC for 20 seconds
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20
Q

What is considered the minimum engine N2 idle speed to consider an engine stabilised ?

A

N2. - 47.9%

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21
Q

What is the engine N1 restricted range ?

A

57 - 75 % N1

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22
Q

What is the engine minimum oil pressure for takeoff ?

A

30 psi

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23
Q

Flex thrust take off shall not be used when the any of the following conditions are present (9 items) :

A
  1. Icing conditions exist
  2. Contaminated runway
  3. Wind shear or inversion
  4. Lift dumpers inop
  5. Anti skid inop (any)
  6. Wing anti ice on
  7. Tail anti ice on
  8. No means established to periodically verify rated thrust
  9. Items affecting performance cause significant increase in crew workload.
24
Q

What is the limitation on APU start cycles ?

A

3 consecutive starts with 2 min between starts

25
Q

What is the time limit before shutting down the APU ?

A

Allow 70 seconds before switching off the batteries, unless external AC power is available

26
Q

What is considered the required bleed pressure to start engines ?

  1. APU
  2. Cross Bleed
  3. External Air
A
  1. APU- 25 PSI to 35 PSI (can be as low as 20 PSI up to 8000ft)
  2. Cross Bleed- 30 PSI
  3. External Air - 30 PSI to 50 PSI
27
Q

What is the engine warm up time required based on start oil temperature ?

A

Oil temp 40 or above - 2 mins
Oil temp 20 - 40 - 3 mins
Oil temp 20 & below - 4 mins

28
Q

What is the time required at idle thrust before engine shutdown ?

A

1 min (Engine oil returns after 15 mins)

29
Q

What should be considered the maximum oil consumption per hour ?

A

1.5 L / HR

30
Q

What is the maximum altitude start for the APU (Both R and RR) ?

A

R Type = FL310
RR Type = FL350

(For an R Type APU if it is cold soaked start is not guaranteed above FL

31
Q

What are the limitations on the engine starter ?

A

4 attempts, 2 mins max, 30 seconds off
15 mins off after 4th attempt

(Must light up within 20 seconds of fuel lever open)

32
Q

What is the maximum fuel asymmetry on ground except during refueling ?

A

500 kg for F100 aircraft weight > 39 000 kg

and

1000 kg for F100 aircraft weight at or < 39 000 kg

33
Q

What is the Total Useable Fuel for:
1. A / T types
2. G types

A

A / T: 10,692kg
G: 10,256kg

34
Q

What is the inidvidual tank quantities for A/T and G type ?

A

A / T: Wing - 7712 & Centre - 2980 = TOTAL 10692
G: Wing - 7744 & Centre - 2512 = TOTAL 10256

35
Q

What is the minimum temp in flight ?

A

-70 deg C

36
Q

Max altitude for fuel suction feed
(i.e maximum altitude without wing fuel tanks)

A

FL150

37
Q

How much fuel can be added to centre tank for trimming purposes?

A

1000kg and must be included to ZFW

38
Q

What is the minimum height for AP engagement after take off ?

A

35 ft

39
Q

What is the minimum height AP for an NPA approach ?

A

250 ft AGL

40
Q

What is the minimum height for AP use height with GS/LOC annunciation ?

A

80 ft

41
Q

What is the minimum height for AP height for cruise mode ?

A

200 ft AGL

42
Q

What is the maximum altitude variation between the following:
1. Field elevation vs PFD
2. Field elevation and Stby ALT
3. CAPT vs FO PFD altitude
4. CAPT vs FO PFD altitude when above FL250 ?

A
  1. +/- 40 ft PFD
  2. +/- 120ft STBY
  3. +/- 30 ft
  4. +/- 100ft
43
Q

What is the RVSM minimum equipment required ?

A

Static ports - 4
ADC - 2
PFD - 2
AOA - 2
AP - 1
ALT ALERT - 1
ATC transponder - 1

44
Q

What is the minimum RVSM cross check limit ?

A

Approx 200 ft (60m)

45
Q

Duration of Emergency lights

A

10 mins

46
Q

Wake turbulence arriving aircraft

A

Medium behind heavy - 2 minutes
Medium behind super - 3 minutes

Does not apply if on visual approach and pilot reports following aircraft in sight

47
Q

Wake turbulence departing aircraft

A

Medium following heavy - 2 mins / 3 mins for intersection or 5NM
Medium following super - 3 mins / 4 mins for intersection or 7NM

48
Q

What is the minimum voltage for APU start ?

A

Battery - 24 Volts
EMERG BUS AC - 112 Volts

49
Q

How long will the battery last for if the only source of power ?

A

30 mins & 1 APU Start

50
Q

What is the normal operating max cabin pressure differential ?

A

7.46 PSI

51
Q

What is the Differential Pressure limited by the outflow valves ?

A

In both Auto or Manual 7.65 PSI

52
Q

What is the required oxygen pressure for the cockpit oxygen bottle ?
1. Nominal
2. 3 Flight Crew
3. 2 Flight Crew

A
  1. 1850 psi
  2. 1500 psi
  3. 1000 psi
53
Q

What is the minimum permitted quantity in each Hydraulic System for normal operation ?

A

70%

54
Q

What is the time required to obtain the maximum brake temperature following an RTO ?

A

5 min for max temp accurate reading
10 mins for subsequent TO

55
Q

What is the maximum brake temp for T/O permitted for take-off ?

A

Top of green band

56
Q

What aircraft are A, G and T types by rego ?

A

Group A - Ex Avianca Aircraft
(NHF, NHG, NHI, NHJ, NHK, NHM, NHN, NHQ, NHV, NHY, NQE)

Group G - Ex Germania Aircraft (NHO, NHP)

Group T - Ex Austrian Aircraft (NHA, NHZ, NPU)