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Citation XLS NJA > XLS Other Limitations > Flashcards

XLS Other Limitations Flashcards

1
Q

45 Minute IFR Fuel Reserve

A

1037 lbs

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2
Q

Min Fuel for Release

A

1935 lbs

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3
Q

XLS Hot Spare Fuel

A

3800 lbs

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4
Q

Emergency Fuel

A

900 lbs

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5
Q

Min Runway Length

A

3800 ft

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6
Q

Min Runway Width

A

50 ft

75 ft if Wet runway and TR credit used

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7
Q

Runway Length, Ops Review Required

A

<4500 ft Dry
<5000 ft Wet/Contaminated
<5000 ft DAAP

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8
Q

IF runway less than 3,999 ft

A

NO T/O and Land

  • above 3,000 ft msl
  • Contaminated or Wet
  • Tailwind

No T/O - with Anti Ice ON

No Land - Runway < 75ft wide and Xwind > 10 kts
No Circle to Land - Ceiling < 1000 ft and Vis < 3 sm

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9
Q

Ocean Reef Limitations

A 
Day Only
Max Xwind - 15 kts Dry/ 10 kts Wet
No Tailwind
No Powered turns on Ramp or Fueling Area
Pull Straight in to be towed
LT/HM PICs may not be PIC, SIC OK
IF SIC is LT, PIC must perform T/O and Land
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10
Q

RVSM Required Equipment

A

1 Autopilot
1 AAD
1 ATC Alt reporting transponder
Static Port Heaters

Any deferral that effects these systems may impact RVSM

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11
Q

Max Zero Fuel Weight

A

15,100 lbs

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12
Q

Max Altitude T/O and Land

A

14,000 ft

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13
Q

Max Operating Speed/Vmo

A

305 kts

260 kts below 8,000 ft

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14
Q

Max Operating Mach/Mmo

A

.75 M

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15
Q

Max Tire Ground Speed

A

165 kts

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16
Q

Min Control Speed - Air / Vmca

A

Flaps 7&15 - 90 kts

Flaps 35 - 92 kts

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17
Q

Min Control Speed - Landing - Vmcl

A

Flaps 35 - 92 kts

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18
Q

Min Control Speed - Ground - Vmcg

A

Flaps 7&15 - 81 kts

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19
Q

Max Differential Pressure

A

9.7 psi

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20
Q

Normal Differential Pressure

A

0-9.6 psi

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21
Q

Pressure Relief Valve Opening

A

9.5 psi

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22
Q

Max Number of Passengers

A

7 Adults + 3 Lap Children

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23
Q

Lap Children Seats

A

3,4 and 10

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24
Q

Max Altitude Crew O2 Mask approval

A

40,000 ft Cabin Altitude

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25
Q

Max Altitude Passenger O2 Mask Sustained Operation

A

25,000 ft Cabin Altitude

26
Q

Other APU Starting Limits

A

No starting during refueling
No starting after Duel Gen Failure
After APU shutdown, no starting until 30 seconds after APU RPM is Zero.

27
Q

Other APU Operating Limitations

A

No APU operating when Aircraft unattended
No APU Operating during deice procedures
No APU Operating if APU Test fail

28
Q

Autopilot Operating Limitations

A

1 pilot, seated and belted during all AP ops
No AP or YD for T/O and Land
Do Not Manually override AP during normal Ops
No AP use if
- Any comparison monitor active
- Either PFD is in ATT reversion

29
Q

Battery Limits for Engine Start

A

3 Attempts/Hour
3 Gen Cross-starts = 1 Batt start
APU Gen Start = 1/3 of Batt start
If GPU used to start, No Batt cycle counted

30
Q

Battery Limits for APU Start

A

9 Attempts/Hour

31
Q

Max GPU Load

A

1000 Amps

32
Q

Max ENG GEN Load on Ground

A

250 Amps up to 4 Minutes

33
Q

Max ENG GEN Load inflight

A

300 Amps

34
Q

Max APU Gen load on Ground

A

200 Amps

35
Q

Max APU Gen load inflight

A

230 Amps

36
Q

Lav Door Limit

A

Must be latched open for taxi, T/O and Landing

37
Q

Refueling Pressure Limit

A

10-55 psi

38
Q

Max Defueling Pressure

A

-10 psi

39
Q

Max Total Fuel quantity

A

6790 lbs

40
Q

Define Ground Icing conditions

A

SAT 10° C and below and visible moisture, including vis <1 sm

Operate WING/ENGINE- ON and TAIL-AUTO in icing conditions

41
Q

Define In flight icing conditions

A

RAT 10°C or below and visible moisture, including vis <1 sm

Operate WING/ENGINE- ON and TAIL-AUTO in icing conditions

42
Q

Ground WING-ANTI ICE heating time

A

During ground operations it may take up to 2 minutes to extinguish WING ANTI-ICE light with N2 at 70%

43
Q

Icing type Limitations

A

Flight in FZRA and FZDZ , or any severe icing is prohibited

44
Q

ENG ANTI-ICE L/R not illuminated when ON

A

IF ambient temp is 15°C or warmer, a small decrease of N2 will indicate system is activated

45
Q

When should you engage ENG anti-ice on

A

3-5 minutes prior to entering icing conditions

46
Q

Flaps Setting for takeoff with Deicing fluid applied

A

Flaps 7, Corrections not provided for flaps 15.

47
Q

Flap Setting in icing conditions

A

Maintain flaps up, except during landing and approach

48
Q

Tail Deicing Limitations

A

Select TAIL-AUTO before entering icing
Do Not operate when -
> 150kts and RAT < -35°C
< 150 kts and RAT < -40°C

49
Q

IF Digital Engine Display in Reversion Mode

A

Do not depart

50
Q

Altitude and Heading Alignment Limitation

A

Do not taxi until Alt and Heading Ground Alignment complete

51
Q

Max Takeoff thrust N1/N2

A

100% N1

102.8% N2

52
Q

Ground Idle Min

A

49.3% N2

53
Q

Flight Idle Min

A

53.2% N2

54
Q

Transient N1/N2 Limits

A

102% N1

  1. 0% N2
  2. 2% N2 for 5 seconds
55
Q

Oil Pressure and Temp Limit - Takeoff Thrust

A

45-160 psi and 10-121.1 °C

56
Q

Oil Pressure and Temp Limit - Flight and Ground Idle

A

25-160 psi and -40-121.1°C

57
Q

Min Oil Temp for Start

A

-40°C

58
Q

Min Oil Pressure limit for 20 seconds

A

0 psi

59
Q

Min-Max Oil Temp and Pressure Transient

A

20-250 psi and 135°C for 400 seconds

60
Q

Maximum Oil Consumption

A

1 qt per 8 hours

61
Q

Engine Starter Limits

A

3 start attempts with 90 second interval in any 30 minute period. After third attempt, 30 minute cooling period

62
Q

Thrust Reverser Limitations

A
  • Idle <60 kts during landing roll or static operation
  • Max deploy time 3 out of every 10 minutes
  • Max deploy time with APU operating - 30 seconds
  • No TR use during touch and goes
  • No TR use to back up aircraft

Citation XLS NJA (7 decks)

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