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Citation Ultra > Limits > Flashcards

Limits Flashcards

1
Q

MINIMUM CREW

A

TWO PILOTS

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2
Q

BAGGAGE WEIGHT LIMITS

NOSE, AFT CABIN, TAIL CONE

A

NOSE: 350 LB
AFT CABIN: 600 LB
TAILCONE: 500

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3
Q

MAX TAXI AND RAMP WEIGHT

A

16,500 LB

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4
Q

MAX TAKEOFF WEIGHT

A

16,300 LB

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5
Q

MAX LANDING WEIGHT

A

15,200 LB

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6
Q

MAX ZERO FUEL WEIGHT

A

12,200 LB

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7
Q

MAX FLAPS EXTENDED (V fe)

A

7 or 15: 200 kias
35: 173 kias

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8
Q

MAX LANDING GEAR SPEED

A

Extending (V lo): 250 KIAS
Extended (V le): 292 KIAS
Retracting (V lo): 200 KIAS

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9
Q

MINIMUM CONTROL - AIR (Vmca)

A

95 KIAS

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10
Q

MINIMUM CONTROL - GROUND (Vmcg)

A

91 KIAS

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11
Q

MAXIMUM (Vmo) BELOW 8000’

A

262

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12
Q

MAXIMUM (Vmo) 8000’ - 28907’

A

292

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13
Q

MAXIMUM (Mmo) ABOVE 28907’

A

M .755 INDICATED

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14
Q

MAXIMUM SPEED BREAK EXTENSION (Vsb)

A

NO LIMIT

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15
Q

MAX AUTOPILOT OPERATION SPEED

A

292 KIAS OR .755M

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16
Q

ENGINE N2 GROUND IDLE LIMITS

A

NORM - 46%
HIGH - 52%

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17
Q

MAX PRESS ALT FOR T/O AND LANDING

A

14,000’ PRESSURE ALTITUDE

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18
Q

MAX TEMP T/O AND LANDING

A

ISA +39 c

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19
Q

MAX CROSSWIND DEMONSTRATED

A

20 KNOTS

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20
Q

MAX TAILWIND DEMONSTRATED

A

10 KNOTS

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21
Q

MAX TIRE GROUND SPEED

A

165 KNOTS

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22
Q

MAX WATER/SLUSH

A

0.5 INCH

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23
Q

VNAV OFF BELOW

A

500’ AGL

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24
Q

MINIMUM AIR TEMPERATURE FOR T/O LANDING

A

-54 C

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25
Q

NOSE TIRE PRESSURE

A

120 +- 5 PSI

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26
Q

APPROX TURB PENETRATION SPEED

A

180

27
Q

MIN A/S FOR SUSTAINED ICING

A

160

28
Q

MAX CALIBRATED OP ALTITUDE

A

FL450

29
Q

MAX LOAD FACTOR IN FLGHT FLAPS UP / 7-35

A

FLAPS UP: -1.52 TO +3.8 AT 16,300 LB
FLAPS 7-35: -0.0 TO +2.0 AT 16,300 LB

30
Q

MAX LOAD FACTOR LANDING / FLAPS 15 - 35

A

+3.5 G AT 15,200 LB

31
Q

MINIMUM ALTITUDE FOR AUTOPILOT USE

A

ENROUTE: 1,000 AGL
NON-PRECISION: 300 AGL
CAT 1 ILS: 180 AGL

32
Q

NOSE AVN FAN FAIL GROUND OPS LIMIT

A

30 MIN or until either PDF HOT ore MFD HOT illuminates, whichever happens first

33
Q

AC POWER SOURCES

A

-TWO 375VA static inverter, each converting 28V DC into 26V AC and 115V AC at 400 HZ
- TWO 26V AC BUSES
- TWO 115V AC BUSES

34
Q

DC POWER SOURCES

A

-TWO 28.5V DC 300A starter/gens
-ONE 24V DC 40A/HR NICAD OR 44A/HR SLAB

35
Q

APPROVED MAX GEN LOAD IN FLIGHT

A

300A

36
Q

BATT LIMIT FOR START

A

3/HR

37
Q

STARTER LIMITS FOR ENGINE STARTS:
BATTERY:
GPU:

A

BATTERY: 3 STARTS PER 30 MIN W/90s REST
GPU: 2 STARTS PER 30 MIN W/90s REST

38
Q

VOLTAGE CONSIDERATION WHEN USING GPU FOR ENGINE START

A

USE OF A GPUE WITH VOLTAGE IN EXCESS OF 28V OR CURRENT IN EXCESS OF 1000A MAY DAMAGE THE STARTER

39
Q

MAX CONTINUOUS GEN LOAD DURING GROUND OPS:
GROUND IDLE:
FLIGHT IDLE:

A

GROUND IDLE: 125A
FLIGHT IDLE: 225A

40
Q

CAN YOU EXCEED MAX GEN AMPS IN EMERGENCY?

A

YES, 50% ABOVE THE ALLOWABLE ( UP TO 450 AMPS) FOR 5 MINUTES

41
Q

MAX PRESS DIFF

A

8.9 +- 0.1 PSID

42
Q

A/C COMPRESSOR LIMIT

A

OFF ABOVE 18,000’

43
Q

MAX FUEL IMBALANCE

A

NORMAL: 200LB
EMERGENCY: 600LB

44
Q

MAX FUEL CAPACITY

A

5814 LB / 862 US GAL

45
Q

SINGLE POINT PRESSURE RANGE

A

15 TO 60 PSI

46
Q

APPROVED HYDRAULIC FLUIDS

A

SKYDROL
HYJET

47
Q

AT WHAT PSI DOES THE OPEN CENTER HYDRAULIC SYSTEM CONTINUOUSLY OPERATE

A

60 PSI

48
Q

WHAT PSI IS REQUIRED TO ACTIVATE THE HYDRAULIC SYSTEM

A

1,350 - 1500 PSI

49
Q

LIMIT GROUND OPS OF PITOT HEAT

A

2 MINUTES

50
Q

DEFINITION OF ICING CONDITIONS

A

VISIBLE MOISTURE (VIS OF 1 MILE OR LESS) AND BELOW 10 C

51
Q

AT WHAT TEMPS SHOULD THE W/S BLEED AIR BE SET TO HIGH

A

OAT < -18 C

52
Q

MIN SPEED FOR FLIGHT IN ICING CONDITIONS

A

160

53
Q

CONTINUOUS USE OF SUPPLEMENTAL OXYGEN IS PROHIBITED ABOVE:
W/ PAX:
CREW ONLY:

A

W/PAX: 25,000’
CREW ONLY: 41,000’ FOR EROS, OR LOWER DEPENDING ON MASK

54
Q

AT WHAT ALTITUDE DOES OXYGEN BECOME AUTOMATICALLY AVAILABLE TO THE CREW AND PAX?

A

13,500’ +- 600’

55
Q

ENGINE NOMENCLATURE

A

PRATT AND WHITNEY JT15D-5D

56
Q

REVERSE THRUST MUST BE REDUCED TO IDLE REVERSE BY WHICH SPEED

A

60KIAS

57
Q

MAX ALLOWED MIXING OF OILS

A

NO MORE THAN 2 QUARTS EVERY 400 HOURS

58
Q

THRUST REVERSER ARE PROHIBITED:

A
  1. DURING TOUCH AND GO LANDINGS
  2. FOR BACKING THE AIRPLANE
  3. ON SOD OR GRAVEL RUNWAYS
59
Q

MAX THRUST REVERSER DEPLOYMENT SPEED

A

115 KIAS

60
Q

MAX DEPLOYMENT TIME

A

15 MIN IN ANY 1 HOUR

61
Q

OPERATING LIMITES FOR T/O
N1
N2
ITT

A

N1: 100%
N2: 97%
ITT: 720 C

62
Q

MAX CONTINUOUS
N1
N2
ITT

A

N1: 100%
N2: 97%
ITT: 720 C

63
Q

START ABORT TEMP

A

550 C

64
Q

STATIC THRUST PRODUCED BY JT15D-5D ISA at SL?

A

3,045 LB THRUST

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