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Tempus Jets > CE-560 N247DG > Flashcards

CE-560 N247DG Flashcards

1
Q

MAX RAMP WEIGHT

A

16,500 LBS

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2
Q

MAX TAKEOFF WEIGHT

A

16,300 LBS

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3
Q

MAX LANDING WEIGHT

A

15,200 LBS

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4
Q

MAX ZFW

A

12,200 LBS

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5
Q

Mmo

A

0.755M

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6
Q

Vmo (8,000’ - 30,400’)

A

276 KIAS

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7
Q

Vmo (sea level to 8000’)

A

261 KIAS

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8
Q

Vmca

Minimum Control Speed Air

A

85 KIAS

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9
Q

Vmcg

Minimum Control Speed Ground

A

86 KIAS

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10
Q

MAX T/O, LDG ALT

A

14,000’

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11
Q

Max TW Component

A

10 kts

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12
Q

Max Water/Slush on Runway

A

½ inch

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13
Q

Max Tire Ground Speed

A

165 kts

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14
Q

Max Ambient Temperature

T/O & Landing

A

ISA +39C

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15
Q

Min Ambient Temperature

T/O & Landing

A

-54C

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16
Q

AP & YD OFF for…

A

T/O & Ldg

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17
Q

Vert Nav system OFF…

A

Below 500 AGL

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18
Q

Max Operating Altitude

A

45,000’

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19
Q

DC Power Source

A

2 x 28.5 Volt Gen

1 x 24 Volt Batt

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20
Q

AC Power Source

A

2 x AC Inverters 26V, 115V @ 400Hz

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21
Q

GPU requirement

A

28 Volt, 1000 Amps

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22
Q

Batt Start Limits

A

3 starts w/in 30 min

30” cool down between starts

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23
Q

GPU Start Limits

A

OR Gen Assist:
2 starts w/in 30 min
30” cool down between starts

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24
Q

Gen Limits

A 
Idle Norm: 125 Amps/Gen on the ground.
Idle High: 225 Amps/Gen on the ground
300 Amps/Gen in flight
450 Amps/Gen 2 min EMERGENCY
Continuous engine ground ops of the StarterGen above 125 Amps at ground idle/225 Amp Flight Idle -- PROHIBITED
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25
Q

GEN OFF LH/RH Caution lite (Amber)

A

LH/RH generator is not connected tot he airplane bus. Both LH/RH lights trigger Master Warning

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26
Q

AC FAIL Caution Lite (RED)

A

AC Bus Voltage >130 VAC or <90 VAC – Triggers Master Warning

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27
Q

INVERTER FAIL 1/2 Caution Lite

Amber

A

AC Bus Voltage >130 VAC or <90 VAC – Triggers AC FAIL Caution Lite. Reset Master Warning will reset AC FAIL Caution Lite

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28
Q

Hydraulic System

A

Open Center, 60psi/1,500psi

Gear/TR/Speed Brakes/Flaps

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29
Q

HYD PRESS ON Caution Lite (Amber)

A

Hydraulic System Pressurized

30
Q

HYD FLOW LOW LH/RH Caution Lite (Amber)

A

<~0.35 gpm

31
Q 
HYD LOW LEVEL 
Caution Lite (Amber)
A

Less than/equal 0.2 gal

32
Q

Tire Speed GS

33
Q

Vlo (Extending)

34
Q

Vlo (Retracting)

35
Q

Vle

36
Q

Landing Gear Horn

A

Either throttle 15 Flaps and Gear not down and locked – cannot be silenced

37
Q

POWER BRAKE LOW PRESS Caution Lite (Amber)

A

Low Brake Press – increase landing factor by 30% (x 1.3)

38
Q

ANTI-SKID INOP Caution Lite

Amber

A

Anti-Skid inop – increase landing factor by 25% (x 1.25)

Will always illuminate w/POWER BRAKE LOW PRESS

39
Q

DISP FAN

A

10 mins, or until either the EADI or EHSI HOT whichever occurs first.
Dispatch into IMC prohibited

40
Q

EADI HOT, EHSI HOT, SG HOT

A

Dispatch prohibited

41
Q

Pilot’s EADI/EHSI

A

Operational (non-reversionary) for T/O

42
Q

EFIS Temp limit on ground

A

45-51C – 1 hour

>51C - prohibited

43
Q

AP Limits

A

AP Torque & Roll Monitor test prior to flight
AP torque test fail – AP prohibited above 14,500’ MSL
AP prohibited if “Roll Monitor” annunciator light illuminates in flight

44
Q

AP Altitude Limits

A

Enroute: 1,000’ AGL
NPA: 300’ AGL
ILS: 180’ AGL

45
Q

Vertical Navigation

A

OFF below 500’ AGL

46
Q

Engine

A

PW JT15D-5A – lightweight, twin-spool, medium bypass ratio (2.1:1) front turbofan
2,900 lb static thrust

47
Q

ITT Limits

A 
Start: 700 <2 sec
T/O: 700 (5 minutes)
Transient: 700
Max Continuous: 680
Idle: 580
48
Q

N2 Limits

A

T/O: 96%
Max Continuous: 96%
Transient: 96%
Idle: 52% (minimum)

49
Q

N1 Limits

A

T/O: 104%
Maximum Continuous: 104%
Transient: 106%

50
Q

Oil Pressure Limits

A

T/O: 60-83 PSIG
Maximum Continuous: 60-83 PSIG
Idle: 40 PSIG (minimum)
Transient: 95 PSIG for 90 seconds

51
Q

Oil Temperature Limits

A 
T/O: 10 to 121
Maximum Continuous: 10-121
Idle: -40 to 121
Start: -40 (minimum)
Transient: -18 to 129
52
Q

OIL PRESS WARN Caution Lite (RED)

A

Oil press <40PSI

53
Q

F/W SHUTOFF LH/RH Caution Lite (Amber)

A

LH/RH Firewall fuel and/or hydraulic valves are closed

54
Q

ENGINE FIRE PUSH Warning Lite (RED)

A

~500F detected. Pressed:

1) Closes Firewall Fuel shutoff valve
2) Closes Firewall Hyd shutoff valve
3) Isolates TRs
4) Trips Gen Field Relay
5) Arms Fire Extinguisher bottle

55
Q

Thrust Reverser Limitations

A

Idle at 60 KIAS
Max reverse 83% N1 above -18C
Max TR deployed 15 min in any 1 hour period (avoid overheating hydraulics)
Engine static operation limited to idle
TRs prohibited during T&Gs
Must be verified operational prior to t/o

56
Q

Fuel

A

892 gal usable – 5,814 total usable fuel
Anti-icing additive must be added if not premix
Max asymmetrical fuel (normal ops): 200#
Max asymmetrical fuel (emer ops): 600#

57
Q

FUEL LOW LEVEL LH/RH Caution Lite (Amber)

A

<185# fuel in respective tank

58
Q

FUEL LOW PRESS LH/RH Caution Lite (Amber)

59
Q

Flap Limits – Vfe

A

7-15: 200 KIAS

35: 173 KIAS

60
Q

Cabin Pressurization Limits

A

0.0 - 8.9 PSI, +/- 0.1 PSID

61
Q

BLD AIR GND Caution Lite (Amber)

A

High flow rate of bleed air has been selected from the right engine for ground operation of the air conditioner

62
Q

CAB ALT 10000FT Caution Lite (RED)

A

Cabin Alt >10,000 Triggers Master Warning

63
Q

EMER PRESS ON Caution Lite (Amber)

A

Emer pressurization manually selected, or automatically activated by ACM overheat

64
Q

AIR DUCT O’HEAT Caution Lite (Amber)

A

Ventilation duct temp exceeds safe limits

65
Q

ACM O’PRESS Caution Lite (Amber)

A

ACM pressure >42 psi

66
Q

Anti-Ice/De-ice Bleed Air

A

1) Engine bullet nose cone
2) Temperature probe
3) Engine inlet lip
4) Stator vanes
5) Windshield
6) Inboard wing

67
Q

Anti-Ice/De-ice Electric

A

1) Pitot
2) Static
3) AOA

68
Q

Icing Speeds

A

Minimum Operating Speed in sustained icing conditions: 160 KIAS.
App/Ldg – Anti-ice ON: Vref +5
App/ldg – Anti-ice OFF: Vref

69
Q

ENG ANTI-ICE LH/RH Caution Lite (Amber)

A

LH/RH engine inlet, stator or wing anti-ice has failed

70
Q

SURFACE DEICE Annunciator (White)

A

Illuminates twice during 12 second boot cycle to indicate proper inflation pressure

71
Q

WING O’HEAT Caution Lite (Amber)

A

Inboard leading edge temp >160 F

72
Q

ENGINE FAILURE OR FIRE DURING TAKEOFF

A

SPEED BELOW V1 – TAKEOFF SHOULD BE ABORTED

  1. Brakes – AS REQUIRED
  2. Throttles – IDLE
  3. Speed Brakes – EXTEND

SPEED ABOVE V1 – TAKEOFF SHOULD NORMALLY BE CONTINUED

  1. After establishing a positive rate of climb – RETRACT LANDING GEAR
  2. A 400 feet, retract flaps at V2+10 and accelerate to VENR

Tempus Jets (4 decks)

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