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
GEN OFF LH/RH Caution lite (Amber)
LH/RH generator is not connected tot he airplane bus. Both LH/RH lights trigger Master Warning
26
AC FAIL Caution Lite (RED)
AC Bus Voltage >130 VAC or <90 VAC -- Triggers Master Warning
27
INVERTER FAIL 1/2 Caution Lite | Amber
AC Bus Voltage >130 VAC or <90 VAC -- Triggers AC FAIL Caution Lite. Reset Master Warning will reset AC FAIL Caution Lite
28
Hydraulic System
Open Center, 60psi/1,500psi | Gear/TR/Speed Brakes/Flaps
29
HYD PRESS ON Caution Lite (Amber)
Hydraulic System Pressurized
30
HYD FLOW LOW LH/RH Caution Lite (Amber)
<~0.35 gpm
31
``` HYD LOW LEVEL Caution Lite (Amber) ```
Less than/equal 0.2 gal
32
Tire Speed GS
165 Kts
33
Vlo (Extending)
250 KIAS
34
Vlo (Retracting)
200 KIAS
35
Vle
292 KIAS
36
Landing Gear Horn
Either throttle 15 Flaps and Gear not down and locked -- cannot be silenced
37
POWER BRAKE LOW PRESS Caution Lite (Amber)
Low Brake Press -- increase landing factor by 30% (x 1.3)
38
ANTI-SKID INOP Caution Lite | Amber
Anti-Skid inop -- increase landing factor by 25% (x 1.25) | Will always illuminate w/POWER BRAKE LOW PRESS
39
DISP FAN
10 mins, or until either the EADI or EHSI HOT whichever occurs first. Dispatch into IMC prohibited
40
EADI HOT, EHSI HOT, SG HOT
Dispatch prohibited
41
Pilot's EADI/EHSI
Operational (non-reversionary) for T/O
42
EFIS Temp limit on ground
45-51C -- 1 hour | >51C - prohibited
43
AP Limits
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
AP Altitude Limits
Enroute: 1,000' AGL NPA: 300' AGL ILS: 180' AGL
45
Vertical Navigation
OFF below 500' AGL
46
Engine
PW JT15D-5A -- lightweight, twin-spool, medium bypass ratio (2.1:1) front turbofan 2,900 lb static thrust
47
ITT Limits
``` Start: 700 <2 sec T/O: 700 (5 minutes) Transient: 700 Max Continuous: 680 Idle: 580 ```
48
N2 Limits
T/O: 96% Max Continuous: 96% Transient: 96% Idle: 52% (minimum)
49
N1 Limits
T/O: 104% Maximum Continuous: 104% Transient: 106%
50
Oil Pressure Limits
T/O: 60-83 PSIG Maximum Continuous: 60-83 PSIG Idle: 40 PSIG (minimum) Transient: 95 PSIG for 90 seconds
51
Oil Temperature Limits
``` T/O: 10 to 121 Maximum Continuous: 10-121 Idle: -40 to 121 Start: -40 (minimum) Transient: -18 to 129 ```
52
OIL PRESS WARN Caution Lite (RED)
Oil press <40PSI
53
F/W SHUTOFF LH/RH Caution Lite (Amber)
LH/RH Firewall fuel and/or hydraulic valves are closed
54
ENGINE FIRE PUSH Warning Lite (RED)
~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
Thrust Reverser Limitations
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
Fuel
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
FUEL LOW LEVEL LH/RH Caution Lite (Amber)
<185# fuel in respective tank
58
FUEL LOW PRESS LH/RH Caution Lite (Amber)
<5 psi
59
Flap Limits -- Vfe
7-15: 200 KIAS | 35: 173 KIAS
60
Cabin Pressurization Limits
0.0 - 8.9 PSI, +/- 0.1 PSID
61
BLD AIR GND Caution Lite (Amber)
High flow rate of bleed air has been selected from the right engine for ground operation of the air conditioner
62
CAB ALT 10000FT Caution Lite (RED)
Cabin Alt >10,000 Triggers Master Warning
63
EMER PRESS ON Caution Lite (Amber)
Emer pressurization manually selected, or automatically activated by ACM overheat
64
AIR DUCT O'HEAT Caution Lite (Amber)
Ventilation duct temp exceeds safe limits
65
ACM O'PRESS Caution Lite (Amber)
ACM pressure >42 psi
66
Anti-Ice/De-ice Bleed Air
1) Engine bullet nose cone 2) Temperature probe 3) Engine inlet lip 4) Stator vanes 5) Windshield 6) Inboard wing
67
Anti-Ice/De-ice Electric
1) Pitot 2) Static 3) AOA
68
Icing Speeds
Minimum Operating Speed in sustained icing conditions: 160 KIAS. App/Ldg -- Anti-ice ON: Vref +5 App/ldg -- Anti-ice OFF: Vref
69
ENG ANTI-ICE LH/RH Caution Lite (Amber)
LH/RH engine inlet, stator or wing anti-ice has failed
70
SURFACE DEICE Annunciator (White)
Illuminates twice during 12 second boot cycle to indicate proper inflation pressure
71
WING O'HEAT Caution Lite (Amber)
Inboard leading edge temp >160 F
72
ENGINE FAILURE OR FIRE DURING TAKEOFF
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