General (10/28/2024) Flashcards

1
Q

Max Ramp Weight

(LR45 Modified)

A

21,750 lbs

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2
Q

Max Certified Takeoff Weight

(LR45 Modified)

A

21,500 lbs.

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3
Q

Minimum Flight Weight

(LR45 Modified, LR45 Not Modified)

A

14,000 lbs.

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4
Q

Max Zero Fuel Weight

(LR45 Modified)

A

16,500 lbs.

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5
Q

Max Certified Landing Weight

(LR45 Modified, LR45 Not Modified, LR40)

A

19,200 lbs.

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6
Q

V MO

A

330 KIAS

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7
Q

M MO

A

.81M

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8
Q

MMO with Mach Trim Inop. & A/P Engaged

A

.81M

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9
Q

MMO with Mach Trim Inop. & A/P Disengaged

A

23,400 to 42,000 FT: .76 -.78 M

Above 42,000 FT: .78 M

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10
Q

STANDBY INSTRUMENTS (Vmo and Mmo)

A

Vmo 325 KIAS

Mmo .75M

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11
Q

VLE

A

260 KIAS

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12
Q

VLO

A

200 KIAS

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13
Q

VFE Flaps 8º

A

250 KIAS

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14
Q

VFE Flaps 20º

A

200 KIAS

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15
Q

VFE Flaps 40º

A

150 KIAS

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16
Q

VMCA Flaps 8°

A

103 KIAS (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (takeoff flap setting, gear retracted))

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17
Q

VMCA Flaps 20°

A

101 KIAS????? (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (takeoff flap setting, gear retracted))

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18
Q

VMCG - Rudder Boost On, APR On

A

102 KIAS (Minimum speed, on the ground during takeoff, at which the aircraft can be controlled by the use of primary flight controls only, after a sudden failure of the critical engine, the other engine remaining at takeoff power.)

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19
Q

VMCG - Rudder Boost On, APR Off

A

100 KIAS (Minimum speed, on the ground during takeoff, at which the aircraft can be controlled by the use of primary flight controls only, after a sudden failure of the critical engine, the other engine remaining at takeoff power.)

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20
Q

VMCL Flaps 8°

A

105 KIAS (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (approach flap setting))

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21
Q

VMCL Flaps 40°

A

98 KIAS (Minimum control speed in flight at which the aircraft can be controlled with a maximum bank of 5 degrees, if one engine fails, the other engine remaining at takeoff power (approach flap setting))

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22
Q

Turbulent Air Penetration Speed

A

250 KIAS or .73M

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23
Q

Max Pressure Altitude – Takeoff and Landing

A

14,000 FT

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24
Q

Max Pressure Altitude Enroute

A

51,000 FT

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25
Max Tailwind ≤ 12,000 FT
10 KTS
26
Max Water/Slush On Runway
.75 IN
27
Min Turn-Around Time
15 Minutes
28
Max Fuel Imbalance
200 lbs
29
Load Factor – Flaps UP
+2.9g to -1g
30
Load Factor – Flaps Down
+2g to 0g
31
EICAS or MFD
SUMRY or FLT Page for Takeoff and Landing
32
Flaps and Gear - Max Altitude for Extension
18,000 FT
33
Autopilot Minimum Altitudes
1. Climb, Enroute, Descent ......................... 500FT AGL 2. LNAV Only................................................400FT AGL 3. LNAV/VNAV ..............................................300FT AGL 4. LPV or DA.................................................200FT AGL
34
Pressurization Delta P
9.9 to -0.5 psid
35
Engine Sync Required Off
1. Takeoff 2. Landing 3. Single – Engine Operations
36
Wing/Stab Heat On
2 Minutes Before Takeoff Thrust
37
Anti-Ice On
+10°C to -40°C and Visible Moisture
38
MAX ITT APR | BR and AR Engines
BR- 1013°C AR- 963°C
39
MAX ITT T/O | BR and AR Engines
BR- 991°C AR- 941°C
40
Max ITT MCT | BR and AR Engines
BR- 991°C AR- 916°C
41
Max ITT MCR temperature | BR and AR Engines
BR- 974°C AR- 900°C
42
Max Start temperature | BR and AR Engines
BR- 991°C AR- 941°C
43
Oil Pressure (Normal Operating Range)
50 to 100 psi
44
Oil Pressure (Starting)
125 psi
45
Oil Temperature (Normal Operating Range)
30°C to 127°C
46
Oil Temperature (Min for Starting)
-28ºC
47
Oil Temperature > 30,000FT
140ºC
48
APU Limitations (6 items)
* 300 Amps Max APU Generator * Ground Use Only * Off During De-icing and Gravity Refueling * No Dispatch With APU FAIL CAS * Starter Cooling: 1 Min, 2 Mins, 15 Mins * 30 Seconds Between Stop and Off
49
GPU Max Amps
1500 Amps
50
Generator Limit
300 Max Continuous Amps
51
Spoiler Deployment Prohibited
Flaps more than 0°
52
Starter On Limit
1 Minute
53
Starter Cooling
• 1 Minute • 2 Minutes • 30 Minutes
54
Thrust Reverser Limitations (5 items)
* Paved Surface * No Backing * No Use During Touch and Go’s * Max Thrust Only Above 40 KTS * Ground Use Only
55
Tire Speed Limit. Tire pressure. Blowout temp (main only) | Nose and main
Nose: 182 KTS, 105 to 115 psi Main: 165 KTS, 165 psi, > 390 F
56
Hydraulic Fluid
MIL-H-5606
57
Radar Off Near People
9 FT (this is what the AFM says)
58
Radar Off Near Large Metal
100 FT
59
Engine Idle Prior to Cutoff (Ground)
1 Minute
60
What type of oil is used on the LR45?
Type II
61
Oil Level Check
Within 1 Hour of Shutdown (Preferably Within 15 Minutes After Shutdown)
62
Max Baggage Compartment
500 lbs
63
Best glide
160 KIAS
64
Driftdown Speed
170-200 KIAS
65
Demonstrated crosswind (not a limitation)
22 knots