LIMITATIONS Flashcards

(80 cards)

1
Q

45-Minute IFR Reserve (lbs.)

A

1121 lbs. (FL300, .74, 16800 lbs)

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2
Q

Minimum Fuel for Release

A

1880 lbs.

DO or ADO on duty may authorize reduction of this quantity

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3
Q

Minimum Fuel for Hot Spare

A

3600 lbs.

DO or ADO on duty may authorize reduction of this quantity

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4
Q

Emergency Fuel

A

759 lbs.

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5
Q

Minimum Runway Length for Release.

A

3500 feet DRY.

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6
Q

Minimum Runway Width

A

60 feet

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7
Q

Max Slope

A

+/- 2%

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8
Q

(Runway Requiremets) Ops Review Required if…

A
  1. Dry: Less Than 4000ft.
  2. Wet/Contaminated: Less than 5500ft.
  3. DAAP Less than 4500

Chief pilot must approve release from or to, or landing on runways with poor braking action.

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9
Q

Exceptions to Runway Requirements…

A

Beaufort, SC (KARW), 3434ft x 75ft, Day and Dry Only.

Port Aransas, TX (KRAS), 3482ft x 70ft. Day Only, Dry Only, Max crosswind 15KTS.

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10
Q

Maximum crosswind for takeoff (STATIC)

A

18 KTS

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11
Q

Maximum crosswind for takeoff (Rolling)

A

25 KTS.

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12
Q

Maximum Crosswind for Landing

A

28 KTS

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13
Q

Maximum Crosswind on a Contaminated Runway

A

Runway = or > 150’…………….. 15KTS

Runway = or < 149’…………….. 10 KTS

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14
Q

Maximum Tailwind for takeoff and landing:

A

10 KTS

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15
Q

The Following Equipment must be operational in RVSM Airspace:

A

Autopilot (1)

Altitude Alerting Device (1)

ATC altitude reporting transponder (1)

Air Data Computers (2)

Pitot Heaters (2) on the probes linked to the ADC in use.

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16
Q

Maximum Ramp/Taxi Weight

A

18,497 lbs.

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17
Q

Maximum Takeoff Weight

A

18,387 lbs

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18
Q

Maximum Landing Weight

A

17042

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19
Q

Maximum Zero Fuel Weight

A

14,220 Lbs

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20
Q

Maximum Operating Altitude

A

45,000 ft.

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21
Q

Maximum Flaps Extended Altitude

A

18,000 ft.

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22
Q

Maximum Altitude OEI in Icing

A

15,000 ft.

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23
Q

Maximum Altitude for TAKEOFF and LANDING

A

14,000 ft

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24
Q

Maximum Altitude for TAKEOFF and LANDING in Icing

A

10,000 ft.

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25
Maximum Operating Speed Vmo
320 KTS.
26
Maximum Operating Mach Number Mmo
.78 mach
27
Turbulent Air Penetration Speed
232 kts/.65 mach
28
Maneuvering Speed
205 Kts
29
Maximum Landing Gear Operating Speed
250 KTS
30
Maximum Tire Ground Airspeed
182 KTS
31
Vfe Flaps 1
180 KTS
32
Vfe Flaps 2 and 3
170 KTS
33
Vfe Flaps Full
160 KTS
34
Minimum Airspeed in Icing - WING STAB anti-ice system INHIBITED (flaps and gear up)
165 KTS
35
Minimum Airspeed in Icing - WING STAB anti-ice system UN-INHIBITED (flaps and gear up)
150 KTS
36
Maximum Airspeed in Icing - YAW DAMPER OFF
180 KTS
37
Vmc TAKEOFF
97
38
Vmc LANDING
91
39
Vmc LANDING in Icing
95
40
Max Differential Pressure (psi)
9.4 psi
41
Max Differential OVERPRESSURE
9.6 psi
42
Max NEGATIVE Differential
- 0.3 psi
43
Max Differential for TAKEOFF and LANDING
0.2 psi
44
Do Not use Autopilot or Yaw Damper for....
TAKEOFF and LANDING ** DO NOT MANUALLY OVERRIDE AUTOPILOT DURING NORMAL FLIGHT.
45
Autopilot or Yaw Damper MINIMUM engagement height TWO ENGINES
600 ft AGL
46
Autopilot or Yaw Damper MINIMUM engagement height OEI
1000 ft AGL
47
Autopilot or Yaw Damper MINIMUM USE height TWO ENGINES
195 ft. AGL
48
Autopilot or Yaw Damper MINIMUM USE height OEI (ONE ENGING INOP)
220 ft AGL
49
Minimum Voltage for Battery Start
24V
50
Minimum GPU voltage for Battery Charging
27V
51
Maximum generator load in flight
390 Amps
52
Maximum generator load on the ground
330 Amps
53
Total Fuel Quantity
5401 lbs
54
Maximum Fuel Imbalance
220 lbs
55
Operate the Engines and Airframe anti-icing systems in accordance with:
4.5.2 Operation of Anti-Ice Systems
56
Minimum Temperature for Landing
-38 C
57
Automated operating (Temperature) Envelope for wing stab heating (Below 16,000ft)
-40 C Amber A-I WINGSTB INHB CAS message is displayed if WING STAB is selected ON outside the operating envelope. Refer to QRH for additional information.
58
Automated operating Envelope for wing stab heating (at or above 16000ft)
-45C Amber A-I WINGSTB INHB CAS message is displayed if WING STAB is selected ON outside the operating envelope. Refer to QRH for additional information.
59
Do Not use the Autopilot in icing conditions when:
* there is ice accumulation on the wing, aft of the protected area. * encountering unusual lateral trim inputs or autopilot trim warnings
60
Aircraft is certificated in Approach Category:
Category B ** however, if operational requirements dictate and approach speed faster than 120Kts, use Category C minima.
61
Time Limitation at Maximum Thrust
10 minutes
62
Time limit at Takeoff Thrust
5 minutes
63
Maximum Continuous Thrust time limit and condition
5 Minutes when in level flight.
64
Climb Thrust time limit and condition
5 minutes in level flight.
65
Max TRANSIENT N1
102%
66
Max TRANSIENT N2
103%
67
Max TRANSIENT ITT
765 C
68
Max TRANSIENT time limit
20 seconds
69
Max ITT for Engine Start
765 C
70
Max Continuous/Climb Thrust ITT
680 C
71
Max ITT at Takeoff Thrust
700 C
72
Max ITT at Maximum Thrust
725 C
73
Ground Idle N2
51.2%
74
Flight Idle N2
55.1%
75
Max N1/N2 (maximum Thrust, takeoff thrust, Max cont thrust, climb thrust)
N1 - 100% N2 - 101%
76
One Engine Inoperative (OEI) ground Idle N2
55.1% N2
77
Min-Max TRANSIENT oil Pressure (20 Seconds)
0-20 psi
78
Min-Max TRANSIENT oil Pressure (400 Seconds)
20-270 psi
79
Starter Limitations.... How many attempts? Cool Down?
Four Attempts: 1st attempt, 1 minute cool down 2nd attempt, 1 minute cold down 3rd attempt, 15 minutes cool down 4th attempt, 30 minutes cool down
80
Unless the batteries are warmed prior to start, GPU assisted engine start must be accomplished when OAT is at or below?
-18 C (AOM 4.5.1 Cold Soaked Airplane)