QUIZLET ADDTL Flashcards
Maximum Takeoff Torque
100%
Maximum Continuous Torque
100%
Maximum Transient Torque
156% (20 seconds)
Maximum Starting ITT
1000°C
Maximum Idle ITT
750°C
Maximum Takeoff ITT
820°C
Maximum Continuous ITT
820°C
Maximum Transient ITT
850°C (20 seconds)
Maximum Takeoff N1
104%
Minimum Idle N1
62%
Maximum Continuous N1
104%
Maximum Transient N1
104%
Maximum Takeoff Propeller RPM
1700 RPM
Maximum Continuous Propeller RPM
1700 RPM
Maximum Transient Propeller RPM
1870 (20 seconds)
Starting Oil Pressure
0-200 PSI
Takeoff Oil Pressure
90-135 PSI
Maximum Continuous Oil Pressure
90-135 PSI
Maximum Transient Oil Pressure
200 PSI
Minimum Starting Oil Temperature
-40°C
Takeoff Oil Temperature
0-110°C
Maximum Continuous Oil Temperature
0-110°C
Oil Temperature Limit for 99-110°C
10 minutes
External Power Volts
28.0-28.4 volts
External Power Amps - Continuously
300 amps
External Power Amps - Momentarily
1000 amps
Generator In Flight Limit - Sea Level to 34,000 feet
100%
Minimum Starting Oil Temperature
-40°C
Takeoff Oil Temperature
0-110°C
Maximum Continuous Oil Temperature
0-110°C
Oil Temperature Limit for 99-110°C
10 minutes
External Power Volts
28.0-28.4 volts
External Power Amps - Continuously
300 amps
External Power Amps - Momentarily
1000 amps
Generator In Flight Limit - Sea Level to 34,000 feet
100%
Generator In Flight Limit - 34,000 to 35,000 feet
95%
Generator Load Limit on Ground - 62-70% N1
75%
Generator Load Limit on Ground - 70-100% N1
100%
Starter Limits
30 sec ON, 5 min OFF
30 sec ON, 5 min OFF,
30 sec ON, 30 min OFF
Approved Engine Commercial Fuels
Jet A, Jet A-1, Jet B
JP-4, JP-5, JP-8
Approved Emergency Engine Fuels
RED 80,
GREEN 91/96, 100,
BLUE 100LL,
PURPLE115/145
Conditions of Emergency Engine Fuels
Maximum of 150 hours between engine overhauls. Operations prohibited if either standby pump inoperative. Crossfeed capability is required over 20,000 feet.
Total Usable Fuel
3611 lbs.
Usable Fuel in Each Main Tank
1273 lbs.
Usable Fuel in Each Auxiliary Tank
533 lbs.
Maximum Fuel Imbalance Between Sides
300 lbs.
Conditions of Fuel Crossfeed
Only during single engine operations.
Yellow Arc of Fuel Gage
Do not attempt a takeoff.
Which fuel tank must be filled first?
Main Tanks
Time Limit with L Fuel Pressure
10 hours before standby pump must be overhauled
Maximum Propeller Reverse RPM
1650 RPM
Minimum Propeller RPM
1050 RPM
Propeller RPM Overspeed Limit
1768 RPM (96% torque or less)
Autofeather Must be Operable for What Conditions?
All flight conditions.
Autofeather Must be Armed for What Conditions?
Takeoff, climb, approach, landing.
Cabin Differential Pressure Gage Green Arc
0-6.6 PSI
Cabin Differential Pressure Gage Red Arc
Above 6.6 PSI
Pneumatic Pressure Gage Green Arc
12-20 PSI
Pneumatic Pressure Gage Red Line
20 PSI
Vacuum Gage Narrow Green Arc (15,000 to 35,000 feet)
2.8-4.3”Hg
Vacuum Gage Wide Green Arc (Sea Level to 15,000 feet)
4.3-5.9”Hg
Vacuum Gage 35K Mark
3.0 PSI
Vacuum Gage 15K Mark
4.3 PSI
Propeller Deice Ammeter Green Arc
26-32 AMPS
Maximum Ramp Weight
15,100 lbs.
Maximum Takeoff Weight
15,000 lbs.
Maximum Landing Weight
15,000 lbs.
Maximum Zero Fuel Weight
12,500 lbs.
Maximum Cargo Weight
550 lbs.
Maximum Flaps Up Load Factor
+3.1g’s , -1.24g’s
Maximum Flaps Down Load Factor
+2.0g’s , -0.0g’s
Maximum Altitude
35,000 feet
Maximum Operating Air Temperature Sea Level to 25,000’
ISA +37°C
Maximum Operating Air Temperature 25,000’ to 35,000’
ISA +31°C
Landing Gear Cycle Limits
1 Cycle X 6 then 15 min cool down
Maximum Temperature for Operating Brake Deice
15°C
Minimum Ambient Temperature for Deicing Boots
-40°C
Minimum Airspeed for Icing
140 knots
Electric heat must be turned off ____ minutes before and during engine start.
2 minutes
Cockpit door must be ____ while using electric heat.
open
All aft facing seats must be in the _____ position and the headset must be fully _____ for takeoff and landing.
upright, extended
Composite mode operation is limited to _____.
failures, training
The pilot and co-pilot Air Data Computers must be _____ for takeoff.
operative
AHRS 1 and 2 must be ____ for takeoff.
operative
The pilot PDF and MFD and co-pilot PFD must be ____ for takeoff.
installed and operational in normal mode
The MFD must be ____ prior to engine start.
operational
During autopilot operations a pilot must be ____.
seated at the controls with the seat belt and shoulder harness fastened
Autopilot preflight check must be ____.
satisfactory prior to each flight on which the autopilot is to be used
Minimum autopilot engage height after takeoff:
400’ AGL
Minimum autopilot use height during cruise:
1000’ AGL
Minimum autopilot use height during approach:
79’ AGL
Minimum autopilot use height during a steep approaches:
160’ AGL
Maximum airspeed for autopilot:
Vmo
Autopilot and yaw damper must not be used during ____.
takeoff and landing
Autopilot system operation with a pitch trim malfunction is _____.
prohibited
Maximum coupled intercept angle intercept angle for NAV and LOC is _____.
90°
Maximum coupled intercept angle intercept angle for LOC BC is _____.
70°
Do not rely on the Terrain Awareness Display for ____.
navigation
Inhibit the Terrain Awareness Display by ____.
selecting TERR INHIBIT switch when winthin 15nm of takeoff, approach, or landing at an airport not contained in the EGPWS Airport Database
The Terrain Awareness alerting must be inhibited by selecting the TERR INHIB switchlight when ____.
the FMS is operating in the DR mode
IFR enroute and terminal navigation is prohibited unless ____.
the pilot verified either the currency of the database or the accuracy of each selected waypoint and navaid by reference to current approved data
The FMS position must be ____.
checked for accuracy prior to use as means of navigation
The FMS shall not be used for navigation ____.
during periods of dead reckoning
FMS based instrument approaches must be accomplished in accordance with ____.
approved instrument approach procedures that are retrieved from the FMS-3000 database
GPS instrument approaches must be conducted with ____.
GPS integrity monitoring (RAIM) and must be available by the Final Approach FIX
To indicated the FMS is in the Approach Mode:
Green APPR or GPS APPR annunciator must be displayed on the PFD at the FAF.
When the NO APPR annunciator is displayed on the PFD:
Use of FMS guidance for conducting instrument approach procedures is prohibited.
Accomplishment of ILS, LOV, LOC BC, LDA and SDF approaches are ____.
not authorized utilizing the FMS from the FAF to the MAP
When an alternate airport is required by the applicable rules ____.
it must be served by an approach based on other than GPS navigation
Use of FMS to capture and track a DME arc outside the published end points is ____.
prohibited
Fuel management parameters are advisory only and ____.
must not replace the primary fuel quantity indications
When using the VNAV system, the barometric altimeters must be used as the primary altitude reference for ____.
all operations
Use of VNAV guidance for a V-MDA approach that includes a step-down fix between the final approach fix and missed approach point ____.
is prohibited
VNAV altitudes must be displayed in the MFD map page or CDU legs page when ____.
utilizing VNAV for flight guidance
Use of VNAV while conducting a missed approach procedure is ____.
prohibited
If the FMS is receiving usable sensor inputs, it meets the ____.
accuracy specifications of VNAV operation in accordance with AC 20-129
VNAV approach guidance to a DA is not authorized if the reported surface temperature is ____.
below the Baro-VNAV minimum temperature limitation specified on the applicable RNAV approach procedure chart
Maximum approved approach angle is ____.
5.5°
One-Engine-Inoperative steep approaches ____.
not approved
Flaps UP steep approaches ____.
not approved
Steep approaches are only approved when the following configuration is established no later than the final approach fix, or 3 nm from the runway during visual approaches: both engines:____, flaps:____, prop levers:____, approach speed:____.
operative, full down, full forward, Vref or Vref+15 with ice
Steep approaches are approved only when using vertical guidance provided by an approved ____.
FMS or ILS or Ground Based Visual Reference System
FMS defined approaches ____.
not approved using autopilot; use of flight director approved
Maximum tailwind for steep approaches ____.
5 knots
Stall Speed (Vso) - Flaps Down, Power Idle, Max Weight
81 KIAS
Stall Speed (Vs1) - Flaps Approach, Power Idle, Mas Weight
89 KIAS
Stall Speed (Vs1) - Flaps Up, Power Idle, Max Weight
96 KIAS
satisfactory prior to each flight on which the autopilot is to be used
400’ AGL
