E145 Limitations UPDATED ACTUAL Questions and
CORERCT Answers
Maximum Altitude for operation after an in flight 10,000 ft.
depressurization is ________ MSL unless MEA or other
constraints require a higher altitude.
Maximum Operating VMO/MMO 320 kts. / .78 Mach
Maximum Operating (KIAS) 8,000 to 10,000 ft. MSL Red Line
Maximum Operating (KIAS) - up to 8,000 ft. MSL 250 kts.
Maximum Turbulence Penetration (Vb/Mb) 250 kts. / 0.63 Mach whichever is lower. 200 at or below 10,000 ft.
Maximum Maneuvering (Va) 200 kts. (Full application of rudder and ailerons, and maneuvers involving angle
of attack near stall, must be confined to speeds below VA.)
Landing Gear Extension (Vloe) 250 kts.
Landing Gear Extended (Vle) 250 kts.
Landing Gear Retraction (Vlor) 200 kts.
Flap Placard Speeds (Vfe) 9° - 250
18° - 200
22° - 200
45° - 145
Maximum Operating Altitude 37,000 ft.
, Minimum Takeoff and Landing Pressure Altitude -1,000 ft.
Maximum Takeoff and Landing Pressure Altitude 8,000 ft.
Takeoff and Landing Temperature Limits: Minimum -40°C SAT (In the event of a landing below -40°C SAT, the aircraft may not
takeoff without further maintenance inspection.)
TAT in cruise flight above 25,000 ft. is limited to -45°C
____________.
Icing conditions may exist in flight whenever: The Total Air Temperature (TAT), is 10°C or below and visible moisture in any
form is present (such as clouds, fog with visibility of one mile or less, rain, snow,
sleet and ice crystals).
Icing conditions may exist on the ground or for takeoff The Static Air Temperature (SAT) on the ground or for takeoff, or Total Air
whenever: Temperature (TAT) in flight, is 10°C or below and visible moisture in any form is
present.
(such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice
crystals).
Icing conditions may also exist when the SAT on the ground and for takeoff is
10°C or below when operating on ramps, taxi ways, or runways where surface
snow, ice, standing water, or slush may be ingested by the engines, or freeze
on engines, nacelles, or engine sensor probes.
Minimum Temperature for Manual Anti-icing Operation -40°C (There is no temperature limitation for automatic Anti-icing System
operation.)
Maximum Temperature for Manual Anti-icing Operation 10°C (There is no temperature limitation for automatic Anti-icing System
operation.)
A runway is considered "Contaminated" when more • Deeper than 1/8th inch (3 mm.) of:
than 25% of the required field length, within the width — standing water,
being used, is covered by: — slush or
— wet snow.
• Deeper than 1/4 inch (11 mm) of dry snow.
• Compacted snow
• Ice
Minimum Decision Altitude During ILS Approach 200 ft AGL
Autopilot Minimum Engagement Height (Takeoff or Go- 500 ft
around)
Autopilot Minimum Use Height 160 ft
Autopilot Malfunction altitude loss: • Cruise - 80 ft
• Maneuver - 40ft
• ILS Approach - 15ft
Descent below_______________________ on a non- Minimum Descent Altitude
precision approach with autopilot engaged is
prohibited.
CORERCT Answers
Maximum Altitude for operation after an in flight 10,000 ft.
depressurization is ________ MSL unless MEA or other
constraints require a higher altitude.
Maximum Operating VMO/MMO 320 kts. / .78 Mach
Maximum Operating (KIAS) 8,000 to 10,000 ft. MSL Red Line
Maximum Operating (KIAS) - up to 8,000 ft. MSL 250 kts.
Maximum Turbulence Penetration (Vb/Mb) 250 kts. / 0.63 Mach whichever is lower. 200 at or below 10,000 ft.
Maximum Maneuvering (Va) 200 kts. (Full application of rudder and ailerons, and maneuvers involving angle
of attack near stall, must be confined to speeds below VA.)
Landing Gear Extension (Vloe) 250 kts.
Landing Gear Extended (Vle) 250 kts.
Landing Gear Retraction (Vlor) 200 kts.
Flap Placard Speeds (Vfe) 9° - 250
18° - 200
22° - 200
45° - 145
Maximum Operating Altitude 37,000 ft.
, Minimum Takeoff and Landing Pressure Altitude -1,000 ft.
Maximum Takeoff and Landing Pressure Altitude 8,000 ft.
Takeoff and Landing Temperature Limits: Minimum -40°C SAT (In the event of a landing below -40°C SAT, the aircraft may not
takeoff without further maintenance inspection.)
TAT in cruise flight above 25,000 ft. is limited to -45°C
____________.
Icing conditions may exist in flight whenever: The Total Air Temperature (TAT), is 10°C or below and visible moisture in any
form is present (such as clouds, fog with visibility of one mile or less, rain, snow,
sleet and ice crystals).
Icing conditions may exist on the ground or for takeoff The Static Air Temperature (SAT) on the ground or for takeoff, or Total Air
whenever: Temperature (TAT) in flight, is 10°C or below and visible moisture in any form is
present.
(such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice
crystals).
Icing conditions may also exist when the SAT on the ground and for takeoff is
10°C or below when operating on ramps, taxi ways, or runways where surface
snow, ice, standing water, or slush may be ingested by the engines, or freeze
on engines, nacelles, or engine sensor probes.
Minimum Temperature for Manual Anti-icing Operation -40°C (There is no temperature limitation for automatic Anti-icing System
operation.)
Maximum Temperature for Manual Anti-icing Operation 10°C (There is no temperature limitation for automatic Anti-icing System
operation.)
A runway is considered "Contaminated" when more • Deeper than 1/8th inch (3 mm.) of:
than 25% of the required field length, within the width — standing water,
being used, is covered by: — slush or
— wet snow.
• Deeper than 1/4 inch (11 mm) of dry snow.
• Compacted snow
• Ice
Minimum Decision Altitude During ILS Approach 200 ft AGL
Autopilot Minimum Engagement Height (Takeoff or Go- 500 ft
around)
Autopilot Minimum Use Height 160 ft
Autopilot Malfunction altitude loss: • Cruise - 80 ft
• Maneuver - 40ft
• ILS Approach - 15ft
Descent below_______________________ on a non- Minimum Descent Altitude
precision approach with autopilot engaged is
prohibited.
