Memory Items Flashcards
The Q400’s maximum operating ambient temperature limit is ____ and the minimum operating temperature limit is ____.
+50ºC or ISA + 35ºC, whichever is lower; -54ºC.
The maximum operating altitude of the aircraft is ____ and the maximum operating altitude for takeoff is ____.
25,000 feet; 10,000 feet.
The Horizon Air values for Maximum Severe Turbulence Speed is ____ and Maximum Maneuvering Speed (Va) is ____.
200 KIAS; 200 KIAS.
The maximum speed for Flaps 0 degrees during cruise/enroute descent is ____ and for approach is ____.
Vmo; Vmo.
The maximum flaps extended speed (Vfe, Horizon Air values) for Flaps 5 is ____.
195 KIAS.
The maximum flaps extended speed (Vfe, Horizon Air values) for Flaps 10 is ____.
175 KIAS.
The maximum flaps extended speed (Vfe, Horizon Air values) for Flaps 15 is ____.
165 KIAS.
The maximum flaps extended speed (Vfe, Horizon Air values) for Flaps 35 is ____.
155 KIAS.
The landing gear operating speed (VLO) is ____ and the landing gear extended speed (VLE) is ____.
200 KIAS; 215 KIAS.
Alternate gear extension speed is ____ and max tire speed is ____.
185 KIAS; 182 KIAS.
What is minimum holding speed (flaps 0)?
200 KIAS.
What is the minimum speed for severe icing (flaps 0)?
200 KIAS.
What is the minimum speed during a takeoff with an emergency (engine fail, windshear, etc.)?
V2
What is the minimum flap retract speed during takeoff?
V2 + 10
During takeoff, what is the minimum normal two engine speed?
V2 + 10
During climbs, single engine, or driftdown operations (flaps 0), what is the minimum speed in icing conditions or with the REF SPEEDS set to INCR?
Solid bug, Vse(ice).
During climbs, single engine, or driftdown operations (flaps 0), what is the minimum speed in non-icing conditions or with the REF SPEEDS set to OFF?
Open bug, Vse.
During cruise or enroute descents, what is the minimum speed with flaps 0?
180 KIAS.
During approach, what’s the minimum speed with Flaps 0, 5, 10 or 15 degrees?
Low speed cue + 20
During landing (landing configuration), what is the minimum speed with REF SPEEDS set to INCR, windshear, or gusts greater than 10 knots?
Solid bug, Vref(ice).
During landing (landing configuration), what is the minimum speed with REF SPEEDS set to OFF?
Open bug, Vref.
The engine starter cranking limit for the first start attempt is ____ seconds maximum time on, followed by ____ minutes off.
70 seconds; 2 minutes.
What must the temperature be (OAT) on the ground and (SAT) inflight for icing conditions to exist?
10ºC and below; 5ºC and below.
T or F: the engine intake bypass doors shall be open for engine operation in icing conditions.
True.
What is the maximum crosswind component approved for takeoff and landing on a hard, dry, or wet runway?
32 knots.
What is the maximum fuel imbalance between contents of main fuel tanks in flight?
600 pounds.
T or F: Tank 1 and Tank 2 auxiliary fuel pumps are required to be on for landing but not for takeoff.
False, they are on for both takeoff and landing.
The minimum battery temperature for takeoff is ____ and the maximum loadmeter reading for takeoff of the standby battery, auxiliary battery, and the main battery is ____.
-20ºC; 0.1 amps.
What is the maximum operating altitude for the landing gear and/or flaps extended?
15,000 feet.
Setting takeoff power prior to brake release, with the nose of the airplane more than 45 degrees out of wind, is prohibited for wind speeds greater than ____ knots.
8 knots.
T or F: inflight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited.
True.
The maximum cabin pressure differential limit is ____ psi and the maximum cabin pressure differential limit during takeoff/landing is ____ psi.
5.95 psi; 0.5 psi.
Bleed air must be off for takeoff whenever:
tailwind component exceeds 10 knots, windshear is suspected, takeoff is being conducted with MTOP power.
Bleed air must be off for landing whenever:
tailwind component exceeds 10 knots, windshear is suspected, reported OAT exceeds 39ºC.
T or F: takeoff in the BASIC mode (AHRS) is prohibited, but takeoff in DG mode is allowable.
False. Both modes are prohibited for takeoff.
Unless the forward and aft baggage compartments are empty, the airplane shall not be operated farther than ____ from a suitable airport for landing.
One hour flying time.
T or F: HOT MIC select switches on the Captain and First Officer ARCDU shall be OFF and the INT/RAD switch on the observer’s Audio Control Panel shall be centered when using the flightdeck speakers.
True.
T or F: the APU is approved for ground operations only.
True.
T or F: the APU does not need to be shutdown prior to takeoff since it is usable airborne.
False.
T or F: the APU may be operated unattended with passengers on board if OAT exceeds 30ºC.
False.
Which of the following refueling limitations for the APU is correct?
It shall not be operated during gravity (overwing) refueling.
What are the APU ambient temperature limitations?
Upper: +50ºC or ISA + 35ºC, whichever is lower.
Lower: -54ºC.
T or F: the APU bleed air shall be selected off when the aircraft is being deiced/anti-iced.
True.
What are the APU starter cranking limitations?
First Attempt: max on 60 seconds, 5 minutes off.
Second Attempt: max on 60 seconds, maintenance check required.
T or F: during autopilot operation, the pilot shall be seated at the controls with harness secured.
True.
Autopilot (coupled) and Flight Director (manual) approaches are approved from a nominal glideslope angle of ____ to maximum of ____.
2.5 to 4 degrees.
AFCS is approved for autopilot coupled approaches to ____.
CAT I limits only.
Autopilot coupled approaches are approved for all flap configurations except:
Flaps 35 with one engine inoperative.
Autopilot coupled approaches have been demonstrated in crosswind components up to ____ knots.
18 knots.
The minimum height for autopilot engagement after takeoff/go-around is ____ feet AFE.
1,000 feet AFE.
Autopilot shall be disengaged at or above ____ feet AFE for HGS approaches flown in AIII mode, approaches flown with an inoperative engine, or approaches flown with flaps 0.
1,000 feet AFE.
For coupled approaches (non-CAT III), the autopilot shall be disengaged at or above ____ feet AFE.
200 feet AFE.
T or F: the autopilot shall be disengaged in severe icing and severe/extreme atmospheric turbulence.
True.
