Memory Items - Limits Flashcards
Limitzzzz
Severe Turbulence Speed
200 KIAS
Maneuvering Speed (VA)
200 KIAS
Max Flaps Speed 5º (VFE)
195 KIAS
Max Flaps Speed 10º (VFE)
175 KIAS
Max Flaps Speed 15º (VFE)
165 KIAS
Max Flaps Speed 35º (VFE)
155 KIAS
Landing Gear Operating Speed (VLO)
200 KIAS
Landing Gear Extended Speed (VLE) doors closed
215 KIAS
Ambient Temp Max (engine)
+50ºC or ISA +35ºC, whichever is lower
Engine Starter Cranking Limits
Start: 1, Max Time on: 70 Seconds, Followed by: 2 minutes off
On the ground (taxi and takeoff roll to the point of lift-off):
_____________ or below when precipitation in any form is present, or fog with visibility of
one mile or less; also when operating on ramps, taxiways, or runways where surface
snow, ice, slush, or standing water may be ingested by the engines or freeze on engines,
nacelles, or engine sensor probes.
OAT is 10ºC
In flight (after lift-off to landing):
_____________ or below and _____________ is present in any form. Ice accretion on
aerodynamic surfaces is not considered to exist at temperatures of -40°C or below.
SAT is 5ºC, visible moisture
Engine intake bypass doors shall be ________ for engine operations in icing conditions
Open
Maximum crosswind component approved for takeoff and landing on a hard, dry, or wet
runway is ______.
32 knots
Maximum fuel imbalance between contents of main fuel tanks is ______ (This is an in-flight
limitation only.)
600 lb
Standby battery, Auxiliary battery and Main battery maximum loadmeter reading for
takeoff is
0.1
Minimum battery temperature for takeoff is
-20ºC
Maximum altitude with the landing gear and/or flap extended is
15,000 ft
Setting takeoff power prior to brake release, with the nose of the airplane more than ____ out
of wind, is prohibited for wind speeds greater than ____ knots.
45°, eight
Tank 1 and tank 2 auxiliary pumps must be ____ for takeoff and landing.
on
Maximum operating altitude
25,000 ft ASL
Maximum operating altitude for takeoff
10,000 ft ASL
Airplane maximum operating ambient temperature limit
+50°C or ISA +35°C, whichever is lower
Airplane minimum operating ambient temperature limit is _____.
-54°C
Ambient temperature conditions on the ground shall be derived by reference to reported
_____.
Ambient temperature conditions in flight shall be derived by reference to indicated _____.
OAT, SAT
Inflight operation of the _____aft of the _____ gate is _____.
Power Levers, FLIGHT IDLE, prohibited
Maximum cabin pressure differential limit
5.95 psi
Maximum cabin pressure differential limit during takeoff and landing
0.5 psi
Bleed air must be _____ for takeoff whenever:
• Tailwind component exceeds _____ knots
• Takeoff is conducted with _____ power selected
• _____ is suspected
off, ten, MTOP, Windshear
For landing, bleed air must be _____ whenever:
• Tailwind component exceeds _____ knots
• Reported _____ exceeds _____
• _____is suspected
off, ten, OAT, 39°C (100°F), Windshear
Takeoff in ______ mode is prohibited (AHRS)
BASIC, DG
Baggage Compartment Fire Extinguishing:
Unless the _____ baggage compartments are empty, the airplane shall not be
operated farther than _____ hour flying time from a suitable airport for landing.
forward and aft, one
_____ select switches on the Captain and First Officer ARCDU shall be _____ and the
_____ switch on the observer’s Audio Control Panel shall be _____, when using the
flightdeck _____.
HOT MIC, OFF, INT/RAD, centered, speakers
APU is approved for _____ OPERATION ONLY.
GROUND
APU shall be _____ prior to takeoff
shutdown
APU shall not be operated _____ with _____ on board
unattended, passengers
APU shall not be operated during _____ refueling.
gravity (overwing)
To maintain steady electrical state, the APU _____ be started during _____.
shall not, refueling
APU ambient temperature limitations (max)
+50ºC or ISA +35ºC, whichever is lower
APU ambient temperature limitations (min)
-54ºC
When the APU has been shut down in _____ below _____ for greater than
_____ hour, it must be preheated prior to start in accordance with applicable maintenance
procedures.
outside air temperature, -35ºC, one
The APU Bleed Air shall be selected _____ when the aircraft is being _____.
off, deiced/anti-iced
APU starter cranking limits (Start 1)
Max Time on: 60 seconds, Followed By: 5 minutes off
APU starter cranking limits (Start 2)
Max Time on: 60 seconds, Followed By: Maintenance action required
(APU) Including the time taken for maintenance action following the second start attempt, a
minimum of _____ minutes must elapse prior to the next start attempt.
30
During autopilot operation, the pilot shall be seated at the _____ with _____ secured.
controls, harness
Autopilot (coupled) and Flight Director (manual) approaches are approved from a
nominal glideslope angle of _____ to maximum of _____.
2.5°, 4°
AFCS is approved for autopilot coupled approaches to _____ limits only.
CAT I
______ approaches are approved for _____ flap configurations.
Autopilot coupled, all
Use of Flaps _____, autopilot coupled is prohibited with _____
35°, one engine inoperative
Autopilot coupled approaches have been demonstrated in crosswind components up to
_____ knots. _____.
18, This is not considered limiting
After takeoff or go-around, the minimum height for autopilot engagement is _____.
1,000 feet AFE
Autopilot shall be disengaged at or above _____ for:
- HGS approaches flown in _____ mode
- Approaches flown with an _____
- Approaches flown with Flap _____
1,000 feet AFE, AIII, inoperative engine, 0°
For coupled approaches, the autopilot shall be disengaged at or above _____.
200 feet AFE
Autopilot shall be disengaged in _____ icing.
severe
Autopilot shall be disengaged in _____ atmospheric turbulence
severe or extreme
Max Flaps Speed 0º (VFE)
Vmo-10kts
Maximum Tire Speed
182 KIAS
Maximum Alternate Gear Extension Speed
185 KIAS
Min Flaps Speed 5º (Vmin)
160 KIAS
Min Flaps Speed 0º (Vmin)
180 KIAS
Min Flaps Speed 15º (Vmin)
145 KIAS
Min Flaps Speed 10º (Vmin)
150 KIAS
Abort engine start if
- Engine ITT approaches or exceeds 920ºC
- NH is not in the green arch within 70 seconds of selecting Condition Lever to START & FEATHER
- Engine Oil Pressure fails to reach 44 psi by start SELECT switch reset
Takeoff Abort required when
- Takeoff warning horn
- Failure of the A/F ARM message to illuminate on ED
- Engine fire or failure
- MASTER WARNING
- Takeoff torque not obtained on either engine
- Exceeding engine limitations
- Windshear encounter
- HGS failure, “TO WARN,” or loss of HGS symbology during takeoff below 500 RVR when the runway centerline is not in sight
O2 required when either pilot detects a situation
- Which could introduce smoke or fumes in the flightdeck, shall state. “Smoke - Don mask,”
- Results in loss of cabin pressure above 10,000 MSL, shall state, “Oxygen - Don mask.”
Max ramp weight
65, 400 lbs
Maximum takeoff weight
65,200 lbs
Maximum landing weight
62,000 lbs
Maximum zero fuel weight
58,000 lbs
Minimum structural design weight
31,753 lbs
