Limitations Flashcards
General Knowledge of 373 limitations
Minimum turning radius
67 feet, 18 feet clearance in front of the nose for wing clearance.
Autoland Maximum Winds
Headwind 25 Knots
Crosswind 15 Knots
Tailwind 10 Knots
Maneuvering Load Limitations Flaps up
2.5g to -1.0g
Maneuvering Load Limitations Flaps down
2.0g to 0.0g
Maximum Take off and Landing Pressure Altitude
10,000 feet
Maximum Runway Slope
2% plus or minus
A narrow runway is considers less then
148 feet
MMO
.82 Mach
Maximum gear retraction speed
235 Knots
Maximum gear extension speed
270 Knots/ .82 Mach
Maximum gear extended speed
320knots/ .82 Mach
Flaps 1 extension speed
240 knots
Flaps 2 extension speed
240 knots
Flaps 5 extension speed
230 knots
Flaps 10 extension speed
210 knots
flaps 15 extension speed
200 knots
flaps 25 extension speed
190 knots
Flaps 30 extension speed
175 knots
Flaps 40 extension speed
162 knots
Maximum pressure differential
9.1 psi
Maximum differential pressure for takeoff and landing
.125 psi
Max differential pressure above 37,000 feet
8.3 psi plus minus .1psi
Max differential pressure 28,000-37,000 feet
7.8 psi plus minus .1psi
Max differential pressure below 28,000 feet
7.45 psi plus minus .1
Max cooling duct pressure
20-25 psi
Windshield Heat must be on for how long prior to take off
10 minutes
Probe Heat must be turned on
prior to takeoff
Wing Anti Ice on take off
do not use until after first power reduction
Autoland max winds - Headwind
Crosswind
Tailwind
25 knots headwind
15 knots crosswind
10 knots tailwind
The use of Aileron can be used with Auto Pilot on…
T or F
is prohibited
Is the Auto Pilot allowed to be used at less then 100 feet at airports pressure altitudes greater then 8,400 feet
No it is prohibited
ILS auto land requires flaps…
30° or 40° with both engines operitive
Maximum and Minimum glide slope angled for Autoland are
3.25° and 2.5°
How low can one use LVL CHG
not below 1000 feet AFE
At what altitude must the Auto Pilot be disengaged except auto land?
50 feet AGL
Maximum Generator Load ground ops
75 KVA-215 amps (ground ops)
Maximum Generator Load air ops
90 KVA-215 amps (air ops)
Maximum Generator Load air ops MAX
75KVA-215 amps (air ops)
Minimum Battery Voltage APU start
23 Volts
Min (NG/Max) Oil pressure
NG 18 psi - MAX 17.4 psi
Minimum starting Oil Temp MAX
-41°
Minimum takeoff Oil Temp MAX
31°
Maximum Oil Temp
155°
Maximum Continuous Oil Temp
140°
Maximum EGT Limits NG Takeoff (5 Min)
950°
Maximum EGT Limits NG Continuous
925°
Maximum EGT Limits NG Start
725°
Engine Starter, how long is a normal engine start cycle and what is the minimum amount of time between cycles?
NG - 2 min with 10 sec between cycles
Max - 3 min with 10 sec between cycles
Extended engine motoring limited to ___ minutes and ___ mins between cycles.
NG 15 min - 2 min for 2 cycles
(cycle 3 and beyond, 5 mins and 10 min between cycles)
Max 5 min - 5 min for 2 cycles
(cycle 3 and beyond, 5 min and 10 min between cycles)
Maximum N1 and N2 speeds
NG 104% and 105%
MAX 104.3% and 117.5%
Can you takeoff in reduced thrust with Anti Skid inoperative?
No
If the runway is contaminated is reduced thrust takeoff allowed?
No (snow, slush, standing water, ice)
Is a go-around permissible after deploying reverse thrust?
No
What is the position for the EEC for takeoff?
On or ALTN (if EEC is in ALTN reduced thrust takeoff is prohibited)
Max Alt for APU bleed and electrical
10,000 feet
Max Alt for APU bleed
17,000 feet
Max Alt for APU electrical
41,000 feet
Minimum Oil for Engine Start
70%
Idle time for Engine Start below -35°
Idle for 2 min before advancing thrush levers
Fuel temperature prior to start must not be less then
3° C above the fuel freezing point or -43° C
APU starter cycles on failed start
15 min cooling down period is required after the third attempt
Warm up time before using bleed air off the APU
1 minute
How long is the APU shut down cycle
120 seconds
Lavatory Fire Extinguisher Bottle has been discharged when
the Nozzle tip turns Aluminum in color
Engine Fire Extinguisher Bottle pressure
800 psi
Configuration for holding in icing conditions
flaps up
In flight max selection of speed brake lever is
FLIGHT DETENT
In flight with flaps 40 do not extend the speed brake lever beyond
ARMED
Do not deploy the speed brake lever below
1000 feet AGL
Alternate Flap duty cycle how long before one can reengage the switch?
15 seconds, to avoid damaging the to the alternate flap motor clutch
Maximum airspeed to extend the flaps with the alternate system
230 knots
Maximum speed if Mach trim fail both channels
280 knots/.82 Mach
Max difference in CA and FO altimeter to remain in RVSM
200 feet
Max difference between CA and FO altimeter on the ground below 5000 Field elevation
50 feet and 75 of the field elevation
Max difference between CA and FO altimeter on the ground above 5001 Field elevation
60 feet and 75 of the field elevation
Weather radar during ground operations.
15 feet of people and 50 feet of spilled fuel
Maximum fuel imbalance
1000 lbs
Tank capacity - wings
center
wings, 1,288 gal or 8,630 lbs
center, 4,299 gal or 28,803 lbs
Intentionally running of the center fuel tank with the LOW PRESSURE light illuminated is
Prohibited
Hydraulic quantity Max/Min
105% and above RF (76%)
Tire ground speed
NG 195 knots - MAX 204 knots
Auto brakes before takeoff
RTO if operable/OFF is inop