Limitations Flashcards
Runway slope
+ / - 2%
Max. T/O and Landing Tailwind component
10 knots
Maximum speeds
Observe Vmo pointed and gear / flaps placards
Maximum flight operational latitude
73 North / 60 South
Maximum operating altitude
37000 ft
Maximum T/O and landing altitude
8400 ft
Severe turbulent air penetration speed
280 KIAS / .73M Applicable to Climb and Descent only
During Cruise, refer to SP.16, Severe Turbulence Supplementary Procedure
Standby altimeters do not meet altimeter accuracy requirements of RVSM airspace.
True or false?
True
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations
200 ft
The maximum allowable on-the-ground altitude display differences for RVSM operations are
Memory
Possible conflicts between the AFM and the FCOM may occur due to separate publication release dates. In the event of a conflict between the FCOM and the AFM
the AFM shall govern
Maximum Taxi Weight
29337 & 29341 :
128,500 lbs (58,286 kgs)
28558 :
140,000 lbs (63,502 kgs)
Maximum Takeoff Weight
29337 & 29341:
128,000 lbs (58,059)
28558:
139,500 lbs (63,276 kgs)
Maximum Landing Weight
29337 & 29341:
114,000 lbs (51,709 kgs)
28558:
114,000 lbs (51,709 kgs)
Maximum zero fuel weight
29337 & 29341:
105,000 lbs (47,627kgs)
28558:
105,000 lbs (47,627 kgs)
The maximum cabin differential pressure (relief valves) is:
Air system
8.65 psi
Do not use aileron trim with:
autopilot engaged.
Maximum and minimum glideslope angles for autoland
3.25 degrees and 2.5 degrees respectively.
Do not use LVL CHG on final approach below
1000 ft AFE
Maximum generator drive oil temperature
157° C
Maximum and minimum limits are
Red
Caution limits are
Amber
Maximum time limit for takeoff thrust
5 minutes
Maximum N1 RPM
106%
Maximum N2 RPM
105%
Maximum Takeoff EGT
930
Maximum Continuous EGT
895
Maximum Start EGT
725
Minimum Oil Pressure
13 psi
Maximum Oil Temperature
165° C maximum
160° C – 165° C allowable for 15 minutes
160° C maximum continuous
Continuous ignition must be on (ENGINE START switch in the CONT position) during
takeoff and landing and during engine anti–ice operations
When flight in moderate or heavy rain, hail, or sleet is encountered or anticipated, engine start switches must be set to
FLT and a minimum of 45% N1 must be maintained except on short final when landing is assured
Both PMCs must be either
OFF or ON for takeoff
Intentional selection of reverse thrust in flight is…
Prohibited
APU Maximum start EGT is
760° C
APU Maximum continuous EGT is
710° C
With APU bleed + electrical load, maximum altitude is
10,000 ft
With APU bleed, maximum altitude is
17,000 ft
APU can operate up to
37,000 ft
With APU electrical load, maximum altitude is…
35,000 ft
Pneumatic pressure (prior to starter engagement)
minimum 30 psig at sea level, decreasing 1/2 psig per 1,000 ft. above sea level.
APU bleed valve must be closed when:
- ground air connected and isolation valve open •engine no. 1 bleed valve open
- isolation valve and engine no. 2 bleed valve open.
APU bleed valve may be open during engine start, but …
avoid engine power above idle
APU
If there are multiple aborted start attempts … minutes of cooling is required between the second and third start attempt.
5
APU
A wait of… is required after the third start attempt.
One hour
The maximum altitude with flaps extended is
20,000 ft
In flight, do not extend the SPEED BRAKE lever beyond the…
FLIGHT DETEND
Do not deploy the speedbrakes in flight at radio altitudes less than…
1000 ft
When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow … after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch
15 minutes
After a completed extend/retract cycle, i.e., 0 to 15 and back to 0, allow … cooling before attempting another extension.
5 minutes
Avoid weather radar operation in …, or within … of fueling operations or a fuel spill.
A hangar - 50 feet (15.25 meters)
The hangar recommendation does not apply to… .
the weather radar test mode.
Do not reset a tripped … circuit breaker
Fuel pump
Maximum fuel temperature is… .
49°C.
Inflight tank fuel temperature must be maintained at least … or … , whichever is higher.
3°C above the freezing point of the fuel being used / –45°C
Lateral imbalance between main tanks 1 and 2 must be scheduled to be …
Zero
Random fuel imbalance must not exceed … for taxi, takeoff, flight, or landing.
1,000 lbs (453 kgs)
Main tanks 1 and 2 must be scheduled to be full if center tank contains more than … of fuel.
1,000 lbs (453 kgs)
Do not apply brakes until …
after touchdown
