Limitations Flashcards
Max operating altitude
45,100’ PA
Max altitude for takeoff and landing
10,000’ PA
Max field elevation
9,500’ MSL
Maximum takeoff and landing tailwind component
15 knots
Runway slope
+/- 2%
The upper deck escape slide must be in the _______position during taxi, takeoff, landing, and whenever the upper deck is occupied.
forward locked
The ladder enclosure door must be closed_____
during taxi, takeoff and landing. Or in flight, except when entering or leaving the cargo hold.
Turbulent air penetration speed
290-310 knots / .82-.85. Whichever is lower
Maximum demonstrated (not limiting) takeoff and landing crosswind
30 knots
Do not operate the _______during refueling.
HF radio
Do not operate the weather radar____
In a hangar or when personnel are within the nose radome
Are standby altimeters RVSM?
No
Maximum allowable in flight difference between CA and FO altitude displays for RVSM is____.
200’
Maximum allowable on-ground altitude display difference between CA and FO for RVSM is_______.
Sea level to 5,000’: 35’
9,500’: 40’
Max difference in altimeters between CA, FO, and field elevation
75’
Target PSI for O2 system for both passenger and crew systems
1,200 PSI.
(CREW O2 can be 950 PSI if not flying over the ocean)
Maximum taxi weight
397, 800 KG
Maximum takeoff weight
396, 893 KG
Maximum landing weight
302, 092 KG
Maximum zero fuel weight
288, 031 KG
When 5G notams are present, what operations are prohibited?
-ILS SA CAT II, CAT II, and CAT III
-Autoland
Maximum differential pressure
9.4 PSI
Maximum differential pressure for takeoff and landing
0.11 PSI
Do not use aileron trim with _____
the autopilot engaged
Minimum height to engage the autopilot after takeoff
250’
Without LAND 2 or LAND 3 annunciated, the autopilot must not remain engaged below______
100’ RA
Minimum autopilot use height if not coupled on an ILS or in go-around mode
50’ below minimums
Max headwind component for autoland
25 knots
Max tailwind for autoland
15 knots
Max crosswind for autoland
CAT II/III: 15 knots
CAT I: 25 knots
Max glideslope angle for autoland
3.25 degrees
Minimum glideslope angle for autoland
2.5 degrees
Autoland may be made with flaps _________ only.
25 or 30
Do not use FLCH below _______’.
1,000’ AFE
Do not use the center VHF radio on _______ MHz or ________MHz.
120.000 or 120.005
ACARS clearances that can only be viewed through the printer must be verified with_______.
The originating ground station
Continuous ignition is required to be ON encountering:
-Heavy rain
-Severe turbulence
-Volcanic ash
-Icing conditions
-Standing water or slush on runway
Continuous ignition is automatically provided when_________.
Nacelle anti-ice is on
Reverse thrust is prohibited________
In flight, or to back the airplane up.
Do not operate the APU below
- (negative) 1000’ pressure altitude
APU start cycle limits
-Between starts 1 and 2: 1 minute (both battery or TR)
-Between starts 2 and 3: Battery- 1 minute. TR- 10 minutes
-Between starts 3 and 4: 75 minutes (both battery or TR)
Avoid rapid and large______
alternating control inputs. (may result in structural failure, even below VA)
Max altitude with flaps extended
20,000’
Use of speedbrakes in flight with flaps past _____ is not recommended.
20
If you lose primary air data, standby system _____ must be applied.
corrections
Do not add/delete waypoints to ______
RNAV/RNP DPs or STAR procedures
If EICAS alert message “UNABLE RNP” displays while on an RNAV approach, pilots must____
go around, unless adequate visual references can be maintained.
Operations are not authorized for _____ or _____ approaches.
RNAV (RNP) or RNP (AR)
NOTE: FAA- RNAV (RNP)
ICAO- RNP (AR)
Approaches using VNAV to DA(H) are not authorized if glide path angle is less than _____ or more than ____ degrees.
2.75; 3.5
If leveling off within 2,000’ after changing altimeter from QNE to QNH or vise versa, ___________
do not use VNAV to execute the level off if QNH is less than 29.70 IN (1006 hPa). After level off complete, VNAV can be re-engaged.
Max fuel tank temperature
+54 degrees C
____ and _____ type fuels are prohibited
Jet B and JP4
In-flight minimum fuel temperature
3 degrees C above the fuel freezing point
Do not cycle _____ and ____ pump switches from ON to OFF to ON with any continuous low pressure indication present.
CWT ; HST
Do not use the terrain display for _____
Navigation
The use of look-ahead terrain alerting and terrain display functions is prohibited within________ for airports not in the GPWS database.
15 NM of takeoff, approach, or landing
What is the maximum crosswind guideline when braking action is reported medium?
10 knots
Are operations allowed with NIL braking action?
No
During autoland, what is the assumed touchdown point?
2,500’ from threshold
What is the minimum threshold crossing height for autoland?
44’
How many HF radios are required for CPDLC?
1
What altitude is the minimum oxygen quantity for each occupant determined?
25,000’ cabin altitude
What is Max EGT for engine starting?
870C (40 seconds)
750 (unlimited)
What is max continuous EGT?
925 C
Minimum oil pressure
10 PSI
Max N1
117.5
Max N2
112.5
Can you reset a tripped fuel pump circuit breaker?
No
What is the flap limitation during fuel jettison?
Do not extend or retract flaps between position 1 and 5
What are the placard flap speeds?
1- 280
5- 260
10- 240
20- 230
25- 205
30- 180
What is the landing gear extension or retraction speed?
270 knots or Mach .82 whichever is less
