LIMITATIONS memory (double diamond) Flashcards
Aircraft limitations expected to be from memory.
MAX takeoff & landing TAILWIND component
10 kts
MAX crosswind component (Allegiant)
29 kts
MAX takeoff & landing pressure altitude
9200 ft PA
MAX wind for PAX door operation
65 kts
MAX wind for CARGO door operation
40 kts (50 kts if nose is oriented into the wind)
MAX wind with PAX or CARGO door open
65 kts
MAX speed with flight deck window open
200 kts
MAX speed for operation of windshield wipers
230 kts
Turbulent air penetration speed BELOW 20,000’
TURB AIR penetration speed BELOW 20,000’
maintain 250 KIAS
Turbulent air penetration speed AT or ABOVE 20,000’
TURB AIR penetration speed AT or ABOVE 20,000’ Maintain 275 KIAS until intercepting .76 Mach
GROUND AIRCONDITIONING with AC PACKS
Do NOT use low pressure ground conditioned air simultaneously with air from the aircraft packs
HP (high pressure) ground air with APU air
Do NOT use HP ground (starting) air simultaneously with APU air
AUTOPILOT engagement on takeoff (min altitude)
Autopilot may not be engaged below 100’ AGL on takeoff (Allegiant)
ILS AUTOLAND autopilot certification
The autopilot is certified to remain engaged throughout the auto landing / rollout or automatic go around
Precision approach with manual landing autopilot limitations
Disconnect the autopilot no lower than 50 ft below the DA
Non-precision approach autopilot limitation
Disconnect the autopilot no lower than 50 ft below the DDA
Visual Approach (ILS APPR mode not used) autopilot limitation
Disconnect the autopilot no lower than 500 HAA
Unless CAT 3 DUAL or CAT 3 SINGLE is displayed on the FMA, the autopilot must be disconnected at either 50 ft below the DA/DDA for the approach or 112 ft AGL, whichever is higher
MAX flap / slat extension altitude
Do not extend the flaps or slats above FL200
MAX fuel imbalance between inner wing tanks
MAX fuel imbalance between inner wing tanks 3,300 pounds
Outer wing tank imbalance
An outer wing tank imbalance of 1,550 lbs (one tank empty / one tank full) is allowed provided the total fuel (outer + inner) in each wing is approximately equal
Fuel must be transferred as necessary to comply with these restrictions
Fuel must be transferred as necessary to comply with these restrictions
Fuel Management:
The center tank fuel must be emptied before the wing tanks are emptied unless…
The center tank fuel must be emptied before the wing tanks are emptied unless…
the center tank fuel is treated as ballast
Takeoff using center fuel…
Takeoff using center fuel…
is prohibited
Max altitude for landing gear extension
Do not extend the landing gear above FL250
VLO(E) Max landing gear extension speed
Max landing gear extension speed 250 KIAS
VLO(R) Max landing gear retraction speed
Max landing gear retraction speed 220 KIAS
VLE Max landing gear extended speed
Max landing gear extended speed 280 KIAS / M.67
Landing gear tire speed
Landing gear tires are limited to 195 kts GS
MAX brake temperature for takeoff
MAX brake temperature for takeoff 300 C
Brake limitations:
Power setting with parking brake on
Do not apply thrust on both engines in excess of 75% N1 with the parking brake on
APU starter duty cycle
The APU starter motor duty cycle is 3 consecutive starts, or attempts, with a :01 minute cooling period between attempts. After the 3rd attempt, a :60 MIN cooling period must be allowed
Engine Starter Duty Cycle Limits
There can be a maximum of 4 consecutive cycles of the engine starter within a :09 MIN period. Each cycle can last up to :02 MIN (maximum) then it must be followed by a :20 SEC rest After the fourth cycle, a period of :15 MIN must be allowed for cooling
Engine Starter Engagement max N2
The starter must not be allowed to engage when the engine N2 RPM is above 20%
Minimum OIL QTY (ECAM indication) before engine start
- 5 quarts PLUS estimated consumption of .5 qt/hr
note: At idle, oil qty indications may decrease by up to 6 qts
Engine OIL system:
Minimum Starting temperature
minimum starting temperature -40 C
Engine OIL system:
Minimum takeoff temperature
Minimum takeoff temperature -10 C
