Limitations Flashcards
Runway slope
+/- 2%
Maximum Takeoff and Landing Tailwind Component
15 knots
Maximum Operating Altitude
43,100 ft pressure altitude
Maximum Takeoff and Landing Altitude
14,000 ft pressure altitude
Do not operate HF radios when refueling.
Yes
RVSM Operations
Do not fly in RVSM airspace on ISFD alone. The standby altimeter does not meet RVSM altimeter accuracy requirements.
Flight Deck Security Door
Verify that an operational check of the Flight Deck Access System has been accomplished according to approved procedures once each flight day.
N780AV - N796AV
The maximum demonstrated crosswind for takeoff is
40 knots (gust included)
the maximum demonstrated crosswind component for landing N780AV - N796AV
37 knots (gust included).
Severe Turbulent Air Penetration Speed
Severe turbulent air penetration speed (in severe turbulence) is defined as:
• 290 KIAS below 25,000 feet
• 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet.
Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is
75 feet.
Maximum Taxi Weight
N780AV - N796AV
228,383 Kilograms
Maximum Takeoff Weight
N780AV - N796AV
227,930 Kilograms
Maximum Landing Weight
N780AV - N796AV
172,365 Kilograms
Maximum Zero Fuel Weight
N780AV - N796AV
161,025 Kilograms
The autopilot must not be engaged below a minimum engage altitude of
Autopilot/Flight Director System
200 feet AGL after takeoff.
Autoland capability may only be used for operations into runways at or below
8400 feet airport field elevation.
N780AV - N796AV # Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below
100 feet AGL.
With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below
100 feet AGL.
If the glidepath angle for approach is greater than 3.77 degrees, the autopilot must be disengaged no later than
50 feet below DH/MDA.
Low Visibility (HUD) Takeoff
Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:
Headwind
25 knots
15 knots
20 knots
Autoland capability may be used with flaps 20, 25, or 30
with both engines operative or with one engine inoperative.
Audio Control Panel (ACP)
Use of the captains or first officers ACP to establish a SATCOM/cabin conference is
prohibited
Automatic Landing
Maximum wind component speeds when landing weather minima are predicated on autoland operations:
Tailwind
Headwind
25 knots
15 knots
25 knots
Oil temperature must be greater than
Engine Oil System
-40° C for engine start.
Reverse Thrust
Intentional selection of reverse thrust in flight is prohibited.
Ground wind operating envelope:
*42 knots, limit engines to taxi power
• for crosswinds greater than 45 knots, limit engines to taxi power
• for winds greater than 65 knots, do not run engines
Takeoff is permitted only in the normal
flight control mode.
The maximum altitude with flaps extended is
20,000 feet.
Fuel Temperature
Maximum tank fuel temperature at takeoff is
49° C (120° F) for Jet A, Jet A-1
Tank fuel temperature prior to takeoff must not be less than
-29° C (-20° F).
When actual fuel temperature is within 3º C of the displayed value, the EICAS advisory message
FUEL TEMP LOW displays.
Taxi Speed
Limitations
Maximum taxi speed on straight line:
30 kt
When vacating a runway on high-speed taxiway:
*DRY. 60KT REDUCING TO 30KT
*GOOD 30
*LESS THAN GOOD 10 KT
For takeoff refer to depth and type of the contaminants available on OPT.
• Prohibited when runway is contaminated with more than:
• Dry snow: 100 mm (4 in)
• Wet snow: 15 mm (3/5 in)
• Standing water: 6 mm (1/4 in)
• Slush: 6 mm (1/4 in)
runway condition code.
• Landing is prohibited with code
1 or equivalent.
Takeoff and Landing on an ICY runway are
prohibited.
Takeoff Restrictions
For the operation on contaminated runway:
• Both thrust reversers must be operative.
The APU battery is designed to support:
two consecutive start attempts. If the APU fails to start after the second attempt, a 5 minute cooling period must be observed before a third attempt is made.
If maximum manual braking is used,
the CAP must be the PF
Manual Flight Operation Policy
Autopilot, Auto Throttle, and Flight director disconnection during any type of approach may be accomplished at the pilot’s discretion when suitable visual references are established on the Final Approach.
Visibility
Ceiling
≥ 5.000 m
≥ 1.500 ft
The use of Reversers in Airports elevation above 7000 AMSL
MANDATORY
Cabin Chime
The use of Cabin chime button is for emergency use only and it will be used as an EMER CALL as follows:
• Pilot incapacitation.
• Flight Deck Smoke or Fire
• When Safety Related items exist (e.g.: CAP is resting). It will be used as an EMER CALL as described in the MOV.
Engine stress and possible engine surge can occur with a strong crosswind or tailwind component if takeoff thrust is set before brake release.
crosswinds exceed 20 knots or tailwinds exceed 5 knots.
HIGH CABIN ALT MODE memo message shows when the departure elevation is at or above
9650 FT
Rudder/Brake Pedals
Push the full pedal – turns the nose wheel up to 8º in either direction.
Nose Wheel Steering Tiller
turns the nose wheels up to 70º in either direction
LOC (armed) – AFDS captures localizer when within range and within
120º of localizer course
FLARE (armed)
During autoland, FLARE displays below 1500 feet RA.
Maximum weight for ejecute a operations on the 787-8 in ONE ENGINE TAXI DEPARTURE
220000 KG
First Officer as PF Conditions,
Less than 1.000 hrs on A/C type.
Visibility
Ceiling
Wind
Runway cond.
Weight.
Visibility : Double the Visibility and/or RVR required for Takeoff and/or Landing according to the airport chart.
Ceiling : Two hundred (200) feet more than the minimum required for the approach. If ceiling does not apply for a given approach, add 200 ft to the decision height (DH).
Wind : Crosswind and/or Tail (component) • 10 Kts (Dry and wet runway)
Runway : Dry, damp or wet. If wet, the related landing performance code Runway condition Assesment (RCA) must not be less than 5.
WEIGHT The first officer may perform the:
Takeoff If the actual TOW is 2.000 kilograms below TOGW shown on the OPT performance Takeoff page.
Landing If the estimated LANDING WT is 2.000 kilograms below the estructural LANDING WT.
First Officer as PF Conditions
More than 1.000 hrs on A/C type
Ceiling and visisility :
Takeoff : Standard minimums.
Approach and Landing. :CAT I minimums.
WIND Crosswind (component)
• 20 Kts with dry runway
• 10 Kts with wet runway
Tailwind (component)
• Aircraft Limitation
RUNWAY CONDITION:
Dry, damp or wet. If wet,
the related landing performance code Runway condition Assesment (RCA) must not be less than 5.
Weight 🎇
Operational Limitations
A/C Technical status
If the aircraft has any deferred item that affects the controllability throughout any flight phase, and the PIC (CAP) considers it necessary.
AUTOLAND
The first officer may perform an autoland, only when the PICis incapacitated.
