-
Minimum altitude for autopilot
engagement after takeoff.
-
Minimum altitude for autopilot
disengagement during non-ILS
approach.
50 feet below DA/MDA.
-
During single channel ILS
approaches, the autopilot must be
disengaged before the aircraft
descends.
below 100 feet AGL.
-
Use of aileron trim with autopilot
engaged is.
prohibited.
-
Maximum allowable wind speeds
during autoland operations are listed
in the table below
- Headwind 25 knots
- Crosswind 25 knots
- Tailwind 10 knots
-
Maximum glideslope angle during
autoland
3.25
-
Minimum glideslope angle during
autoland:
2.5
-
An autoland may only be
accomplished with flaps.
25 or 30.
-
Continuous ignition must be ON
when encountering:
- – Heavy rain
- – Severe turbulence
- – Volcanic ash
- – Icing conditions
- – Standing water or slush on
- runway
- NOTE: Continuous ignition is
- automatically provided when
- nacelle anti-ice is ON.
-
Engine Limit Display Markings
- The engine limit display markings on
- EICAS must be used to determine
- compliance with the maximum and
- minimum limits and precautionary
- ranges. If EICAS markings show
- more conservative limits than those
- specified in this section, the limit
- markings displayed on EICAS must
- be observed
-
Do not extend flaps above
20,000 feet.
-
FUEL SYSTEM
- Do not reset a tripped fuel pump
- circuit breaker
-
Center Wing Tank (CWT) fuel pumps must
be off for taxi, takeoff and climb unless
CWT contains at least how much fuel?
17,000 pounds of fuel.
-
If the FUEL LOW CTR L or R
message is displayed, both CWT
override/jettison pumps must be
selected?
Off
-
If the FUEL PRESS CTR L or R
message is displayed, the
corresponding CWT override/jettison
pump must be selected
Off
-
Fuel system warning
- DO NOT CYCLE CWT
- PUMP SWITCHES FROM
- ON TO OFF TO ON WITH
- ANY CONTINUOUS LOW
- PRESSURE INDICATION
- PRESENT
-
Lateral Fuel Imbalance
- Lateral fuel imbalance must not
- exceed 3,000 pounds for main tanks 1
- and 4.
- Lateral fuel imbalance must not
- exceed 6,000 pounds for main tanks 2
- and 3.
-
Window heat must be on for all
normal flight operations
-
Window heat may be inoperative on one No. 1 or one No. 2 window provided?
- Operation is not predicated on flights into known or forecast icing, windshield air
- systems are operative and remaining No. 1 and No. 2 window heat systems are
- operative.
-
Do not use Nacelle Anti-Ice (NAI) if OAT or TAT exceeds.
10c
-
NAI must be AUTO or ON during all flight operations when icing conditions (as
indicated in the table below) exist or are?
Anticipated.
-
The autopilot or flight director must be
used during the final approach segment
down to the DA/MDA for the following
approaches:
- GPS and RNAV (GPS) approaches.
- LOC BC approaches.
- Any other approach where raw data is
- not being monitored
-
Modification of a published GPS or RNAV
(GPS) approach procedure from the FMC
NAV database, other than in accordance
with flight crew procedure or ATC
clearance is.
Not Permitted.
-
The final approach segment lateral route may?
not be modified.
-
Unless both FMCs are being updated by
GPS, one pilot must monitor raw data
during the final approach segment of?
VOR and NDB approaches.
-
Raw data must be monitored
during VOR and NDB approaches.
Outside U.S. airspace.
-
Raw data course guidance must be
monitored during?
- ILS (GS out), LOC, LDA
- and LOC BC approaches.
-
Maximum operating pressure
altitude?
45,100 feet
-
Maximum takeoff and landing
pressure altitude?
10,000 feet
-
-
Maximum tailwind component,
takeoff and landing:
10kts
-
Maximum demonstrated crosswind,
takeoff and landing
30kts
-
Turbulent air penetration speed
290-310 KIAS/0.82-0.85M.
-
Maximum allowable inflight difference between Captain and First Officer PFD altitude
displays for RVSM operations:
200ft
-
Maximum speed operating in RVSM airspace
0.90M
-
Maximum Taxi Weight
878.0 (Freighter) 873.0 (BCF
-
Maximum Takeoff Weight
875.0 (Freighter) 870.0 (BCF)
-
Maximum Inflight Weight, Landing Flaps
670.0
-
Maximum Landing Weight
652.0
-
Maximum Zero Fuel Weight
610.0
-
Minimum Flight Weight
361.2 (Freighter) 367.5 (BCF
-
-
Landing Gear Operating Speeds
- Retract or extend: 270 KIAS/0.82M
- Extended: 320 KIAS/0.82M.
-
The smoke barrier door must be
closed during?
- taxi, takeoff, flight and
- landing.
-
Ground wind limits for all doors
- – 40 knots while opening or closing.
- – 65 knots while open.
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