Limitations Flashcards
(800) Extended Engine Motoring
Starter usage is limited to 15 mins for the first two extended engine motorings. a minimum of 2 mins is needed between each attempt.
For the third and subsequent extended motorings, starter usage is limited to 5 mins. a minimum of 10 mins is needed between each attempt
Weight Limitations (800) Max Zero Fuel
138,300lbs
Weight Limitations (800) Max Takeoff
174,200lbs
Weight Limitations (800) Min Operating
80,800lbs
What must not be operated during refueling operations
HF Radios
Max allowable in-flight difference between captain and FO altitude display for RVSM
200ft
(800) Normal Starter duty cycle
Multiple consecutive start attempts are permitted, each start attempt limited to 2 minutes of starter usage
minimum of 10 seconds is needed between start attempts
Use what VHF # for primary communications the ground
VHF-1 because the antenna is on top
Max takeoff and landing altitude
8400
Or
13,500 for 27A
In flight do not extended the speed brakes past what point?
Flight Detent
Weight Limitations (800) Max Taxi
174,700lbs
Max differential pressure (800)
9.1 PSI
MAX start EGT
red line but equates to 725C
Engine Ignition must on AUTO/CONT for what phases
T/O, Landing, Anti-ice operation and operation in heavy rain
Maximum scheduled lateral fuel imbalance is?
0
Weight Limitations (800) Max Landing
146,300lbs
Maximum flight operational latitude
82N and 82S
Rapid and large alternating control inputs may result in what?
structural failure at any speed, including below VA
Maximum takeoff and landing tailwind component
10 knots
Avoid WX radar operation in what or around what
In a hanger
What fuel is allowed
JET A, JET A-1, JP-5, JP-8
Do not deploy speedbreaks below what ALT ?
1000ft RA
Maximum Speeds
VMO Pointer and gear / flap placards
Alternate Flap Duty Cycle
when extending or retracting flaps, allow 15 seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to ALTERNATE FLAP motor clutch
After a complete extend and retract cycle 0-15 and back to 0 allow 5 mins for cooling before trying again
Autoland flap and engine requirements
Flaps 30 or 40 // both engines operative
On revenue flights what must be installed regarding L1 Door
The escape slide retention bar (girt bar), taxi, takeoff, landing
Maximum operating altitude
41000ft
APU bleed valve must be closed when?
Ground air connected and isolation valve is open,
engine no.1 bleed valve open,
isolation and engine no.2 bleed valve open
APU bleed valve may be open during engine start, but avoid engine power above idle
Maximum Tank fuel Temp
49C
MAX Wind Component for Autoland (800)
Headwind: 25kts
Tailwind: 10kts
Crosswind: 20kts
Crosswind CAT2/3: 15kts
Do not use what VHF # for ATC communications with ACARS operational
VHF-3
Holding in ICE conditions with flaps extended is ?
Prohibited
inflight tank fuel temp must be what in flight?
3C must be maintained above the freezing point of the fuel used or -43C
For single channel operating during approach, when shall the autopilot be disengaged
50ft AGL
Use of Aileron trim with the autopilot engaged is
Prohibited
(800) Do not engage the autopilot below what ALT
400ft AGL
Operation with Assumed temperature reduced takeoff is not permitted with what INOP
anti-skid inoperative
Reverse Thrust is not permitted when
in-flight
Maximum time limit for takeoff thrust
5 mins
Max Runway Slope
+/- 2%
If a fuel pump circuit break trips, can you reset it?
NO
After 3 consecutive APU aborted start attempts, how long is the cooling period required (800)
15 mins
The max alt for flaps extended is ?
20,000ft
MAX and MIN glideslope angle for for autoland
2.5 to 3.25 degrees
The Use of what Fuel is prohibited
JP-4 and JET B
When can you not use LVL Change on APP
Do not use below 1000 AFE
APU Max config ALT’s
APU bleed + electric load = 10,000ft in flight, 15,000 ground only
APU bleed = 17,000ft
APU Electrical Load = 41000ft
Engine limit display markings (What colors)
Red = max and min limits Amber = caution limits
Do not open the main deck cargo door in actual or anticipated winds exceeding?
40 knots for the 800 per FCOM 2
Random later fuel imbalance is ? Taxi, T/O, Flight, Landing
1000lbs / 453KGs
Maximum allowable on the ground altitude display differences for RVSM operations
Sea level to 5000ft = 50ft
5000ft to 10,000ft = 60ft
Maximum difference between Capt/FO/Ground for all = 75ft
Maximum demonstrated T/O and Landing crosswind
33kts
Severe Turbulent Air Penetration Speed (whatever is lower)
280KIAS or .76M
Intentionally dry running the center tank fuel pump (low pressure light illuminated) is?
prohibited
Main tanks must have how much fuel if the center tank contains more than ?
full / 1000lbs
