Limitations Flashcards
Max Runway Slope
+/- 2% -
FCOM Vol. 1 L.10.2
Maximum takeoff and landing tailwind component
10 knots
FCOM Vol. 1 L.10.2
Maximum demonstrated T/O and Landing crosswind
- 400 = 35kts
- 800 = 33kts
FCOM Vol. 1 L.10.2
Maximum Speeds
Observer VMO Pointer and gear / flap placards
FCOM Vol. 1 L.10.2
Maximum flight operational latitude
- 400 = 73N and 60S
- 800 = 82N and 82S
FCOM Vol. 1 L.10.2
Maximum operating altitude
- 400 = 37000ft
- 800 = 41000ft
FCOM Vol. 1 L.10.2
Severe Turbulent Air Penetration Speed (whatever is lower)
- 400 = 264KIAS or .65M
- 800 = 280KIAS or .76M
In cruise: SP.16 Supplementary Chart
FCOM Vol. 1 L.10.2
On revenue flights what must be installed regarding L1 Door
The escape slide retention bar (grit bar), taxi, takeoff, landing
FCOM Vol 1 L.10.3
What must not be operated during refueling operations
HF Radios
FCOM Vol 1 L.10.3
Max allowable in-flight difference between captain and FO altitude display for RVSM
200ft
FCOM Vol 1 L.10.3
Maximum allowable on the ground altitude display differences for RVSM operations
-400:
Sea level = 40ft for Captain/FO
5000ft = 45ft for Captain/FO
10000ft = 50ft for Captain/FO
-800:
Sea level to 5000ft = 50ft
5000ft to 10,000ft = 60ft
Maximum difference between Capt/FO/Ground for all = 75ft
FCOM Vol 1 L.10.3
Weight Limitations (800) Max Taxi
174,700lbs
AFM or FCOM Vol 1 L.10.4
Weight Limitations (800) Max Takeoff
174,200lbs
AFM or FCOM Vol 1 L.10.4
Weight Limitations (800) Max Landing
146,300lbs
AFM or FCOM Vol 1 L.10.4
Weight Limitations (800) Max Zero Fuel
138,300lbs
AFM or FCOM Vol 1 L.10.4
Weight Limitations (800) Min Operating
80,800lbs
AFM or FCOM Vol 1 L.10.4
Max differential pressure (400)
8.65 PSI
AFM or FCOM Vol 1 L.10.4
Max differential pressure (800)
9.1 PSI
AFM or FCOM Vol 1 L.10.4
Flight with freight in the Main Deck Cargo Compartment without at least one air conditioning pack is ? (400)
Prohibited
AFM or FCOM Vol 1 L.10.4
Use of Aileron trim with the autopilot engaged is
Prohibited
AFM or FCOM Vol 1 L.10.5
(400) Do not engage the autopilot below what ALT
1000ft AGL
AFM or FCOM Vol 1 L.10.5
(800) Do not engage the autopilot below what ALT
400ft AGL
AFM or FCOM Vol 1 L.10.5
For single channel operating during approach, when shall the autopilot be disengaged
50ft AGL
AFM or FCOM Vol 1 L.10.5
MAX Wind Component for Autoland (400)
Headwind: 25kts
Tailwind: 10kts
Crosswind: 15kts
Crosswind CAT2/3: 15kts
AFM or FCOM Vol 1 L.10.5
MAX Wind Component for Autoland (800)
Headwind: 25kts
Tailwind: 10kts
Crosswind: 20kts
Crosswind CAT2/3: 15kts
AFM or FCOM Vol 1 L.10.5
MAX and MIN glideslope angle for for autoland
2.5 to 3.25 degrees
AFM or FCOM Vol 1 L.10.5
Autoland flap and engine requirements
Flaps 30 or 40 // both engines operative
AFM or FCOM Vol 1 L.10.5
Are autolands authorized on the 400LF? What about the normal 400?
NOPE
YUP
AFM or FCOM Vol 1 L.10.5
When can you not use LVL Change on approach?
Do not use below 1000 AFE
AFM or FCOM Vol 1 L.10.5
Engine limit display markings (What colors)
Red = max and min limits Amber = caution limits
AFM or FCOM Vol 1 L.10.7
Maximum time limit for takeoff thrust
5 mins
AFM or FCOM Vol 1 L.10.7
Engine Ignition must on AUTO/CONT for what phases
T/O
Landing
Anti-ice operation and
(800) operation in heavy rain
AFM or FCOM Vol 1 L.10.8
Operation with Assumed temperature reduced takeoff is not permitted with what INOP
Anti-skid inoperative
AFM or FCOM Vol 1 L.10.8
Reverse Thrust is not permitted when
in-flight
AFM or FCOM Vol 1 L.10.8
APU Max config ALT’s
APU bleed + electric load = 10,000ft APU bleed = 17,000ft APU Electrical Load = 400 - 35000ft 800 - 41000ft
AFM or FCOM Vol 1 L.10.9
(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
(400)
minimum of 20 seconds in between start attempts
3 minutes needed between second and subsequent attempts
AFM or FCOM Vol 1 L.10.9
(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
AFM or FCOM Vol 1 L.10.9
APU bleed valve must be closed when?
Can APU bleed valve be open during engine start?
- 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
AFM or FCOM Vol 1 L.10.10
After 3 consecutive APU aborted start attempts, how long is the cooling period required (800)
15 mins
AFM or FCOM Vol 1 L.10.10
The max alt for flaps extended is ?
20,000ft
AFM or FCOM Vol 1 L.10.10
Holding in ICE conditions with flaps extended is ?
Prohibited
AFM or FCOM Vol 1 L.10.10
In flight do not extended the speed brakes past what point?
Flight Detent
AFM or FCOM Vol 1 L.10.10
Rapid and large alternating control inputs may result in what?
Structural failure at any speed, including below VA
AFM or FCOM Vol 1 L.10.10
Do not deploy speedbreaks below what ALT ?
1000ft RA
AFM or FCOM Vol 1 L.10.11
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
Avoid WX radar operation in what or around what
In a hanger / within 50ft of fueling operations or fuel spill
If a fuel pump circuit break trips, can you reset it?
NO
The Use of what Fuel is prohibited
JP-4 and JET B
Maximum Tank fuel Temp
49C
inflight tank fuel temp must be what in flight?
3C must be maintained above the freezing point of the fuel used or -43C (800) -45C (400) whichever is higher
What fuel is allowed
JET A, JET A-1, JP-5, JP-8
Intentionally dry running the center tank fuel pump (low pressure light illuminated) is?
prohibited
Maximum scheduled lateral fuel imbalance is?
0
Random later fuel imbalance is ? Taxi, T/O, Flight, Landing
1000lbs / 453KGs
Main tanks must have how much fuel if the center tank contains more than ?
full / 1000lbs
Do not open the main deck cargo door in actual or anticipated winds exceeding?
45kts
MAX start EGT
(400) 725C
(800) red line but equates to 725C
AFM or FCOM Vol 1 L.10.8
MAX Taxi weight (-400 except 311GT)
144,000lbs
MAX takeoff weight (-400 except 311GT)
143,500lbs
MAX landing weight (-400 except 311GT)
121,000lbs
MAX zero fuel weight (-400 except 311GT)
113,000lbs
Minimum Operating Weight (-400 except 311GT)
78,000lbs
Do not use what VHF # for ATC communications with ACARS operational
VHF-3
Use what VHF # for primary communications the ground
VHF-1
Maximum generator drive oil temp
157C
MAX N1 RPM (400)
106%
AFM or FCOM Vol 1 L.10.8
MAX N2 RPM (400)
105%
AFM or FCOM Vol 1 L.10.8
MAX T/O EGT (400)
930°
AFM or FCOM Vol 1 L.10.8
MAX Continuous EGT (400)
895°C
AFM or FCOM Vol 1 L.10.8
Minimum Oil Pressure
13 psi
AFM or FCOM Vol 1 L.10.8
MAX Oil Temp
165C
160C-165 Allowable for 15 mins
160C maximum continuous
AFM or FCOM Vol 1 L.10.8
Both PMC/s must be either (Blank) or (blank) for takeoff (400)
OFF or On
AFM or FCOM Vol 1 L.10.8
APU MAX start EGT (400)
760C
AFM or FCOM Vol 1 L.10.9
APU Max continuous EGT (400)
710C
AFM or FCOM Vol 1 L.10.9
APU can operate up to ? (400)
37000ft
AFM or FCOM Vol 1 L.10.9
Pneumatic pressure for start PSI (400)
30PSI at sea level, decreasing 1/2 PSI per 1000ft
AFM or FCOM Vol 1 L.10.9
If there are multiple aborted start attempts of the APU, (blank) mins cooling is required between the 2nd and 3rd attempt. how many is needed after the 3rd failed attempt (400)
5 mins // 1 hour
AFM or FCOM Vol 1 L.10.10
Should you Functionally operate the Main Cargo Compartment Air Supply Shutoff vale prior to each flight or each series of flights by the same crew on the same day? (400)
YUP
Should the Main Deck Cargo compartment Smoke Detector System be inspected prior to each flight or each series of flights by the same crew on the same day? (400)
YUP
Should you do a preflight inspection of the Secondary Main Landing Gear Position Indicating System prior to each flight or series of flights by the same crew on the same day (400)`
YUP
Maximum T/O and LDG Altitude
8,400
FCOM Vol. 1 L.10.2
Also, -400F aircraft with CABIN ALTITUDE and TAKEOFF config lights, as well as a High Altitude Landing Switch have a maximum of 9,000 feet pressure altitude.
FCOM Vol 1 L.10.3
-400LF and -800 what operational check must be done once each flight day?
Flight Deck Door Access System Check
FCOM Vol. 1 L.10.2
When can yo not operate one or both engine bleed air switch on HIGH
Takeoff, Approach, Landing
AFM or FCOM Vol 1 L.10.5