Extra - Limitations - 409MC Flashcards
400F, 400C, 400P
Maximum operating Altitude
-8
Maximum operating Altitude
LCF
Maximum operating Altitude
400F, 400C, 400P:
45,100’ PA
-8
43,100 PA
LCF
43,100 PA
L.10.2
400F, 400C, 400P, -8
Maximum Altitude for Takeoff and Landing
LCF
Maximum Altitude for Takeoff and Landing
400F, 400C, 400P, -8
10,000’ PA
LCF
7,300’ PA
L.10.2
400F, 400C, 400P, -8
Maximum Field Elevation
LCF
Maximum Field Elevation
400F, 400C, 400P, -8
9,500’ MSL
LCF
7,300’ MSL
L.10.2
Runway slope
+/- 2%
L.10.2
-4
Turbulent Air penetration
-8
Turbulent Air penetration
-4
290 to 310 KIAS / 0.82 - 0.85 Mach, whichever is lower
-8
310/0.83
L.10.2
-4
Maximum Tire speed (takeoff)
-8
Maximum Tire speed (landing)
-4
235 mph / 204 kts
-8
260 mph
L.10.2
Minimum flight crew
Captain and First Officer
L.10.2
Maximum Takeoff and Landing Tailwind component
15 Knots (LCF - 10 kts)
L.10.2
Ground wind limits for all doors
LCF Swing Tail
40 knots when opening or closing
65 knots while open
LCF Swing tail: 30 Knots while opening and closing
L.10.2
Takeoff and landing crosswind limits
refer to _____
FCOM L.10.3
-8
Reserve tanks 1 and 4 must remain full above the maximum fuel transfer weight of ________
375,286KG
L10.5
For Zero Fuel Weights greater than ___________(Variable Zero Fuel Weight) comply with decrease maximum weight limits
*For Zero Fuel Weights greater than (276, 691 Kgs) (Variable Zero Fuel Weight) comply with decrease maximum weight limits (see table in Weight and Balance Manual). WBM VOL 1 (1.1.6 / 1.1.7 / 1.1.8)
L.10.5
The maximum weight limits may be less as limited by __________, _________, and _________ limits in FCOM limitations section.
Refer to the __________ manual for additional specific airplane loading limitations.
The maximum weight limits may be less as limited by (Center of Gravity), (Fuel Density), and (Fuel Loading Limits) limits in FCOM limitations section.
Refer to the (Weight and Balance Manual) manual for additional specific airplane loading limitations.
L.10.5
Maximum differential pressure (relief valves)
9.4 psi
L.10.6
Maximum allowable cabin pressure differential for takeoff and landing
0.11 psi
L.10.6
Do not operate the APU below __________
- 1,000’ PA
L.10.6
The APU may be used to supply bleed air to air conditioning pack number 2 for takeoff, provided __________ remain closed.
If an engine failure occurs do NOT change air conditioning bleed configuration until ____________ has been achieved to meet engine out performance.
The APU may be used to supply bleed air to air conditioning pack number (2) for takeoff, provided (isolation valves) remain closed.
If an engine failure occurs do (NOT) change air conditioning bleed configuration until (engine-out acceleration height)has been achieved to meet engine out performance.
L.10.6
Do NOT use APU __________ in flight
Do NOT use APU (Generator power) in flight
L.10.6
APU operations between ________ and _______ pressure altitude is limited to “no load” only
APU bleed air should not be used above _________
APU operations between (15,000 feet) and (20,000 feet) pressure altitude is limited to “no load” only
APU bleed air should not be used above (15,000 feet pressure altitude)
L.10.6
APU start cycle restrictions are:
1 and 2 _____ _______
2 and 3 _____ _______
3 and 4 _____ _______
APU is normally started on ______. The TR wait column are not applicable to aircraft without a TR start source.
If the TR should overheat with the start source switch in TR starting power is transferred to the _____ and the start continued on battery power. Any further start attempts with an overheated TR are ________.
A failure of the TR, other than an overheat does ______ provide automatic switching)to the APU Battery. Under these conditions, moving APU start source switch to BATTERY removes the TR from the Starting Circuit and allows APU starting on ______ power
Between Battery TR
Starts Wait Wait
1 and 2 1 min 1 min
2 and 3 1 min 10 min
3 and 4 75 min 75 min
APU is normally started on (Battery). The TR wait column are not applicable to aircraft without a TR start source.
If the TR should overheat with the start source switch in TR, starting power is transferred to the (battery) and the start continued on battery power. Any further start attempts with an overheated TR are (inhibited).
A failure of the TR, other than an overheat, does (NOT) provide automatic switching to the APU Battery. Under these conditions, moving APU start source switch to BATTERY removes the TR from the Starting Circuit and allows APU starting on (battery) power.
L.10.6
the use of aileron trim with the autopilot engaged is ________
prohibited
L.10.7
the autopilot must not be engaged below ________ after takeoff
250 feet
L.10.7
the autopilot must be disengaged before the airplane descends more than _________ below minimums unless it is coupled to an ILS _____________ or in the _________
the autopilot must be disengaged before the airplane descends more than (50 feet) below minimums unless it is coupled to an ILS (glideslope and localizer) or in the (go-around mode).
L.10.7
WITHOUT LAND 2 or LAND 3 annunciated, the autopilot must not remain engaged below _______
WITHOUT LAND 2 or LAND 3 annunciated, the autopilot must not remain engaged below (100 feet RA)
L.10.7
Do not use FLCH on final approach below ________ AFE
Do not use FLCH on final approach below 1,000 feet AFE
L.10.7
When using autobrakes during Autoland operations, touchdown is assumed to occur at 2,500 feet from the runway threshold. ________ feet must be added to the advisory landing distance in the PI chapter or to the TLR WITHOUT Autoland distance provided
______ if using (ACARS) or (TLR with Autoland distance)
When using autobrakes during Autoland operations, touchdown is assumed to occur at 2,500 feet from the runway threshold. (1,000) feet must be added to the advisory landing distance in the PI chapter or to the TLR WITHOUT Autoland distance provided
N/A if using (ACARS) or (TLR with Autoland distance)
L.10.7
Automatic landings may be made with flaps _______
Automatic landings may be made with flaps (25 or 30 only)
L.10.7
Maximum GS angle for autoland is ________
minimum GS angle for autoland is _________
Maximum GS angle for autoland is (3.25)
minimum GS angle for autoland is (2.5)
L.10.7
Automatic landings require ____ operating hydraulic systems
Automatic landings require (4) operating hydraulic systems
L.10.7
Max wind component for Autoland
Headwind _____
Tailwind _______
Crosswind _______
Crosswind CAT II/III ______
Headwind
Headwind (25kts)
Tailwind (15kts)/(LCF 10kts)
Crosswind (25kts)
Crosswind CAT II/III (15kts)
L.10.7
The minimum threshold crossing height is ______
The minimum threshold crossing height is (44’)
L.10.7
ACARS is limited to the transmissions and receipt of messages, which will not create an ____________ if the message is improperly received
ACARS is limited to the transmissions and receipt of messages, which will not create an (unsafe condition) if the message is improperly received
L.10.8
PDC, D-ATIS, Oceanic Clearance, W/B, Performance Data messages can be transmitted and received over ACARS if they are ____________ per approved operational procedures
PDC, D-ATIS, Oceanic Clearance, W/B, Performance Data messages can be transmitted and received over ACARS if they are (verified) per approved operational procedures
L.10.8
ATC clearance data received through the FMC which can only be viewed on the flight deck printer must be independently ________ with the origination group station.
ATC clearance data received through the FMC which can only be viewed on the flight deck printer must be independently (verified) with the origination group station
L.10.8
Do NOT operate HF radios during ___________operations
Do NOT operate HF radios during (refueling) operations
L.10.8
N409MC, N480MC, N496MC - N499MC
Do NOT use the center VHF radio on _______ or ______ unless the left and right VHF radio communication systems are operational
N409MC, N480MC, N496MC - N499MC
Do not use center VHF radio on (120.000 MHz) or (120.005 MHz) unless the left and right VHF radio communication systems are operational
L.10.8
LCF, N419MC, N429MC, N464MC, N465MC, N471MC
Do NOT use the center VHF radio for voice communications with an operational __________ system, except for FIR boundary reports
LCF, N419MC, N429MC, N464MC, N465MC, N471MC
with an operational ACARS system, except for FIR boundary reports, Do NOT use the center VHF radio for voice communications with an operational (ACARS) system, except for FIR boundary reports
L.10.8
For Communication/Navigation/Surveillance(CNS) and RVSM required equipment refer to __________
L.10.9, L.10.10, QRM 3.1, QRM 3.2
The flight crew must use oxygen when cabin altitude is ABOVE _________. If 100% or Emergency is not needed, set the regulator to ________.
The flight crew must use oxygen when cabin altitude is ABOVE (10,000 feet). If 100% or Emergency is not needed, set the regulator to (Normal).
L.10.11
WITHOUT operable main deck signaling/alert system
Supernumeraries are ______ from accessing the main deck cargo any time the aircraft is moving
With operable main deck signaling/alert system
Supernumeraries are prohibited from accessing the main deck cargo compartment during _________, ______, and _______
WITHOUT operable main deck signaling/alert system
prohibited
With operable main deck signaling/alert system
(taxi), (takeoff), and (landing)
L.10.12
A maximum of _____ supernumeraries are allowed access to the main deck cargo compartment in-flight for cargo or liven animal operation
3
L.10.12
Supernumeraries must be _______ to return to their seats at the onset of a smoke, fire, or pressurization event, turbulence and prior to landing.
(signaled)
L.10.12
There must be at least _____ portable oxygen unit with a full face mask attached to it provided for each supernumerary allowed to enter the main deck cargo compartment during flight
one
L.10.12
During the flight, the supernumerary must carry the ______________ unit whenever he or she is in the main deck cargo compartment
(portable oxygen)
L.10.12
There must be at least ______ portable oxygen unit with a full face mask attached to it provided for each supernumerary allowed to enter the main deck cargo compartment during flight.
one
L.10.12
For aircraft WITHOUT an automatic aural and visual system installed, supernumeraries must also _________ the full-face mask and initiatee the oxygen flow whenever the main deck cargo compartment is accessed during flight. see placard on the smoke barrier door to determine requirement status.
don
L.10.12
