(HPA) B737-800 Limitations Test with CFM56-7 Engines Flashcards
The maximum takeoff/landing tailwind component is _______ knots.
10 or 15
Depending on Particular Option
(AOM Vol. 1 L.10.1, 10.2)
On _________ _________ the escape slide retention bar must be installed during ________, _________, and __________.
Revenue Flights
Taxi, Takeoff, Landing
(AOM Vol. 1 L.10.1, 10.2)
Runway slope limits: ________%
+/- 2%
AOM Vol. 1, L.10.1, 10.2
Maximum Operating Altitude: __________ feet
41,000
AOM Vol. 1, L.10.1, 10.2
Maximum demonstrated takeoff and landing crosswind is ______ kts with winglets and ______ kts without winglets.
33 kts
36 kts
(AOM Vol. 1, L.10.1, 10.2)
Do not exceed speeds placarded for the ______ and ______.
Gear
Flaps
(AOM Vol. 1, L.10.1, 10.2)
The Mach/Airspeed warning clackers can be silenced only by ________ __________ below Vmo/Mmo (340 KIAS/ .82M)
Reducing Speed
AOM Vol. 2, 15.20.7
Va (Turbulent a/s) is _____ KIAS/______ M.
280 KIAS
.76M
(or 250 KIAS if below 15,000 feet and under MLW)
(AOM Vol. 1, SP.16.21)
Maximum Taxi Weight: ____________
156,000
AOM Vol. 1, L.10.3
Maximum Takeoff Weight:___________
155,500 lbs
AOM Vol. 1, L.10.3
Maximum landing weight:____________
144,000 lbs
AOM Vol. 1, L.10.3
Maximum zero fuel weight:__________lbs
136,000 lbs
AOM Vol. 1, L.10.3
Maximum Differential Pressure:_________psi
9.1 psi
AOM Vol. 1, L.10.4
With engines bleed air switches on do not operate the a/c packs in _______ for ________, _________, and __________.
High
Takeoff, Approach, Landing
(AOM Vol. 1, L.10.4)
__________ _________ must be on when icing conditions exist or are anticipated, except during: ________ and _______ below _______ SAT.
Engine, TAI
Climb, Cruise, -40˚C
(AOM Vol. 1, L.10.4)
Do not use _________ trim when autopilot is engaged.
Aileron
AOM Vol. 1, L.10.5
Do not use A/P for takeoff below ________ feet AGL
400
AOM Vol. 1, L.10.5
Do not use the A/P for single channel operation below _____ feet AGL.
50
AOM Vol. 1, L.10.5
The use of flight deck auxiliary power outlets in the flight deck is ______ _______ without operational regulatory approval.
Not, Allowed
AOM Vol. 1, L.10.8
Maximum and minimum engine (CFM56-7) limits are in ______.
Red
AOM Vol. 1, L.10.8
Engine (CFM56-7) caution limits are in ________.
Amber
AOM Vol. 1, L.10.8
Engine ignition (CFM56-7): Must be “ON” for _______ and _______, operations in _______ _______ and during ________ ______ operations.
Takeoff, Landing
Heavy Rain
Anti Ice
(AOM Vol. 1, L.10.8)
Intentional selection of reverse thrust in flight is __________.
Prohibited
AOM Vol. 1, L.10.8
Maximum altitude for using the APU as a bleed air source and an electrical source simultaneously: __________ feet
10,000 feet
AOM Vol. 1, L.10.8, 10.9
Maximum altitude for using the APU as a bleed air source only: _________ feet.
17,000 feet
AOM Vol. 1, L.10.8, 10.9
Maximum Altitude to use the APU as an electrical source only: ___________ feet.
41,000 feet
AOM Vol. 1, L.10.8, 10.9
APU bleed valve closed when:
a) Ground air _________ and the ________ _______ is open
b) Eng#1 _______ _______ is open
c) Eng#2 _______ _______ is open and the _______ ______ is open
a) connected, Isolation valve
b) bleed valve
c) bleed balve, Isolation valve
(AOM Vol. 1, L.10.8, 10.9)
It is normal to have the APU _______ _______ open during engine ________; However, avoid engine __________ settings above _______.
Bleed Valve, Start
Power, Idle
(AOM Vol. 1, L.10.8, 10.9)
Maximum flap extension altitude: ___________ feet
20,000 feet
AOM Vol. 1, L.10.9
Holding in _______ _______ with flaps __________ is prohibited.
Icing Conditions, extended
AOM Vol. 1, L.10.8, 10.9
Do not deploy the speedbrakes in flight at radio altitudes below ________ feet AGL
1,000 feet AGL
AOM Vol. 1, L.10.9
In flight do not extend the speedbrake lever beyond the _______ ______ position.
flight detent
AOM Vol. 1, L.10.9
Alternate Flap duty cycle:
After releasing “Alternate Flaps” position switch wait __ seconds before reengaging.
Complete cycle “flaps 0 to 15 and back to 0” allow ____ minutes off before another extension.
15 Seconds
5 Minutes
(AOM Vol. 1, L.10.9)
Weather Radar:
Do not operate within ____ feet near ________ or _________
50 ft
Personnel, Fuel Spill
(AOM Vol. 1, L.10.10)
The restrictions to hanger and personnel do not apply to the ________ _______ mode.
Radar Test
AOM Vol. 1, L.10.10
Maximum fuel temperature: _______
49˚C
AOM Vol. 1, L.10.11
Minimum fuel temperature: _________________ or __________ whichever is higher
3˚C above the freezing point of the specific fuel onboard
-43˚C
(AOM Vol. 1, L.10.11)
Maximum allowable fuel imbalance between tanks one and two must be scheduled to be ______.
0
AOM Vol. 1, L.10.11
Random fuel imbalance must not exceed _________ lbs. for ________, __________, __________, or _________.
1,000 lbs
Taxi, Takeoff, Flight, Landing
(AOM Vol. 1, L.10.11)
Main fuel tanks one and two must be full if _______ _______ contains _______ _______ ________ lbs.
Center Tank
More Than 1,000 lbs.
(AOM Vol. 1, L.10.11)
Do not apply brakes until ______ ______.
After Touchdown
AOM Vol. 1, L.10.11
