It is the ___ responsibility to open the cabin door. ___ may only open the door only in the even of an emergency.
It is the ___ responsibility to close the cabin door for departure.
Agent's
Flight Attendants
#1 Flight Attendant's
GENERAL 25.1
The heater blanket will be left off during falling or frozen precipitation events. As soon as the de-icing crew requests the aircraft be configured for de-icing, the flight crew will_______.
ARM the overwing heater blankets
GENERAL 30.1
Takeoff with light coatings of frost up to_____ on the lower wing surface due to cold fuel is allowable. However, all other wing surfaces must be free of snow, ice and frost.
____________ is acceptable on the upper surface of the fuselage (above cabin windows) provided all vents and ports are clear
1/8"
HOARFROST (fine crystalline texture frost)
(FAA Advisory Circular AC 20-117 permits up to 1/8" of frost on the bottom of the wing under the fuel tanks.)
GENERAL 30.2
Having an operative overwing heater system (does / does not ) relieve the flight crew of the requirement to check the airplane surfaces of frost, snow and ice accumulation
DOES NOT.
Cold Weather Operations 30-2
If operating with standing water/slush, the static port heaters must be on if
temperature is _______ or below. (AFM)
5°C (40°F)
GENERAL 30.2
If the heater blankets are inoperative and the temperature is less than ____ degrees and high humidity or visible moisture is present.
10oC ( 50oF )
GENERAL 30.3 COLD WX OPS
After engine start, if the oil pressure remains above the normal range (40-55psi) after the oil temperature has stabilized within limits, what action will you take?
Shut down the engine.
30.4 GENERAL... COLD WX OPS
Periodic engine runup, with engine anti ice system on, to as high a thrust setting as practical should be performed to minimize the possibility of ice buildup. use the following power settings:
_____% N1 for 15 seconds
_____% N1 for 40 seconds
Such runups need not be made more frequently than at ____ minute intervals.
70% N1 for 15 seconds
60% N1 for 40 seconds
No more frequently than 10 minute intervals.
30.4 GENERAL COLD WX OPS
TAXI
Single engine taxi WITHOUT an operating APU will cause the ____________ to shed.
Overwing Heater Blanket to shed...
GENERAL 30.5 ( COLD Wx )
Studies have shown anti-icing fluid loses its effectiveness on highly curved surfaces at a faster rate. ( T or F )
TRUE
Because of this information, delay the extension of flaps until just prior to takeoff...
GENERAL 30.5 ( COLD Wx )
CAUTION
When operating flaps during low temperatures, closely monitor flap indicators for positive movement. If flaps stop prior to reaching the desired position, what action should you take?
IMMEDIATELY place the FLAP / SLAT handle to the indicated position.
GENERAL 30.5 ( COLD Wx )
BEFORE TAKEOFF or LANDINGPROCEDURE
If takeoff or landing is to be made on a runway contaminated by standing water, slush, snow or ice, what action should you take regarding the APU?
The APU should be started (bus switches on, and air switch off, obviously ). This will serve as a backup power source should you lose an engine.
GENERAL 30.6 ( COLD Wx )
Takeoff Procedure.
With a contaminated runway, a static takeoff should be performed. Advance the throttles
to ____ EPR and _____N2
1.4 EPR
80% N2
The throttles will be approximately vertical.
GENERAL 30.7 ( COLD Wx )
Engine Anti-Icing in flight During Severe Icing Conditions
Maintaining ____ % N1 minimizes the possibility of fan blade icing which can cause engine vibration at low thrust settings.
70% N1
GENERAL 30.10
Approach and Landing
Fuel Heat should be turned on for one minute prior to approach whenever the fuel temperature is ___oC or below.
0oC or below.
GENERAL 30.11
After Landing -Taxi Procedure
To reduce the possibility of flap damage after making an approach in icing conditions, or landing on a runway covered with snow or slush, do not retract the flaps / slats to less than _____ until the flap area has been checked free of contaminants
15o EXT
GENERAL 30.12
It is acceptable to have a thin coating of hoarfrost on the fuselage, provided all vents and ports are clear. If the hoarfrost extends down to the area of the windows, what action must you take?
The fuselage must be deiced.
GENERAL 30.14
Deicing / Anti-icing Fluid types
There are four types of fluid AA uses for deicing / anti-icing. Can you name them, and their associated color?
Type I orange or colorless
Type II yellow or colorless
Type IV green or colorless
and last but not least.... Hot water
GENERAL 30.14
Fluid Types
Type III fluids are NOT authorized for use under AA's deicing program. ( T or F )
TRUE
GENERAL 30.16
De-icing fluids:
Anti-icing fluid that has failed must be flushed off. Another coating of anti-icing fluid cannot be directly applied on top of a contaminated fluid.
( T or F )
TRUE
GENERAL 30.16
De-icing Fluids:
Hot water may be used to remove wing ice when the ambient temperature is ____oC ( _____oF )
or above and no active precipitation is present or forecast. There is NO holdover time for hot water.
5oC or 40oF
GENERAL 30.18
De-icing Procedures:
APU and Engine Bleed Air Switches must be OFF prior to start of de-icing and remain OFF until one minute after de-icing is completed.
( T or F )
TRUE
GENERAL 30.21
Preparing for De-icing:
Both engines will normally be _______ for de-icing / anti-icing. Coordinate with the local de-icer
Shut Down
GENERAL 30.24
CABIN PRE-TAKEOFF CONTAMINATION CHECK
This check is performed by the flight crew from inside the passenger cabin, and is required:
( three items )
Anytime the holdover time has expired during, snow, frost, etc
Within 5 minutes of takeoff anytime of a flight crew assessed change in intensity.
During conditions of heavy snow, provided TYPE IV fluid has been used.
STARTING 15.8 Bulletin
1. Engine Warm-up: If the engines have been shut down for more than two hours, warm engines up for ____ minutes at low power settings.
Five minutes
STARTING 15.8 Bulletin
When airplane is exposed to tailwinds in excess of ____ knots, reverse engine rotation may occur, increasing the probability of a hot start.
20 knots
STARTING 15.8 Bulletin dated 5-29-12
If starter capacity is limited, place fuel lever to ON at ____ % N1 but no less than ____% N2
On at 5% N1
No less than 20% N2
STARTING 15.8
For starting EGT of ___°C through ____°C, create an Info toMaintenance entry in E6. No Maintenance action is required.
If EGT limit of ____° is exceeded for any period of time, immediatelyshut down the engine. Record the peak EGT and duration of overtemp in E6. Request maintenance to come out to the aircraft.
465°C through 500°C
500°C
STARTING 15.8 Post Start Overtemp
If EGT is between ___ to___°C after stabilized idle, engine shutdown is not required. Make an INFO-ITEM entry in the AML.
If EGT exceeds____°C, immediately shut down engine. Contact maintenance and make an AML entry
480 to 590°C
590°C
STARTING 15.8
For 94xx and 96xx (TWA) airplanes, engine data is displayed on an electronic Engine Display Panel (EDP).
N1, N2, and EGT Indicator digits will _____when a hot start is imminent or maximumvalue is exceeded
FLASH
Single engine taxi is not authorized when:
Jet blast will be excessive.
Ramps and taxiways are slippery.
Icing conditions exist.
Autobrakes, if operative, must be armed prior to landing when any of the following conditions exist:
Runway length less than 7000 feet
• RVR less than 4000 or visibility less than 3/4 mile
• Runway contaminated with standing water, snow, slush, or ice
• Braking conditions reported less than good.
In addition, use of autobrakes is recommended when landing with gusty winds or crosswinds.
Landing Flaps: Flaps 28 normally used:
On dry runways which are more than 7000 feet in length.
At airport elevations above 6000 feet, but may be required at other airports.
Flaps 40 is required for landing when:
Anti-skid system (all or part) is or may be inoperative.
Flaps 40 is recommended for landing when:
Airplane is very light.
Approach is steeper than normal.
Airport elevations 6000 feet or less.
Landing with a tailwind, gusty winds or crosswinds.
Landing on wet / slippery runways,
Landing on runways 7000 feet or less in length,
Braking action is reported less than good,
Captain's judgment...
Climb to cruise altitude at the following speeds:
Below 10000'
above 10000'
250 KIAS, or clean MIN MAN whichever is greater, to 10,000'
290 KIAS to flight plan cruise mach with aircraft weight 120,000 pounds or less.
300 KIAS to flight plan cruise mach with aircraft weight greater than 120,000 pounds.
TWA Intersection takeoffs (are / are not) authorized when performing RNAV SIDS on FMS aircraft unless coded and in the database.
ARE NOT
The GFMS may command up to _____ bank angle (FMS up to 25°) with
NAV selected.
When flying RNAV SIDS the pilot-flying must ensure the aircraft is properly configured for the airspeed being flown
27°
Day Visual Approach Briefing
The approach briefing shall include:
Identify the landing runway (runway changes do not require a new briefing).
Identify the back-up instrument approach, if available (need not be briefed).
Instrument Approach or Night Visual Approach Briefing
The approach briefing shall include:
Airport and approach name
Page number and revision date
Briefing strip information
Weather minima - Visibility, RVR, and Ceiling, whichever is applicable.
Approach Speed
A minimum of ____knots is to be applied to VREF (1.3 VS) for all normal
configuration approaches.
5 knots
Add to Vref the greater of _________of the steady state winds above 20 kts or ________ of the gust factor. Whichever is greater.
1/2 the steady state wind above 20kts or ALL the gust
Approach Speed
The maximum wind correction should not exceed ____knots. Maintain resulting speed (VREF plus additive) until initiation of landing flare.
20 knots
Normal nosewheel tire inflation pressure:
160-170 psi
Normal main gear tire inflation pressure:
190-200psi
Preflighting your fuel gauges, you press the test button. What numbers do you see?
No Aux tanks: 3000 each tank, 9000 on totalizer
WITH Aux tanks: 3000 each tank, 15000 total
To preclude engine FOD, the manufacturer recommends a maximum taxi speed of ______.
20 knots
Power backs are no longer approved. T or F
TRUE
For RNAV SIDS, engage NAV at ___feet AFL
400 feet AFL
TAXI – TAKEOFF 20.3
During an RNAV SID, the GFMS may command up to ___ bank angle (FMS up to ___)
with NAV selected.
GFMS up to 27°
FMS up to 25°
15.2 APPROACH LANDING GO AROUND
Captains and F/O baro altimeter ref:
CAT III -
CAT II -
CAT I -
NON ILS MDA -
VFR -
CAT III - TDZE or Threshold elevation
CAT II - TDZE or Threshold elevation
CAT I - DA (decision altitude)
NON ILS MDA - MDA rounded up to the next 100'
VFR - Captains discretion
15.2 APPROACH LANDING GO AROUND
Captain and F/O radio altimeter setting:
CAT III -
CAT II -
CAT I -
VFR -
CAT III - 50'
CAT II - RA
CAT I - STOWED
VFR- Captains discretion
15.2 APPROACH – LANDING – GO-AROUND
A stabilized approach must be established before descending below:
• IMC _____ feet AFL.
• VMC _____ feet AFL.
IMC 1000 feet AFL.
VMC 500 feet AFL.
15.2 APPROACH – LANDING – GO-AROUND
APPROACH – LANDING – GO-AROUND 20.3
Callout “AIRSPEED” with landing flaps, anytime approach speed is:
____knots below app speed
____ knots above app speed.
-5 knots
+10 knots
Rate of Descent:
Callout –“SINK RATE”
• When below: If descent rate exceeds:
2000 ft: ____ fpm
1000 ft: ____ fpm
Inside FAF: ____ fpm
2000 fpm
1000 fpm
1000 fpm
Callout “COURSE” / “GLIDESLOPE”
On final, when any crewmember observes during an ILS approach,
> ____ dot deviation of localizer indication on the PFD.
> ____ dot on the G/S.
Vertical: Half scale on VDI (1000 ft. AFL and below)
Callout “COURSE”for the following approach deviations:
VOR approach: ____
NDB approach:_____
LOC approach:_____
VOR approach: 2o
NDB approach: 5o
LOC approach: 1/3 dot
With less than 4000 RVR (1200 m) or 3/4 mile
• Landing weight based on ______ limits.
wet runway limits.
the pilot may not descend below
100 feet above the touchdown zone elevation using the approach
lights as a reference unless ________ or _________are also distinctly visible and identifiable to the pilot
the red terminating bars or
the red side row bars
Conditions Requiring a Go-Around from a CAT II / III Approach:
• Below 300 feet (RA), if satisfactory tracking performance is not maintained.
• The following are conditions requiring a go-around from a CAT II / III approach that may not be dictated by crew coordination procedures:
Failure of required airplane or ground equipment prior to DH (CAT II) or prior to touchdown (CAT III).
Autothrottle disengages (autoland only).
Captain determines that a landing cannot be safely accomplished within the touchdown zone.
Maximum Wind Limits – Landing
Tailwind (AFM):
10 knots
Maximum Wind Limits – Landing
Max Demonstrated _______
Braking Action Fair _______
Braking Action Poor_______
_________ and __________ are required for all non-ILS approaches when the weather is less than 1000/3. The DFGC switch must be positioned to the operative Flight director/autopilot system.
Autopilot
Flight director
Non-ILS Approach Go-Around Requirements:
A go-around is required if the following conditions occur and a visual approach and landing cannot be
accomplished:
RNAV approach:
UNABLE RNP or UNABLE APPROACH message displayed, unless other means of navigation available at Captain’s discretion.
RNAV: 1 dot lateral
1/2 scale vetical
Non-ILS Approach Go-Around Requirements: A go-around is required if the following conditions occur and a visual approach and landing cannot be accomplished:
(Deflection/Deviation)
VOR:
NDB:
LOC:
VOR: 5°.
NDB: 10°.
LOC: Full scale localizer deviation
NON ILS APPROACHES;
The pilot flying autopilot and flight director are required for all NON-ILS when the weather is less than:
1000 / 3
(added 9/3/14)
Wing Landing Lights
Wing landing light motors should be allowed to cool for _____ minutes after initial extension or retraction and _____ minutes after each subsequent extension or retraction.
Lamps should not be operated in still, ambient air for periods of over _____minutes due to excessive heat build-up.
1-1/2 minutes
3-1/2 minutes;
10 minutes
Automatic Landings – General (AFM)
Do not conduct an automatic landing if:
Six items...
Align (ALN) mode is not displayed on FMA by 100 feet radio altitude.
Either engine becomes inoperative at an altitude greater than 50 feet above runway.
Automatic Ground Spoilers are not armed and operational.
Any unusual control position or other abnormal conditions exists in the manual flight control system.
RUDDER CONTROL MANUAL Light is illuminated.
Landing overweight
Autothrottle (AFM) AD 1997-04-10
Autothrottle must be __________ if engine stall (surge) is detected
Disconnected.
Automatic Landings – Requirements for Making...
Runway:
• Do not autoland on a runway that:
(two items)
the localizer is unusable inside the runway threshold or
localizer is unusable for rollout guidance.
Battery Limits:
Fully charged batteries will supply Emergency Power for approximately _____minutes
30 minutes
Battery Limits
Normal Voltage ......
Minimum Voltage: Emer Pwr Selector ON (battery under load) .........
25-33 Volts
25 Volts
DC Bus Limits
Voltage .......
22-30 Volts
35.2 SYSTEMS
NOTE
______ reset(s) of the APU generator is permitted for each APU start.
If an APU generator required resetting more than _________, a
numbered “info to maintenance” entry in the E-6 logbook should be
made.
Only ONE reset of the APU generator is permitted for each APU start. If an APU generator required resetting more than ONCE PER DAY, a numbered “info to maintenance” entry in the E-6 logbook should be made.
SYSTEMS 15.1
Dispatch for Unpressurized Flight
Maximum altitude when aircraft is dispatched for unpressurized flight is
________feet. Passenger unpressurized flight (is / is not) authorized.