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MEMORY ITEM-
LOSS OF ALL ENGINES
- Emergency Power-ON
- Engine Ignition-Override.
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MEMORY ITEM-
Cabin altitude Warning/Rapid Depressurization.
- Oxygen MAsk---ON 100%
- Outflow Valve Control Lever---Manual (Down)
- Outflow Valve Closed---Full forward Locked
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L or R Start Valve Open light
- (above E/O acceleration altitude)
- Autothrottles Disconnect.
- Throttle Idle on affected side.
- Crossfeed Valve closed.
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MEMORY ITEM-
Stabalizer Trim Uncommanded (runaway)
- Autopilot-OFF
- Primary Trim-Opposite the Runaway.
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MEMORY ITEM-
Double Generator Failure
Emergency Power Selector-ON
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MEMOORY ITEM-
Air Conditioning Smoke / Fumes and Cockpit Smoke Removal-Unpressurized?
- Cockpit Oxygen Mast / Smoke goggles
- Oxygen Mask On-100%
- Crew communications Establish
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MEMORY ITEM:
Tail compartment High Temp Light
- Pneumatic Crossfeed Valves closed.
- Airfoil Anti-Ice-OFF
- Aircon - HP Bleed OFF
- (avoid icing conditions)
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On Departure the Rudder Unrestricted Light should be extinguished by.... ------ /83 or ------/83
The Rudder moves from -- degrees to --- degrees when fully limited at --- kts.
- 180 / 200 kts.
- 22-2.5 degrees at 300 knots
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On approach the RUDDER TRAVEL UNRESTRICTED LIGHT should be illuminated by ---/82 or ---/kts on an 83.
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What is the DC BUS VOLTS range and Load Limit?
22-30 volts with a load limit of 1.0.
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What is the Power On Battery voltage?
29 +/-4 volts.
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When does the aural trim warning sound?
What is the normal travel of the primary and secondary trim?
Aural warning 2 degrees in 30 seconds.
- Primary 1/3 degree per second.
- Secondary-1/10th of a degree per second.
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What will cause the APU to shutdown inflight?
- 1. APU Fire
- 2. Overspeed.
- 3. Speed Sensing Failure.
- 4. DC Power Interruption.
- 5. Misc other Faults.
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What is the Min Airfopil Pressure and Altitude?
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Don't takeoff if the Brake Temp exceedes --- degrees c.
205 degrees C
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What are hot brakes?
200-400c
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What are overheated brakes?
Over 400 c
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Describe the Stall Sequence:
- • SPD LOW is displayed in the FMA Pitch Window
- • Slats will go to full extend (if at mid-sealed)
- • Approaching stall the stick shaker will activate
- • At stall speed, the klaxon and aural warning of "STALL" will sound and
- STALL Lights will illuminate
- • Stick pusher will activate (if slats are fully extended, and both computers
- detect the stall).
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When does the rudder go mannual?
- 1. When the lever is selected to manual.
- 2. When the right system pressure is low (950 psi)
There is a 135 knots min / 12 knot max xwind.
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What are the fuel tank quantities?
- L and R Main Tanks-9266
- Center Tank-20596
- Aux Tanks-3785
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What is the positive pressure relief?
8.32 psi and she blew!
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"Normal" Differential Pressure / Normal Max.
7.77 psi +/- .3 psi (8.07)
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Power Back EPR LIMIT.
1.30 EPR
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MAX / MIN OAT.
+50 / -54 c
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Normal MAX limits for Takeoff N1 N2 EPR.
Orange Radial Lines.
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Maximum and Minimum Limits.
Red Radials.
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Reverse Thrust Limit - Inflight.
Prohibited.
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Minimum oil on a through flight?
Overnight?
- Through flight - 10 quarts.
- Overnight- 14 quarts.
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Minimum oil quantity for dispatch.
4 quarts plus 2 quarts per hour up to a mix of 12 quarts (4 hours).
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APU Air must be ____ for flight.
OFF
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Start Temp Limits Ground and Flight? How Long?
- 475 Ground
- 625 Air.
- Momentary.
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Engine Driven Generator Load Limits?
- 1.0 continuous.
- 1.5 up to 5 min.
- Over 1.5 for 5 seconds.
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APU Starter duty -
- Start 5 Start 5 Start
- Then 1 hour rest.
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TWA EFIS Pannels-
Max Limits N1 N2 EGT / Normal TO N1 N2 EGT/Precautionary EGT
RED RAdials Flashing Numbers/Orange RAdial or ARC/Amber Arc
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What is on the LEFT HYDRAULIC SYSTEM.
- L reverser.
- Elevator Augmentation.
- Inboard Flight Spoilers.
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NWS is reduced _______ the failed Hydraulic System?
Opposite
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What Eqt uses both Hydraulic Systems?
- Brakes
- Flaps
- NWS
- Slats
- Ground spoilers
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What is on the RIGHT HYDRAULIC SYSTEM?
- Aft Stairs
- Rudder
- R reverser
- Gear
- Outboard flight spoilers
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Do not arm the ground spoilers prior to....
Gear Extension.
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Flap Selection which is prohibited?
13 to 15 degrees (14)
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How much pressure from the transfer pump can you expect in a system with a failed main pump?
Apx. 2000 psi to the unpowered side.
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Max Cruise EGT?
540c (continuous)
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Max Takeoff Thrust EGT and Time?
- 595 2 min Orange Radial
- 590 / up to 5 min
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Where do the Hydraulic Pressure guages measure pressure?
At their respective pumps.
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Takeoff Reserve Thrust Limit?
ETG and Time?
- 630c and 2 min Red Radial
- 625 / up to 5 min.
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Max Fuel Imbalance?
L/R Main tanks?
FWD / AFT AUX?
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When MUST autobrakes be used?
- RW< 7000 feet.
- RVR < 4000 3/4
- BA< GOOD
- Contamination
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the Hydraulic LOW PRESSURE lights are sensing from what location?
The end of the L/R spoiler lines.
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When MUST Flaps 40 be used?
When is it also reccomended?
Anti-Skid inoperative (must)
- Tailwind R
- Wet/slippery R
- RW < 7000ft R
- BA< Good R
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What are the considerations for weather below 4000 RVR 3/4 miles?
- No FO Landings.
- WET
- 15 Kt Crosswind.
- Autobrakes Mandatory.
- Takeoff Alt?
- Landing Data Braking Chart.
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What is the Main Engine Starter Duty Cycle?
- 30+30+30 = 90 seconds on then 5 min off.
- Subsequent starts 30 sec on / 5 min off.
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the Hiyraulic HIGH TEMP lights are sensing from what location?
The resivior.
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APU Temp Limits? MCT? Momentary?
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Main Engine Start Temp writeup?
- 425 to 475. Warm.
- Over 475 Hot Start.
- 480 to 590 post start over temp.
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Brake Overheat Light on? off?
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What are the normal hydraulic pressures? High? Low?
- 2800-3100
- 1300-1600 (Limitations allow 1700 in low)
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What does the WHEEL NOT TURNING light indicate?
1 wheel turning 20% slower than the others.
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When does the voice recorder "record"?
anytime there is electric power.
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When does the APU LOW OPIL PRESSURE Light go out?
It goes out at 95%.
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Max Temp to park the brakes?
300c
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When is the Flight Recorder recording?
At least 1 engine running and brakes released.
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TWA EFIS-
High Oil Temp
High Oil Pressure
Min Low Oil Pressure
Precautionary Ranges?
- High Oil Temp...Red light
- High Oil Pressure..Flashing.
- Min Low Oil Pressure..Red Light
- Precautionary Ranges..Amber Lights.
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Mach Trim Inop Speed Limit?
78 is great!
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Inner ply of cracked windshield glass speed limits?
- This is the most restrictive crack.
- 235 below 10,000.
- No restriction above 10,000.
- Windshield Heat selected OFF!
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When you set the Standby Altimeter, what are you setting with the "setting"?
- The Standby Altimeter.
- The CADC for Altitude Capture/Levelout and Altitude Alert.
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At touchdown the autospoilers deploy. Describe the sequence.
- Mainn wheel spin up causes Flight Spoilers up to 60 degrees.
- Strut compression drive the Ground Spoilers up 60 degrees.
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Landing Gear Extend Speed Limit?Retract speed Limit?
- 300 to extend.
- 250 to retract.
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219 thrust #'s
- 21,000 MAX
- 21,700 RSV Thrust.
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Which Fuel Pump is powered when only the GSB is powering the aircraft?
The Right Aft Pump.
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No more than ____# of fuel may be used from the Center Tank before transferring _____ the fuel from the Aux Tanks.
8500# / ALL
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During takeoff you select reverse thrust to ABORT...what else then happens in a Non-TWA aircraft?
- 1. Reverse.
- 2. Spoilers up 60degrees.
- 3. Autobrakes activated below 70 knots MIN / above 70 knots MAX.
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If a Fuel Tank quantity reads.... 9999 , what is indicated?
A Tank Fault is indicated.
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What will automatically shutdown the APU on the ground?
Any APU FAULT LIGHT.
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If a Fuel TAnk quantity reads.... [BLANK] , what is indicated?
A channel fault is indicated.
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How many lights do you get on a Fire test?
14
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When is Fuel Heat Required?
- Before takeoff or landing if .....Fuel Temp 0c or below. (at least 1 min prior)
- Note: Fuel Filter Pressure Drop is a QRH Procedure which will also direct application of Fuel Heat.
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What shuts down the APU Inflight?
- 1. Overspeed 108/110%
- 2. Loss of Speed Sensing.
- 3. Fire
- 4. DC Power Loss / Interruption.
- 5. Other Misc Faults.
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What does the Aircon Auto-Shutoff do?
- The system is armed with the switch position and cabin pressure of 1.3psi or more.
- If a 70% bleed pressure difference is detected between engines, BOTH packs will be shutdown.
- The Landing Lights will be retracted with the gear/handle.
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The main engine LOW OIL PRESSURE LIGHT and the OIL PRESSURE GUAGE come from __________ sources.
Different.
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With only battery power available, what boost pump will be powered?
"The 28V DC Transfer Bus Pump" in the right main tank.
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When do you hear the APU Fire aural warning?
- Only when the APU is really on FIRE!
- (not during the test)
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What happens when you pull an Engine Fire Handle?
- 1. Electric
- 2. Hydraulics
- 3. Pneumatics
- 4. Fuel shutoff at the Spar/Wing.
- 5. Silences the Bell
- 6. Arms the Bottle.
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When the Cabin Altitude goes above 10,000ft what happens? 14,000 feet?
- 10,000
- 1. Warning Light
- 2. Aural Warning.
- 3. Seat Belt Sign ON
- 14,000
- 1. Masks Deploy (15 min of O2)
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When do the Emergency Lights come on? How are they extinguished?
- 1. Select them on.
- 2. Loose DC Emergency Bus Power.
You need Emer DC BUS power and DC Transfer Bus power to extinguish.
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When you press the cargo fire extinguisher, what happens?
- The first bottle is discharged.
- The second is armed to discharge 15 min later at a slower rate.
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What are the sources of power for the DC transfer Bus?
- LDC
- RDC
- Battery
- GSB via TR 2
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What Busses will you have with the Emergency Power selected ON?
- Emergency AC
- Emergency DC
- Battery
- Battery Direct
- DC Transfer
- (The Battery Charger is disconnected)
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What instruments do you have with ONLY the battery?
- N1
- N2
- Standby Horizon/AS/ Altimeter.
- Mag compass
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With Emergency Power selected ON, What instruments will you have?
The Emergency Power "shovel"
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What is the OVRD IGN limit?
2 min on, 3 min off, 2 min on , then 23 minutes OFF.
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What is "ALPHA SPEED"?
Min Maneuvering speed for the existing configuration.
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When does the STANDBY LIGHTING come on?
When the Emergency Power is selected "ON".
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"SPEED LOW" is flashing, why?
Your speed is 10% below ALPHA SPEED.
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Where are the first Excessive Pitch Cheverons?
- +25 degrees nose up.(
- -7) degrees nose down.
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Describe the engine runup during ground operation in icing conditions.
- 70% N1, for 15 seconds, every 10 minutes.
- Make a stable runup before takeoff.
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How many joules is the ignition?
- 20 joule in Override and Start.
- 4 Joul normal and continuous.
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When does the PLI (Pitch Limit Indicator) come into view?
- Displayed whenever Windshear Computer (WSC) is operational.
- The IAS is 60 knots or greater and the airplane is at or below 1500 feet radio altitude.
- If the slats are extended, the PLI will be displayed at any altitude.
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What does the Radio Rack Fan Light indicate in flight? on the Ground?
- Flight Both Fans have failed.
- Ground One Fan Failed / Call Mtce.
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When "should" the engine Anti-Ice be on and when "MUST" the airfoil Anti-Ice be on?
At or below 6c with visible moisture.
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A pack will "trip" for what 3 reasons?
- 1. Low flow over the heat exchanger.
- 2. Low flow through the pack (psi)
- 3. Over temp conditions (compressor discharge, turbine inlet, or outlet duct temperature is
- excessive.)
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What does the elevator Augmentation system do?
- A 3000 psi hydraulic power augmentor system provides elevator control for
- additional nosedown capability in extreme, high angle-of-attack flight
- conditions. Supplied by the left hydraulic system, the power augmentor
- system activates during an extreme stall condition after elevator control tabs
- have been displaced approximately 10° airplane nosedown with respect to
- the elevator surface. A blue ELEVATOR PWR Light on the annunciator
- panel is provided to indicate when hydraulic pressure is used to drive the
- elevator.
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What are the APU Load Limits and Altitudes?
- 1.25 On the Ground.
- 1.0 Inflight
- .70 250 to 300
- .625 above 300
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What parts of the airfoils are anti-iced?
- The leading edge slats, fwd strakes, ram air scoor.
- When selected, the Horizontal Stabalizer.
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What are the engine driven generator limits?
- 115 +/- 8 volts
- 400 +/- 20 cycles.
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How can you check to see if the EMERGENCY DC Bus is powered in addition to BUS OFF lights?
The Capt's Pitot Heat Meter will indicate zero.
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In addition to an instrument failure, a FLAG in the STANDBY HORIZON may indicate what failure?
The DC Transfer Bus May be unpowered.
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When is the tail deiced?
- The tail (horizontal stabalizer) is deiced:
- 1. Every 20 min (15 auto mode)
- 2. 1 min before landing flaps.
- 3. After exiting icing condition prior to shutting off the system.
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What pitch will cause a tail-strike on takeoff?
10.5 degrees.
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