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121 Cards in this Set
- Front
- Back
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During multi-engine operation, fuel flow will not differ more than __________.
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200 PPH
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The engine format provides an FE menu option that shows additional engine information. With this option turned ON, what additional information will be displayed
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Oil pressure and Oil Temp
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With the engines operating at idle speed what should the minimum indicated oil pressure be?
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10 PSIG
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With the hydraulic switches in the normal position and the engine operating at idle, how much pressure should be indicated?
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2850 - 3150 PSIG
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Which hydraulic systems are used to pressurize the APU accumulators?
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Left APU accumulator from #1 system and the right APU accumulator from #4 system
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Over what percent of N1 RPM is an overspeed condition that requires engine removal?
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110%
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The TF-39 engine ignition duty cycle is __________.
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1 min ON, 14 min OFF; or
2 min ON, 3 min OFF, 2 min ON, 23 min OFF |
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With the engines operating at takeoff rated thrust (TRT), the maximum indicated oil pressure should read __________.
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48 PSIG
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Steady State operation, what is the maximum time at temperature with a T.I.T. reading of 931 °C - 940 °C?
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5 minutes
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What would the correct procedure be if the starter valve open light does not go off after the starter button pops or is pulled out?
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Shut down engine with engine fire pull handle
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When performing normal engine starting using one operating APU, when will the external power cart be removed?
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After two engines are providing electrical power to the buses
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What is the maximum time to idle RPM after T.I.T. is indicated?
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2 minutes
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When is the ground observer authorized to leave the headset while engines are operating without the pilot's permission?
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If the aircraft jumps the chocks
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If both VIA 1 and VIA 2 N1 values are outside the _____ percent tolerance for greater than 3 seconds, each VIA will display its own value, a caution CWA message ENGINE MISCOMPARE will be displayed on an MFDU, and the appropriate fault code(s) will be sent to MADARS
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1.5%
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In the event of a compressor stall during engine acceleration, what would be the correct procedure?
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Immediately retard throttle(s) to idle position to relieve the stall and perform a normal engine shutdown
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How long can an ATM operate without normal hydraulic pressure?
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15 Seconds
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What is the engine starter duty cycle?
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1 min ON, 30 sec OFF, 1 min ON, 30 sec OFF, 1 min ON, 30 min OFF, or
2 min ON, 5 min OFF for any number of cycles |
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After moving the engine fuel and ignition switch to stop, the P&D valve must start to dump:
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Within 3 seconds
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If both VIA 1 and VIA 2 fuel flow values agree within 500 PPH, the __________ value will always be displayed.
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average
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Where are the fire extinguisher bottles located on the aircraft?
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In the lower aft corner of number 4 main landing gear wheelwell
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Approximately how many brake applications are available from the emergency parking brake accumulator?
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Three
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When an engine indication signal is invalid or missing, the respective dial is replaced with a __________.
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white XXX
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For takeoff power runs, what is the minimum safe distance behind the aircraft?
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800 feet
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At Takeoff power, what is the maximum time at temperature with a T.I.T. reading of 941 °C - 960 °C?
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2 minutes
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Where does brake pressure come from with the brake selector switch in the emergency position?
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Emergency/park brake accumulator
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Where are the APU fire extinguisher bottle select switches located?
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Flight engineer panel and loadmasters forward control panel
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If both VIA 1 and VIA 2 T.I.T. values are outside the 25 °C tolerance for greater than _____ seconds, each VIA will display its own value, CWA message ENGINE MISCOMPARE will be displayed on an MFDU, and the appropriate fault code(s) will be sent to MADARS
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5 seconds
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What is the engine temperature normalization (cool down)time?
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5 minutes minimum after starting or before shut down
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Prior to starting a newly installed engine or an engine with extended periods of non-operation, you must:
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Prime the fuel, oil, and hydraulic lines
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Where are the brake controls and indicators located?
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At the pilot's center instrument panel
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Which panel is the FSS arm light located?
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Flight engineer's panel
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Transient T.I.T. (except Starting), what is the maximum time at temperature with a T.I.T. reading of 961 °C - 970 °C?
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30 seconds
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When an engine thrust reverser is not locked and not fully extended for more than 5 seconds, __________ above the respective N1 dial
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NLKD is shown in inverse yellow video
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The engine fire pull handles, when pulled, will mechanically and __________ isolate the affected engine from all systems except the __________ system
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Electrically, oil
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What action is reuired by the flight engineer's position if the APU GEN FAIL light comes on during APU and engine operation?
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Immediately shut down the APU
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For cooling purposes, the APU should be run unloaded for __________ prior to shut down
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2 minutes
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What must be available if the APU is to be operated with the compartment door open?
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A fireguard with an adequate fire extinguisher must be at the compartment
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When the fire pull handles are pulled, how is the fuel to the engine shut off?
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Mechanically at the front wing beam mounted shutoff valve and electrically at the fuel control
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The emergency/park brake accumulator is pressurized by which hydraulic system?
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Hydraulic system number 4
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If the NLKD indication is invalid, __________ above the N1 dial
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a yellow XXX will be displayed
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If both VIA 1 and VIA 2 values are within 1.5 percent, the following logic applies. If both VIA 1 and VIA 2 N1 values are less than 102 percent, the __________ of the two is displayed. If either VIA value is above 102 percent the __________ value is displayed and will continue this condition until both VIA 1 and VIA 2 values are below __________ percent
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lower, higher, 100
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During APU start, what is the maximum duration for transient EGT between 715 °C and 824 °C?
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20 Seconds
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If bothe VIA 1 and VIA 2 N2 values are within 2.0 percent, the following logic applies. If both VIA 1 and VIA 2 N2 values are less than 98 percent, the __________ of the two is displayed. If either VIA value is above 98 percent, the __________ value is displayed and will continue this condition until both VIA 1 and VIA 2 values are below __________ percent
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lower, higher, 96
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During APU start, which of the following EGT reading would indicate a malfunction?
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716 °C - 824 °C
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What is the normal operating limit for CSD oil temperature?
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-50 °C to 135 °C
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The fire extinguisher bottle select switches provide the capability of releasing __________ or __________ containers to a single __________.
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One, both, nacelle
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If transitioning from external power to APU power causes the V/UHF2 radio to become inoperative, the operator must __________.
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turn the V/UHF2 radio off, then back to on, and the radio will return to normal operation
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During engine start, which of the following conditions would require an immediate shutdown?
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(a) No oil pressure indication at Idle RPM
(b) Fuel flow exceeds 900 PPH before lightoff • both a and b |
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The specified oil pressure is __________ to __________ PSIG with engine(s) operating at stabilized 80 percent of N2 RPM
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20 to 48 PSIG
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An overheat condition occurs during engine operation; what would the indications be?
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A flashing overheat warning light on the pilot's center instrument panel and a flashing fire light at the flight engineer's panel
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When and with whom will UHF/VHF radio communication be established during an engine run?
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Just before engine start with Ground Control/Tower
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What are the minimum N1 and N2 engine overspeed limits that require troubleshooting to determine the cause and correction as required?
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106% to 110% and 102% to 105%
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During multi-engine operation throttle alignment will not differ more than __________.
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1/2 knob
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What is the APU's MAX start time from the START light to ON SPEED, 0 and above?
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30 Seconds
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Before starting and during operation of the ATM's __________ to prevent ATM pump cavitations
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The electric suction boost pumps must be on
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If the engine does not light off in 30 seconds after the engine fuel and start ignition switch is placed to run, what action should be taken by the operator?
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Place the engine fuel and start ignition switch to stop, allow engine to motor for 30 seconds, then pull the starter button out
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When starting an APU without external power (battery start) what equipment must be available?
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A fire truck shall standby during starting and single APU operation
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A thrust reverser extended is indicated by a __________ above the N1 indication for the respective engine
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A Yellow NLKD and Green THR REV
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How long can the APU operate with the EGT reading between 691 °C and 746 °C?
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3 Minutes
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What is to be done if the battery voltage check shows less than 22.5 Volts in a battery?
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The battery shall be replaced or the battery electrical plug shall be disconnected
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If both VIA 1 and VIA 2 T.I.T. values are within 25 °C, the __________ value will always be displayed
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Higher
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With the brake supply switch in the EMER position, how much hydraulic pressure is required to turn on the EMER HYD pressure light?
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1300 PSIG
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If an "overpressure" (3400 PSIG) should occur on any of the hydraulic systems, what action must you take?
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Shutdown the engine normally and determine the cause
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If both VIA 1 and VIA 2 fuel flow values are outside the 500 PPH tolerance for greater than _____ seconds, each VIA will display its own value, a CWA advisory message ENGINE MISCOMPARE will be displayed on an MFDU, and the appropriate fault code(s) will be sent to MADARS
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5 seconds
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In the event of a complete failure of both VIA/AIU units, the BIP supports critical display functions to the MFDU. Engine parameters monitored by the BIP are __________.
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N1 and N2 RPM, T.I.T., and thrust reverser position for each engine
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In the event of an emergency, during engine operation, who will notify ground control or tower using the aircraft radios and what information will be relayed?
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Copilot, giving airplane tail number, location, and type of emergency and request fire department assistance.
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When an engine start valve is OPEN, __________.
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a white box is centered on the respective engine instruments, and the respective START VALVE OPEN annunciator on the FE panel illuminates, as well
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During engine starting, an immediate engine shut down would be accomplished if which of the following conditions existed?
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Turbine inlet temperature rapidly approaches or exeeds 800 °C
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What is the critical fan speed operating range?
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78% to 84% N1 RPM
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If a CSD is disconnected during an engine run, how can it be reset?
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By operating the reset handle on the constant speed drive with the associated engine stopped
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If the number 2 hydraulic Boost Pressure Low light on the flight enginer's hydraulic system control panel illuminates, what is indicated?
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The output pressure of the suction boost pump is below 25 PSI
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If an AIU or VIA fails, MFDU OIL TEMP display may be lost or erratic. To restore display, you must __________.
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open circuit breakers for failed subsystem AIU/VIA No. 1 or AIU/VIA No. 2
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What is the maximum main landing gear strut extension for engine run?
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Extended no more than 20 inches
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What is the operational requirement during multiple engine starts if time elapse exceeds 20, but less than 90 minutes?
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The operator will perform a one minute motor
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With the APU operating, what is the maximum continuous EGT?
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691 °C
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What is the normal operating limit for the scavenge engine oil temperature?
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-50 °C to 177 °C
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If both VIA 1 and VIA 2 N2 values are outside the 2.0 percent tolerance for greater than _____ seconds, each VIA will display its own value, a CWA caution message ENGINE MISCOMPARE will be displayed on an MFDU, and the appropriate fault code(s) will be sent to MADARS
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3 seconds
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ENGINE FIRE:
(PILOT'S POSITION) |
(1) RETARD THROTTLES TO START IDLE POSITION
(2) APPLICABLE FIRE PULL HANDLE - PULLED (3) APPLICABLE PUSH TO DISCHARGE BUTTON - PUSHED |
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APU FIRE:
(PILOT'S POSITION) |
(1) RETARD THROTTLES TO START IDLE POSITION
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WING/PYLON FIRE:
(PILOT'S POSITION) |
(1) RETARD THROTTLES TO IDLE POSITION
(2) APPLICABLE FIRE PULL HANDLE - PULLED (3) APPLICABLE PUSH TO DISCHARGE BUTTON - PUSHED |
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EXCESSIVE FLUID LEAK - ENGINE RUNNING:
(PILOT'S POSITION) |
(1) RETARD THROTTLES TO START IDLE POSITION
(2) DIRECT COPILOT TO NOTIFY GROUND CONTROL GIVING AIRPLANE TAIL NUMBER, LOCATION, AND TYPE OF EMERGENCY, AND REQUEST FIRE DEPARTMENT ASSISTANCE |
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JUMPING CHOCKS:
(PILOT'S POSITION) |
(1) RETARD THROTTLES TO REVERSE POSITION
(2) DIRECT COPILOT POSITION TO POSITION BRAKE SUP SWITCH TO ALT (3) APPLY AIRPLANE BRAKES AND/OR STEERING AS NECESSARY |
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WHEEL WELL, UNDERFLOOR (FWD-MID-AFT) OR PTU AREA FIRE WITH ENGINE(S) AND APU(S) OPERATING:
(PILOT'S POSITION) |
(1) RETARD THROTTLES TO START IDLE POSITION
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ENGINE FIRE:
(FLIGHT ENGINEER'S POSITION) |
(1) POSITION APU/OFF/EXT PWR SWITCH TO UNAFFECTED ELECTRICAL POWER SOURCE
(2) FUEL BOOST PUMP SWITCHES - OFF (3) PTU SWITCHES - OFF (4) ATM PUMP SWITCHES - OFF |
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APU FIRE (3 DIFFERENT CONDITIONS):
(FLIGHT ENGINEER'S POSITION) |
CONDITION No. 1:
WITH A MINIMUM OF ONE ENGINE GENERATOR OPERATING: (1) SELECT UNAFFECTED ELECTRICAL POWER SOURCE (2) APPLICABLE APU FIRE PULL HANDLE - PULLED (3) APPLICABLE AGENT DISCHARGE BUTTON - PUSHED CONDITION No. 2: ENGINE GENERATORS NOT OPERATING, AND EXTERNAL ELECTRICAL POWER CONNECTED: (1) APU/OFF/EXT PWR SWITCH - EXT PWR (2) APPLICABLE APU FIRE PULL HANDLE - PULLED (3) APPLICABLE AGENT DISCHARGE BUTTON - PUSHED CONDITION No. 3 ENGINE GENERATORS NOT OPERATING, AND EXTERNAL ELECTRICAL POWER NOT CONNECTED: (1) POSITION APU GEN SELECT SWITCH TO UNAFFECTED APU (2) APPLICABLE APU FIRE PULL HANDLE - PULLED (3) APPLICABLE AGENT DISCHARGE BUTTON - PUSHED (4) NOTIFY GROUND CONTROL, GIVING AIRPLANE TAIL NUMBER, LOCATION, AND TYPE OF EMERGENCY, AND REQUEST FIRE DEPARTMENT ASSISTANCE |
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WIN/PYLON FIRE:
(FLIGHT ENGINEER'S POSITION) |
(1) NOTIFY PILOT OF AFFECTED ZONE
(2) FSS ARMED - discharge affected zones |
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EXCESSIVE FLUID LEAK - ENGINE RUNNING:
(FLIGHT ENGINEER'S POSITION) |
(1) POSITION APU/OFF/EXT PWR SWITCH TO UNAFFECTED ELECTRICAL POWER SOURCE
(2) FUEL BOOST PUMPS SWITCHES - OFF (3) PTU SWITCHES - OFF (4) ATM PUMP SWITCHES - OFF (5) ELECTRIC SUCTION BOOST PUMP SWITCHES - OFF (6) DEPRESS AFFECTED ENGINE HYDRAULIC PUMPS |
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WHEEL WELL, UNDERFLOOR (FWD-MID-AFT) OR PTU AREA FIRE WITH ENGINE(S) AND APU(S) OPERATING:
(FLIGHT ENGINEER'S POSITION) |
(1) NOTIFY PILOT OF AFFECTED ZONE
(2) FSS ARMED - discharge affected zone |
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During engine starting, operation of ignition system to agree with starter duty cycle is __________.
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permissible
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Use of continuous (low energy) system is __________ during ground operation and should be __________ except when troubleshooting the system
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not required, avoided
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The starter inlet pressure will be a minimum of _____ PSIG after the starter valve is open and the pressure is stabilized
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13
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If fuel flow exceeds _____ PPH, prior to or at T.I.T. increase, __________ the engine
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900, shut down
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The maximum time after placing the fuel and start ignition switch to run to get an indication of light-off is _____ seconds
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30
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Starting time for T.I.T. increase (light off) to idle is _____ minutes maximum
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2
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List the oil pressure limits for the following:
Starting __________ Idle _____ PSIG min 80% N2 __________ PSIG Above _____ N2 _____PSIG max |
positive indication
10 PSIG 20 to 48 PSIG 80%, 48 PSIG |
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List the oil consumption limits for the following:
Home station departure __________ Enroute departure __________ |
2 PPH max
4 PPH max |
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List the scavenge oil temperature limits.
Normal operation _____ to _____ Maximum _____ |
-50 °C to 177 °C
177 °C |
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The CSD oil temperature limits are:
Normal operation _____ to _____ Caution _____ to _____ Maximum _____ |
-50 °C to 135 °C
135 °C to 160 °C 160 °C |
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List the T.I.T. and maximum time at temperature, (steady state) operation.
____ to _____ for _____ minutes maximum _____ to _____ for _____ minutes maximum up to _____ continuous |
931 °C to 940 °C for five minutes
916 °C to 930 °C for 30 minutes 915 °C |
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The maximum T.I.T., and time at temperature for takeoff power is:
_____ to _____ for _____ minutes |
941 °C to 960 °C for two minutes
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The transient T.I.T., and time (during start) is:
_____ to _____ for _____ seconds over _____ for _____ seconds |
799 °C to 860 °C for 25 seconds
over 860 °C for two seconds |
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Maximum time at temperature, maximum reverse:
_____ for _____ seconds |
960 °C for 30 seconds
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The transient T.I.T., and time (except starting) is:
_____ to _____ for _____ seconds |
961 °C to 970 °C for 30 seconds
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The N1 idle should be _____ to _____
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17% to 29%
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The fan must rotate within _____ minutes after engine start
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5 minutes
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The N2 idle should be _____ to _____
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61% to 67%
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List the normal RPM range for the following:
N1 _____ to _____ N2 _____ to _____ |
17% to 106%
61% to 102% |
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List the overspeed limits for the following:
N1 _____ to _____ N2 _____ to _____ |
106% to 110%
102% to 105% |
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The engine must be removed if the N1 RPM exceeds _____, or the N2 RPM exceeds _____.
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110%, 105%
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Do not operate an engine in the critical fan speed range of _____ to _____ except for transients
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78% to 84%
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Acceleration time, idle to takeoff power, is __________ maximum
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10 seconds
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List the APU start and operating limits:
APU EGT Normal start maximum _____ Transient during start _____ to _____ For a maximum of _____ seconds Full load continuous ____ to _____ Full load transient _____ to _____ Full load transient time limit is _____ minutes |
Normal start maximum 715 °C
Transient during start 715 °C to 824 °C For a maximum of 20 seconds Full load continuous 600 °C to 691 °C Full load transient 691 °C to 746 °C Full load transient time limit is 3 minutes |
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The APU ON SPEED light shall come on within _____ seconds (0 degrees F and above) or 60 seconds (-65 degrees F to 0 degrees F) after the __________ light comes on
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30 seconds, APU START
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Normal APU voltage is _____ to _____ volts
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112 to 118 volts
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Normal APU generator frequency is __________ Hz
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400 (±) 6 Hz
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With the APU generator on and supplying bleed air, the APU generator transient frequency limits are _____ to _____ Hz
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380 to 420 Hz
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List the DC voltmeter limits:
Minimum _____ volts Normal operation _____ to _____ volts Caution _____ to _____ volts Maximum _____ volts |
Minimum 19 volts
Normal operation 25 to 30 volts Caution 19 to 25 volts Maximum 30 volts |
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List the DC loadmeter limits:
Normal operation _____ to _____ Caution _____ to _____ Maximum _____ |
Normal operation 0 to 1.0
Caution 1.0 to 1.5 Maximum 1.5 |
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List the engine generator frequency limits
Minimum _____ Hz Caution _____ to _____ Hz Normal operation __________ Hz Caution _____ to _____ Hz Maximum _____ Hz |
Minimum 380 Hz
Caution 380 to 394 Hz Normal operation 400 (±6) Hz Caution 406 to 420 Hz Maximum 420 Hz |
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The AC voltage limit (normal operation) is _____ to _____ volts
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110 to 121 volts
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List the AC loadmeter limits:
Normal operation _____ to _____ Caution _____ to _____ Maximum _____ |
Normal operation 0 to 1.0
Caution 1.0 to 1.1 Maximum 1.25 |
