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52 Cards in this Set
- Front
- Back
- 3rd side (hint)
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Disclaimer: I wrote these cards for my own personal study. They haven't been QAd or approved by any airline, aircraft manufacturer, or regulatory agency. |
DYODD |
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ENGINE SD Symbology What does it mean when the Thrust Rating text is White? Magenta? |
White = Manually set modes Magenta = FMS modes and limits |
ENG 001 VOL 2, 7-11 |
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ENGINE SD Symbology What does a White T mean on the EPR Gauge? How about a Magenta V? |
White T = Throttle Position Magenta V = Computed EPR Thrust NOTE: When the T's in V, the throttle's set to computer thrust rating. |
ENG 001 VOL 2, 7-11 |
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ENGINE SD Symbology When do the N1 pointer and digits turn from white to red? |
If N1 exceeds limits |
ENG 001 VOL 2, 7-11 |
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ENGINE SD Symbology When will TGT pointer & digits turn from white to amber? Red? What does the Cyan Lightning Bolt mean? |
Amber = TGT amberline limits are exceeded for more than 5 minutes. Red = Redline limits are exceeded Bolt = Ignition is requested on |
ENG 001 VOL 2, 7-11 |
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ENGINE SD Symbology When is the Red Start Limit hash mark displayed? When does it disappear? |
Displayed during engine ground start. Removed at idle. |
ENG 001 VOL 2, 7-11 |
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ENGINE SD Symbology When do the N2 Pointer & Digits turn from white to red? |
If N2 exceeds limits. |
ENG 001 VOL 2, 7-11 |
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ENGINE SD Symbology What do white Fuel Flow digits mean? What does cyan FUEL OFF mean? |
White = Digital fuel flow indication (Normal) Cyan = Engine fuel valve is closed. |
ENG 001 VOL 2, 7-11 |
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2ndary ENGINE SD Symbology What does the Green Arc on the Oil Pressure Gauge mean? When do the digits turn amber or red? |
Green = Valid Range Amber or Red = Abnormal |
ENG 002 Vol 2, 7-11 |
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2ndary ENGINE SD Symbology What turns the Oil Temp digits from white to amber or red? |
Abnormalities |
ENG 002 Vol 2, 7-11 |
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2ndary ENGINE SD Symbology What does the cyan mark mean on the oil quantity gauge? What turns the digits from white to amber? |
Cyan mark = Initial quantity for consumption reference Digits turn to amber to show abnormalities. |
ENG 002 Vol 2, 7-11 |
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2ndary ENGINE SD Symbology What turns Engine Vibration digits from white to amber? |
Abnormalities |
ENG 002 Vol 2, 7-11 |
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2ndary ENGINE SD Symbology When does the APU white parameter box appear? |
When the APU inlet door is open |
ENG 002 Vol 2, 7-11 |
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2ndary ENGINE SD Symbology What turns the % RPM digits from white to red? |
Abnormalities |
ENG 002 Vol 2, 7-11 |
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2ndary ENGINE SD Symbology What turns the % EGT digits from white to red? |
Abnormalities |
ENG 002 Vol 2, 7-11 |
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Thrust rating of BR 715s? |
21,000 lbs |
ENG 003 Vol 2, 7-21 |
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Engine starter duty cycle |
-3 start attempts, max 3 min duration each -15 seconds between attempts -After 3 tries, allow 15 min of starter cooling |
ENG 004 Vol 2, 7-21 |
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Requirements for engine auto-start |
-IGNITION switch- AUTO -ENG START switch- Pulled -FUEL switch- ON |
ENG 005 Vol 2, 7-21 |
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Does auto-start provide TGT protection? |
Yes- no fuel introduction unless TGT is below 150C |
ENG 005 Vol 2, 7-21 |
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Does auto-start automatically motor the engine for 30 seconds before introducing fuel? |
Yes |
ENG 005 Vol 2, 7-21 |
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What would cause an auto-abort during ground engine Auto Start? |
-(impending) hot start (700C) -hung start -3 min starter duty time exceeded -fuel ON condition not met (TGT >150C) -loss of valid N2 input -certain failures of both channels of EEC |
ENG 006 Vol 2, 7-21 |
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Can we auto-start in flight? |
NO. Auto-Aborts aren't available. |
ENG 007 Vol 2, 7-21 |
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Engine warmup/cool down times |
Sitting >2 hours, 3 min warmup. 3 min cool down prior to s/d (Verify ENGINE COOL alert message on EAD) |
ENG 008 Vol 2, 7-21 |
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Approximate standard day engine indications after stabilized start: |
EPR = 1.0 N1= 20% TGT= 400 N2 = 60% FF = 700 Oil press = 45 |
ENG 009 FCTM |
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3 main components of FADEC |
Throttle Throttle module EEC |
ENG 010 Vol 2, 7-21 |
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When is EEC auto relight armed? |
Engine start to shutdown |
ENG 011 Vol 2, 7-21 |
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What causes automatic activation of BOTH ignition systems? |
-Combustor instability -Significant water/ice ingestion -Flameout |
ENG 011 Vol 2, 7-21 |
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How long will a single ignition system unit be automatically energized after either ENG ANTI ICE has been selected ON? |
60 Seconds |
ENG 011 Vol 2, 7-21 |
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How do we select emergency thrust? |
By pushing the thrust levers thru the mechanical gate |
ENG 012 Vol 2, 7-21 FCTM, 3.0 QRH |
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What is thrust management based on in emergency thrust? |
N1 (no longer EPR) |
ENG 012 Vol 2, 7-21 FCTM, 3.0 QRH |
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What will happen to ATS when on emergency thrust? |
ATS disconnects automatically |
ENG 012 Vol 2, 7-21 FCTM, 3.0 QRH |
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What is MAXIMUM power? |
Thrust limit achieved at the forward throttle gate |
ENG 012 Vol 2, 7-21 FCTM, 3.0 QRH |
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When landing one engine inop, how long will the reverser on the inop engine deploy for? |
30 seconds after nose wheel compression |
ENG 013 Vol 2, 7-21 |
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When do we see the amber U/L displayed on the EPR arcs EAD? |
When reversers are out of stowed position |
ENG 013 Vol 2, 7-21 |
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When do we see REV in green?When will we see REV in red? What happens automatically when in red? |
Green= Reversers are approx 90% deployed. Red=Uncommanded reverser deployment in flight. EEC will automatically reduce thrust on affected engine to idle. |
ENG 013 Vol 2, 7-21 |
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What is emergency reverse power? |
Pulling reverse thrust levers thru the mechanical gate- can cause damage, call mx |
ENG 014 Vol 2, 7-21 |
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When would we see Amber REV where EPR should appear on the EAD? |
When using emergency reverse power |
ENG 014 Vol 2, 7-21 |
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What does ENG EXCEEDANCE RESET switch do? |
Resets any exceedence on the EPR, N1, TGT, and N2 primary engine synoptic displays |
ENG 015 Vol 2, 7-21 |
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APU starter motor duty cucle |
Limited to 3 consecutive start attempts, then wait 30 min |
ENG 016 Vol 1, L10 |
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How is APU fuel normally supplied |
Right main tank |
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Can L or C fuel tanks supply APU? When using C tank for APU, should you turn on a R Main Tank fuel pump? |
YES and YES |
ENG 017 Vol 2, 7-30 |
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What could be a problem when using C fuel tanks to fuel the APU? |
When quantity is <800 lbs, using C fuel pumps can force air into APU fuel line and cause APU flameout or prevent start |
ENG 017 Vol 2, 7-30 |
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How long is the APU automatic delay? |
40 seconds, to allow the APU Inlet Door to open |
ENG 018 Vol 1, SP 7 |
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How long is APU bleed air inhibited after start? |
2 min |
ENG 019 Vol 2, 7-12 |
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How do we verify APU shutdown? |
Absence of APU information block on SD ENG display (about 1 min) |
ENG 020 Vol 1, SP 7 |
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Shutting down APU with no external power: |
BATT switch and EMER PWR selector must remain ON until shutdown is complete |
ENG 021 Vol 1, SP 7 |
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Shutting down APU WITH external power connected: |
EXT Power or the GROUND SERVICE ELEC PWR switch (along w BATT switch and EMER PWR selector) must remain ON til shutdown is complete |
ENG 021 Vol 1, SP 7 |
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What and why is the delay for APU shutdown? |
No Power Break Power Transfer (NBPT) - 17 seconds |
ENG 022 Vol 2, 7-30 |
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When is APU shutdown delay bypassed? |
When APU FIRE CONT toggle is moved to OFF & AGENT ARM position OR -If external ground APU toggle is moved to shutoff OR -If an APU Fire is detected |
ENG 022 Vol 2, 7-30 |
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When does the APU auto shutdown on the ground? |
-When conditions are present that could damage the APU -Amber APU AUTO SHUTDOWN alert is displayed |
ENG 023 Vol 2, 7-30 |
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When does the APU auto shutdown in flight? |
-APU Overspeed or APU Compartment Fire. -If an APU FAULT condition occurs in flight, APU automatically shuts down 10 min after landing. |
ENG 023 VOL 2, 7-30 |
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Normal APU fuel usage on deck is ___ lb/hr |
350 |
No reference. From initial training memory stick. |
