Systems Flashcards

(54 cards)

1
Q

Wing landing light limitations
Allow to cool:
____ min aft initial ext/ret
____ min aft ea subsequent ext/ret
Operate lamps in still air for no more than ____ mom

A

1.5 min initial
3.5 min subsequent
10 min still air

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2
Q

Max weights

  • Taxi
  • T/O
  • Landing
  • Zero fuel weight
  • Lateral fuel imbalance
A

122 taxi
121k t/o
110k land
100.5 zfw
1500 lat imbalance

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3
Q

Speed Breaks may not be used with flaps greater than ____ degrees

A

20

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4
Q

Rated thrust BR715 eng

A

21k lbs

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5
Q

Eng start duty cycle limits

A

3 attempts w/ max 3 min duration
15 sec between attempts
15 min cooling after third attempt

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6
Q

Reasons for AUTO abort during eng start on ground (6)

A

Hung start
Starter duty time limit - 3 min
Hot start - 700 deg C
Fuel on condition not satisfied. TGT Above 150C
Loss of valid N2 input
Failure of EEC (some, not all)

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7
Q

3 components of FADEC Full Authority Digital Eng Control

A

Throttle
Throttle Module
EEC Electronic Eng Control unit

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8
Q

EEC provides auto ignition of (one/both) ignition systems
if (any 4 conditions) are detected and
maintained until _____

Eng ignition auto on for ___ sec aft either ___ switch is selected on

A

Both
Combustor instability / significant water ingestion / significant ice ingestion / Flameout
Conditions no longer exist

60 sec / Eng Anti-ice

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9
Q

APU starter cycle limited to _____ consecutive start attempts.
Then wait ______ min prior to further attempts

A

3
30

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10
Q

APU
___ sec delay during start for door to open
____ min for air after start is initiated
On shutdown,
- APU runs for approximately ____ sec for No Break Power Transfer
- door closes approximately ____ min after RPM begins decreasing

A

40 sec
2 min
17 sec
1 min

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11
Q

APU Auto Shutdown
Grnd: if _____
Airborne: only if ____ or ____
If APU FAULT in flight, auto shutdown ____ min aft landing

A

Any condition that could damage APU
APU OVERSPEED or aAPU COMPARTMENT FIRE
10 min

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12
Q

Fire Warning test on battery power only

A

Same as with ext power except:
- FO Master Warning light will not illuminate
- cyan PODS TEST PASS will not be displayed

  • After APU is started, must re-accomplish FWTest
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13
Q

Eng Fire indications

A
  • L/R ENG FIRE handle illuminates
  • FUEL switch illuminates
  • AURAL/VOCAL Warning sound
  • ENGINE L/R FIRE alerts on EAD
  • MASTER WARNING lights flash
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14
Q

APU FIRE indications

A
  • APU FIRE alert on EAD
  • MASTER WARNING lights flash
  • Aural warning (3x)…
  • FIRE light on ext APU grnd control pannel illuminates.,, exterior horn audible until fire extinguished
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15
Q

When smoke or fire is detected in the cargo compartment, the following will occur:

A
  • MASTER WARNING lights will flash and MASTER CAUTION lights will illuminate.
  • CARGO SMOKE voice warning
  • CARGO SMOKE FWD (or AFT) level 3 alert will be displayed on the EAD and on the SD AIR page
  • LAND AT NEAREST SUITABLE AIRPORT displayed EAD and SD AIR page
  • DISCH CARGO AGENT will also be displayed on the EAD and the SD AIR page.
  • On the AIR synoptic page, smoke detectors detecting smoke will display as red triangles.

After approximately 1 minute after the first bottle has been discharged, the PUSH light on FWD (or AFT) CARGO SMOKE AGENT 1 DISCH switchlight will extinguish when the LOW light illuminates and the level 1 alert CARGO AGENT 1 LO will be displayed on the SD AIR page.

Six (6) minutes after the first bottle has been discharged, the following will occur:
Level 1 alert DISCH CARGO AGENT will again be displayed on the EAD and SD AIR page.
MASTER CAUTION lights will illuminate and can be extinguished by pushing the illuminated AIR cue light on the SCP.

PUSH light on FWD (or AFT) CARGO SMOKE AGENT 2 DISCH switchlight will illuminate flashing (amber). When the appropriate switchlight is pushed to discharge the fire-extinguishing agent from the second bottle, the PUSH light will go steady. In addition, the DISCH CARGO AGENT alert disappears on the EAD and SD AIR page.
LOW lights on FWD and AFT CARGO SMOKE AGENT 2 DISCH switchlights and level 1 alert CARGO AGENT 2 LO will illuminate after the second bottle has been depleted after about 2 hours.

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16
Q

LAVATORY FIRE indications

A
  • MASTER CAUTION lights illuminate
  • LAVATORY SMOKE alert on EAD
  • HI-LO chime on PA
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17
Q

Pulling FIRE HANDLE does what (4)

A
  • shuts off fuel
  • shuts off hydraulic
  • trips generator off
  • silences AURAL/VOCAL warnings if MASTER WARNING light has not been pushed
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18
Q

Cargo Smoke test is disabled for ____ min aft establishing electrical per

A

6 min

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19
Q

Eng and APU fire extinguishing consists of ___ fire extinguisher agent containers and associated AGENT LOW lights

A

2

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20
Q

What type of smoke detectors are mounted in recessed pans in ea cargo compartment ceiling
How many and what type of fire extinguishers?

A

Photoelectric
Only two for both cargo bins… Halon

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21
Q

Cargo smoke
How many detectors must activate to trigger the alarm if in normal mode?
What if CARGO SMOKE DET SYS is in SINGLE

A

2
1

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22
Q

How long can the cargo fire suppression system suppress a cargo fire for?

A

Approx 80 min

23
Q

What normally powers the rudder
If HYD CONT RUDDER switch is in the off position, how is it controlled?

A

Rt hyd system
Rudder pedals move the control tab (Manual mode)

24
Q

What are the two types of rudder limiting systems?

A

PRIMARY. Mechanically limited operated by ram air pressure from pitot tube on leading edge of vertical stabilizer

SECONDARY. Two positions, restricted and unrestricted… controlled by Flight Control. Computer (FCC) as a function of speed

25
What is the Elevator Augmentation System, what is it comprised of, How is it activated
Augments elevator control during deep stall recovery providing addl nose down authority Comprised of 2 hyd boost cylinders powered by Lt Hyd sys. Has accumulator back up in event sys psi is lost Activated by pushing the control columns full fwd
26
Spoilers are ____ controlled by ____ and ____ powered
Electrically controlled Spoiler Electronic Control Unit Hydraulically powered
27
Auto spoilers are deployed how (2)
On abort.. by selecting reverse on the throttles On landing, main wheel spin-up OR ground shift signal from nose gear
28
Avionic terms DU ECP SDCP VIA PDF, ND, EAD, SD, MCDU, SISP EIS control panel
Display Units (6) EIS (Electronic Instrument System) Control Panels (2) System Display Control Panel (1) Versatile Integrated Avionics (2) Primary Flight Displays, Navigation Displays, Engine and Alert Display, System Display Multifunction Control and Display Unit (box..where I program jet) Source Input Selection Panel (far left CA to choose source of info displayed on PFD EIS Control panel (upfront with map/plan baro etc )
29
How long are the runways that are displayed whe “ARPT” selected on EIS control panel?
5k min
30
Functions of the 2 onboard VIAs (5)
Data display Felt mgmt computing Central Aural Warning MASTER WARNING / MASTER CAUTION activation Felt data acquisition
31
If the Flight Director is off, it will automatically display for
GO AROUND WINDSHEAR detected
32
IRUs ADIRU 1 is powered by…___ and backed up by _____ ADIRU 2 is powered by ____ and backed up by …___ giving a min of ____ min power if AC power is lost
EMER AC bus / aircraft battery R AC bus / an independent battery/ 30 min
33
ADIRU Normal alignment takes about _____ min Fast takes about ____ min … is accomplished by turning selector from NAV to OFF to NAV within ____ sec
10 min 3 min; 5 sec
34
Fuel Start Pump switch is AC or DC powered
DC
35
Fuel capacity
L 9266 R 9266 C 6077 Total; 24609
36
APU fuel consumption/hr
350 lbs per hr
37
Left Hyd powers
Spoilers (L/R inboard) L Eng thrust reverser Elevator augmentation system (Both sys power slats, flaps, rudder stop limiter, nose wheel steering, brakes)
38
Rt hydraulic sys powers:
Spoilers (LbR Outboard) Rudder Rt Eng thrust reverser Gear (Both sys power slats, flaps, rudder stop limiter, nose wheel steering, brakes)
39
Both hydraulic systems power
Slats Flaps Rudder stop limiter Nosewheel steering Brakes
40
Gear warning horn vocal warning when:
- gear not down and locked / flaps in landing range (CANNOT BE SILENCED) - gear not down and locked / throttles retarded / airspeed <210 / altitude <1200 (MAY BE SILENCED)
41
Max break temp ____ C for elevations up to ______ feet MSL ____ min for Peak temp to occur Overheat light on at ____ C, resets at ___ C
115C 2,200 ft MSL (120k lbs. V1 140kts) 15 min 260C. 230C
42
Break temp differential up to ____ C considered normal
60C
43
Turn capability / rudder pedals & steering wheel
Rudders only - up to 17 deg Steering Wheel - up to 82 deg
44
T/O Warning will occur if a/c on grnd and both throttles advanced if:
Brakes Flaps Slats Spoilers (if any extended 2 deg or more) Stabilizer (not in green band) Rudder (trim not centered)
45
Predictive Windshear WARNING (landing) Automaticity activated in flight below _____ ft Radio Alt - AURAL ALERTS generated below _____ ft RA & inhibited below ____ ft AGL - Max effective range _____, _____ for CAUTION, _____ for ADVISORY
2300’ even if radar is off 1200’ RA / 50’ AGL 1.5 NM (“WARNING”, red) / 3 NM (lMONITOR RADAR DISPLAY”, amber) / 5 NM (WINDSHEAR icon ONLY on ND ONLY.. no aural)
46
Predictive Windshear WARNING (on takeoff) warnings inhibited from ____ until ____ Max effective range _____ Note: _____________
100kts. / 50ft AGL 3 NM Radar MUST BE ON to receive any predictive alerts on grnd / t/o
47
Electronic Instrument Systems (EIS) alert colors and meanings
Red Boxed - lvl 3 - MASTER WARNING - Emergency conditions, immediate attention - inhibited from V1 to 400’ AGL! But no longer than 25 sec in flight Amber Boxed - lvl 2 - MASTER CAUTION - Abnormal Operational Conditions, immediate attention - inhibited at various speeds… if inhibited during t/o, released at 400 RA, aft 25 sec in flt, or 1000 AFE Amber (no box) - lvl 1 - MASTER CAUTION may illuminate - conditions may require MX attention prior to t/o, logbook entry, confirmation of desired condition - inhibited at various speeds… if inhibited during t/o, released at 400 RA, aft 25 sec in flt, or 1000 AFE Cyan (blue) - lvl 0 - general operational or a/c status info - NOT inhibited
48
Takeoff/ Landing essential checklist items complete (GREEN BOX) items T/O (6) Landing (3)
T/O sequentially: - stab in green - rudder trim centered - slats in t/o - flaps in t/o - parking break not set - spoilers armed Landing; landing gear down, flaps in landing range, spoilers armed
49
Windshear REACTIVE - - Alert AND GUIDANCE Available on T/O up to _______;
1500 ft
50
Evacuate flow. (6) to Easy Victor; (3) Egress; (2)…. 11 tot
PARK BRAKE set* *Outflow VALVE OP* *EMER PWR selectorON* *EMER LT switchON* SPEED BRAKE leverRET FLAP/SLAT handle 25 *Notify flight attendants: "EASY VICTOR, EASY VICTOR, EASY VICTOR."* *FUEL switches OFF* *ENG FIRE handlesPULL* (*Fire AGENT(S) (if reqd)DISCH*) *APU FIRE CONT switchOFF & AGENT ARM* (*APU FIRE AGENT(S) switches (if reqd)DISCH*) *Notify flight attendants: "THIS IS THE CAPTAIN. EVACUATE, EVACUATE."* *Advise the tower.* *BATT switch OFF*
51
What happens when the AUTO FLIGHT button is pushed? (4)
ALWAYS engages the ATS Above 200 ft in HEADING MODE ONLY… engages the auto pilot Above 400 ft engages the auto pilot in NAV or HEADING mode Subsequent pushes change the auto pilot in use
52
Wingspan Length Height Wheel base
93’ 124’ 29’ 16’
53
Turning radius Nose Tail Wings Min surface needed for 180 deg turn
66’ 65’ 59’ 81’. (Roughly nose turn radius 66’ + wheel base - 16’) So if the nose clears, the tail should
54
Fuel tolerances on ground
1500 max wing imbalance +1000; -200 actual gauge reading vs planned block fuel on fly plan (unexplained) +/-300 FSR vs Gauges (contact fueler to confirm wing fuel panel validated… if not, contact MX)