Pitch & Power / V Speeds Flashcards

Question

Maximum tailwind component

Answer 1

71kt (red linke) Minimum control Speed. The minimum speed at which it is possible to maintain directional control of the airplane in the air, wirth one engine wind milling and the other engine at T/O power (at MTOM, CG max. aft)

Answer 2

85kt | The recommended safe one engine inoperative speed provides a margin above VMCA

Answer 3

not published

Answer 4

>1542kg 123kt | <1542kg 117kt

Answer 5

188kt (red radial)

Answer 6

69kt | Stall speed in a specific configuration (gear + flaps up, 0° bank, at MTOM)

Answer 7

62kt | Stall speed in the landing configuration (gear down, flaps LDG, 0° bank, at MLM)

Answer 8

25 USG each wing + 1 USG not usable | 94.6l + 4l

Answer 9

13.7 USG each wing | 52l

Answer 10

2500 RPM for 20 sec

Answer 11

+3.8 -1.52

Answer 12

Visibility 1500m | Ceiling 300ft

Answer 13

Power levers ................................................... IDLE ............................................................. Strobe lights / Position lights .......................... ON ............................................................... Propeller area ................................................. CLEAR ........................................................ Engine master (L/R) ....................................... ON ............................................................... Annunciations / Engine / System page .......... CHECKED ................................................... Glow annunciation .......................................... OFF ............................................................. Start key.......................................................... START ......................................................... Oil pressure .................................................... CHECKED ................................................... Annunciations / Engine / System page .......... CHECKED ................................................... Strobe lights .................................................... OFF .............................................................

Answer 14

1Power....................................................OFF 1 2Brakes................................................APPLY 2 3ATC.................................................INFORM 3 If necessary: 4Engine Masters (2)..................................OFF 4 5Fuel selectors (2)....................................OFF 5 6Electric Master........................................OFF 6 In case of fire: 7Cabin heat & defrost................................OFF 7

Answer 15

1 PPAA Above safe altitude 7Alternator (dead engine)..........................OFF 7 8Fuel selector (dead engine).......................OFF 8 In case of fire: 9Cabin heat & defrost................................OFF 9 10Canopy.........................UNLATCH if necessary 10 Max airspeed 117 KIAS

Answer 16

``` After touchdown (if necessary): 1Engine Masters (2)..................................OFF 1 2Fuel selectors (2)....................................OFF 2 3Electric Master........................................OFF 3 ```

Answer 17

1Approach.........................................NORMAL 1 ``` If time/situation allows: just before touchdown: 2Power lever...........................................IDLE 2 3Engine Masters (2)..................................OFF 3 4Fuel selectors (2)....................................OFF 4 ``` Immediately after touchdown: 5Electric Master........................................OFF 5

Answer 18

``` 24V 10 Ah Main battery 2x 12V 1.3 Ah Alternator excitation Emergency Battery (standby gyro and flood flood light) for 1.5h ECU backup battery ELT battery ```

Answer 19

approx. 150 FPM Gear Down minus approx. 200 FPM Windmilling Propeller minus approx. 200 FPM

Answer 20

- 80% Performance ENGINE FAILURE 1) pitch 5° 2) T/O power set 3) gear up 4) speed 85kt 5) X engine failed 6) X power Lever idle 7) X engine master off No PPAA calls On safe altitude perform emergency checklist

Answer 21

2° bank towards operative engine + rudder | Slip indicator 1/2 displacement towards operative engine

Answer 22

ENGINE FAILURE autopilot off POWER 1) max power set PERFORMANCE 1) gear up 2) flaps up 3) minimum speed 85kt 4) target speed 100kt ANALYSIS 1) X engine failed ACTION - - troubleshooting if time permits -- 1) X power Lever idle 2) X engine master off 3) X Alternator off 4) X fuel selector off

Answer 23

ENGINE PROBLEM autopilot off POWER 1) (other engine) power lever max PERFORMANCE 1) gear up 2) flaps up 3) minimum speed 85kt 4) target speed 100kt ANALYSIS -- call out the problem -- DECISION: shut down X engine ACTION 1) X power Lever idle 2) X engine master off 3) X Alternator off 4) X fuel selector off

Answer 24

after starting final approach (leaving intermediate approach altitude or circuit altitude ENGINE FAILURE 1) autopilot off 2) power as required 3) flaps APP 4) Va App OEI 85kt 5) gear up -- if necessary -- 6) X engine failed 7) X power lever idle 8) X engine master off

Answer 25

avoid a go-around by all means! 1) Go-around 2) Power (check slip indication) 3) (if not already set) Flaps APP 4) Gear up (if terrain clearance assured, even before pos. ROC) 5) Flaps UP 6) -- Rotate smoothly to 5° ANU -- 7) FD off

Answer 26

Between 50ft and 35ft on instrument runways

Answer 27

``` Height Airframe Security Engine Location Lookout ```

Answer 28

45° bank, 115kt 60% load; speed 115 KIAS, 1° ANU. During turn increase power 5-10% Tolerance: ± 100 ft, ± 5 KIAS

Answer 29

Level flight, wings level, clean, power to idle STALL, reduce AoA Simultaneously set full power smoothly Level the wings Start pitch-up to approx. 8° ANU earliest at VYSE 85 KIAS When a steady climb is established announce “Go around” and follow standard go-around procedure

Answer 30

Level flight, wings level, clean, power to idle STALL, reduce AoA Simultaneously set full power smoothly Level the wings Start pitch-up to approx. 8° ANU earliest at VYSE 85 KIAS When a steady climb is established announce “Go around” and follow standard go-around procedure

Answer 31

Slight descent, wings level, landing configuration, at an imaginary RWY altitude power idle and flare STALL, reduce AoA Simultaneously smoothly set full power Level the wings Start pitch-up to approx. 3º-5º ANU earliest at 75 KIAS (1.2 VS0) When a steady climb is established announce “Go around” and follow standard go-around procedure Observe maximum flap / landing gear retraction speeds

Answer 32

1) Go-around 2) Power 3) Flaps APP (expeditiously, but min. 76 KIAS) 4) Gear up (after positive ROC checked) 5) Flaps UP (at min. 82 KIAS

Answer 33

Planned flight time < 6h Additional fuel: 15min holding at 15000ft overhead dest = 2USG (DA42) Weather req (Eta ± 1h) Ceiling >= 2000ft or circling height + 500ft Visibility >= 5km 2 separate RWYs with desperate approach procedures Min 1 non GNSS approach

Answer 34

CAT 1 - NPA NPA - NPA + 200ft, Vis + 1000m Circling - circling

Answer 35

10NM to both sides from the centerline and beyond radio fix Obstacle clearance 1000ft to 5000ft, 2000ft above

Answer 36

Same RWY or parallel < 760m (2500ft) Medium / Light 2min Heavy / Light 2min Super / Light 3min

Answer 37

Same RWY or parallel < 760m (2500ft) Medium / Light 3min Heavy / Light 3min Ssuper / Light 4min

Answer 38

Medium / Light 5NM Heavy / Light 6NM Super / Light 8NM

Answer 39

``` MTOM Light <= 7000kg Medium > 7000kg <= 136000kg Heavy > 136000kg Super A380 ```

Answer 40

IMC 500ft AAE | VMC 300ft AAE

Answer 41

2.5% or as published

Answer 42

30l fluid, min 22l Normal mode 2 pumps, 30s, 90s pause, ~2.5h High mode 1 pump continously, ~1h Max button 2 pumps 2min, ~30min Alternate mode RH bus, pump #2, only high mode Windshield spray 5sec