GeneralKnowlege

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Author:
daczygma
ID:
250167
Filename:
GeneralKnowlege
Updated:
2013-12-02 09:00:32
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Boeing 757 300 GeneralKnowlege CZY
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Boeing 757-300 GeneralKnowlege CZY
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  1. PITCH & POWER 757-300
    LEVEL / 10.000 FT / 100.000 KG
    • 5.0°
    • 1.24
  2. PITCH & POWER 757-300
    LEVEL / 5.000 FT / 100.000 KG
    • 5.0°
    • 1.20
  3. PITCH & POWER 757-300
    LEVEL / 5.000 FT / 100.000 KG

    FLAPS 1
    (Vref 30 + 60)
    • 8.0°
    • 1.23
  4. PITCH & POWER 757-300
    LEVEL / 5.000 FT / 100.000 KG

    FLAPS 5
    (Vref 30 + 40)
    • 7.5°
    • 1.24
  5. PITCH & POWER 757-300
    LEVEL / 5.000 FT / 100.000 KG

    FLAPS 15
    (Vref 30 + 20)
    • 8.5°
    • 1.26
  6. PITCH & POWER 757-300
    LEVEL / 5.000 FT / 100.000 KG

    FLAPS 20 + Gear Down
    (Vref 30 + 20)
    • 5.5°
    • 1.28
  7. PITCH & POWER 757-300

    FINAL APPROACH 3°/ 1.500FT / 100.000 KG
    FLAPS 25 + Gear Down
    (Vref 25 + 10)
    • 1.5°
    • 1.20
  8. PITCH & POWER 757-300

    FINAL APPROACH 3°/ 1.500FT / 100.000 KG
    FLAPS 30 + Gear Down
    (Vref 30 + 10)
    • 0.5°
    • 1.24
  9. CAT I ILS MINIMA
    200 ft / 550 m

    • 250 ft / 1.000 m
    • If no AP and FD used in APP mode!
  10. CAT II ILS MINIMA
    100 ft / 300 m

    Landing minimum without autoland is limited to 350 m

    LAND 2: Dual channel autoland or automatic approach to 50 ft and manual landing

    • NO AUTOLAND: Single channel automatic approach to 80 ft and manual landing
  11. CAT IIIa ILS MINIMA
    • 50 ft / 200 m = Fail Passive / max. with SE
    • (min ASA LAND 2)

    • 15 ft / 200 m = Fail Operational
    • (min. ASA LAND 3)
  12. CAT IIIb ILS MINIMA
    • 15 ft / 125 m
    • 0 ft / 75 m

    Minimum ASA Status LAND 3
  13. MINIMUM HYDRAULIC SYSTEMS FOR AUTOLAND
    3 hydraulic systems
  14. BELOW ALERT HIGHT (200 FT) WITH LAND 3 INDICATED ONLY AN . . . . WILL REQUIRE A GO-AROUND

    [4]
    • ILS deviation warning
    • ILS transmitter failure
    • ASA status "NO AUTOLAND"
    • A/P disconnect
  15. DE-ICING

    Engine Anti-Ice Switches ... ?
    All Bleed Switches ... ?
    • Engine Anti-Ice Switches ... OFF
    • All Bleed Switches ... OFF
  16. FORMEL TURNRADIUS
    (25° bank)
    • (TAS / 100)2
    •          3
  17. FORMEL CWC
    • WW + 20 = %
    • (CWC in % vom Wind)
  18. APU-TO-PACK TAKEOFF
    Used to make a takeoff using no bleed from engines. Air for left pack opertion is supplied from the APU.

    NOT ALLOWED IF ICING CONDITIONS EXIST FOR TAXI OR TAKEOFF

    NOT ALLOWED AFTER FUSELAGE HAS BEEN DE-ICED
  19. RNAV / GPS APPROACH MINIMUM ANP
    Min. ANP = 0.3 or better on both FMCs

    Set RNP = 0.3 on FMC POS REF 2 PAGE
  20. COMMUNICATION FAILURE
    Try air to ground and air to air communication on appropriate frequencies

    If no contact could be established with ground or air stations:

    Transponder 7600 ... SET

    Blind Transmissions ... SET

    • Last assigned Speed and Level ... MAINTAIN
    • for 7 minutes (if radar surveillance provided)
    • for 20 minutes (if no radar surveillance provided)
    • following the time of squaking

    CRAR ... CHECK

    • Speed and Level ... ADJUST
    • acc. filed flightplan, rejoin route, proceed to IAF

    • Descend ... COMMENCE
    • as close as possible to EAT / ETA resulting from FP

    • Standard Intrument Approach ... PERFOM
    • Land (if possible) within 30 minutes after ETA or last acknowleged EAT wichever is later
  21. NOMINAL (NORMAL) CLIMB GRADIENT OF A MISSED APPROACH
    2.5 %
  22. STANDARD SID CLIMB GRADIENT
    3.3 %
  23. REQUIRED LANDING DISTANCE (DRY)
    Actual Landing Distance x 1,67
  24. REQUIRED LANDING DISTANCE (WET)
    Actual Landing Distance x 1,92

    oder RLD (dry) + 15%
  25. ACTUAL LANDING DISTANCE INCLUDES ...
    • Sea Level
    • Standard Day
    • No Wind
    • No Slope
    • VREF Approach Speed
    • Anti Skid Operative
    • Automatic speedbrake
    • NO REVERSE THRUST
  26. ADDITONAL MARGIN FOR AUTOBRAKES (EFRAS)
    200 m
  27. REDUCED THRUST PROCEDURE IS NOT ALLOWED IF ...
    • EFRAS calculation is not available for rwy in use
    • the runway is contaminated
    • the Anti-Skid is inoperative
    • alternate thrust setting (N1) is used
  28. APPROACH STABILIZATION CRITEREA
    (at 1.000 ft)
    • Landing configuration
    • Target speed
    • Adequate power
    • Rate of descent
  29. VISUAL APPROACH
    • Daylight conditions
    • RVR >= 800 meters
    • ATC approval
    • PIC should have AD in sight and identified
    • whenever possible according to the traffic pattern
    • Glide path should be 2.5 - 3.0 °
    • Full use of avail. navigation and landing aids
    • as close as possible to the instrument approach
    • missed approach coordinated with ATC or standard MAP

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