GeneralKnowlege

• 5.0°
• 1.24

• 5.0°
• 1.20

• 8.0°
• 1.23

• 7.5°
• 1.24

• 8.5°
• 1.26

• 5.5°
• 1.28

• 1.5°
• 1.20

• 0.5°
• 1.24

200 ft / 550 m

• _{250 ft / 1.000 m}
• _{If no AP and FD used in APP mode!}

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

• 50 ft / 200 m = Fail Passive / _{max. with SE}
• _{(min ASA LAND 2)}

• 15 ft / 200 m = Fail Operational
• _{(min. ASA LAND 3)}

• 15 ft / 125 m
• 0 ft / 75 m

_{Minimum ASA Status LAND 3}

3 hydraulic systems

• ILS deviation warning
• ILS transmitter failure
• ASA status "NO AUTOLAND"
• A/P disconnect

• Engine Anti-Ice Switches ... OFF
• All Bleed Switches ... OFF

• (TAS / 100)²
•          3

• WW + 20 = %
• _{(CWC in % vom Wind)}

Used to make a takeoff using no bleed from engines. Air for left pack opertion is supplied from the APU.

<sub>NOT ALLOWED IF ICING CONDITIONS EXIST FOR TAXI OR TAKEOFF

NOT ALLOWED AFTER FUSELAGE HAS BEEN DE-ICED</sub>

Min. ANP = 0.3 or better on both FMCs

_{Set RNP = 0.3 on FMC POS REF 2 PAGE}

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}

2.5 %

3.3 %

Actual Landing Distance x 1,67

Actual Landing Distance x 1,92

_{oder RLD (dry) + 15%}

• Sea Level
• Standard Day
• No Wind
• No Slope
• V_REF Approach Speed
• Anti Skid Operative
• Automatic speedbrake
• NO REVERSE THRUST

200 m

• EFRAS calculation is not available for rwy in use
• the runway is contaminated
• the Anti-Skid is inoperative
• alternate thrust setting (N1) is used

• Landing configuration
• Target speed
• Adequate power
• Rate of descent

• 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