Emirates LVO’s summary General OM/A section 8 p.165
Company policy that all Cat II/III approaches are planned planned to use auto-land. Check Crew Aircraft and Airport Airfield m in RVRs for LVPs given on related Jeppesen Chart ( 10-AWO) List of auto-land approved approved airfields with specific DHs and RVRs, and Approach ban.
A/C serviceable
QRH 5.04 – 5.04 – Equipment list. Check before approach only required if aircraft is not f ully serviceable
Take-off Requirements Abbreviations: HIRLHIRL High intensity runway edge lights HICL – HICL – High intensity centre line lights RL – RL – Runway edge lights CL – CL – Runway centre line lights RCLM – RCLM – Runway centre line markings
Facilities HICL spaced 15m or less. HIRL spaced 60m or less. Multiple RVRs & all 3 must be working RL & CL, Multiple RVRs RL & CL RL &/or RCLM Nil (day only)
LVPs in Force OM/A Section 8 p 273 Approach Ban OM/A Section 8 p.159 4.2, 161 T/O Alternate OM/A section 8 p.19, 34 Auto Call Out
Min RVRs/Visibility / OM/A section 8 p.27,28 p.27,28
* ILS freq. + course frozen in receiver, PERF APP page data frozen
Mid 125m 150m (CAT D)
Stop 125m 150m (CATD)
Remarks LVPs to be in force at airfield. Both crew members to be Cat 3 qualified. 90m visual segment to be avail from cockpit at the start of T /O. The required takeoff RVR as shown on the 10-AWO chart has been achieved for all RVR reporting points.
150/200m/D
150/200m/D
150/200m/D
The reported RVR/VIS of the initial part of the take-off run can be replaced by pilot assessment. Night ops: At least RL & stop end lights required
200/250m(CAT D) 250/300m(CAT D) 500m
Take off should be discontinued if visual references are lost: - below 100kts OM/A section 8 p.276
LVP’s consist of take-offs where RVR <400m (if <150m special training required) & landings where RVR <550m (Cat II/III). LVP’s must be in force to conduct a low visibility approach. ATC will initiate LVP’s according to local regulations usually, RVR <400m cloud base <200 ft. Note: If RVR<500m -CM1 Takeoff
No approach beyond OM or ‘equivalent ‘equivalent position’ (EP) if RVRs less than applicable minima. EP from DME, NDB, VOR, SRE, PAR fix or any other that independently establishes position. If OM or EP unavailable, use 1000’. Each 10-AWO chart indicates the Approach Ban Point appropriate to the State requirements. Required If no return possible, Absolute minima Cat IIIA (50’ 200m) limits wit hin 420Nm 1HR OEO (i.e. single engine considered), or 840Nm 2HRS OEO if a/c is EK ET OPS qualified, no MEL restriction prohibits 120 min. ETOPS and departure departure outside USA. A343 900 Nm / A345 940Nm For A332/343-345 2500, 1000, 400, 300, 200, 100, 50, 40, 30, 20, 10. Also ‘100 above’ and ‘minimums’ except for Cat IIIB approaches with no DH
FCOM 4.5.70
Crew Calls/Actions (FCOM 4.5.70) Note key heights: 1000’: 1000’ : G/A for faults 800’: 800’ : ‘Ldg Inhibit’ 700’: 700’ : *Data lock 350’: 350’: Land’ FMA only exit by G/A 200’: 200’ : Red Auto-land 200’: 200’ : Alert Height 50to40’: 50to40’: ‘Flare’ FMA 30’: 30’: Thrust redn. 10’: 10’: Auto call out ‘Retard’
Touch 125m 150m (CAT D)
Event ATC calls during departure (if no surface movement radar) Passing ‘1000’ above TDZE FMA ‘LAND’ by 350’RA If DH set & auto call Out ‘100 above’ If DH set & auto Call Out ‘Minimums’ If no DH set and at ‘100’ RA FMA ‘FLARE’ by 40’ RA Auto Call Out ‘30’RA Auto Call Out ‘Retard’ @ 10’ RA FMA ‘ROLLOUT’ on LDG
PF (Capt)
“Checked” Cx ILS Course, “Land green” “Checked” “Continue” or “Go-around Flaps” “Continue” Monitor Monitor thrust reduction & flare Retard thrust levers & monitor Monitor lat guidance externally
PNF (F/O) Transmit to ATC “Entering Runway”, “Rolling“, ”Airborne” as appropriate – “STEER LEFT/RIGHT“ “One Thousand” Monitor Auto Call Out “Checked” Monitor Auto Call Out Monitor Auto Call Out or “FLAPS …” “One Hundred” Monitor Auto Call Out “Flare” Monitor Auto Call Out Monitor eng parameters “Rollout”
Select & control rev thrust
Spoilers, Rev Green, DECEL, 70kts” - “STEER LEFT/RIGHT“
ATC calls during AUTOLAND (if no surface movement radar) Lighting Elements in Operation
Transmit to ATC “On ground”, “RW Vacated” as appropriate RVR = Met Vis X Day
Met Vis to RVR OM/A Section 8 p.30
Autopilot Limits (FCOM 3.1.22) Absolute Minima and Visual References Cat I: Visibility Refs DH RVR Cat II/III: Visibility Refs DHs RVRs OM/A Section 8 p. 31, 32
Max Wind Limits RVR Tx Failure Failures (Gnd Equipt:) Lido GEN part RARSupplement appendix H 890/910
Night
HI Approach and Runway Lightings 1.5 2.0 Any type of lighting installation other than above 1.0 1.5 No lighting 1.0 N/A NB: Table not usable for visibility less than 800m or calculating take-off or Cat II/III minima or when a reported RVR is available Slope limits: 2.5°-3.15°. for airfield elevations lower than 9200ft. In emergency Auto-land acceptable up to MTOW 229T. Automatic rollout performance has been approved on dry and wet runways, but performance on snow-covered or icy runways has not been demonstrated. Min LDG weight 123T Cat I DH: 200’ RVR: 550m Cat II DH: 100’ RVR: Cat IIIA DH: 50’ RVR: Cat IIIB DUAL No DH RVR: 75/75*/75 note *1 visibility 800 m (inc with DH) 350*/150/75 note*1 3 200/100*/75/note*1 3 consecutive {A345 / RVR: 125/150/75} To be confirmed App light sys elements. consecutive lights lights from: CL of app lts, TDZ Note*1 No visual ref required when no DH Threshold or threshold from: CL of app lts, lights, CLs or RLs a combination of EK / EK / At least one centreline light is attained and can be markings, lights or ident TDZ lights, CLs or RLs these is attained and can be maintained in case of CAT IIIB with DH lights. Visual glide slope Lateral ref req’d maintained. No lateral ref required indications. Touchdown *Reduced to 300m zone, zone markings or upon APT capability lights. Runway edge lights.
* To be confirmed (No Rollout for BSCU Channel, A/Skid or NWS faults. Increase Midpoint RVR to 125m) Note*1: Not below 75m when stop end of RWY is required by LDG distance Captain discretion * To be confirmed ( Minimum Minimum RVR mid point 125m for Contaminated runway.) Max Wind Limits FCOM 3.01.22 p.4 Stabilisation: 1500 ft aal / OM/A S.8 p .159 Stabilisation For CAT II/III requirement to be stabilised no later than 1500 ft AGL Head 35kts, Crosswind 20kts, Tail 10kts (Runway state may affect) * To be confirmed All All 3 required for take-off at 125m visibilities if ‘relevant’. On landing, minimum of one reading required required from either of Touchdown or Mid Point but if only Touchdown available then the speed must be expected to be below 60kts in Stop End. Above 1000’ Between Resolve by 1000’ or GA. (If reversion occurs, you must re-enter new DH in Perf App Page.) 1000’ & 200’ (Alert Ht)
Go-around for any failure (except ISIS) that affects landing capability. (ENG FIRE continue).
Below Alert Ht (<200’) Auto land Light QRH EK
Loss of AP’s, LOC/GS signals, LOC above 15’, GS above 100’, radalts diff >15’, A/C off beam. Note: Above Note: Above 200 ft RA if the transmitter fail. Lasts less than 7’, the FMA retains the LOC & G/S mode or LAND and AP’s are able to regain these modes. If more than 7’ AP’s trip OFF / triple clicks / HDG V/S reversion. FCOM 4.05
supplement. S6.2
Landing
Disconnect autopilot at taxi speed. Note: CL lighting alternate red/white for last 900m & all red for final 300m
Crew Limitations
F/O / The visibility is more than 500 m as specified in FOM 15.7.1 (for RWY with no facilities). Captains / 50 hours or 20 sectors on type (Including (Including line TRG), + 100m/CAT II/III RVR min. unless previously qualified until a t otal of 100hrs or 40 sectors on type (Including line TRG )
OM/A Section 8 p.274 Section 5 p.18
© Krissch Krisschyy 05/2010 / version 1.8 / 12/0 7/2010
