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Propunere Dan ILIE 03/01/2011

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BRIEFING (TYPICAL)

The briefing should include the normal items as for any IFR arrival and in addition the

following subjects should be covered prior to the first approach:

both pilots qualified; runway width minimum 45 m; Two engines, dual channel approach with flaps 40

__________________________________________________________________________________

review destination and alternate weather; review airfield and runway operational status CAT II / CAT IIIA; brief aircraft systems status; brief review of task sharing:

The approach, go-around and landing shall be flown by the LHS; At approaching minimums LHS starts to look for visual references, progressivelyincreasing external scanning as DH is approached. RHS must stay on instruments throughout the approach and until reaching taxi speed;

review approach procedure and callouts (stabilization gate at 1000 ft); review applicable minima, go-around procedure, ATC calls;

Goaround will be dual channel except after engine failure or autopilot malfunction; brief review of procedure in case of malfunction below 1000ft; review the taxi-in phase;

No paperwork will be accomplished during low visibility taxi; The airport diagram will be in view of both pilots at all times during low visibility taxi;

review the seat position and approach lights as required.LIMITATIONS

Maximum headwind component: /300/NG - 25 knots

Maximum crosswind component: /300 - 15 Kts

/NG - 20 Kts

Maximum tailwind component: /300/NG - 10 kts

No forecast or reported windshear

Glideslope capture by 1500 feet AGL

Note:Once the briefing and approach checks are complete, the approach must be flown as CATII/IIIAeven if the weather improves above the defining criteria


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APPROACH LIGHTING, RUNWAY LIGHTING AND MARKINGS

The most commonly used is the Calvert Approach Lighting System.

150 m

300 m

900 m

Threshold lights (green) unidirectional

Runway Edge lights < 60m

Touchdown Zone lights mirroring approach barrettes

White centreline lights Cat III every 15m (7.5), Cat II 30m (15)

Last 900m alternating red and white

Last 300m red only

Runway end lights (red) directed at threshold


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VISUAL SEGMENT AT DH=100ft WITH RVR 350m VISUAL SEGMENT AT DH=50ft WITH RVR 200m

(TYPICAL CAT II) (TYPICAL CAT III A)

The A/C system requirements for automatic approach and landing to CATII/IIIA minima:

1. Dual Channel Autopilot engaged2. Low Range Radio Altimeter and display for each Pilot3. Decision Height (DH) Light/Display for each Pilot4. Two Digital Air Data Computer Systems5. Windshield Wipers for each Pilot6. ILS Receiver and display for each Pilot7. Flight Mode Annunciator for each Pilot8. Two IRU's (associated with the engaged autopilots) in NAV mode/ For 7-800 -Two ADIRU's

(associated with the engaged autopilots) in NAV mode

9. Dual Hydraulic Systems10.The A/C configuration will be flaps 40, Leading Edge Devices fully extended 11.Two sources of electrical power. (The APU generator may be used as an independent power

source.)

12.Both Engines Operating


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Approach - All Engines - Fail Passive

Below

1500 feet

ILS deviation monitor system test

FLARE armed annunciates

Second A/P couples with flight controls

At 800 feet Second A/P must be engaged

At 500 feet Verify AFDS status

FLARE armed

no steady A/P WARNING light.

At 400 feet Stabilizer is automatically trimmed nose up.

At 50 feet FLARE engaged

At 27 feet A/T begins retarding

Rollout After touchdown

A/T disconnects after 2 seconds

disengage A/P

use rudder to maintain directional control

Dual Autopilot Approach and Go-Around Warnings Fail Passive

WARNING When Cause Pilot Response

Steady red A/P

disengage

warning light

Below 800 RA

during approach

Stabilizer out of

trim

Disengage A/P and execute

manual landing (see note)

or manual go-around.

During GA Elevator position

not suitable for

single autopilot

operation


manual level off

OR

Select higher go-around

altitude

No FLARE arm

annunciation

500 above field

elevation during

approach

Pitch and roll

monitors may not

be enabled, or

only first A/P up is

engaged




Flashing red A/P

disengage

warning light

and wailer

Below 800 RA

during approach

A/P

disengagement

Execute manual landing or

manual go-around.

Flashing red A/T

disengage

warning light

Anytime A/T

disengagement

Cancel A/T disengage

warning and control thrust

levers manually.

Flashing red

Autoland

Warning light

(as installed)

Below 500

Below 200

A/P disengages or

stab trim warning

occurs

ILS deviation

warning occurs




Note: Execute manual landing only if suitable visual reference is established


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If a failure of any ground based equipment occurs, TAROM policy is to abandon the approach and

refer to the following tables for guidance:

APPROACH LTS NOT

ALLOWED

FOR OPS

WITH

DH>50FT

NOT

ALLOWEDMINIMA AS FOR NIL FACILITIES

APPROACH LTS EXCEPTLAST 210 m

NO EFFECT NOTALLOWED

MINIMA AS FOR NIL FACILITIES

APPROACH LTS EXCEPT

THE LAST 420 mNO EFFECT MINIMA FOR INTERMEDIATE FACILITIES

SBY POWER FOR THE

APPROACH LTSNO EFFECT NO EFFECT

WHOLE RUNWAY LT

SYSTEMNOT ALLOWED

DAY MINIMA AS FOR NIL FACILITIES NIGHT

NOT ALLOWED

EDGE LTS DAY ONLY; NIGHT NOT ALLOWED

CENTRELINE LTS DAY-RVR

300 m

NIGHT

NOT

ALLOWED

DAY

300 m NIGHT

550 m

NO EFFECT

CENTRELINE LTS

SPACING INCREASED

TO 30 m

NO EFFECT

TDZ LTS DAY 300 m NIGHT 550 m NO EFFECT

SBY POWER FOR

RUNWAY LTSNOT ALLOWED NO EFFECT

TAXIWAY LT SYSTEM NO EFFECT EXCEPT DELAYS DUE TO REDUCED MOVEMENT RATE

FAILED OR

DOWNGRADED

EQUPIMENT

EFFECT ON LANDING MINIMA

CAT

IIIA

CAT II CAT I NON PRECISION

ILS SBY TRANSMITTER NOT ALLOWED NO EFFECT

OUTER MARKER

No effect if published with equivalent

positionNot applicable

MIDDLE MARKER NO EFFECTNO EFFECT UNLESS USED AS

MAPT

TDZ RVR ASSESSMENT

SYST

MAY BE TEMPORARILY

REPLACED WITH MID-

POINT RVR IF APPROVED

BY THE STATE OF THE

AERODROME. RVR MAY

BE REPORTED BY HUMAN

OBSERVER

NO EFFECT

MID-POINT OR STOP-

END RVRNO EFFECT

ANEMOMETER NO EFFECT IF OTHER GROUND SOURCE IS AVAILABLE

CELIOMETER NO EFFECT

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