fctm chapter14 precision approaches

AIRBUS 'NDUSTRE

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A310/300.600 FLIGHT CREW TRAINING MANUAL14 - PRECISION APPROACHES

14.00 TABLE OF CONTENTS

14.01 - CAT il - CAT ilr BRIEF|NG

14.02 . CAT II DETAILED PROGMMME

14.03 . CAT III DETAILED PROGMMME

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A310/300.600 FLIGHT CREW TRAINING MANUAL

14 - PRECISION APPROACHES

LEFT INTENT]ONALLY BLAI.I K

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14 . PRECISION APPROACHES

14.01 CAT II . CAT II I BRIEFING

01 - GENERAL

A ILS CAT II . CAT III DEFINMONS

The following definitions are taken from the French regulations, which are in compliancewith the recommendation ol ICAO Annex 10 for Category ll and lll operations.

a. Category ll Precision Approach

An electronically guided final approach conducted to a decision height of 100 to 200 ftwith a runway visual range (RVR) providing an acceptable probability of obtainingadequate visual reference to conlrol lhe aircraft lor continuing the approach, roll-outand clearing.

b. Decision Height (OH) - CAT ll

The lowesl height measured by a radio altimeter at which a go-around procedure mustbe initiated if :

- visual relerences are not obtained or are inadequate to ensure a successful approachand landing ;

- or taking into account the available environmental visual references, the position orthe track of the aircraft are such that they jeopardize the success ol the end of theapproach and ubsequent landing.

(The Cat ll DH shouH be not less than 125 % of the Minimum Use Height certificatedlor the AFS).

c. Runway Visual Range (RVR) - CAT ll/lll

The maximum visibility in the direction of takeoff or landing lrom a specific point onthe axis of the runway at a height is corresponding to the average eye level of the pilotat touch down.

In practice, the minimum R\4l value for each landing category is determined in srcha way thal the probability of obtaining adequate visual references lor the end of theapproach is high.

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A310/300-600 FLIGHT CREW TRAINING MANUAL14 - PRECISION APPROACHES

14.01 CAT il - CAT ilt BR|EFTNG (CONT',D)

01 . GENERAL (CONT'D)

A rLS CAT ll - CAT ilr DEF|NTTIONS (CONTD)

d. Category lll Precision Approach With Decision Height

An electronically guided final approach conducted to a decision height of 0 to 100 ftwith a RVR providing an acceptable probability of visual contact at the DH and thepossibility of controlling the aircraft manually during roll-out and clearing.

e. Minimum Approach Break-off Height (MABH)

The lowest height of the wheels above the ground such that il a go-around is initiatedwithout external visual references :

- in normal operation, the aircraft does not touch the ground during the procedure

- with critical engine failure during go-around, it can be demonsirated that takingaccount of this failure probability, an accident is extremely improbable.

(For 1r,310 and 4300-600, MABH has been determined to be 15 ft).

l. Decision Height CAT llt

The height of the wheels above the ground read on a radio ahimeter, at which ago-around must be initiated if :

- there are no external references :

- or the external references have not enabled confirmation that the aircraft is correctlypositioned and tracking in relation to the runway.

g. Fail-passive Automatic landing System

An auto landing system is fail-passive if in the event ol failure it disengages without anysignificant deviation of trim, flight path or attitude. After a lailure either the landing iscompleted manually, or a manual go-around is executed il visr.ral references are notsufficient.

h. Fail-operational Automatic l-anding System

An auto landing system is fail-operational if in the event of failure the operation can becontinued by the remaining part ol the system.

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A310/300-600 FLIGHT CREW TRAINING MANUAL


14.01 CAT lt - CAT lll BRIEF|NG (CONT',D)


A rLS CAT [ - CAT ilr DEFTNITTONS (CONTD)

i. Alert Height (of failoperational syslems)

The height of the wheels above the ground above which a go-around would be initiatedif a failure occured in one part of the syslem.

Below this height the probability of a failure is such that if part of the system fails theoperation can be continued by the remaining part while complying with the safetycriteria (i.e. the height below which the risk of a double lailure can be considered asextremely improbable).

(For A310 and A300-600, alerl height is 't00 ft).

l. Relationship Between DH And Minimum RVR

1. GENEML

The visual reference required by a pilot at and below DH depends on the task thathe has to carry out.Research using simulators and flight irials has shown that in general :

- visual contact needs to be eslablished about 3 sec. above DH to enableassessment of the exlernal references and evaluation ol the flight path in relationto those references ; the duration of this decision process reduces to about 1 sec.when a fail-operational automatic landing system is used.

- to eslablish lateral position and cross-track velocity, not less than 3 axial lightsegments ot the approach lights, runway centreline or edge lights shouH bevisible.

- lo maintain a lateral level, a cross-bar of the approach lights, threshoH or TDZlights should be visible.

- to control the flight path in the vertical plane, including the flare, using purelyexternal cues, a point on the ground which has a low or zero rate of apparentmovement relative to the aircrafl (i.e. the aiming point) shouH be visible.

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14.01 CAT il - CAT ilt BRTEFING (CONT'D)

01 - GENERAL (CONT'D)

A !19 qAT il - AAILILqEIIIjIQN€ (coNrD)

j. Relationship Between DH and Minimum RVR (cont'd)

2. CATEGORY II

For CAT ll operations, Ref. 6 specifies the following minimum visual segments :

auiomalic to touch down or manual .. . . . . . . . . . . 90 mautomatic to DH ... . . . . . . 120 m

The geometry of the 1300-600 in the average approach attitude is such thatat 100 ft a visual segment of 120 m is obtained when the fonvard visibility fromcockpit to ground is 278 m (See Fig. 1).

1?om

FI(i. 1 . THBORETICAL VISTIAL SECTCilT IN CAT I @NDMOiSi AT DH

SVR : SLAI'IT VISUAL MNGESVR is the range over which a pilot of an aircraft in the final stages olapproach or landing can see the markings or the lights as described inBVR definition.

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14.01 CAT il - CAT ilt BR|EF|NG (CONT'D)


A ILS CAT il - CAT ilr pEFTNTTTONS (CONTD)

f. Relationship Between DH and Minimum RVR (cont'd)

2. CATEGORY il (END)

Since it is unusual for a fog to be perfectly homogoneous there is normally adiflererence between the RVR and the "slant visual range" SVR from cockpit toground. ln stable fog conditions with surface visibilities greater than 600 m. The fogdensity normally increases with height above ground, in which case the SVR at DHis less lhan the RVR. However in the range below RVR 600 m. not only is therelation RVR and SVR variable and difficult to predict, but also there may be rapidand localised reductions in visibility.Since there is as yet not practicable way of measuring the SVR at DH, for regulatorypurposes il is necessary to determine a value of RVR which will provide anadequate visual segment at DH with an acceptably high probability.

For this purpose it has been established that the use of the lollowing values ofminimum RVR in actual CAT 1l operations has resulted in an observed approachsuccess rate bdter than 95 % :

DH(feet)

RVR (metres)

ManualTake-OverAt DH

Automaticto Touch - down

100 - 120 400 350121 - 140 450 400141 500 500

3. CATEGORY III WT}.I DECISION HEIGHT

With a failoperational landing system, CAT lll operations can be conducted with aDH below 50 tt (ICAO Cat lll B). The DH is required to be not less lhan ihe MABHwhich for the 4300-600, using auto go-around mode, has been certificated as 6 ft.When the DH is in the landing flare, it shouH be below the height at which the pitchchanges mainly |ake place (Ref. 5).

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14.01 cAT il - CAT ilt BRIEFTNG (CONT'D)


A ILS CAT il - CAT ilr DEFTNTTTONS (END)

j. Relationship Between DH and Minimum RVR (end)

3. CATEGORY lil WTH DECTSTON HETGHT (END)

For this category of operations, the visual segment at DH should be sufficient to :

- enable confirmation that the aircraft is correctly positioned relative to the TDZ ;- if fail-operation auto roll-out function not available', provide assurance that

references will be adequate for manually controlling the ground roll.

The minimum visual segment to lulfill these criteria has been established as60 m. (Ref. 1). At 15 ft. wheel height the SVR required to provide this visualsegment is 115 m (see Fig.2 below). lt isthereforeconsidered that for DH 15 ftan RVR of this order will provide srfficient visual references with an acceptablyhigh probability.

RG. 2 - THEOREnCAL VFIIAL SEGilENT IN CAT I! OONDMONS AT D}I 15 |t

' aircraft without mod. 5757

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14.01 CAT il - CAT ilt BR|EF|NG (CONT',D)


B. THE CERTIFICANON

The operators will be cleared for category ll and lll approaches provided they satisfyspecilic requirements linked to the capability of :

1. THE CREW2. THE AIRCRAFT3. THE AIRPORT FACILIT1ES

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A310/300.600 FLIGHT CREW TRAINING MANUAL14 . PRECISION APPROACHES

a. Crew Requirements (Example laken from French rcgulaiions, Ret. Page 1)

GROUND SCHOOL

. l0towledge of guidance and piloling systems

plus satety and waming devicas.

. Arcraft handli.rg mgthods, cr€w assignment and

task-shadng

. Beview ot ths Regulations (operational minima,

decision height)

- oUALIFICATION Crests)

. RECURRENT AI.INUAL CHECK

must compulsorily ex€cutg :

. a precision approach to 100 ft tollowed by a lancling

with RVR conesponding to CAT ll minima

. a precision approach lo 100 ft with missed app@ach

procedur€ initiated :

- at 100 ft due to lack of visual reterences

- or between 100 and 200 ft due to system failures

$rith RVFI corresponding to CAT ll minima.

Not mandatory (up to checker discretion) :

Exscut€ an approach down to 100 tt with missed

approach between 1Oo ft and a del ined height, due to

lack of visual ref€ronces, with Cat ll R\/R.

FLIGHT TRAINING (ACruAL ORSTMULATED)

. Arto-Flight :

1/3 lrrith fully operational systems

2i/3 with lailures and alarms during approach

INITlAL QUALIFICATlON. Release lo CAT I minima is a prerequisite. Delivery of proticiency certificate valid lor 12 montl(DH 1s0 ft)

ts involving a period ot temporary minima

TEMPOMRY PERIOD TO REACH CAT II MINIMA. Each quali{ied pilot must d€monstrate 20 approaches using CAT ll procedures in actual (or non actualcondit ions), with the aircraft type and equipment designad tor that aircratt with a decision h€ight (DH)testricted at 15O ft before clearanc€ to op€rate at CAT ll minima is obtained,

M!NIMUM INITIAL REQUIREMENTS

. Must satisty all CAT ll qualification requirements.

. Elgedence on type at l€ast 200 hrs for Captain, 50 hrs for F/O

GROUND SCHOOL. As per CAT ll may be abddged if sutticient CAT llexperience already obtained.

- OUALIFICATION CHECK (in tlight unless obtained forapproved simulator

- RECURRENT ANNUAL CHECK (approval simulator)

2 automatic approaches to DH with go-around,including one wth one engine at idle.

trffi'l

FLTGHT TRATNTNG (ACruAL ORSIMULATED)

applicable for aircraft having fail-operationalauto-systems

4 automatic approach€s to DH including :

. 2 landangs with min. RVR

. 1 go-around at min DH. both engines operating

. 1 go-around at or abovs min DHwith 'l eng. at ir

INIT1AL QUALIFICAT]ON. Delivery ol proficiency certiticate valid for 12 monucompetency check.

rs, renewable only atter successful completion of recurrent

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1. MINIMUM EOUIPMENTncludinq items required fcrr land mode enqaqemenl

EQUIPMENTCATI

ManualCATIArto

CATIIArto

fin CMD)

cATmAilo

fin CMD)REMARKS

Arlo Pilot

AP disconn. pb

Flight Direclot

FD bars

Arto Throttlo (sPD)

Hydraulic systems

Pitch Trim

Yaw Damper

tRs

EFIS CFITc

Hodzons

ILS Receivers

PFD LOC/GS

Marker Beacon

Radio Atimeters

Radio Atimeters displays

PFD OH Waming

FMA

Arto call-out

WARNINGS

EXCESS DEVAUTOLANIDAP OFFATS (WLDP)

Failur Waming Compt

l\linrlshield Wipers

Wndow Heat

Rain repellent

Generators

Engine rim

See

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Associatsd with FD lor Cal I

Associated with AP tor Cat ll

3 independent sources

1 associated wilh FD tor cat I

Associated with AP|FD in use

Cat ll : side according

to task allocation

lor CAT l1 :CMI side req'd

APU GEN may replace

one ENG GEN

b. The Aircratt Requirements - CAT ll/lll

NOTE : This list is lor training intormation only. For the delinitive Flight Manual andregulatory requirements, refer to FCOM 2.02 and the MEL.

For Cat lll without DH (Batch C mod lor A.310, mod 5686 for 4300-600) rolloutmode musl be operative.

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01 - GENEBAL (GONT'D)

B. THE CERTTFTCATTgN (CONTD)

b. The Aircrafl Requirements - CAT ll/lll (cont'd)

2. GENEML

The following table gives the bwest DH for each category for which the aircraft havebeen or will be certificated. lt also shows some typical operational RVRs which arecurrently used or envisaged.

ICAO Cateoorv DH feet RVR metres

200800 or 600with centre

line guidance

il 100 350i l l

(fail-op)with DH 15 115no DH 75

It should be noted that the operaiional DH at a particular runway may be limited tohigher values than in the above table because of obstacle clearance considerationsor the limitations of the ground installation.

The 4300-600 is certificated for the following categories of precision approach :

- Cat ll in failpassive or fail-operational configuration '- Cat lll with DH 15 ft in fail-operational conliguration- Cat lll without DH in fail-operational configuration provided mod. 5686 is

incorporated.

One autopilot engaged in LAND mode constitutes fail-passive configuration.For fail-operational Cat lll capacity, both autopilots must be engaged in LAl.lD andat least one ATS in SPD. The detailed minimum equipment requirements for eachcategory are given on 14.01 Page 9.

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14.01 cAT ll - cAT lll BRIEFING (CONT'D)


B. THE CERI]FICATION (CONTD)

b. The Aircraft Requirements - CAT ll/lll (cont'd)

2. GENEML (END)

It is recommended to use the maximum available automatic capacity whenever anautomatic precision approach is required, in order to :

. Optimize the margin ol safety and reduce the effect of component lailure on thecompletion of lhe approach.

. Maintain pilot proficiency in automatic approaches.

. Exercise the equipment.

For the purpose of determining the applicable minima published on approachcharts, the aircraft is in approach category C.

3. AFS OPEMTING LIMITATIONS IN AUTOMATIC APPROACH AI.ID LAT.IDINGPHASES

- minimum approach speed Vt-s + 5 kt.- the approach conditions, aircraft and systems configuration and speed shouH be

slabilized not later than passing 500 ft a.g.l (unless DFA mode operative).- CG limits FWD 18 % - AFT 35 %.- miu demonslrated wind conditions.

' ll batch C mods are not incorporated, AP should be disengaged at touchdownwhen any of above limits are exceeded.

ArtolandArto rollout'

(basic)Arto rollout

with batch C modsheadwind 30tailwind 10crosswind 20

1055

301020

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14.01 CAT il - CAT ill BRIEF|NG (CONT'D)


B. THE CERTTFICAION (CONTD)

b. The Aircratt Requirements - CAT ll/lll (end)

3. AFS OPEMTING LIMITATIONS IN AUTOMATIC APPROACH AI{D LA}.IDINGPHASES (END)

- min speed for auto roll out : Basic : 60 kt

with batch C mods * :zero

- aircraft certificated configuration Slats 30/Flaps 40, both engines operating (butsee 08.04 Page 16).

- Cat ll approaches to touch down are permitted only on Cat ll or Cat lll quality ILSbeams.Cat lll approaches are permitted only on Cat lll ground facilities.

- the aircraft is certificated for automatic landing on Cat ll and lll facilities only.- localizer beam capture : the lollowing graph gives the max permissible angle ol

interception as a function of geed and distance to the threshoH.

6 7I 910 11 12 (NM)

- GLIDE beam capture :Glide interception aftitude shouH be between 1000 ft and 3000 lt.Vertical +eed should be between + 500 ft and - 1250 ft.Maximum speed shouH be 200 kt lAS.

+ Mod. 5686 lor 4300-600.

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14.01 CAT il - CAT ilt BR|EFING (CONT'D)


B. THE CERTIF|CATION (CONTD)

c. Airport Requirements CAT ll/lll

In order to be able to operate to Category ll or lll minima, the runway environment andthe ground equipment must be meet the applicable criteria, summarised below.

1. OBSTRUCT]ON CLEARANCE LrMrT (OCL)

- for any precision approach runway, the obstacle clearance must be consideredin the determination of DH and the related RVR.

- no obstacle should protrude through reference surfaces in the transition of missedapproach areas, nor should there be any obstacle within the Obstacle Free Zone.Exceptions are made for essential visual and electronic equipment.

- the detailed obstacle clearance criteria covering approach and go-around phasesare published in ICAO PAI.IS-OPS.

2. TERRAIN PROFILE

Under lhe approach path shouH be free of excessive uplor down-slopes anddiscontinuities, since the radio ahime,ter provides an input signal to the auto-pilot forgain programming during a coupled approach lrom 1000 ft and for pitch controlduring llare from about 50 ft. Before a runway is approved for Cat ll or llloperations, the terrain profile as well as the runway is investigated for its slitabilityin accordance with established criteria.Similarly lhe runway profile itsell musl be within specified limits.

Note that the radio altitude at DH published on the Cat llllll approach charts takesaccount of any difference between touch-down elevation and the level of terrainbelow the approach of the extendd centr+line.

3. ILS INSTALLATION PERFORMAAICE AA,ID RELIABILITY

Must conform to the appropriate specifications contained in ICAO Annex 10.

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14.01 cAT il - CAT ilt BRIEFING (CONT',D)


B. THE CERT1FTCATION (CONTD)

c. Airport Requirements CAT ll/lll (conl'd)

4. ILS CRIT]CAL AREAS

Localizer and glidepath antennae must be isolated within a defined area in orderto prevenl electromagnetic interterence of ILS signal transmissions. The associated"sensitive areas" musl be protected from incursions by taxying aircraft and vehicleswhen any automatic landing operation is in progress.

5. HIGH INTENSITY APPROACH LIGHT]NG

Should be provided ol which the lasl 300 metres musl conform to the specificationsot ICAO Annex 14 shown in Fig. 1. This is a recommendation for Cat lll, andmandatory for Cat ll.

6. RUNWAY LIGHNNG AND MARKINGS

Should conform to the specifications of Annex 14 and should include :

- white painted centre-line

- touchdown zone markings

- distance marks including a distance code

- runway threshold lights

- high intensity runway edge lights

- centr+line lights exlending over the full length of the runway with distance coding

- touchdown zone lights required for Cat lll but not mandatory for Cat ll"

The required standard runway lighting is shown in Fig. 1.

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14.01 CAT il - CAT ilr BRIEFTNG (CONT'D)


B - THE CERIFTCAIoN (END)

c. Airport Requirements CAT ll/lll (end)

7. RVR MEASURING DEVICES

ShouH be inslalled near the threshoH and at the mid-point.Some authorities also require RVR measurement at the stop-end for Cat llloperations.

The table below gives a *lmmary ol the principal ground equipment requirements,lor quick reference :

EOUIPMENT REOUIRED CAT I CAT II cAT ilt

ILS category

Approach lighting

Runway centreline lights

Touchdown zone lights

RVR measJrement

I for RVR 800 mllfor RVR 600 M

YesNo for RVR 800 mYes for RVR 600 m

No

l l

Yes

Yes

NoThreshoHMid-rwv

ll for DH 50 ftl l l lor DH 15 ft

No

Yes

YesThreshoHMid-rwy

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A310/300-600 FLIGHT CREW TRAINING MANUAL14 . PRECISION APPROACHES

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APPENT'X A

- EFFECT OF PTTC+I ON VISIAL SEGMEhN -

NORMALPfTCtIArTlTUDE

P]TCH UP

PTTCH DCI'VN

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f urcrlzEnlmR^LGEOtiETRt/

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LEFT INTENNONALLY BLAAIK

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APPENDTX B

TI{RESHOLD CROSSING HEIGHT & TOUCH-DOVI'N POINT

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LEFT INTENT]ONALLY BLANK

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AIRBUS INDUSTRIE hfuof;rhg & FEht A!€,,i6/'bns St-9|Dtr,n Dtv&n Y/,

A300.600 FLIGHT CREW TRAINING MANUAL


APPENDX B

gFr

THRESHOLD CROSSING HEIG}IT & TOUCT}DOWN POIiTT

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31 MAR 96/REV 1714{1 (14{r5.CGM)

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LEFT INTENT]ONALLY BLANK

31 MAF| 96/REV 1714{1

14 - 0tPage : 20

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AIRBUS INDUSTRIE hhohhg A FEht Wrdtbtls iflptt Dtrb|' V

A310/300-600 FLIGHT CREW TRAINING MANUAL14 - PRECISION APPROACHES

14.01 CAT lt - CAT ilt BRIEF|NG (CONT'D)


(a) : 15 W200m1175''rl/175m in case of CAT lll A.(1) : lf discrepancies reported, or under FAR, see AIRPORT MIN EQUIPMENT LIST,

RVFI requirements.(2) : For USA ONLY.

C . GENEML BEQUIREMENTS TO INITIATE PRECISION APPROACHES

CAT I CAT II cAT illMINIMA

300 200 200 100 0 Min DI/DH FT800 700 500 350 12s(a) Min TDZ RVFI Meters (1)

175 12s(a) Min MID RVR Meters {1}

125(a) Min ROOL-OUT RVR Melers (1)x X X X CONFIG All pnn nnpral inn

A

I

R

P

L

A

N

E

X X X X Ldo llaos 30/40I 2

AP./ F.D.AP channel ( in land mocie)

1 z 2 AP disconnect oush butlon1 1 1 1 FD channel

I 2 2 FD bars on EFIS disolavATS ATS channel (in SPD mode)

1 I 2

PFD

FMA indications1 1 1 2 2 Attitude indications

1 2 2 Airsoeed indications

t 2 2 ILS indications (LOC and GS)1 1 1 2 RADIO

ALTIM.Transceivers

1 2 F)iqnlavs1 1 2

WARNINGS

AP off l iohts or aural warnino1 ATS MN-DP)

1 2 AUTOLAND liohts

2 2Excessive deviations (LOC andGSI

1 1 2 2 ILS Receivers1 1 I Markers receiver or eouivalent fix indicaiion2 2 2 5 l.R-S. (at leasl one associated to AP)

1 2 3 3 4 EFIS CRTsI I STDBY Horizon

t Auto callout1 2 F.W.C

1 Anli-skid1 Enoine trim (EEC)

x (2) Both Thrust Reversers Serviceable1 1 1 Window heat (CM11 1 1 WindshieH wioer'cM11 1 I Rain reoellent (CM1)

I 1 I 2 Electric Dower {oenerators. eno. or APU)lX=

31 MAR95/BEV1714-O1

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c - GiENEUBE4'TREMENTS TO TNTT]ATE PRECTSTON APPTQAQ|-|ES (END)

Either;X= Required.15 fV200m/175m/175m in case ol CAT lll Alf discrepancies reported, or under FAR, see AIRPORT MIN EQUIPMENT LlSlRVR requirements.For USA ONLY.(3) : lf discrepancies r@orted, see AIRPORT MIN EQUIPMENT LIST.lf discrepancies reported, see AIRPORT MIN EQUIPMENT LIST.

t r -

(a)(1)

(2)(3)

CAT I CAT II cAT illMI

NI

M

300 200 200 100 0 Min DI/DH FT800 700 500 350 12s(a) Min TDZ RVR Meters (1)

175 12s(a) Min MID RVFI Meters (1)

125(a) Min ROOL-OUT RVR Meters (1)

E

Precision Approach Radar AERoDRoME

E

ILS CAT I (3)

E rLS CAT il (3)X rLS CAT ilr (3)

X X X TDZ CL (3)x X x X X HIALS HIRL (3)

X X x FAR RWY Lenqth + 15oh (min + 1000 tt)

X x x Braking action "medium" (V.3)

30 30 30 Max. allowable headwind component (no qusts)wX

20 20 20 Max. allowable crosswind comoonent10 10 10 Max. allowable tailwind comoonent

x X No heaw precipitationX x X X Use of FD compulsory P

Roc

x x x Use of AP in CMD compulsory

X X Automatic CAT ll/CAT lll APP

31 MAR 96/REV 17 A3IO/3OO€oO1401

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AIRBUS INDUSTRE TAtofthg t F(tffi Qpelc/;br g.ppott Dtvt/oti Yl/



14.01 CAT il . CAT ilt BRTEF|NG (CONT'D)

01 - GENERAL (END)

AIRPORT MINIMUM EOUIPMENT LIST

CAT I CAT II cAT ill150 ft 100 ft

X ILS STBY TMNSMITTER

JEP 450 m 450 m HIALS (min. Inn€r Lighting)

JEP

JEP

x (a)

X

X

X

X

x

DAY

NIGHT

RWY EDGE LTS/TDZ LTS

JEP 30m 30m 15m CENTER LIGHTS (Max. Spacing)

X X X STBY PWR tor ALL RWY LIGHTSx X X X WIND MES. EOUIP. OR SUBSTIT.

max 1/3 US providedpattern unaltered ALL ALS and RWY LIGHTING

(a) Simultaneous tailure between runway lights and TDZ lights not acceptable.

RVR REQUIREMENTS FOR

CAT I

ll no TDZ RVFI available, MID RVR may

substitute TDZ.

lf no TDZ nor MID RVFI available. a minimum

meteorological visibility of 8OO m is required

to initiate an approach lo a DH of 200 tl.

CAT II

EUR rDZ + MtD RVF| are required.lf TDZ R\E not available. MID and Roll OutR\m vMin L<rg RVR.lf MID R\n not availabl€. Roll out R\n V200 m.

FAR TDZ + Rotl out R\R are required and mustbe \zlrlin Ldg RVR. lt Roll Out R\rFt not avai-lable, MID R\lR vuin Ldg RvR.

cAT ill

EUR TDZ + MID + Rolt out RVFIs are required.MID or Roll Out R\R may be massingprovided remaining RVR's Vtvtin Ldg RVR.

FAR rDZ + MID + Rotl out RVFrs ars requirect.

31 MAR 96/REV 1714-O1

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AIRBUS NDUSTRIE TAtuohhg AFqlfi Oc€rtotb|69tpDp,tt Dwril/|. YJ/


14.01 CAT il - CAT ilr BRTEFING (CONT'D)

02 - OPERATING PROCEDURE

A ABBREVIAT]ONS

The following is a glossary of abbreviations used in the text :

AFS Aurtomatic Flight SystemATS Arto-Throttle SystemCM1 Pilot occupying left seatCMz Pilot occupying right seatDH Decision HeightDFA Delayed Flap ApproachFD Flight DirectorFMA Flight Mode AnnunciatorGA Go-AroundHp Height of Pilot's eyes above main wheelsHt Heighl corresponding to decision TimeIRS Inertial Reference SystemLIS Localizer InertialSmoothingMABH Minimum Approach Break-Off HeightOCL Obstacle Clearance LimitPFD Primary Flight DisplayPF Pilot FlyingPNF Pilot Non-FlyingRA Radio AltimeterRVR Runway VisualRangeSVR Slant Visual Bange from cockpit to groundTDZ Touch Down ZoneWGD Windshield Guidance DisplayWLDP Warning Light Display Panel

31 MAR 96/REV 171401

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14.01 CAT il - CAT m BR|EFING (CONT'D)

02 - oPERATING PROCEDURE (CONT'D)

cAT t/il/il|

B. PRIOR TO OR DURING DESCENT

| ' Seats adjusiemenl. Crew qualification. Check destination and alternate weather. Check fud at destination and alternateo Check airfield facilities status (lLS, LIGHTS, etc). Check aircraft system statuso Review minima, app and go-around proc, fill in landing data cardo Set DH/DA (for NO DH, set DH = - S tt). Review distribution of tasks *. Review procedures in case of malfunctiono Rwieur special ATC calls as required. Use of Ar.rtobrake - Cockpit lighting

' (Task sharing)

The standard Category ll and lll approach procedures for A310/300€00 assume use ofthe maximum automatic capacity of the AFS.For Cat ll & lll operations on line flights, the Gaptain is the Pilot Flying PF (controlting theaircrafi by means of the AFS). The woft-load is distributed in such a way that the pFprimary tasks are supervising and decision making, and the CM2 primary task ismonitoring operation of the AFS.ln srmmary the tasks are shared as follows :

CMl - has hands on controls and throttles throughout approach, landing andgo-around

- sets speed and GA altitude on FCU- takes manual control in errent of AP disconnection- monitors llight inslruments

CM2 - monilors tlight instruments headdown lhroughout approach, go-around orlanding until roll-out is complete

- calls any dwiation or faibre warning- calls barometric heights as required, and monitors auto call-out or calls

radio heights *

- monitors FMA and calls mode indications as required *

AtlCAT IIand €

cAT illoperations

30 NOV96/REV t8 A310/300600t4-o1

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AIRBUS 'NDUSTRIE

IATtoi/.thg &HtgN +/eu b|6g.p'f/tt}tvtbi V

A310/300-600 FLIGHT CREW TRAINING MANUAL1 4 . PRECISION APPROACHES


02 - oPERAT|NG PROCEDURE (CONT'D)

(coNrD)

cM1approaching DH :

- starts to look for visual references, progressively increasing externalscanning as DH is approached

at or before DH, (if his decision is to continue) :- calls "LANDING.' scans mostly head-up to monitor the flight path and flare (in.Cat ll or lll A)

or the track (in Cat lll B) by vis.ral references (The DH is the latest point bywhich a decision to continue should be made).

cM2at DH (identified by aural and visual warning) :

- if decision not yet announced by CM1, calls "lrIlNlMUM,,- if no response lrom CMl, initiates go-around

IF DECISION IS TO GO.AROUND :CM1 - calls'GO AROUND ltap 20,'

- initiates go-around by the go-lever, monitors throttle advance- monitors rotalion by pFD, cross-checks standby horizon- check positive ctimb (VSl + rad. alt.)- commands configuration changes

B.

Operationswilh DH -+

ArlCATIIand

cAT illoperations

t-I cMl

cATil Ioperations I

without +lDHI

L

CM2 - monitors throttle movement, sets thrust if necessary, monitors engineinslruments- monitors flight path by flight inslruments- selects configuration changes

if no failure by Alert Height (100 fr), cails ..LAND|NG'- monitors flare by flight instruments- monitors lateral guidance during flare with FD- monitors thrusl reduction- monitors ground roll by scanning afternately instrument and external

references (stpplemented by WGD. if installed)- selects and controls reverse thrusf- disengages auto-pilot not later than 60 kl*.

' with modification tsz, wGD & yaw-bar appear at Ap disconnect ;'* with modification vs7, auto roll-out function can be used to full stop.

30 Nov 96/REV 18t4-01

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AIRBUS INDUSTRIE htud1hg E Ft9ht Q€ratb^ss..pptt Dttl',bn !l/


14.01 CAT il - CAT ilr BR|EF|NG (CONT'D)

02 - oPERAT!NG PROCEDURE (CONT'D)

B. PR|OR ro OR DUBN_q_pESaENr (CONTD)

- CAT II & III OPERANONS TYITH DH

10mhilure

abotre Al-lgoaround

Dll + 100

CMI qL scanning CMl.+ scanning$q- - -AH (lf fallop.)G-lvll m lrsils.C1!t2 m lrsts.

. CAT lII OPERANONS WITHOUT DH

hllutpabors Al-lguamund

CM2stnp m insts.]

I .l . - /

Rut|WAY

At{ -

- CMI m hst6.--- CM2mlnsts.- CMl albmablvort

nmlrp and fi hsts

Al Cat ll & lll opentionE:

- Cill on qfiofe & thrciles hroughorn appmadr landing and goaround

-Cl,fQ, stap an lrsts. untilend ol gound rdl

31 MAR 96/REV 1714-01 (14{17.CGM)

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AIRBUS INDUSTRIEI|oinhg AFIght Opeulbrl'lgJ€|cp/tt Dftbn

A310/300-600 FLIGHT CREW TRAINING MANUAL14 . PRECISION APPROACHESSUMMARY OF TASK SHARING / CALL OUTS

GUIDE OF ADDITIONAL PROCEDURES . CAT II - CAT III

'with mod. 5757 (,{310), 5686 (4300-600) no yaw bar until AP disconnect ; auto rollout usableto tull-stop.

31 MAR 96/REV 1714Ol (14{10.PCX)

t4-01Page: 28

FINAL APPROACI.I

CONDITIONS cMl cM2

Follow conlrclsSet speed + GAalt. on FCUMonltor tllght path

lilonitorfrl. path + onglnes + FMA modee

HFAD DOWN lhrdlraholrl

At/TOl-At,tO LT. TEST I

checx bBem dev. wamino I

OM. reEI@

start waich. 1,9!.8@-e!!!!wLJ

drrt watch

BARO ALT.1000 tr AAL

fullow or contsols lhrottlca . E@lBARO ALT.700 fr AGL

ILS course sel t7t6-1

RAD. ALT.400 fi AGL

Check no frags, no excess d€v.

RAD. ALT.DH + 100 tl

' l.$ES-l-Exlemal scanning . mosthy head up

. ugglqlMonltor auto call-out

lf sufficienl vis. refs & ttl path OK:

not laler lhan DH(wtr€n au6l wamings stops)

HEADUP

II

ILAIDING I-

I

-@@ll no response, initbte GA

ar uF|. lr no

announced

RAOAT'50t140 ft30 fr

20 tt10 tt

Vrsually monilor tlaro

Monitor or control throttles to idle

Monilor aulo call-out (call racl. ans' if Inop)

.@l

Check vaw bar'TOUCH OOWN

Before 60 h

ISE-ECT REVEFSF]

Monitor nose lowering

lp-iE6fiiiffi;trI'CAI.ICEL REVERS€

. IRoLL OUT I Check spoiteE

. @ffi;;lChock AUTOBMKE greenMonilor N1/EPR, EGT, call sp€€ds

ll vis. lrfs ml lufficirnt or flt path nol OK :, r.* ." t-..,.........T. 1".^ "-- I

I l I l3€r-EGE6]' lrdvarrce throttles Isal€ Dlich. I Ctrect THR & GOAROUND FMA't

r-by hodzon I Monitor or s€t thrust. lESsiiiml

I1 Monitor lli & eg. insts

aI DH

POSITIVE CLIMB

. IGOAROUNT

-:IGO LE\ERS

Follow controls &Monitor rotation tc

Cross-chcck stanc. IGEAR UP I.

A310/300€00

Chatvi AP45

AIRBUS INDUSTRIE f tAftohhe e FEht +€tdbu S.+pon Dt'^s/n V/


14.01 CAT il - CAT lll BRTEF|NG (CONT'D)

02 - oPERATTNG PROCEDURE (CONT'D)

B. PRrOR TO OR DURTNG DESCENT (CONTD)

FLIGHT PARAMETER DEVIATION CALLS

Parameter f deviation exceeds Call reouiredIAS + 10kt

- 5kr "SPEED'

rate of descent 1000 ft / Min "SINK RATE"

pitch attitude 10 nose up0 "PITCH"

bank anole 7 "BAIIK"localizer EXCESS

DEVIATlONWABNING

0.3 dot (PFD) "LOCALIZER"

glide slope 1 dot "GLIDE SLOPE"

These calls would normally be made by the pilot monitoring and acknowledged by thepilol al the controls. Howa/er any CM who sees a derriation outside the above limits shouldmake the appropriate call.lf any of these limits are exceeded approaching DH a go-around may be necessary.

ATC CALLS

Clearance to carry out a Cat ll or lll approach must be requested to Approach Control,who will check the status ol the ILS and lighting and protect the sensitive areas lromincursion by vehicles. Such an approach may not be undertaken until the clearance hasbeen received.Before the outer maker RVR values for touch-down, mid-runway and end-runway whereavailable, will be transrnitted. The approach chart will confirm the minimum values required.

sE/-T rcsff/oN

The correct seat adjustement is essential in order to take full advantage of the visibilityover the nose. The seat is correctly adjusted when the pilot's eyes are in line with thered and white balls.

USE OF LAI{DING LIGHTS

Al night in low visibility conditions can be detrimental to the acquisition of vislal references.Reflected light from water droplets or snow may actually reduce visibility.Landing lights wouH therefore not normally be used in Gat ll or lll weather conditions.

31 MAR 96/REV 1714{1

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A310/300-600 FLIGHT CREW TRAINTNG MANUAL14 - PRECISION APPROACHES

14.01 CAT il - CAT ilt BRtEFtNc (CONT'D)

02. oPERAT!NG PROCEDURE (CONT'D)

B. pRtoR TO OR DUR]NG pESCENT (CONTD)

Example of possible briefing.

CAT IIPRECISION APPROACHES

CHECK LIST

The briefing should cover the lollowing and should preferably be completed pRIOR TOT}IE DESCENT.

CREW BRIEFING

- Check destination and alternate weather.- Check crew qualifications current.' check status of airfield lacitities (lLs, approach and runway lighting,

measurements).- Check aircraft systems status.- Review applicable minima, approach and go-around procedure (heights and

auto brake for landing.- Review distribution of tasks.- Review procedures in case of a mallunction (including 1o0o ft) limit

switching/reverting to higher minima (go-around thereshold).- Review ATC calls required.- Check seat positions cockpit light.

31 MAR 96/REV 171401 14-01

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AIRBIIS INDIi.STR'E f7Alt''inhg E Flght Ope'ld/tbns9LB|Df/n D[^t'l Yl



14.01 CAT il - CAT ilt BRIEFTNG (CONT'D)


B. PRIOR TO OR DURTNG DESCENT (END)

THE AIRCRAFT REQUIREMENTS

EQUIPMENTCAT IIAUTO

IN CMDEQUIPMENT

CAT IIAUTO

IN CMDAUTO PILOT 1 PFD LOC/GS 2AP DISCONN. PB 2 MARKER BEACON 1FLIGHT DIRECTOR 1 MDIO ALTIMETERS 1FD BARS 2 RADIO ALTIM ETERS DISPLAYS 2HYDRAULIC SYSTEMS G+BorYi lAPl

Y+GorBi lAP2PFD DH WAFINING

1

APP OFF WARNING 1 FMA 1PITCH TRIM 1 EXCESS DEV 2YAW DAMPER 1 FAILURE WARNINGS COMP. 1IRS 2 WINDSHIELD WIPERS (CMD SIDE) 1EFIS CRTs 3 wrNDow HEAT (CMD SrDE) 1HORIZONS 3 RAIN REPELLENT 1ISL RECEIVERS 2 GENERATORS 1

NOTE : This list for training inlormation only - For the definitive Flight Manual andregulatory requirements refer to FCOM 2.02 and MEL.

31 MAF 96/REV 1714{1

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14.01 CAT il - CAT ilt BRIEF|NG (CONT',D)

02 - oPERAT|NG PROCEDURE (CONT',D)

c. APPROACH C/L (BEFORE START1NG APP)

D. INITIAL APPROACH

Seatposi t ion. . . . ADJUSTATOOlearanceforOATl l l l l l . . . . . REOUESTEDAdvise ATC of intentions in case of go-aroundRadio Aids . SETand CHECKFDSwitches.. . . . . . .ONAP.. . CMDA/THB(asrequired) . . . . . . . .ONArtobrakes.. . . . ASREQUIREDCockpit l ighting .. ADJUSTRemark : Landing lights not recommended (CAT lVlll).

E. ON INTERCEPT HDG

ND .. . . . . . ROSEMODEVOR/NAV/lLSswitch ... BOTH ILSAr.r to landtesl . . . . . . . . PERFORMLAt ' lDmode . . . ENGAGE2nd AP (if available)Checkcapabi l i tyonFMA ; . , , . . . . . . . . .CATyl l / l l l

F. LDG C/L (PRTOR TO FAF)

Vapp (Vret+ 5minimum).. . SELECTEDGA ahitude SELECTEDRwy HDG SELECTEDILS CRS on both ND's . CHECKED

31 MAR 96/REV 1714-01

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14.01 CAT il - CAT ilr BRTEF|NG (CONT',D)

02 - oPERATING PROCEDURE (CONT'D)

G. FAILURES AI.ID ASSOCIATED ACT]ONS

A summary of failure cases and associated actions is given in this section, based on thedetailed inlormation provided in the FCOM.

It shouH be noted that for some cases the actions presented in the chart have beensimplified for the sake of standardization.

ln general lhere are three possible responses to the lailure o{ any system, instrument orelement of the AFS duing the approach :

- CONTINUE the approach to the planned minima ;

- REVERT to higher minima and proceed to a new DH ;

- GO-AROUND and reassess the capability.

The nature ol the failure and the point of its occurence will determine which response isappropriate.

As a general rule, if a failure occurs above 1000 ft a.g.l the approach may be continuedrarerting to a higher DH, at the Captain's discretion and provided the appropriate conditionsare met (see nexl page, conditions lor Downgrading). In specific cases Cat ll status canbe restored by transler switching provided the failure occurs above 1000 ft.

Below 1000 ft (and down to 100 ft when configuration in fail-operational) the occurenceof any failure necessitates a go-around, if sufficient visual references not yet acquired,and a reassesment ol capability.

Another approach may then be undertaken to the appropriale minima lor the failure case.

When failoperational, in general a single failure below 100 ft does not necessitate ago-around, the lew exceptions to these rules are indicated in the chart.

31 MAR 96/REV 1714{1

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14.01 cAT il - cAT lil BRIEFING (CONT'D)


H. DOWIGRADING CONDITIONS

Downgrading lrom Category lll to Category ll permitted only if :

- Decision to downgrade before 1000 ft AGL ;- At least SINGLE MODE available ;- RVR at leasl equal to Category ll minima ;- Procedure and Category ll minima have been included in approach briefing.

Downgrading from Category ll to Category I permitted only if :

- Decision to downgrade before 1000 ft AGL ;- At least F.D Mode available :- RVR at least equal to Category I minima ;- Procedure and Category I minima have been included in approach briefing.

NOTE : Switching from one AP to another permitted before 1000 ft AGL.

a. Slats/flaps not at 30"/40'

- Automatic landing has not been certificated for this configuration, but has beendemonstrated in 20"/20o configuration.The minima shouH therefore be raised to CAT l.However, in case ol operational necessity, the approach may be coupled down to100 ft, or for 20o120" to touchdown. The speed should be Vls for the actualconfiguralion.

b. Engine Failure

- The corresponding yaw damper may disconnect ;lf N'2 engine fails, AP2 may disconnect due to loss of yellow pressure (with mod.4941 only, if both AP remain engaged, disconnect 1 AP) ;

- ATS remains armed and engaged, (if batch C mods. are not incorporated, +eedholding may de degraded and manual throttle is recommended) ;

- Automatic yaw compensation for engine failure is provided by the rudder channeland yaw damper during approach and auto go-around until retraction of slats.

31 MAR 96/REV 17t4{1

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(Al,tr/hthg A FW operdtb'ifgtpport Dlvb/o,n Y,





H. DoW{GRADTNG qgNglTONl (CONTD)

b. Engine Faibre (end)

lf the faifure occurs above 1000 ft :

- Normally time should be allowed to complete appropriate single-engine operationprocedure after ECAM ac{ions ;

- Approach may be continued automatically to Cat | " minima ; slowly increase thruston live engine by approx. 20% Nr or 0.1 EPR lo maintain Vls + 5 ;

- Rudder trim has no effect on rudder position when AP engaged with slats out, butthe selected trim input becomes effective as soon as AP is engaged.

lf the failure occurs between 1000 ft and 100 ft :

- lf insuflicient external references, make an automatic ao-around, perform ECAt\tactions and appropriate single-engine operation procedure. Another automaticapproach to Cat | ' minima may be made with the aircraft manually trimmed (UnlessBatch C mods are incorporated, manual throttle control is recommended).

lf the failure occurs at or below 100 ft :

- The automatic approach should be continued with ATS engaged.

At landing :

Batch C mods incorporated : may continue automatically, monitor auto roll-out.W'lthout batch C mods : disengage AP at touchdown.

Note that compliance with Cat ll or Cat lll performance criteria has not beendemonstrated with one engine inoperative.Autoland with one engine inoperative has been demonstrated but it is not certificated.ln case of operational necessity, the automatic approach may be continued to Cat tlminima rather than divert.

30 NOV96/REV t814-O1

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AIRBUS INDUSTR/E ftAl.E/hhg & FltJht cp€,rdtbns Spport Dhf,c,a Y1,/


14.01 CAT il - CAT ilt BRIEF|NG (CONT'D)

02 - oPERAT|NG PROCEDURE (CONT'D)

H. powvcBAplNc coNptTloNs (coNTD)

c. Radio Altimeter Failure

. SINGLE

- APIFD disengages on side of {ailed rad. alt. ; valid FD can be transferred to lailedside.

- Radio heights continue to be indicated on both PFDs, lrom the good rad. alt.

- DUAL

Both AP lost ; FDs revert to basic modes (and flash for 10 sec.) ' ;Revert to CAT I minima and carry out a manual raw data approach with FPV.

d. ILS Failure . LOC or GS

1. RECEIVER

. SINGLE

- AP/FD disengages on failed side ; valid FD can be transferred.

' ILS raw data indications on associated PFD are lost but remain on ND(supplied by receiver on other side). On aircraft with Mod. 3803 ILSinlormation can be transferred ,rom the other side.

. DUAI-

- Both AP lost ; FDs revert to basic modes (and flash lor 10 sec.).

31 MAR 96/REV 17 ,c1o/3oo-6oo14{1

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A'RBUS INDUSTRIEhahhg A F@ht Oc€td/tbr'J S..ppott Dtv&ion


14.01 CAT il - CAT ilt BRIEFING (END)


H. powlcRAprNc coNDtTIONS (CONTD)

d. ILS failure - LOC or GS (end)

2. TMNSMITTER

- AP remains engaged in existing phase to enable auto GA to be initiated ; attitudeat moment of ailure is maintained :

- Affected ILS index (LOC or GS or both) removed.

- Excess deviation warning occurs (scale flashes) ;

- FD bar(s) flash for 10 sec.

NOTE : in this case there is no red LOC or GS warning flag.

e. ADC Failure

- In GS track and LAND track phases the AP/FD is not affected by ADC failure ;

- Associated ATS disengages but can be r+engaged in SPD after transfer switching tothe valid ADC ;

In case of dual ADC failure, use stand-by ASI and altimeter ; refer to Abnormalcheck-]ist.

' with Mod. 4936 - 7 - I

t. Wth 2 AP engaged, below 100' (Alert Ht.) disconnection of one AP does not resultin change of capacity on FMA ; Cat lll operation may be continued in this case.

g. No Land Track at 400 ft

lf this fauh occurs without any other failure indications, it may be due to an internalmalfunction within the FCC or in the FAlvl symbol generator. The subsequent approachmay be executed using AP or FD in LAl.lD mode to CAT I limits, but monitoring ILSraw data and disengaging at 200 ft.

3I MAF 96/REV 1714-01

14-01Page : 37

4310/300-500

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AIRBUS INDUSTRIE fiA


14.01 CAT lt - CAT ilr BRTEF|NG (CONT'D)


H. povvr{cRAprNc coNDrIloNS (coNTD)

h. AUTOLAND warning is only active below 200 ft rad. alt. with CAT ll or lll capacityavailable and at least 1 AP in LA|ID track.

Possible causes :

- excess deviation

- "AP OFF'warning

- long flare (not on ground 13.5 sec. after 50 ft rad. ah.)

- radio altimeters differ by more than 10 ft for longer than 1 sec.

- LIS function test shows loc. beam deviation.

i. ROLL-OUT" warning indicates loss of auto decrab and auto roll-out functions. Thewarning can only occur during GLIDE TMCK or LAlrlD TMCK phases.

Possible causes :

- discrepancy between runway heading and RWY CRS selected, detected at ILSreceivers ;

- difference be{ween IRS heading signals ;

- wheel speed sensor failure detected above 30 ft.

After touchdown, FMA indications reverts to LAlrlD ingead of ROLL-OUT, and yawbar does not appear.

With batch C mods. incorporated, ROLL-OUT warning is not provided.In case of rollout failure, the AP cannot be engaged in LATJD mode, or disengagesif already in LAITJD mode.

31 MAR 96/REV 1714-0't

14-01Page :38

4310/300-600

Chatvi AP45

.AIRBUS INDUSTR'E f tAlrohhg e Fligfi oEle,l',b|.l guF,!E,n DivsOn Yl



14.01 CAT ll - CAT lil BRTEFTNG (END)

02 - oPERATTNG PROCEDURE (END)

H. DOWIGRAS|NG CONDTTTONS (END)

i. No 'llafe" Green Annunciation by 30 tt R.A

In the extremely remote case of a failure of the flare function which has not beendetected during the continuous internal test process, the action would be either toimmediately initiate a go-around or to flare manually using the available externalreferences. Since there is no supervisory override facility available in the LAND TRACKphase, the lorce required to override the autopilot in pitch (the break-out threshold) isapproximately 46 kg ; in order to flare manually, the AP must there{ore be disengaged.

31 MAR 96/REV 1714{1

14-01Page :39

A3'10/300€00

Chatvi AP45

AIRBUS INDUSTREhoining e Fhght Optdtbns 9gcrllt Dtv*bn


LEFT INTENTIONALLY BLAt'lK

31 MAR 96/REV 1714{1

14-01Page :40

A310/300-600

Chatvi AP45

AIRBUS INDUSTRIEInining & Filgffi Apefotbns SJppod Divbion


1 4 . PRECISION APPROACHES

14.02 DETAILED PROGRAMME

FFS CAT ll Training Syllabus Page 03and Session Guide "

FFS CAT ll Evaluation Syllabus. Page 07and Session Guide *

* lnstructor's FCTM

31 MAR 96/REV 17't4-02

't4 - 02Page: 1

A310/300-600

Chatvi AP45

AIRBUS INDUSTR'Eftofr1fr1? &, Flight Ope|otbnss/.,/F1poil Dlvlsbn



LEFT INTENTIONALLY BLANK

31 MAR96/REV1714-O2

14-02Page:2

A3't0/300-600

Chatvi AP45

AIRBUS 'NDUSTRIEfiahhg A F@ht Operatbns Sppo/ Divlsbn

A310/300-600 FCTMCourse :Name :

FFS : CAT ll TRAININGCM

TAKE-OFF DATAINIT PAGE

CO RTE FROM/TO

i !fP91!t?9 iFLT NBR

LAT LONG

TRIP DIST

CRZ WND

ALTN

ALTN DIST

FL to ALTN

ATIS

RIA/Y: r5R

WND: VAF/4 kt

VlSl : 400 m

CEILING : 250 ft

TEMP: ZoC

DEW POINT: 1"C

Q N H : 1010 hPa/29.83 inHg

Q F E: 994 hPa/29.35 inHs

R\ /Y COND: DRY

OBSERVATION:

i 4338.1N i i 00122.1E I

COST INDEX

50

INIT NE)CT PAGEzFcclzFw

A310:24.60/0 - 94 t

24.6"/"-n72 lbA30G6fi):

23.8o/o - 1O4l23.9/"- n9 976 tb

BLOCK

26t57 200 tb

PERF PAGE310 300-600 TO. FLAPS

T.O C.G"' 250/o

FLEX

15Trainees to calculate:

1 - TAKE-OFF SPEEDS2 - FLEXTEMP

INSTRUCTOR'S NAME:

PROGRESS IS NORMAL.

NEED E)ORA

READY FOR

TRAINING

EVALUATION

INSTRUCTOB'S SIGNATURE TRA]NEE'S SIGNATURE

28 FEB 99/REV 19cAT2-1

14-02Page : 3

4310/300€00

Chatvi AP45

CAT II TRAINING

PF SESSIONNORMAL PROCEDURES

ILS APPBOACH

ONE ENGINE OUT PROCEDURE

INITIATION OF CHECK-LISTS

REJECTED TAKE-OFF

MANUAL LANDING

GENERAL PERFORMANCEFLYING ACCURACY

USE OF FLIGHT GUIDANCE SYSTEM

USE OF FD. AUTOPILOT

IFR PROCEDURES

CREW COORDINATION

GENERAL PROGRESS

GENERAL PERFORMANCE

PNF SESSIONNORMAL PROCEDURES

USE OF CHECK.LISTS

SUPPORT OF PF

CM1 INCAPACITATION

31 MAR96IREV 17cAT2-1

14-02Page : 4

A,310/300-600

Chatvi AP45

AIRBI,S tNDatSTRTE hhoining & Fluht Opeptbnssurlpot Divf,ion Vl



(1 session of 02.00 h per crew)

01 . BRIEFING TOPICS

CAT 2 and low visibility training

02. SESSION OBJECTIVE

To consolidate the CAf 2 VACBIconditions so that the crew reachlicensing purposes.

FFS CAT II TRAINING SESSION GUIDE

training with practical il lustration of low visibility flyingthe level of proficiency to pass a CAT 2 evaluation for

UJo5(5EoF'(,3trFaz

r.i .,i.. |:|t , :

03. SESSION PROFICIENCY CRITERIA

(rBD)

04. SESSION GUIDE

I ltem 1

I ltem 2

- Ensure that the trainee does not waste time in setting-up prior to start- Enter STBY HORIZON flag (no warning on ECAM or FMA, CAT 2 not

allowed). Restore.- Stress the necessity to tune and identify the appropriate NAV AIDS,

especially the ILS of the R\lf/ in use (YAW-BAR lor T/O guidance).- An appropriate take-off alternate should be inserted in the SEC F/PLAN.

- Brief the crew that visibility will be reduced to zero on the take-off run toillustrate the effectiveness of the YAW-BAR.(NOTE : YAW-BAR will appear only if the ILS is availitble for the same R\Aff

direction)- Ask the PF to continue T/O for training pruposes, usirrg the YAW-BAR only.- Frwze SIM just prior to V1, increase visibility to shour aircraft on centerline,

then continue the take-off.

- Ensure that the crew can give a concise CAT 2 approach briefing..- Stress task sharing, weather minima, crew qualification, alternate planning,

fuel requirements, aircraft and airfield servicibility, SOP, flight decklightning, etc...

- Check crew seating position- LO or MED autobrake is recommended- Check autoland limitations and OEB's.

IIIa-3(5.tro.F:o'l)Gt-az,

: , ; : .i r l

I ltem 3

I

30 NOV 96/REV 18cAT2-1tG

14-02Page: 44

A310/300-600

Chatvi AP45

A'RBUS INDUSTRIEIroining & Fltght Operafbns tuppoft Divbbn



ir.iiililiir,ii' [U',n. . : . .J_

i!,'..$'l, ' i i

troF. , ,(J.,iJ.

1,,,;fi,.r iF ',,4:

' . t , -2"

, .lJ;l ..j , r l. . . - -

"3 'tS.,::.r,fi,i,

, , , Q. 'Fo, ir:

.' fi,-,l-" 'a '=

, ' j .

i l I ,11.. . ! i$ i l

,' u , i;s1",i. ., .rjj!:5i:j:.:

tlr r:i)::,,!.i.i i:!$j

;,i ' : ;

. ; . . ' - r: . : , - . ; : .

il; t

FFS CAT il TRATNTNG SESSTON GUTDE (CONT'D)

04 - sEsstoN GUTDE (coNT'D)

I ltem 4

I ltem 5

I ltem 6

I ltem 7

- The crew must check autoland function prior to approach (CAT 3 SINGLE,cAT 3 DUAL).

- The crew must acknowledge all FMA changes.- The crew must call and acknowledge approach std. call-out.- Check that GA alt is properly set.- Freeze the approach at DH 150 and review visual segment [change RVR

s50 M (CAT 1) to RVR 350 M (CAT 2)1.- Ask crew to switch landing lights ON and OFF, to show the change in visual

clues.- Vary the flight deck lightening to il lustrate the necessity to low intensity.

- Freeze SIM at DH 100 ft and review visual segment at RVR 350 M and vert.vis. 100 ft (CAT 2 min).

- Release SIM and perform autoland.- Observe FLARE mode latest at 30 ft RA- Observe autobrake 'DECEL"

NOTE : With max reverse and selected 'LO" autobrake, DECEL may NOTappear. Reverse thrust may be applied only when nose gear is onthe ground (see OEB).

- Check autopilot roll-out mode.NOTE : During landing roll when starting manual braking, disconnect

autopilot at the same time.

- Reduce visibility to zero and insert eng failure at 100 kt (before V1).- Ensure that the PF is using YAW-BAR guidance during rejected take-off.

Insert STBY horizon when ILS established but above 1000 ft AGL.NOTE : There is NO ECAM warning and NO approach capability change on

FMA, but CAT 2 approach is NOT allowed (CAT 1 only).

30 NOV 96/REV 18cAT2-1lG

14-02Page : 48

4310/300-600

Chatvi AP45

l :t'i;l

i i;i!AIRBUS INDI'STRrc hIninng & FIUht Ope|,c/tbnsslripott Division Vl

A310/300.600 FLIGHT CREW TRAINING

.=

:lr: i t;:,j ; : : i ! . : : : t '

MANUAL

: : t . l1r

:::=':*::t : , i' : : :.,.,1:irr::j::::1ii

iii'

,,,,,,:.;

14 . PRECISION APPROACHES ! {

FFS CAT il TRATNTNG SESSTON GU|DE (END)

04 - sEssroN GUIDE (END)

I ltem 8

I ltem 9

r ltem 10

r l tem 11

I ltem 12

I ltem 13

I ltem 15

A. Insert LOC transmitter failure before OM (restore).NOTE :- AP's and FD's remain engaged in approach mode (G/S and LOC green)- LOC index is removed- LOC scale flashes ONLY if LOC transm. failure occurs when aircraft is

captured on the localizer.CAUTION : NO RED LOC WARNING

B. Insert LOC transmitter failure for the second time at 200 ft RA.- Check indications mentioned in A plus RED AUTOLAND WARNING- Crew must initate GA if visual references are not sufficient

- Insert A/THR failure at 500 ft RANOTE : A/THR is not mandatory for CNT 2; it is only recommended (Airline

pot icy).

- Ensure that crew continues the approach- Insert "ZERO RVR" and check that GA with manual thrust is initiated at DH.- Restore A/THR for next approach

- Insert eng. failure at or below 100 ft (when viusal), and illustrate single eng.capability of the autopilot (CAT 3A).

- Autoland is allowed.

- lf ATT warning is inserted :- Check that PF is ONLY using STDBY HORIZON during GA.- Attitude warning must be analysed after GA.

- Captain's (CM1) failure to respond to standard call-out is to be consideredas his incapacitation.

- Once the incapacitation has been established the CM2 must make a goaround.

- Insert engine failure at 500 ft RA.- Check that the eng failure is noticed without delay- ln this case go around must be initiated.

NOTE : Sometimes failure is noticed too late (below 100 ft) and thereforeautoland is performed.

Insert Ay'P failure at 80 ft RA, Manual landing is allowed if visual references aresufficient.

. '

|.Ilcl: -

,;rii-..-(5

' i l r

l-,1ii1,6;l t ' t . .3

;',,ffl'-3n

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F'a..-.1.:.2,r:;;;-r.-?

. : ..

- ,

t .

I t ; "" . 'Fl

. . " : t j

s0 Nov 96/REV 18cAT2-1rG

14-02Page:4C

A310/300-600

Chatvi AP45

AIRBUS INDUSTRIETloining & Flight Operotbns,!-,ppof Dir4r,bn



30 NOV 96/REV 18cAT2-1rG

14-02Page : 4D

4310/300-600

Chatvi AP45

FFS - CMCAT II TRAINING


M. REF +

INITT/O

130 FT I 1 - COCKPIT PREPAFED BY INSTRUCTOR200 M ENGINES RUNNING, FUEL FREEZE

I 2 . TAKE.OFF FOG PATCHES. FOLLOW YAW BARI 3. MDAR VECTOBS - CAT II BRIEFING

17O FT I 4-APPROACH.2APs00 M FREEZE AT 150 FT. REVIEWVISUAL SEGMENT - BELEASE130 FT T 5 . FREFZE AT lOO FT. REVIEWVISUAI- SEGMENT - RELEASE -400 M AUTOLAAID

INIT T/O I FUEL FREEZE

130 FT I 6 -TAKE-OFF- FOG PATCHES

200 M RE.JECTED TME.OFF (ONE ENGINE FAIL ABOVE 1OO KT) . Restore


130 FT r 7 . TME.OFF. RADAR VECTORS DO!\INWND

400 M STANDBY HORIZON FLAG . RESET ( ABOVE 1OOO FT)I 8 - APPROACH 2 AP. DH 1OO FT

LOSS OF LOC TMNSMITTER AT 2OO FT. AUTOLAAID WARNING . GO AROUND - RestoTe

130 FT I 9 - APPROACH 2 AP - DH 1OO FT. 1 ATHB ONLY

OM REMAINING ATHR FAILS AT 5OO FTCONTINUE TO DH - NO VISUAL - GO AROUND- Restore ATHR

130 FT I 10 - RPPROACH .2 AP - DH 1OO FT - ENGINE FAILURE BELOW lOO FT400 M LAI{D'r30 FT T 11 . APPROACH 2 AP - DH 1OO FT - CHECK ATT WARNING AT 2OO FT (OR 2 RAD ALT FAILURE)

400 M MAI{UAL GO AROUND (USING STDBY HORIZON IF NECESSARY)130 FT . 12 - APPROACH 2 AP - DH 1OO FT400 M CM1 INCAPrcITATION ABOVE DH - GO AROUND130 FT I 13 - APPROACH - 2 AP. DH 1OO FT

400 M ENG FAIL ABOVE 1OO FTGO AROUND. CLEAN UP

OFT 14. RELIGHT - APPROACH .2 AP - DH 1OO FT

OFT NO VISUAL CONTACT. GO AROUND

130 FT I 15. APPROACH - 1 AP. DH 1OO FT400 M AUTOPILOT DISCONNECT AT 80 FT - MATIUAL LA^IDING

31 MAR96/REV 17 4310/300€00cAT2-1

14-02Page : 5

Chatvi AP45

AIRBUS INDUSTRIE hholning & Flight Operofbns &rpporf Division V

A310/300-600 FCTMGourse :Name:Date :

CM

GENERAL COMMENTS


14-02Page : 6

A310/300-600

Chatvi AP45

AIRBI'S 'NDUSTR'E

hhaining A. Ftght Ope:,q,tbns fuppott DivHon Yl

A310/300-600 FCTMCourse :Name:Date :

FFS : CAT ll EVALCM

TAKE.OFF DATAINIT PAGE

CO RTE FROM/TO

i LFBO/LFBOL--------- - - - - -

GREEN aJ

FLT NBR

LAT

i +sse.rn i'

"or, '*o=*'

LONG

o0122.1E i

50

TRIP DIST

CRz WIND

ALTN

LFBD

ALTN DIST

FL to ALTN

ATIS

RWY: 15 H

WIND: VAR/4 kt

VlSl : 400 m

CEILING : 250 ft

TEMP: 29

DEW POINT: 1'C

Q N H : 1020hPa/30.12 inHg

Q F E: 1002 hPa/29.59 inHq

R\ /Y COND: DRY

OBSERVATION:

INIT NEXT PAGE I PERF PAGEzFcGlzFw | .10 300_600

A310:24.60/o-94t.

24.60/o-207 230tbA300-600:

23.8/o - 104 t23,*/"- 29 270 tb

V1

BLOCK

26t57 200lb

TO. FLAPS

T.O C.G

25o/"

FLEX

15

NOTE:

Trainees to calculate:

1 - TAKE.OFF SPEEDS2. MMTHRUST

INSTRUCTOR'S NAME:

SATISFACTORY

INSTRUCTOR'S SIGNATURE

UNSATISFACTORY

TRAINEE'S SIGNATURE

28 FEB 99/REV 19cAr2-2

14-02Page: 7

4310/300-600

Chatvi AP45

CAT II EVALUANON

PF SESSIONNORMAL PROCEDURES

ONE ENGINE OUT PROCEDURE

INITIATION OF CHECK-LISTS

MANUAL fiRUST HANDLING




IFR PROCEDURES

CREW COORDINATION

GENERAL PERFORMANCE


USE OF CHECK-LISTS

SUPPORT OF PF

[-l srrsFAcroRY

31 MAR 96/REV 17cAT2-2

14-02Page : 8

Chatvi AP45

ATRBUS /,NDU9r/R[E h ffiEtuoining & Flight qF/erdtbnsl&port Divith,n V,



FFS CAT II EVALUATION SESSION GUIDE


31 MAR96/REV17cAT2-2lG

,s10/300-600 14-02Page : 8A

Chatvi AP45

;:,r:j

; AIRBUS INDUSTRIE" hoining &. Ffgfn Opeutbns&ppof Dir4sion

A310/300.600 FLIGHT CREW TRAINING MANUAL1 4 . PRECISION APPROACHES

FFS CAT II EVALUATION SESSION GUIDE

1.2.3.



Evaluation in CAT 2 weather conditions and :

ln normal configurationWith engine failureWith autothrust failure


Demonstration of competence to operate aircraft in CAT 2 weather conditions as Captain orFirst Otficer.

03 - SESSION PROFICIENCY CRITERIA

(rBD)

ftem 3 and 4 are mandatory lor qualification and Recurrent Training (DGAC - Decision 3437\.

04. SESSION GUIDE

- Avoid using lNlT function as much as possible.- Connect the exercises with the radar vectoring.- Lead the session as close as possible to line-oriented flight philosophy.- Use headsets- Remember the importance of task sharing and good crew coordination.- Crew is assessed as Captain and First Officer.- Don't let yourself get involved in a discussion during session. Make your own judgement

and revert to your instructor role again if for example an exercise is unsatisfactorily carriedout.

31 MAR96/REV17cAT2-2tG

14-02Page : 88

4310/300-600

Chatvi AP45

FFS. CMCAT II EVALUATION


M. REF T

INIT T/O

130 FT 1 - COCKPIT PREPARED BY INSTRUCTORRVR 2OO ENGINES RUNNING. FUEL FREEZE

2 - TME-OFF - MDAR VECTORS - BRIEF|NG (CAT il)

3 - APPROACH - 2 AP - DH 1OO FT. NO VISUAL CONTACTGO AROUND - MDAR VECTORS. DOIVNIWND

130 FT 4 - APPROACH - 2 AP . DH 1OO FT-RVR 350 AUTOLAND

5 - TAKE.OFF - FOG PATCHES

6 - APPROACH .2 AP . DH lOO FTENG FAIL ABOVE 2OO FTGO AROUND

130 FT 7 - APPROACH .2 AP - DH 1OO FT. 1 ATHR ONLYRVR 350 REMAINING ATHR FAIL AT 5OO FT

AUTOLAND

31 MAR 96/REV 17cNf2-2

14-02Page: 9

A310/300-600

Chatvi AP45

AIRBUS INDUSTRIE hltokng & Floht Operutbns Wpot Divbion Yl

A310/300-600 FCTMGourse :Name :Date :

CM

GENERAL COMMENTS

28 FEB 99/REV 19 4310/300-600cAT2-2

14-02Page: 10

Chatvi AP45

AIRBUS INDUSTRIE hInning & Fligu Operofbns grppof Division V



14.03 DETAILED PROGRAMME

FFS CAT l l l Training Syllabus ... Page 03and Session Guide *

FFS CAT lll Evaluation Syllabus Page 07and Session Guide .

* lnstructor's FCTM

31 MAR96/REV17 A310/300-60014-03

14-03Page: 1

Chatvi AP45

AIRBUS 'NDUSTRIEkainng & Flight Operdlbns Support Divirion



31 MAR 96/REV 1714-03

14-03Page:2

A310/300-600

Chatvi AP45

AIRBI'S INDI'STRE TAl'oinhg & Floht Opeotbns s@ipoi Divbbn V

A310/300-600 FCTMCourse :Name:

FFS : CAT lll TRAININGCM

TAKE-OFF DATA

LAT LONG;;i 4338.1N i i 00122.1E i

CO RTE FHOM/TO

PAGE

ALTN/CO RTE

FLT NBR

CRZ WND

TRIP DIST

FL to ALTN

ALTN DIST

ALTN

Q N H : 1020 hPa/ inHs

VlSl : RVB 125 m

WND: VAN4kt

ATIS

R\Aff: 15 R

CEILING : 25 ft

DEW POINT: 8'C

TEMP:

COST INDEX

CRz FUTEMP TROPOf-------:T- ----1

I FL 50/ -59'c ! i -t - - - -L-____- i L______-_____

50QFE: 1002hPa/ inHg

OBSERVATION:

R\Aff COND :

IN]T NE)ff PAGEZFCGIZFW

A310:24,60/o - 941

24.670-207 230tbA300-600 :

23.8o/o - 104 t23.8/"-29n6b

BLOCK

26r57 200 lb

PERF PAGE310 300-600

TO. FLAPS

T.O C.G

TOGA

15/0

25V"

NOTE:

T/O SPEEDS

INSTRUCTOR'S NAME :

t lPROGRESS IS NORMA1.,.. . . . . . . . . . . . . .

NEED E)CTRA TRAINING

READY FOR EVALUAT]ON

INSTRUCTOR'S SIGNATURE TRAINEE'S SIGNATURE

14-03Page : 3

28 FEB 99/REV 19GATS-1

A310/30G600

Chatvi AP45

CAT III TRAINING

PF SESSIONCAT III BRIEFING

INSTRUMENT FAILURE

ENGINE FAILURE

REJECTED TAKE-OFF



USE OF FD - AUTOPILOT

IFR PROCEDURES

CREW COORDINATION

GENERAL PROGRESS

GENERAL PERFORMANCE


USE OF CHECK-LISTS

SUPPORT OF PF

CM1 INCAPACITATION

31 MAR 96iREV 17cAT3-1

14-03Page : 4

4310/300-600

Chatvi AP45

AIRBUS INDUSTRIETroinkg & Fhght Operatbns &.rppod Dlvlston

A310/300-600 FLIGHT CREW TRAINING MANUAL1 4 . PRECISION APPROACHES



CAT 3 low visibility training.


Complete CAT 3 training so that the crewCAT lll evaluation for licencing purposes.

03. SESSION PROFICIENCY CRITERIA

(TBD)

FFS CAT III TRAINING SESSION GUIDE

reach the level of proficiency to pass

fi'g

r . i l$, .3.

31 MAR96/REV17cAT3-1rG

14-03Page: 4A

4310/300-600

Chatvi AP45

' : - ' ,' i

AIRBUS INDUSTRIE TAlroining & Flght Ope|iotbnss.r€pot Di*An V/


1 4 . PRECISION APPROACHES

, i . . . . -

04. SESSION GUIDE

I ltem 1

I ltem 2

I ltem 3

I ltem B

I l tem 12

FFS CAT ilr TRATNTNG SESSTON GU|DE (END)

- Ensure that the trainee does not waste time in setting-up prior to start- Enter STBY HORIZON flag (no warning on ECAM or FMA, CAT 2 not

allowed). Restore.- Stress the necessity to tune and identify the appropriate NAV AIDS,

especially the ILS of the R\AA/ in use (YAW-BAR for T/O guidance).- An appropriate take-off alternate should be inserted in the SEC F/PLAN.

- Brief the crew that visibility will be reduced to zero on the take-off run toillustrate the effectiveness of the YAW-BAR.(NOTE : YAW-BAR will appear only if the ILS is available for the same R\Aff

direction)- Ask the PF to continue T/O for training pruposes, using the YAW-BAR only.- Freeze SIM just prior to V1, increase visibility to show aircraft on centerline,

then continue the take-off.

- Ensure that the crew can give a concise CAT 3 approach briefing..- Stress task sharing, weather minima, crew qualification, alternate planning,

fuel requirements, aircraft and airfield servicibility, SOP, flight deckl ight ing, etc. . .

- Check crew seating position- LO or MED autobrake is recommended- Check autoland limitations and OEB's.

- Reduce visibility to zero and insert eng failure at 100 KT (before V1).- Ensure that PF is using YAW-BAR guidance during rejected take-off.

- With an ILS CAT 2, CAT 2 minimums only are available.In France, some airports are allowed to use CAT 3 minimums withDH 50 FT.

lU., Cl . ::.:.5,,, - r iO'

' i i,.i$,oF

, ( )rl..lI'':', !c.,

rF"{l

ii=j., . .

, . " . . . ; . -' . r , t

::lir,,ii iiii:i;iiii tr:: . t 'J l

! i : ;

: ; i r : . ;

- : ' . .i [ . 1 . : ]

;ili ,;i;vF.rqiti;!1^r , . . :

30 NOV 96/REV 18cAT3-1lG

14-03Page : 48

A310/300-600

Chatvi AP45

FFS. CM

CAT III TRAINING(1 session of 02.00 h per crew)

M. REF T

I INIT T/O FUEL FREEZE

I 1 . COCKPIT PREPARED BY INSTRUCTOR. CAT IIIT/O BRIEFINGENGINES RUNNING

RVR rsc T 2 -TME.OFF

T 3. HOLDING CAT II I BRIEFING

RVR zoo 4. APPROACH CAT III DUALRVR rzs REVIEWVISUAL SEGMENT

60 FT DH 50 FT. FREEZE AT 50 FT - RVR 2OO M30 FT DH 20 FT - FREEZE AT 20 FT. RVR I25 M

AUTOLAAID

RVR 150 5 - TME.OFF - FOG PATCHES FOLLOWYAWBAR

30 FT 6. RPPROACH ABOVE 1OOO FTRVR 125 REVIEW LOSS OF ILS TMNSMITTER

REVIEW LOSS OF ILS RECEIVERSREVIEW LOSS OF RADIO ALTIMETERREVIEW LOSS OF STANDBY HORIZONREVIEW INSTRUMENT FAILURES

7 - AUTOLAT{D

30 FTRVR 150 T 8 - TME-OFF FOG PATCHES

ENGINE FAILURE ABOVE 1OO KTRE'ECTED TME.OFF

RVR 150 9.TME.OFF

30 FT 10 - APPROACH CAT III DUAL DH 20 FTRVR 125 LOSS OF LOC TMNSMITTER AT 2OO - AUTOLAf{D WARNING

GO AROUND - Restore

30 FT 11 . APPROACH CAT III DUAL DH 20 FT

RVR rzs CHECK ATT WARNING AT 1OOGO AROUND USING STAAIDBY HORIZON

30 FT I 12 - APPHOACH CAT IIIDUAL. ILS PERFORMANCE IIRVR 125 ENG FAIL AT 2OO FT. GO AROUND - CLEAI UP

60 FT 13. APPROACH CAT III SINGLE DH 50 FT

150 M AUTOPILOT DISCONNECT AT 50 FT. GO AROUND . Restore

lso M 14 - APPROACH CAT III DUAL. CMl INCAPACITATION - CM2 GO AROUND

150 M 15 - APPROACH CAT III DUAL DH 50 FT

150 M BOTH MDIO ALTIMETER FAIL AT 1OO FT. GO AROUND. RestoTe

30 FT 16 - APPROACH CAT III DUAL DH 20 FT - ENG FAiL BELOW 1OO FT

125 M AUTOLAID

31 MAR96/REV17 4310/300-600cAT3-1

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AIRBUS 'NDUSTRIE

TAlruinng & Flight OpeEtbns Srpporf Dhli bn V


CM

GENERAL COMMENTS


14-03Page : 6

p|310/300-600

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AIRBUS 'NDUSTRIE

hinining & Flilht Opeotbnsgr|pot Division V

A310/300-600 FCTMCourse :Name :Date :

FFS : CAT lll EVALCM

TAKE-OFF DATAINIT PAGE

CO RTE FROMiTO

LFBO/LFBO

ALTN/CO RTE

FLT NBR

LAT

i +gge.rNl'-aos-ili.i;ii__I9I9_oo122.1E

I r -: '! i

J

CRz FUTEMP Il_ol9JL

50

TR]P DIST

CRZ WND

ALTN

ALTN DIST

FL to ALTN

ATIS

R\MY: 1sB

WND: VAR/4 Kt

VISI RVFI 125 m

CEILING:

TEMP:

25 tl

DEW POINT: 8€

Q N H : 1020 hPa/29.83 inHg

Q F E: lOO4hPa/24.41 inHs

R\ /Y COND : DRY

OBSERVATION

INIT NE)CT PAGEZFCG/ZF'AI

A310 :24.60/0 - 94 t

24.60/o-207 230|/bA30G600:

23-T/" - 1Ol t23.7/0- m 270 tb

BLOCK

26ts7 200 tb

PERF PAGE310 300-600

TO. FLAPS

T.O C.G

TOGA

15/0

25o/"

NOTE:

T/O SPEEDS.

INSAUCTOR'S NAME:

SATISFACTORY

INSTRUCTOB'S SIGNATURE

UNSATISFACTORY

r--:_lTRAINEE'S SIGNATURE

28 FEB 99/REV 19CATS-2

14-03Page:7

A310/300-600

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CAT III EVAL

PF SESSIONCAT II I BRIEFING

ONE ENGNINE OUT PROCEDURE

IN]TIATION OF CHECK-LISTS

MANUAL ROLL.OUT




IFR PROCEDURES

CREW COORDINATION

GENEML PERFORMANCE


USE OF CHECK-LISTS

SUPPORTOF PF

I-_l smsFAcroRY

31 MAR 96/REV 17cAT3-2

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4310/300-600

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AIRBUS INDUSTRIEIroining & Fhght Opetoltbnss.r.r|poft Dvision V

A310/300.600 FLIGHT CREW TRAINING MANUAL1 4 . PRECISION APPROACHES

CAT III EVALUATION SESSION GUIDE

LEFT INTENTIONALLY

31 MAR 96/REV 17cAT3-2tG

A310/300-600 14-03Page : 8A

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A'RBUS INDUSTRIE


CAT III EVALUANON SESSION GUIDE(1 session of 01.00 h per crew)

01 - BRIEFING TOPICS

CAT 3 low visibility training.


Demonstration of competence to operate aircraft in CAT 3 operations.

03 - SESSION PROFICIENCY CRITERIA

Items 3 and 5 only are mandatory for qualification and Recurrenl Training(DGAC - Decision 3437\.

31 MAR 96/REV 17cAT3-2tG

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FFS. CM

CAT III EVALUATION(1 session of 01.00 h per crew)

M. REF+


1 . COCKPIT PREPARED BY INSTRUCTORENGINES RUNNING

30 FT 2 - TME-OFF. HOLDING CAT III BRIEFING

125 MZERO 3 - APPROACH - 2 AP. DH 50 FT - NO VISUAL CONTACT

TFRO GO AROUND - RADAR VECTORS

30 FT 4 - APPROACH .2 AP. NO DH125 M AUTOLAND

ZERO 5 . APPROACH .2 AP - DH 50 FTOR GO AROUND

AIITOIANf)60 Fr 6-APPROACH -2pP- DHsOFT125 M VISUAL CONTACT . AUTOLAND

ROLL OUT FAULT

31 MAR 96/REV 17 4310/300600cAT3-2

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AIRBUS INDUSTRIE (Airoining & Fligft Qpe',d,bns S4p4tt DivisAn V/


CM

GENERAL COMMENTS

28 FEB 99/REV 19cATs-2

14-03Page: ' t0

4310/300€00

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fctm chapter14 precision approaches

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