10/05/20151 h.m.e.1 curso de refresco performance de equipo b-767-300 instructor : hugo montes e....

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• CURSO DE REFRESCO

PERFORMANCE DE EQUIPO B-767-300

• Instructor : Hugo Montes E.

PERFORMANCE B-767/300

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• DIAPOSITIVAS PRESENTADAS A BASE:

• MOTORES : G/E CF6-80C2B6F

PERFORMANCE B-767/300

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2 + 1 = 3 KTS

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SXXX FIELD LENGTH (FT) 12000

CLEARWAY……. 1200 FT.STOPWAY …… 1000 FT.NORMAL V1 …. 140 KIAS

CLEARWAY MINUS STOPWAY800 FT. - 1000 FT = - 200

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SPIM RWY 15 A/C OFF T° 30° C WIND CALMSTANDING WATER 6mm.

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SPIM RWY 15 A/C OFF T° 30° C WIND CALMSTANDING WATER 6mm.

189.4 - 22.3 = 167.1

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Maximum Reverse Thrust

No Reverse Thrust

Revisar Tabla a usar

V1 = 154-17 = 137ktsVR = 160kts

V2 = 166kts .

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• HACER COMPARACIÒN CON OPT.

• DATOS: MATRICULA CC-CZW-W SPIM - RWY 15- T 30G C - WIND CALM QNH 29.94 A/C OFF - FLAPS 5

STANDING WATER 6 m.m.. ANTI/ICE OFF C.G STD

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V1 (MCG) LIMIT WEIGHT .-

Is the maximun weight at which the airplane can accelerate to V1(MCG) speed and

still stop within the field lenght available for the reported braking action.

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SPIM TEMPERATURE 30° C HEADWIND 20 KTSLANDING WEIGHT 140,000 KGS.VREF 30 +10 KTSBRAKING CONF. AUTOBRAKE 3

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SPIM TEMP. 30° C HEADWIND 20 KTSLANDING WEIGHT 140,000 KGS.VREF +10 KTS - NO REVERSESANTI-SKID OFF (FLAPS 30°)

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SPIM MEDIUM REPORTED BRAKING ACTI.HEADWIND……………………………. 20 KTSLANDING WEIGHT ……………….. 140,000 KGS.VREF30 … +10 KTS TEMP….. 30° C ANTI-SKID OFF (FLAPS 30°)

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M.C.T.

M.C.T.

L.R.C.Engine INOP

.78/290/250

LEVEL OFF

OPTIM. DRIFTDOWNSPEED

DRIFTDOWN SPEED / LEVEL OFF ALTITUDE

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L.R.C.Engine INOP

.78/290/250

LONG RANGE CRUISE DIVERSION FUEL AND TIME

.78/

290/

250

LEVEL OFF

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LONG RANGE CRUISE DIVERSION FUEL AND TIME.

• Tables are provided for crews to determine the fuel and time required to proceed to an alternate airfield with one engine inoperative. The data is based on single engine Long Range Cruise speed and .78/290/250 descent.

Enter with Air Distance as determined from the Ground to Air Miles Conversion table and read Fuel and Time required at

the cruise pressure altitude. Adjust the fuel obtained for deviation from the reference weight at checkpoint as

required by entering the Fuel Required Adjustment table with the fuel required for the reference weight and the actual

weight at checkpoint. Read fuel and time required for the actual weight.

PERFORMANCE B-767/300

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GEAR DOWN/ENGINE INOP.

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SPIM A/C 0N RWY. 15 / T° 26° C / WIND CALMANTI-SKID INOPERATIVE

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188,300 kgs. - 22,700 kgs. 165,600 kgs.

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V1….. 158 - 31 = 127 Kts.Vr…………………………158 Kts.V2……………… ………..163 Kts.

188,300 kgs. - 22,700 kgs. 165,600 kgs.

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• HACER COMPARACIÒN CON OPT.

• DATOS: MATRICULA CC-CZW-W SPIM - RWY 15- T 30G C - WIND CALM QNH 29.94 A/C OFF - FLAPS 5 . ANTI/ICE OFF C.G STD

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• COMO PODRÁN APRECIAR EN LOS ANALISIS DE PISTA DE MEJICO POR EJEMPLO POR LA PISTA 05L CON 20° DE OAT FLAPS 5 DA LOS SIGUIENTES PESOS Y VELOCIDADES:

1. STANDARD ..    153,400    KGS.       V1  152  /  VR  153   / V2   158.

2.  ALTERNO  1..    155,500    KGS.       V1  151  /  VR  152  /  V2  156.  3.  ALTERNO  2 ..   156,200    KGS.      V1  150   / VR  151  /  V2   156.

• ASIMISMO ESTOS C.G AUTORIZADOS CORRESPONDEN A LIMITES DELANTEROS DE 20% MAC (ALT. 1 FWD CG LIMIT FOR T.O), O DEL 25% MAC ( ALT. 2 FWD CG LIMIT FOR T.O).

PERFORMANCE B-767/300

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“A”

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PESO ACTUAL PARA T.O

160,000 KGS.

V1 = 156VR = 156V2 = 161

MÁXIMA TEMPERATURA ASUMIDA 50° C

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PESO ACTUAL PARA T.O160,000 KGS.

V1 = 152VR = 156V2 = 161

MÁXIMA TEMPERATURA ASUMIDA 54° C

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MUCHAS GRACIAS .

Hugo Montes Espinoza

PERFORMANCE B-767/300