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21/04/23 121/04/23 H.M.E. 1
• 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
D C21/04/23 44H.M.E.
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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