1. PERFORMANCE DE EQUIPO B-767-300
PERFORMANCE B-767/300
CURSO DE REFRESCO
PERFORMANCE DE EQUIPO B
Instructor : Hugo Montes E.
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2. DIAPOSITIVAS PRESENTADAS A BASE: MOTORES : G/E CF6-80C2B6F
PERFORMANCE B-767/300
DIAPOSITIVAS PRESENTADAS A BASE:
MOTORES : G/E CF6-80C2B6F
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3. QRH - OPERATIONS INFORMATION - OI 1.1
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4. 2 + 1 = 3 KTS
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5. CLEARWAY MINUS STOPWAY
SXXX
FIELD LENGTH (FT)
CLEARWAY…… FT.
STOPWAY …… FT.
NORMAL V1 …. 140 KIAS
CLEARWAY MINUS STOPWAY
800 FT FT =
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7. SPIM RWY 15 A/C OFF T° 30° C WIND CALM
STANDING WATER 6mm.
FCOM VOL PERFORMANCE INFLIGHT PI.10.7
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9. SPIM RWY 15 A/C OFF T° 30° C WIND CALM
STANDING WATER 6mm. =
FCOM VOL PERFORMANCE INFLIGHT PI.10.7
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10. QRH - OPERATIONS INFORMATION - OI 1.1
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11. V1 = 154-17 = 137kts VR = 160kts V2 = 166kts . Maximum Reverse Thrust
Revisar Tabla a usar
No Reverse Thrust
VER COMPARACION CON OPT.
V1 = = kts
VR = kts
V2 = kts
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12. HACER COMPARACIÒN CON OPT. DATOS: MATRICULA CC-CZW-W
SPIM - RWY T 30G C - WIND CALM
QNH A/C OFF FLAPS 5 STANDING WATER 6 m.m.
. ANTI/ICE OFF C.G STD
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13. FCOM VOL 1 - PERFORMANCE INFLIGHT -- PI.10.7
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14. FCOM VOL.1 PI 10.10
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15. 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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16. FCOM VOL. 1 PI 10.11
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18. FCOM VOL 1 PI 11.1
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20. QRH - PERFORMANCE INFLIGHT PI-QRH.10.1
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21. QRH - PERFORMANCE INFLIGHT PI-QRH.10.1
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22. QRH - PERFORMANCE INFLIGHT PI-QRH.10.1
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23. FCOM VOL. 1 PERFORMANCE INFLIGHT ALL ENGINES PI.11.1
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24. FCOM VOL. 1 PERFORMANCE INFLIGHT ALL ENGINES PI.11.3
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25. FCOM VOL. 1 PERFORMANCE INFLIGHT ALL ENGINES PI.16.6
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26. FCOM VOL. 1 PERFORMANCE INFLIGHT ALL ENGINES PI.11.5
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27. FCOM VOL. 1 PERFORMANCE INFLIGHT ALL ENGINES PI.16.6
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28. BRAKING CONF. AUTOBRAKE 3
SPIM TEMPERATURE 30° C
HEADWIND KTS
LANDING WEIGHT 140,000 KGS.
VREF KTS
BRAKING CONF. AUTOBRAKE 3
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31. ANTI-SKID OFF (FLAPS 30°)
SPIM TEMP. 30° C
HEADWIND KTS
LANDING WEIGHT 140,000 KGS.
VREF KTS NO REVERSES
ANTI-SKID OFF (FLAPS 30°)
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33. SPIM MEDIUM REPORTED BRAKING ACTI. HEADWIND……………………………. 20 KTS
QRH-PERFORMANCE INFLIGHT- ADVISORY INFORMATION PI-QRH.11.5
SPIM MEDIUM REPORTED BRAKING ACTI.
HEADWIND……………………………. 20 KTS
LANDING WEIGHT ……………….. 140,000 KGS.
VREF30 … KTS TEMP….. 30° C
ANTI-SKID OFF (FLAPS 30°)
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35. PI- QRH- 13.1
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36. PERFORMANCE INFLIGHT- QRH / ADVISORY INFORMATION PI-QRH.11.7
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37. PERFORMANCE INFLIGHT- QRH / ADVISORY INFORMATION PI-QRH.11.7 / 11.8
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38. PERFORMANCE INFLIGHT- QRH ENGINE INOP. PI-QRH. 12.1 / TEXTO PI-QRH.13.3
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40. PERFORMANCE INFLIGHT- QRH ENGINE INOP. PI-QRH. 12.6
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41. PERFORMANCE INFLIGHT- QRH ENGINE INOP. PI-QRH. 12.5
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42. DRIFTDOWN SPEED / LEVEL OFF ALTITUDE
OPTIM. DRIFTDOWN
SPEED
LEVEL OFF
M.C.T.
M.C.T.
L.R.C.
Engine INOP
.78/290/250 B A
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43. PERFORMANCE INFLIGHT- QRH ENGINE INOP. PI-QRH. 12.7
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44. LONG RANGE CRUISE DIVERSION FUEL AND TIME
LEVEL OFF
L.R.C.
Engine INOP
.78/290/250
.78/290/250 B D C A
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45. LONG RANGE CRUISE DIVERSION FUEL AND TIME.
PERFORMANCE B-767/300
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 INFLIGHT- QRH ENGINE INOP. PI-QRH TEXT.
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52. GEAR DOWN/ENGINE INOP.
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54. SPIM A/C 0N RWY. 15 / T° 26° C / WIND CALM ANTI-SKID INOPERATIVE
FCOM VOL. 1 PERFORMANCE INFLIGHT - TEXT PI.16.4
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56. 188,300 kgs. -
22,700 kgs.
165,600 kgs.
FCOM VOL. 1 PERFORMANCE INFLIGHT - TEXT PI.16.4
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57. V1….. 158 - 31 = 127 Kts. Vr…………………………158 Kts. V2……………… ………..163 Kts.
188,300 kgs. -
22,700 kgs.
165,600 kgs.
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59. FCOM VOL. 1 PERFORMANCE INFLIGHT - TEXT PI.16.4
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63. HACER COMPARACIÒN CON OPT. DATOS: MATRICULA CC-CZW-W
SPIM - RWY T 30G C - WIND CALM
QNH A/C OFF FLAPS 5
. ANTI/ICE OFF C.G STD
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76. PERFORMANCE B-767/300
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:
STANDARD ..  153,400  KGS.  V1  152  /  VR  153   / V2   158.
2. ALTERNO  ,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).
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77. “A”
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78. MÁXIMA TEMPERATURA ASUMIDA 50° C
PESO ACTUAL PARA T.O
160,000 KGS.
MÁXIMA TEMPERATURA ASUMIDA 50° C
V1 =
VR =
V2 =
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79. MÁXIMA TEMPERATURA ASUMIDA 54° C
PESO ACTUAL PARA T.O
160,000 KGS.
MÁXIMA TEMPERATURA ASUMIDA 54° C
V1 =
VR =
V2 =
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82. MUCHAS GRACIAS . Hugo Montes Espinoza PERFORMANCE B-767/300 15/04/2017
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