Aircraft Performance Data: Regulations and Tables
Regulations
Leg 15: (B) Leg 15 y Fig 117: (B) Leg 15 y Fig 185A: (A) Leg 15 y Fig 205: (C) Leg 15 y Fig 215: (C) Fig 115, 116, 117, 118, 118A, 118B, 118C: (B) Fig 118A: (B) Fig 190, 195, 195A, 196, 196A: (A) Fig 206: (B) Fig 214 y 182A: 321/42 Fig 214 y 183 y 183A: (B)
Equipment
Fig 112: (C) Fig 125: Wind 050°(B) Ilust 4(B) TO the station(A) from the station(B) Fig 129: (A) Fig 130: A(B) B(C) C(B) D(B) Fig 131: A(B) B(B) C(A) D(A) E(B) F(C) Fig 135 y 138: (B) Fig 136 y 138: (C) Fig 137 y 138: (A) Fig 139: 165(B) 4°(C) 174(A) 5.0NM(A) R-345(C) 354(C) Fig 140 y 141: A(A) B(B) C(C) D(C) E(B) F(A) G(B) H(B) I(C) Fig 142 y 143: A(A) B(C) C(C) D(C) E(B) F(C) Fig 156: (B) Fig 157: (C) Fig 223: (C) Fig 224: (C) Fig 225: (A) Fig 226: (C) Fig 227: (B) Fig 228: (C) Fig 241:(A) Fig 242: (A)
Calculating “V” Speeds
Fig 45, 46 y 47: A1(A) A2(C) A3(A) A4(B) A5(B) Fig 53, 54 y 55: R1(A) R2(C) R3(B) R4(B) R5(A)
Fig 81, 82 y 83: G1(B) G2(C) G3(A) G4(C) G5(B) Fig 237 y 238:(A)
Calculating Takeoff Power (EPR)
Fig 53, 54 y 55: R1(C) R2(A) R3(C) R4(B) R5(A) Fig 81, 82 y 83: G1(A) G2(C) G3(B) G4(A) G5(C)
Climb Performance
Fig 48, 49 y 50 en route: W1(A) W2(C) W3(A) W4(B) W5(C) Fig 48, 49 y 50 TOC: W1(B) W2(C) W3(B) W4(B) W5(A)
Fig 56, 57 y 58 en route: V1(A) V2(C) V3(B) V4(A) V5(C) Fig 56, 57 y 58 TOC & BURN : V1(C) V2(A) V3(B) V4(A) V5(A)
Fig 59 y 60: T1(A) T2(C) T3(C) T4(C) T5(B) Fig 231:(A) Fig 235 y 236: (C)
Landing Performance Tables and Graphs
Fig 73 y 75: L1(B) L2(C) L3(A) L4(A) L5(A) Fig 73, 74 y 75: L1(A) L2(B) L3(B) L4(C) L5(C) Fig 88: 114,000(C) 118,000(B) 5,400FT DRY(B) Fig 88 y 89:(B) Fig 89: 50FT OBSTACLE(C) 122,000(B) Fig 90: 5900FT(C) 134,000(A) 5200FT(B) 125,000(C) Fig 91: 119,000(B) 122,000(A) 140,000(C) 126,000(A) Fig 91 y 92: 140,000(B) Fig 92: 140,000(C) Vref+30(B) 172KTS(B) 162KTS(B) 145KTS(B) 160KTS(A)
Fig 93: 110,000(A) Vref+20(B) 118KTS(B) 152KTS(A)
Miscellaneous Performance
Fig 63 y 64: Q1(C) Q2(B) Q3(C) Q4(A) Q5(A) Fig 68 y 69 IAS: O1(C) O2(B) O3(B) O4(A) O5(C)
Fig 68 y 69 FUEL: O1(A) O2(C) O3(A) O4(C) O5(C) Fig 84 y 85 IAS: H1(A) H2(C) H3(B) H4(B) H5(C)
Fig 84 y 85 FUEL: H1(C) H2(A) H3(B) H4(A) H5(C) Fig 86 y 87: S1(B) S2(B) S3(A) S4(B) S5(A)
Engine-Out Procedures
Fig 70: 144,500(B) 25,000(C) 151,500(C) 16,000(A) Fig 71 y 72: D1(A) D2(B) D3(C) D4(C) D5(B)
Flight Planning Graphs and Tables
Fig 51 y 52 TIME: L1(B) L2(B) L3(B) L4(A) L5(A) Fig 51 y 52 WEIGHT: L1(C) L2(B) L3(A) L4(A) L5(B)
Fig 61 y 62 TIME: X1(C) X2(B) X3(C) X4(B) X5(A) Fig 61 y 62 FUEL: X1(B) X2(C) X3(B) X4(A) X5(C)
Fig 66 y 67 TIME: Z1(B) Z2(C) Z3(B) Z4(B) Z5(A) Fig 66 y 67 FUEL: Z1(A) Z2(A) Z3(B) Z4(C) Z5(C)
Typical Flight Logs, TAS Mach, Specific Range
Fig 94, 95 y 96: ETE Buffalo Intl(A) FUEL Buffalo Intl(A) VORTAC 42(C) Fig 98, 99, 100 Y 102: ETE DFW to IAH(B) FUEL DFW to IAH(B) CUGAR, 31(B) CUGAR,29(A) Figure 103: TAS(B) Fig 103, 104, 105 y 106: Use 13°E(B) Los Angeles(B) Fig 107, 115, 116, 117, 118 y 118C: ETE .78Mach(A) ETE .80Mach(C) ETE .82Mach(B) Figure 115, 116 y 117: TRM VORTAC(B) Fig 115, 116, 117, 118 y 118C: FUEL .78Mach(B) ARLIN(B) Fuel .80Mach(B) FUEL .82Mach(B) Fig 115, 116, 117 y 118C: IPL VORTAC(C) Fig 119, 120, 121 y 122: ETE ORD .78Mach(C) FUEL ORD .78Mach(B) .78Mach(A) ETE ORD .80Mach(B) FUEL .80Mach(C) Fig 158, 159, 160 y 160A: ENROUTE N711JB(C) Fig 158, 159, 160 y 160A y 161: FUEL N711JB(B) Fig 168, 169, 169A, 171 y 172: ETE Buffalo Intl(B) FUEL Buffalo Intl(A) Fig 168, 171, 172 y 173: PMM(C)
Fig 179, 180A, 181 y 182: EAB 90(C) Fig 179, 180, 181, 182 y 182A: EAB 90(A) Fig 179, 180, 181, 182 y 183: EAB90(B) SWL-SIE ETE(A) Fig 182, 214, 216, 216A, 217 y 218: ENROUTE PHL for TNA 90(B) Fig 214, 216, 216A, 217 y 218: Taxi at BDL(B) FUEL PHL for TNA 90(C)
Fig 185A, 202, 203, 203A, 204, 205A, 206: FUEL LAS-SFO(B) ETE LAS-SFO(C) Fig 190, 191, 192, 193, 193A, 194, 195, 195A: DEN for PIL 10(A) PIL 10 at MSP(A) Fig 202: Prefix B(B) “/I” Indicate(B) Fig 214: MD90(A)