IFR VFR - MultiMania

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16.7 W & B Empty Weight Dry Ewdry (ACFT + STD & Special Equipment) + unusable fuel/oil + hydraulic fluid + de-icing Empty Weight EW + removable equipment (kitchen kit,…) Basic Empty Weight BEW (CofA) + crew weight + crew luggage weight + lunch Dry Operating Weight DOW (=APS) + traffic (pay)load (passengers, mail, cargo) + reserve fuel + Trip Fuel (+ Extra Fuel) Zero Fuel Weight ZFW Landing Weight LAW minimum* T-O Weight TOW + Taxi Fuel (+/-200kg) (Start, Taxi, RunUp, APU ops.) Taxi Weight TAW or Ramp Weight RW or All Up Weight AUW Reserve Fuel= Holding Fuel + Alternate Fuel + Contingency MinTOF= Reserve Fuel + Trip Fuel TOF= MinTOF (+ Extra Fuel) Block Fuel= TOF + Taxi Fuel ZFW + Block Fuel = TAW = RW = AUW ZFW + TOF = TOW +Take Off Fuel (TOF) Operating Weight OW + traffic (pay)load RMK/ Regulated TOW= the lowest of ‘Perfo Limited TOW’ & ‘Structural Limited TOW’. * LAW= TOW – Used Fuel (Rwy, MTO,…) - 28 -
16.8 SPEEDS 16.8.1 Definitions I C E - T IAS CAS (RAS) EAS* - TAS Pitot Indication Corrected for Instrument Error IAS Corrected for Position Error CAS Corrected for Compressibility Error. *EAS: at High Speeds Only: M.4+, 300kts+ An approx. of EAS can be made by a Corrected RAS which is the EAS at SL (cf. Aristo) 16.8.2 Stalling Speeds (CAS) VS Stalling Speed. The greater of: • CASMIN at stall (or at min. steady flight & stick full back) • 94%.VS1G (α = αCRIT) VS1G One G Stall. CASMIN at which ACFT’s Lift still equal Weight (and α = αMAX) VMS1 The Minimum Speed in the Stall*, for a specified configuration. VS1 VSO - EAS Corrected for Density Error The Stalling Speed*. Just after VMS1, for the configuration under consideration. The Stalling Speed* in Landing configuration (Flaps+Undercarriage). *(or min. steady flight, if no stall) 16.8.3 TO Speeds (CAS) Take Off speeds are determined by Flaps Setting, Density and AUW SPEED Definition RMK & Specifications V MCG V MCA V EF Min. Contr. Speed on the GND TO enabled & safely continued! Min. Contr. Speed on the AIR (TO config) Engine Failure Speed 1 # out No use of nose wheel steering! 30ft laterally max. 1 # out Straight flight can be made (5° bank & 20° HDG max.) Rudder Force: 150lbs max. Speed at witch # is assumed to fail Alti or T ⇑ -> V MCG ⇓ V MCG ≤ V MCA Alti or T ⇑ -> V MCA ⇓ VMCA≤1.2.V S V MCG ≤ V EF ≤ V 1 V GO Lowest V 1 Continued TO possible within TODA V 1 Take-Off Decision Speed f( field length, ACFT config, AUW) TORR≤TORA;TODR≤TODA;ASDR≤ASDA V 1 ≥ V EF + ‘2 sec’ V MCG ≤ V 1≤ V R & V MBE V STOP Highest V 1 Interrupted TO possible within ASDA V R Rotation Speed All# || 1# out f( flaps settings, PA, T, AUW) V MU Minimum Unstick Speed= Lowest V LOF Under any conditions V LOF V MBE V 2 Lift Off Speed (Unstick Speed) Max.Breake Energy Speed Free Air Safety Speed reached at SH with 1#out Main Gear Leaves the GND f(flaps setting, AUW) Full stop within brakes capabilities 450° -> 500°C max. = Lowest safe climbing speed f(flaps setting, PA, T, AUW) Alti or T ⇑ ->V R ⇑ (car + de thrust) V R ≥ 1,05. V MCA V R ≥ V 1 V R ≥ Speed to reach V 2 at SH VR ≥ Speed to ensure V LOF V LOF ≥ 1,1.V MU (booth #)… 1.08 VLOF ≥ 1,05.V MU (1# out)… 1,04 V1 ≤ VMBE otherwise TOW must ⇓ Alti or T ⇑ -> V2 ⇓ V2 ≥ 1,1. V MCA V 2 ≥ 1,2.V S (2 & 3 #Turbo & Jet) V 2 ≥ 1,15.V S (4 # Turbo & Jet) V 3 Steady Initial Climb Speed All # V3 ≥ V 2 + 10kts RMK/ V4 is required for noise abattement VZF is the Minimum Manoeuvring Speed with Zero Flaps - 29 - CL αcrit αmax α
Page 1 and 2: FPL 1. Aeronautical Information Ser
Page 3 and 4: 3. Section of Cruising Altitudes -
Page 5 and 6: 4. Aerodrome Criteria Control Zone
Page 7 and 8: 6.3 TO ALTN* (1#out**): should be l
Page 9 and 10: R E S E R V E F U E L 6.7.2 JAR-OPS
Page 11 and 12: 200ft 400ft 152ft 304ft 35ft Min 0N
Page 13 and 14: 9.5.1.2 From an NDB Station NDB 1ON
Page 15 and 16: 10. Doc 8168 PANS-OPS RMK/ - Bank A
Page 17 and 18: The NAT Region: Comprise some FIRs
Page 19 and 20: 14. METEOROLOGY SERVICES FOR AVIATI
Page 21 and 22: 14.3 Infos to ACFT in flight 14.3.1
Page 23 and 24: 15. Charts 15.1 Low Level Forecast
Page 25 and 26: 16.3 MRJT 16.3.1 Optimum Altitudes
Page 27: 16.6 Gradient : TAS GoC [Rad] ≅TA
Page 31 and 32: 17. PSR - PET(CP) DEP - Taxi Fuel H
Page 33 and 34: 18. Point of Equal Time (CP :Critic

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