===== Boeing 737-500 ===== {{:wiki:737.jpg?450|}} The Boeing 737 series is the world's most popular aircraft family. The shortened B737-500 variant has a capacity of a maximum of 140 people. The specific B737-500 modeled in Aerofly FS 2 is based on an aircraft with the classic "steam gauge" cockpit, retrofit high-bypass CFM56 engines for better fuel economy and retrofit cockpit devices such as a Universal FMS to allow modern navigation. ==== Flight Plan Editing in the CDU ==== The flight management system of the exact 737-500 that we are simulating is a retrofit and therefor is identical to the ones found in the Learjet 45 and Q400. The interface to the flight management system (FMS) is called a control display unit (CDU). The CDU is the device that pilot interact with in the cockpit, the computers performing all the calculations are called flight management computers (FMC). We added a tutorial on how to create a flight plan in the 737, Learjet 45 and Q400:[[aircraft:universal_uns1_fms|Universal UNS-1]] {{ :wiki:b737_cdu.jpg?300 |}} ===== V Speeds and Ranges ===== [[aircraft:basic_flight_information|What are the v-speeds?]] **Take Off Speeds** ^ Boeing 737-500 Take-Off Speeds^^^^ ^Take-off Weight ^ 737-500 18.5K ^^^ ^/1000kg ^V1 ^Vr ^V2 ^ ^70 | | | | ^65 | | | | ^60 |147 |147 |152 | ^55 |140 |140 |146 | ^50 |132 |132 |139 | ^45 |123 |123 |132 | ^40 |113 |114 |124 | ^35 |104 |104 |117 | | | | | | | |ISA Vmcg=106 || |Typical wet v1=dry V1-10kts |||| **Landing Speeds** ^Boeing 737-500 Landing Speeds ^^^^^^ ^Landing Weight ^737-500 18.5K ^^^^^ ^ ^Flaps ^^^^^ ^/1000kg ^40 ^30 ^15 ^^^ ^70 | | | ||| ^65 | | | ||| ^60 |140|144|154 ||| ^55 |134|139|148 ||| ^50 |128|133|141 ||| ^45 |122|125|135 ||| ^40 |114|117|125 ||| ^35 |107|109|116 ||| **Flap Setting Speeds** ^Boeing 737-500 Landing Flap-Speed Schedule ^^^^ ^Flap Position^Up to 53070kgs^Above 53070kgs^Above 62823kgs ^ ^Flaps UP |210 |220 |230 | ^Flaps 1 |190 |200 |210 | ^Flaps 5 |180 |190 |200 | ^Flaps 10 |170 |180 |190 | ^Flaps 15 |150 |160 |170 | ^Flaps 25 |140 |150 |160 | ^Flaps 30 |Final Approach Speed ||| ^Flaps 40 |Final Approach Speed ||| **Flight Notes** **Speed, Height, Distance Conversion** * Level flight deceleration allow 10kts/nm & 1kt/sec (deceleration is faster at lower weights) * Descending deceleration allow 5kts/nm & 0.5kt/sec * Idle descent allow 3nm/1000' **Approach Profile Planning** * Aim for 250kts, 10,000ft by 30nm out * Aim for 210kts, On ILS at 12nm **Cruise N1** * N1 = (2 x Alt/1000) + 10   eg at FL350 = 70+10 = 80% N1 **or** FF = (IAS*10)/2 -200  eg 250kts = 2500/2 -200 = 1050 kg/hr/engine **N1's & Pitch Attitudes** ^Phase of Flight ^^^ ^ ^%N1 ^Attitude (Nose Up) ^ ^Level Flight ^^^ ^250kts |65 |4 | ^210kts |60 |6 | ^Flap 1 190kts |60 |6 | ^Flap 5 180kts |62 |7 | ^Gear Down, Flap 15, 150kts |70 |8 | ^Gear Down and On Glideslope ^^^ ^Flap 15 150kts |52 |4.5 | ^Flap 25 140kts |52 |4 | ^Flap 30, Vref + 5 |55 |2.5 | ^Flap 40, Vref + 5 |62 |1 | **Climb Speeds** If ECON info not available, use 250KIAS until 10,000ft then 280KIAS/M0.74 thereafter * **Best Angle = V2 + 80** * **Best Rate = V2 + 120**