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Enroute Performance
B737 Performance · Chapter 2

B737 Enroute Performance

Opening your chapter…

B737 Performance chapter 2, Enroute Performance. By the end of this chapter you can explain what sets optimum versus maximum altitude, how cost index shapes cruise speed strategy, what actually moves top of descent, how drift down and its two strategies work, and why engine-out cruise can beat two-engine cruise on fuel mileage.

  • 5 pages
  • 66 min of reading
  • 12 question chapter check
  • Notes, highlights and progress saved

What this chapter covers

  1. 1
    Optimum altitude and maximum altitudeWritten from Compiled from 737-800 performance principles and standard cruise planning practice
    13 min read
  2. 2
    Cost index and cruise speed strategyWritten from Compiled from 737-800 performance principles and standard cruise planning practice
    14 min read
  3. 3
    Descent planning and top of descentWritten from Compiled from 737-800 performance principles and standard cruise/descent planning practice
    13 min read
  4. 4
    Drift down: obstacle clearance and fixed speed strategiesWritten from Compiled from 737-800 performance principles and standard drift down and ETOPS planning practice
    14 min read
  5. 5
    Engine-out cruise and fuel flow characteristicsWritten from Compiled from 737-800 performance principles and standard cruise fuel planning practice
    12 min read

B737 enroute performance terms

Optimum altitude
The cruise level with the best fuel mileage, or lowest cost in ECON, for the current 737 weight.
Maximum altitude
The lowest of the 41,000 ft certified limit, the buffet limited altitude and the thrust limited altitude.
Buffet limited altitude
Where the manoeuvre margin to buffet runs out. The default margin is 1.3g, about a 39 degree bank.
Thrust limited altitude
Where the aircraft can just achieve a minimum climb rate, commonly 300 ft per minute. It falls in hot conditions.
Cost index (CI)
Ratio of time cost to fuel cost. CI 0 is maximum range cruise, CI 500 flies near VMO or MMO.
Long range cruise (LRC)
A fixed speed giving up 1 percent fuel mileage for about 3 to 5 percent more speed. Not wind corrected.
Maximum range cruise
The speed for the best fuel mileage, flown with cost index 0.
Step climb
Climbing in steps as fuel burns off to stay close to the rising optimum altitude.
Top of descent
Start of the idle descent. A headwind in descent moves it closer to the destination.
Driftdown
After an engine failure at cruise: maximum continuous thrust and the shallowest descent to a sustainable level.
ENG OUT CRZ page
FMC page giving the driftdown speed, engine-out maximum altitude and level-off altitude.
Net flight path
The driftdown profile with a safety margin applied, which must clear terrain by set amounts.
TSFC (thrust specific fuel consumption)
Fuel flow per unit of thrust. It improves at higher thrust settings.

Try a question from this chapter

Chapter check, question 1 of 12

What mainly determines optimum altitude in cruise?

B737 enroute performance questions

What is the maximum altitude of the 737-800?

The certified maximum is 41,000 ft. On the day, FMC maximum altitude is the lowest of that limit, the buffet limited altitude and the thrust limited altitude.

What does cost index 0 mean on the 737?

Cost index 0 treats time as free and fuel as the only cost, so the FMC flies Maximum Range Cruise. Cost index 500 does the opposite and flies close to VMO or MMO.

What is driftdown on the 737?

After an engine failure at cruise, the aircraft usually cannot hold altitude. Driftdown uses maximum continuous thrust on the remaining engine at the speed for the least descent rate, down to a level where single engine cruise is possible.

Is long range cruise the most economical speed?

Not always. LRC is a fixed speed that is not corrected for wind, roughly equal to a cost index of about 30. In a strong headwind the airline's wind corrected ECON speed can be better.

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