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Landing Performance
B737 Performance · Chapter 3

B737 Landing Performance

Opening your chapter…

B737 Performance chapter 3, Landing Performance. By the end of this chapter you can explain the difference between dispatch certified data and QRH advisory data, apply the approach and landing climb gradient checks, work through dry, wet and contaminated landing field length factors, set VREF and command speed correctly, read a brake cooling schedule, and use the TALPA runway condition code system.

  • 8 pages
  • 111 min of reading
  • 12 question chapter check
  • Notes, highlights and progress saved

What this chapter covers

  1. 1
    Dispatch certified data and QRH advisory dataWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    14 min read
  2. 2
    Approach climb, landing climb, and VMCLWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    14 min read
  3. 3
    Dry landing field length and the 1.67 factorWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    13 min read
  4. 4
    Wet and contaminated landing field lengthWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    14 min read
  5. 5
    VREF and command speedWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    15 min read
  6. 6
    Brake cooling and thermal fuse plugsWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    13 min read
  7. 7
    TALPA and the runway condition codeWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    15 min read
  8. 8
    TALPA advisory distance and the 455 metre air distanceWritten from 737-800 performance principles, TALPA/RCAM regulatory material, and QRH-PI concepts
    13 min read

B737 landing performance terms

Performance dispatch
Certified pre-departure checks of landing climb and landing field length that give a limiting landing mass.
QRH-PI landing distance
Advisory in-flight landing distance for the runway condition expected at arrival.
CAT.OP.MPA.303
EASA rule: LDA must be at least 115 percent of the landing distance at the estimated time of arrival.
Approach climb gradient
2.1 percent with one engine inoperative, flaps 15 and gear up.
Landing climb gradient
3.2 percent with all engines, landing flap and gear down.
MACG (missed approach climb gradient)
PANS-OPS assumes 2.5 percent unless the chart publishes a steeper figure.
1.67 factor
Dry dispatch: the full stop distance must fit within 60 percent of the LDA, the same as distance times 1.67.
Wet runway factor
LDA must be at least 115 percent of the dry dispatch requirement.
VREF
Landing reference speed, at least 1.23 times the stall speed in landing configuration and never below VMCL.
Command speed wind additive
Half the steady headwind plus the full gust, between VREF plus 5 and VREF plus 15 knots.
Thermal fuse plugs
Wheel plugs that melt at roughly 177 to 199 degrees C to deflate a tyre after a hot brake stop.
Brake cooling schedule
QRH-PI table showing the cooling time or fuse plug melt risk after an RTO or landing.
RCAM (runway condition assessment matrix)
Turns observed runway contaminants into a runway condition code for each third of the runway.
RwyCC (runway condition code)
Scale from 6, dry, to 0, nil braking, with a matching braking action term.
TALPA
Takeoff and Landing Performance Assessment framework that introduced RCAM and the 455 m air distance.

Try a question from this chapter

Chapter check, question 1 of 12

Under EASA, which of these is a legal dispatch requirement rather than advisory information?

B737 landing performance questions

What is the 1.67 factor in landing performance?

For dry runway dispatch, the aircraft must stop within 60 percent of the landing distance available. Multiplying the actual landing distance by 1.67 is the same check.

How is VREF wind additive calculated on the 737?

With the autothrottle disconnected, add half the steady headwind plus the full gust increment, with a minimum of VREF plus 5 and a maximum of VREF plus 15 knots or flap placard speed minus 5. With autothrottle landing, set VREF plus 5.

What is RCAM in aviation?

The Runway Condition Assessment Matrix. Airports use it to turn the observed contaminant, depth and temperature into a runway condition code from 6, dry, to 0, nil braking, for each third of the runway.

What did TALPA change in the QRH landing distances?

The assumed air distance from threshold to touchdown rose from 305 m to 455 m, all advisory distances now carry a 15 percent margin, and the data follows the full RwyCC scale.

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