FAA AGI Advanced Ground Instructor study materials
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5,000 Feet, 30 Degrees, and a 3,500-Foot Runway

FAA AGI Advanced Ground Instructor · Put your knowledge to work in context.

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5,000 Feet, 30 Degrees, and a 3,500-Foot Runway

You are flying a four-seat, fixed-gear, normally aspirated airplane at maximum gross weight from a 3,500-ft dry asphalt runway at 5,000 ft MSL field elevation. The altimeter setting equals 29.92, and the outside air temperature is 30 °C. The POH, at 5,000 ft pressure altitude and ISA, lists a takeoff ground roll of 1,500 ft and a total distance over a 50-ft obstacle of 2,700 ft. The POH notes approximately a 10% increase in takeoff distance per 10 °C above ISA and about a 10% decrease per 10 kt of direct headwind. Wind is 210° at 10 kt; you are using runway 18. Trees 40 ft high stand just off the departure end.

1. Estimate density altitude and the corrected total distance over a 50-ft obstacle.

Read the worked answer

Density altitude. ISA temperature at 5,000 ft is 15 − (2 × 5) = 5 °C. You are 25 °C above ISA. Using roughly 120 ft of density altitude per degree Celsius above standard:

5,000 + (25 × 120) = 8,000 ft density altitude

Distance correction for temperature. 25 °C above ISA at 10% per 10 °C = a 1.25 multiplier:

2,700 × 1.25 = 3,375 ft

Wind correction. Wind 210° on runway 180° is 30° off the nose. Headwind component = 10 × cos 30° ≈ 8.7 kt; crosswind = 10 × sin 30° = 5 kt. At roughly 10% per 10 kt of headwind, the reduction is about 9%:

3,375 × 0.91 ≈ 3,070 ft

That is the answer only if your technique matches the POH test pilot's. It does not include any margin for a slower-than-book rotation, a slightly lean mixture error, or a soft spot in the asphalt.

2. Given the obstacle and the runway length, is this departure acceptable? What margin standard should you apply?

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No - this departure should be refused as loaded.

  • Corrected total distance is about 3,070 ft against a 3,500 ft runway: roughly 430 ft, or 12%, of unused surface. That is not a margin; it is measurement error, pilot technique variance, and a slightly high thermometer.
  • The 12,000+ ft density altitude means the airplane will accelerate slowly, rotate at a higher true airspeed, and climb at a shallow angle. Once past the trees, the airplane must still out-climb the terrain and any rising ground beyond.
  • The POH figure covers a 50-ft obstacle, so a 40-ft tree line is nominally covered - but only at the exact weights, temperatures, and techniques the manufacturer tested. If the actual temperature is 32 °C rather than 30 °C, or the wind goes calm, the margin is gone.
  • A reasonable personal standard is at least 60% of the available runway for the planned total distance at gross weight on a hot day with obstacles. You would need about 2,100 ft of corrected distance to have that margin; you have 3,070.

Legal fixes: reduce weight (fuel or payload - 10% weight reduction buys roughly 20% distance reduction), wait for a cooler hour, or use a longer runway. Temperature is the highest-leverage variable and the one you can control by scheduling.

3. The pilot proposes departing at 0630 when the temperature is 12 °C. Evaluate that plan and identify the traps in the "cool morning" solution.

Read the worked answer

It is a real improvement, but verify it rather than assuming it.

At 12 °C you are 7 °C above ISA: density altitude ≈ 5,000 + (7 × 120) = 5,840 ft. The multiplier is about 1.07, giving 2,700 × 1.07 ≈ 2,890 ft - comfortably inside the 60% margin standard.

Traps to check:

  1. The wind credit disappears. Morning calm is common; that removes the 9% headwind reduction but also removes the crosswind. Recompute with zero wind rather than carrying the afternoon number forward.
  2. Use the actual altimeter setting, not field elevation. A 30.10 setting at a 5,000 ft field drops pressure altitude below 5,000 and helps; a 29.80 hurts. Pressure altitude is not elevation.
  3. Morning fog and dew point spread. A 2 °C spread at dawn often means radiation fog on a rural single-runway field with no approach - you may not be able to launch at 0630 at all.
  4. Engine and oil temperature. A cold start, an immediate full-power takeoff, and a leaned-for-altitude mixture is a recipe for rough running right at rotation. Allow a proper run-up and use the POH leaning procedure.
  5. Sunrise and obstruction lighting. Trees off the departure end are much harder to see in the low sun angle of early morning than at midday.