Area I · Task F — Performance and Limitations

Cessna 172S Steam Performance & Weight and Balance — PPL Oral Exam Questions

Takeoff and landing performance, density altitude, weight and balance computations, and aircraft limitations from the POH. Below are real DPE-style questions for the Cessna 172S Skyhawk SP (Six-Pack / Steam Gauges). Every answer cites a primary FAA source — no fabricated regulations, no shortcuts.

13 questionsPOH Section 4PHAK Chapter 11Airplane Flying Handbook (FAA-H-8083-3C)

Aircraft profile

Cessna 172S Skyhawk SP (Six-Pack / Steam Gauges)

Engine
Lycoming IO-360-L2A, 180 HP, fuel-injected
Fuel system
Gravity-feed, fuel selector BOTH/LEFT/RIGHT. The 172S has no separate fuel shutoff — OFF position integrated into selector on most airframes, but student should confirm on their specific aircraft.
Avionics
Six-pack steam gauges: ASI, AI, ALT, TC/TI, DI/HI, VSI
VS0 / VS1
40 KIAS (stall, landing config) / 48 KIAS (stall, clean) kt
VA
varies by weight, see POH kt
Max gross
2550 lbs lbs

DPE oral questions · performance & weight and balance

13 questions a DPE may ask in this section

  1. Question 1 · PA.I.F.K1

    How does density altitude affect aircraft performance?

    What a DPE expects to hear

    • High density altitude = reduced performance
    • Longer takeoff roll
    • Reduced rate of climb
    • Higher true airspeed for same IAS
    • Reduced engine power output (naturally aspirated)
    • Density altitude increases with: high pressure altitude, high temperature, high humidity

    SourcePHAK FAA-H-8083-25C Chapter 11; AFH FAA-H-8083-3C

  2. Question 2 · PA.I.F.K1

    What is the purpose of weight and balance calculations?

    What a DPE expects to hear

    • Ensure aircraft is within maximum gross weight limits
    • Ensure center of gravity (CG) is within approved limits (forward and aft limits)
    • Aircraft outside CG limits may be uncontrollable
    • Aft CG: reduced longitudinal stability, can be unrecoverable in stall
    • Forward CG: increased stability but may not have sufficient elevator authority for flare

    SourcePHAK FAA-H-8083-25C Chapter 10

  3. Question 3 · PA.I.F.K2

    What effect does a headwind have on takeoff performance? A tailwind?

    What a DPE expects to hear

    • Headwind decreases takeoff roll (aircraft reaches Vr at a shorter ground distance)
    • A 10-knot headwind component reduces takeoff roll significantly
    • Tailwind increases takeoff roll — the rule of thumb is a 10-knot tailwind increases takeoff distance by approximately 21%
    • Crosswind component matters too — maximum demonstrated crosswind component is in the POH

    SourceAFH FAA-H-8083-3C; POH performance charts

  4. Question 4 · PA.I.F

    Passengers decide to switch seats just before start. Does this matter if total weight is the same?

    What a DPE expects to hear

    • YES — moving weight changes CG
    • Passenger to back seat moves CG aft = less stable, harder to recover from stall

    SourcePHAK Chapter 10; ACS Task I.F

  5. Question 5 · PA.I.F

    We have a 50-foot obstacle at the end of this 2,500-foot runway. Walk me through your configuration and procedure.

    What a DPE expects to hear

    • Set flaps to manufacturer recommended setting (e.g., 10° C172, 25° Warrior)
    • Full power before brake release
    • Rotate at calculated speed, climb at Vx until obstacle cleared
    • Then accelerate to Vy and slowly retract flaps

    SourceACS Task IV.E; POH Section 4

  6. Question 6 · PA.I.F

    Wind is 20 knots at 30° to the runway. Is this landing legal and how will you adjust flap setting?

    What a DPE expects to hear

    • No regulatory crosswind limit for private pilots — must adhere to POH maximum demonstrated crosswind and personal minimums
    • Strong crosswind = smaller flap setting recommended for better directional control

    SourceACS Task IV.B; POH Section 4/5

  7. Question 7 · PA.I.F

    What are your criteria for a stabilized approach and at what altitude must these be met?

    What a DPE expects to hear

    • Final landing configuration, correct flight path, target airspeed (+10/-5 knots), steady rate of descent
    • For VFR: stabilized by 500 feet AGL

    SourceACS PA.IV.B.S6; AFH Chapter 9

  8. Question 8 · PA.I.F

    It's 95°F at an airport with 5,000-foot elevation. How does this affect our ground roll vs. standard day at sea level?

    What a DPE expects to hear

    • High density altitude = significantly longer takeoff roll
    • Less engine power, less propeller thrust, wings require higher true airspeed to generate lift
    • Must reach much faster groundspeed before rotation

    SourceAviation Weather Handbook Chapter 8; PHAK Chapter 11

  9. Question 9 · PA.I.F

    We're flying at max gross weight. How does this extra weight change our takeoff and climb performance?

    What a DPE expects to hear

    • Higher liftoff speed = longer ground roll
    • Extra mass reduces rate of climb
    • Increases stall speed in all configurations

    SourceACS Task I.F; PHAK Chapter 11

  10. Question 10 · PA.I.F

    Wind is 15 gusting to 25. Why might we choose Flaps 10° or 20° instead of full flaps?

    What a DPE expects to hear

    • Partial flaps allow higher approach speed — greater safety margin above stall during sudden wind lulls
    • Also reduces wing area acted on by crosswind, making rollout easier to handle

    SourceACS Task IV.B; POH Section 4

  11. Question 11 · PA.I.F

    On a short-field landing, how do you get the most stopping power without blowing the tires?

    What a DPE expects to hear

    • After touchdown: retract flaps AND apply maximum braking while holding control wheel FULL BACK
    • Flap retraction and back pressure transfer weight from wings to main wheels, increasing tire-pavement friction

    SourcePOH Section 4; ACS Task IV.F

  12. Question 12 · PA.I.F

    We're landing at an airport with density altitude of 8,000 feet. Will our approach speed on the indicator be higher, lower, or the same as at sea level?

    What a DPE expects to hear

    • Indicated airspeed will be THE SAME as sea level
    • However true airspeed and groundspeed will be significantly higher — results in longer landing roll

    SourceAviation Weather Handbook Chapter 8; PHAK Chapter 11

  13. Question 13 · PA.I.F

    During takeoff roll, what engine or flight instrument indications would cause you to immediately abort?

    What a DPE expects to hear

    • Sluggish acceleration, rough engine operation, static RPM below POH range, zero or negative airspeed indication halfway down runway

    SourcePOH Section 4; ACS Task IV.A

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