{
  "open_checklist_version": "1.0",
  "id": "cessna-152-c-152test",
  "title": "Cessna 152 — C-152test",
  "aircraft": {
    "make": "Cessna",
    "model": "152",
    "category": "standard_normal"
  },
  "provenance": {
    "source": {
      "kind": "third_party_checklist",
      "title": "Cessna/152/C-152test.txt"
    },
    "transcription": {
      "method": "format_conversion",
      "date": "2026-08-13",
      "converted_from": "doc"
    },
    "contributors": [
      {
        "name": "Open Checklists project",
        "role": [
          "transcriber"
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    ],
    "revision": {
      "file_revision": "0.1.0",
      "updated": "2026-08-13"
    }
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  "verification": {
    "source_fidelity": "unreviewed",
    "operational_review": "none",
    "completeness": "full",
    "known_issues": [],
    "reviews": [
      {
        "type": "source_comparison",
        "reviewer": "ai-dual-pass-review",
        "date": "2026-08-14",
        "notes": "Automated AI review: two independent transcription passes + numeric/item-count disagreement resolution. Not human-verified; baseline for community correction."
      }
    ]
  },
  "rights": {
    "status": "licensed",
    "upstream_holder": "freechecklists.net",
    "upstream_license": "content-reuse permission granted by the site author for this replacement project",
    "notes": "Transcribed from the freechecklists.net archive under the author's reuse grant. Individual checklist wording may be substantially the source's; per-file contributor authorship is unknown."
  },
  "sections": [
    {
      "phase": "other",
      "phase_label": "Knowledge Test",
      "title": "C-152test",
      "criticality": "normal",
      "items": [
        {
          "type": "challenge",
          "text": "NAME _________________________",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "DATE _________",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "CFI",
          "tickable": true,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "1. Engine Model Number is                  HP          Max RPM",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "2. Engine Oil Capacity is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "3. Minimum Fuel Octane is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "4. Maximum Takeoff Weight is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "5. Required Onboard Documents are",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "6. Nose Strut Extension is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "7. Maximum Mag. Drop is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "8. Best Rate of Climb Airspeed is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "9. VNE is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "10. Clean Stall Speed is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "11. Minimum Oil Pressure is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "12. Total Usable Fuel is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "13. Maximum Demonstrated Crosswind is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "14. Engine Restart Procedures are",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "15. Power off Emergency Glide Speed is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "16. Stall Recovery Procedure is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "17. In the Emergency Landing Pattern, Downwind Alt is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "18. The Basic Steps in an Engine Failure Situation are (List 5):",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "   1.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "   2.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "   3.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "   4.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "   5.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "19. The First Step in an Engine Fire Emergency is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "20. How is an Alternator Failure Detected",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "21. What are Alternator Failure Corrective Steps",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "22. Most Probable Causes for Engine Roughness is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "23. How is the Engine Primed",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "24. Maximum Starter Cranking Period is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "25. Recommend Final Approach Airspeed with Flaps Full is",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "26. What is the Rate of Climb at 1670 lbs, 15 C, @ Sea Level",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "27. What is the Takeoff Distance 1670 lbs, 20 C, @ Sea Level, no wind component",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "28. At 75% Power, RPM is:  _____________  and GPH is approx.: _______________",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "29. If OAT is 10 deg C, PA 3000 TAS is: ________________________",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "30. Determine if the Aircraft is within weight and CG limits.",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "Basic Aircraft Weight 1155.9 lbs. @ 29.93”",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "Pilot and Front Pax 340.0 lbs. @ 39.0”",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "Fuel 24.5 gal @ 6 lbs./gal 147.0 lbs. @ 42.0”",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "Baggage 20.0 lbs. @ 64.0”",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "31. Determine the takeoff distance over a 50’ obstacle and liftoff airspeed.",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "Given: Pressure Alt: 3500 MSL, AOT 25 C, 1670lb. Gross Weight, 5 Knt. headwind.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "32. Determine fuel burn, time and distance to climb.",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "Given: Max gross weight, climb speed 67 KIAS, 0 wind, takeoff pressure altitude 1500’ MSL, OAT 25 C, cruise pressure altitude 7500’ MSL, cruise OAT 8 C.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        },
        {
          "type": "challenge",
          "text": "33. Determine landing distance and approach airspeed over a 50’ obstacle.",
          "tickable": true,
          "source_confidence": 0.95
        },
        {
          "type": "challenge",
          "text": "Given: Destination pressure altitude 525’ MSL, OAT 18’ C, landing weight 1580 lbs.,0 wind.",
          "tickable": true,
          "indent": 1,
          "source_confidence": 0.9
        }
      ]
    }
  ]
}