{ "open_checklist_version": "1.0", "id": "beechcraft-t-34b-mentor-t-34btest", "title": "Beechcraft T-34B Mentor — T-34Btest", "aircraft": { "make": "Beechcraft", "model": "T-34B Mentor", "category": "standard_normal" }, "provenance": { "source": { "kind": "third_party_checklist", "title": "Beechcraft/T-34B Mentor/T-34Btest.txt" }, "transcription": { "method": "format_conversion", "date": "2026-08-13", "converted_from": "doc" }, "contributors": [ { "name": "Open Checklists project", "role": [ "transcriber" ] } ], "revision": { "file_revision": "0.1.0", "updated": "2026-08-13" } }, "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." }, "units": { "airspeed": "kt", "altitude": "ft", "fuel": "usgal", "weight": "lb", "pressure": "inhg", "temperature": "f" }, "sections": [ { "phase": "other", "phase_label": "T-34B Test", "title": "Beechcraft T-34B Mentor — T-34Btest", "criticality": "normal", "items": [ { "type": "note", "text": "NAME : Date:", "tickable": false, "source_confidence": 1.0 }, { "type": "note", "text": "CFI: Grade:", "tickable": false, "source_confidence": 1.0 }, { "type": "challenge", "text": "Engine model number is HP Max RPM", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Engine Oil Capacity is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Minimum Fuel Octane is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Maximum Takeoff Weight is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Required Onboard Documents are", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Main Strut Extension is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Maximum Mag. Drop is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Best Rate of Climb Airspeed is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "VNE is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Maximum Gear Extension Speed is?", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Clean Stall Speed is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Maximum Gear Retraction Speed is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Minimum Oil Pressure is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Total Usable Fuel is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Maximum Demonstrated Crosswind is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Avoid Continuous Engine RPM Operation Between", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Engine Restart Procedures are", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Power off Emergency Glide Speed is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Prop overspeed procedures are", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Spin Recovery Procedure is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "In the Emergency Landing Pattern downwind altitude is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "At best glide speed, windmilling engine, the T-34 will travel ______\n miles for each 1000 feet of altitude.", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "The basic steps in an engine failure situation are (list 5):\n\n1.\n\n2.\n\n3.\n\n4.\n\n5.", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "The first step in an engine fire emergency is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "How is an alternator failure detected?", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "What are alternator failure corrective steps", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Most probable causes for engine roughness are", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "How do you prime the engine?", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Maximum starter cranking period is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Recommend final approach airspeed with flaps full is", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "The landing gear horn will operate if the throttle is reduced below", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "What is the average rate of climb at sea level, 75 deg F, 2985 Lbs?", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "What is the Takeoff Distance, 2985 lbs, 50 deg F, sea level?", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "At max range power setting of 19”/1900 RPM, 5000 ft, max gross wt, what\n is CAS and fuel flow? ________________ and .", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Determine if the aircraft is within weight and CG limits.\n\nGiven:\n\n Item Weight Arm Moment\n BEW 2236.8 85.6 191470.6\n P/P 180.0 87.0\n Rear Pax 180.0 138.0\n Fuel (50 gal x 6) 300.0 80.0\n\n Oil 22.5 46.0\n\nAircraft within weight and CG limits.", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Determine the takeoff distance over a 50’ obstacle and liftoff\nairspeed.\n\nGiven:\n\n Air Temp: 50 deg F\n Pressure Alt: sea level\n Weight: 2975 lbs\n Headwinds: 0 kts\n\nTakeoff distance:\n\nLiftoff airpseed:", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "What is the specific range (nm/lb fuel) at 5000 ft, 2775 lbs., TAS\n125?\n\nSpecific range:", "tickable": true, "source_confidence": 1.0 }, { "type": "challenge", "text": "Determine landing distance and approach airspeed over a 50’ obstacle.\n\nGiven:\n\n Landing Wt. 2975 Lbs.\n Flaps: 100 % Dn.\n Pressure Alt: Sea Level\n Headwinds: Zero\n\nLanding distance:\n\nApproach airspeed:", "tickable": true, "source_confidence": 1.0 } ] } ] }