1976 Cessna 150M Airplane Pilot's Operating Handbook (P/N D1055-13-RPC-750-9/83)
190 Pages • 9.87 MB • Instant, Printable PDF
Cessna Models Covered & Key Technical Specifications
Model: 150M
Sub-models / Variants: Standard, Commuter, Commuter II
Model Year: 1976
Serial Numbers: 15077380 and on (revised seat belt/shoulder harness system); earlier restraint configuration also described
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Engine: Teledyne Continental O-200-A
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Horsepower Rating: 100 BHP at 2750 RPM
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Fuel Capacity: 26 gallons (Standard), 38 gallons (Long Range)
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Maximum Takeoff Weight: 1600 lbs
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Propeller: McCauley fixed pitch, 69 inches diameter
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Oil Capacity: 6 quarts (7 quarts with filter)
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Max Demonstrated Crosswind Velocity: 13 knots
Cessna Manual Features & Selected Content Preview
The 1976 Cessna 150M Pilot's Operating Handbook covers Commuter and Commuter II equipment configurations, operating limitations, flight procedures, and routine care. This reprint bears the document code D1055-13-RPC-750-9/83.
Search, navigation and diagram detail: An embedded OCR layer supports text search, although recognition errors affect some words and diagram labels. PDF bookmarks open all nine main sections. Small labels in the Electrical System schematic are readable with zoom; individual avionics supplements have no separate bookmarks.
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Normal and emergency procedures: Preflight inspections, cold weather operation, spin recoveries, rough-engine checks, carburetor icing, spark plug fouling, and electrical power-supply malfunctions.
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Performance and loading: Takeoff and landing charts, climb and cruise data, airplane weighing procedures, equipment weights and arms, and center-of-gravity calculations.
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Engine and fuel systems: Teledyne Continental O-200-A descriptions, lubrication and ignition systems, carburetor and primer operation, and standard versus long-range fuel arrangements.
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Airframe and instruments: Wing flap and tricycle landing gear systems, hydraulic brakes, pitot-static instruments, vacuum instruments, and early versus later restraints.
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Electrical and avionics: Electrical System schematic, alternator checks, over-voltage protection, audio control panel operation, and selected avionics self-test procedures.
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Handling and servicing: Towing, tie-down, individual-wheel jacking, longitudinal leveling, flyable storage, engine oil servicing, and propeller care.
This handbook is for owners and pilots who need operating information and routine care guidance for the 150M.
Flight Procedures, Performance and Loading
Normal and emergency checklists have amplified explanations. The Three View drawing and Taxiing Diagram support aircraft familiarization and ground handling. Limitations cover airspeed terminology, maneuvering speeds, instrument markings, and flight load factors.
Performance tables cover stall speeds, takeoff ground roll, obstacle clearance, and landing distance, with altitude, temperature, wind, and runway-surface corrections. Separate range and endurance charts address standard and long-range tanks.
The Loading Graph, Center of Gravity Moment Envelope, sample loading problem, and cabin dimensions support payload planning. Actual empty weight and installed equipment must come from the individual airplane's records.
Engine, Electrical and Instrument Systems
System descriptions explain the O-200-A's lubrication, dual magnetos, carburetor heat, and priming arrangements. The Fuel System schematic traces tank venting and gravity feed; the Vacuum System diagram identifies the pump, relief valve, filter, and instrument connections.
Electrical coverage connects the alternator, regulator, battery, over-voltage sensor, and protected circuits. Its distinction between excessive and insufficient charging helps identify the type of power-supply fault before electrical repair work begins.
The handbook warns that voltage transients during starting or external-power use can damage avionics transistors.
Restraint Variants and Ground Servicing
Supplement D1055S1-13 is incorporated into the reprint and describes the revised seat belt and shoulder harness system from S/N 15077380. Earlier restraint arrangements and optional inertia-reel harnesses are also illustrated; this is a restraint-system change, not a blanket starting serial number for the handbook.
Servicing references distinguish oil-screen and full-flow-filter arrangements, give fuel and lubrication specifications, and explain Cessna Progressive Care. Ground-handling coverage includes individual-wheel jacking and longitudinal leveling; full-aircraft jacking and extended storage are referred to the separate Service Manual.
Jacking cautions explain how pressure on unsupported tailcone skin can buckle it. The handbook is an operating and care reference, not a workshop repair manual for engine overhaul or component rebuilding.
Check current aircraft-specific documentation and applicable airworthiness directives before any repair or return to service.
Avionics Supplements and Coverage Limits
Optional-equipment material covers the ELT, RT-524A transceiver, RT-308C Nav/Com, R-546E ADF, R-402A marker beacon, and RT-359A transponder with EA-401A altitude encoder. Procedures include ADF bearing-reliability tests, marker-beacon lamp tests, and transponder self-tests.
Nav/Com limitations: The RT-308C coverage is for VOR navigation; localizer audio reception does not provide course-deviation guidance. Only printed pages 1-3 of the RT-528E-1 supplement and 4-5 of the RT-328T supplement are included. Their remaining text pages are missing.
Page order: The ADF and transponder supplements contain their text pages, but these are out of sequence. ADF material is split between PDF pages 171-172 and 185-188; the transponder appears on PDF pages 179-184 in printed-page order 5, 6, 3, 4, 1, 2.
PDF Contents and Page Breakdown
One printable, English-language 190-page PDF: 6 front-matter pages, 144 pages covering Sections 1-8, 39 pages in Section 9, and 1 back cover. All 17 notes pages and the incorporated restraint-system update are already included in that total.
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