1969–1976 Cessna 150, F150, A150 & FA150 Aircraft Service Manual (P/N D971C3-RAND-1600-7/75)
358 Pages • Printable PDF • 31.31 MB • Download
Cessna Models Covered & Key Technical Specifications
Models: 150, Reims F150, A150, Reims FA150
Models & Model Codes:
150 — Cessna: 150J, 150K, 150L, 150M
F150 — Reims/Cessna: F150J, F150K, F150L, F150M
A150 — Cessna: A150K, A150L, A150M
FA150 — Reims/Cessna: FA150K, FA150L, FA150M
Sub-models / Variants: 150 Standard, 150 Trainer, 150 Commuter, 150 Commuter II, Reims/Cessna F150, 150 Aerobat, Reims/Cessna F150 Aerobat
Model Years: 1969–1976 (1969, 1970, 1971, 1972, 1973, 1974, 1975, 1976)
Serial Numbers: 150J 15069309–15071128, 150K 15071129–15072003, 150L 15072004–15075781, 150M 15075782–15077005 / beginning 15077006, F150J F15000390–F15000529, F150K F15000530–F15000658, F150L F15000659–F15001143, F150M F15001144–F15001248 / beginning F15001249, A150K A1500001–A1500226, A150L A1500227–A1500523, A150M A1500524–A1500609 / beginning A1500610, FA150K FA1500001–FA1500081, FA150L FA1500082–FA1500261, FA150M FA1500262–FA1500281 / beginning FA1500282
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Gross weight: 1600 lb
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Engine model: Continental O-200-A (150, A150); Rolls-Royce O-200-A (Reims F150, FA150)
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Propeller: 69" McCauley (Fixed Pitch)
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Standard fuel capacity: 26 gal total
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Long-range fuel capacity: 38 gal total
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Electrical system: 14 VDC (12-volt battery)
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Nose gear strut pressure (extended): 20 psi
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Main tire pressure: 21 psi
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Wing span: 32' 8-1/2" (Conventional), 33' 2" (Conical Camber)
Cessna Manual Features & Selected Content Preview
Cessna's 1969–1976 150 Series Service Manual (document reference D971C3-13) covers the 150, Reims F150, A150 Aerobat, and Reims FA150 Aerobat, including Standard, Trainer, Commuter, and Commuter II versions. This Change 3 edition is dated June 15, 1975, and includes the October 18, 1977 Temporary Change 1 engine-data page.
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Airframe servicing: Ground handling, hoisting, jacking, leveling, storage, lubrication charts, inspection schedules, and Cessna Progressive Care program guidance.
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Landing gear and brakes: Flat and tubular main gear service, Cleveland and McCauley wheel repair, nose-strut and shimmy dampener servicing, and hydraulic brake bleeding.
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Flight controls: Aileron, flap, elevator, trim-tab, and rudder troubleshooting and rigging, including trim-actuator disassembly, inspection, and reassembly.
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Powerplant service: Engine removal and installation, carburetor adjustments, magneto-to-engine timing, exhaust inspection, and McCauley propeller and spinner installation.
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Instruments and electrical systems: Pitot-static leak tests, vacuum-system diagnosis, fuel-transmitter calibration, battery and alternator troubleshooting, and system-specific wiring diagrams.
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Structural repair: Damage assessment, skin and spar repairs, control-surface balancing, and exterior painting material and compatibility guidance.
Written for aircraft mechanics, this manual provides reference information for experienced personnel and step-by-step procedures for less experienced mechanics.
Airframe Service and Flight-Control Rigging
The fuselage, wings, and empennage sections cover component removal and installation, with separate information for cabin doors, windows, seats, and harnesses. Fuselage station diagrams and jacking and leveling views support component location and aircraft positioning.
Daily servicing guidance and 50-, 100-, and 200-hour inspection charts are accompanied by special inspection requirements. Lubrication information distinguishes flap-actuator configurations by serial range and modification status, including SK150-37B and SK150-41.
Flight-control sections address cable routing, bellcranks, pulleys, travel checks, and rigging. The flap chapter distinguishes early freewheeling actuators from installations with motor shutoff at both travel limits, helping mechanics select the applicable checks before adjusting the system.
The wing-adjustment section warns that mishandling the eccentric attachment bushings can misalign their bolt holes and damage the bolt hole in the wing spar.
Landing Gear, Wheels, and Hydraulic Brakes
Separate procedures distinguish flat spring-steel gear from tubular gear. Wheel service also separates Cleveland assemblies from McCauley aluminum- and steel-flange configurations, with a dedicated fastener-torque chart.
Main Wheel Alignment illustrations accompany the alignment checks; tubular-gear camber and toe-in are nonadjustable. Nose-gear coverage extends to shock-strut disassembly, torque links, steering rods, and shimmy dampener repair. Brake sections cover master cylinders, lining replacement, and bleeding.
For tubular-gear axles bonded with EC2216, the removal notes explain why heating the bond ages the aluminum axle and requires axle replacement.
Engine, Fuel System, and Propeller Service
Engine troubleshooting charts address starting problems, rough running, low power, and oil-pressure faults. Related sections cover engine mounts, the external oil filter, induction components, throttle and mixture rigging, and the Engine Oil Schematic.
The gravity-feed fuel-system chapter covers tanks, vent checks, shut-off valve replacement, primer components, and fuel-strainer disassembly. Propeller installation details distinguish the different spinner and bulkhead arrangements.
Overhaul limits: Internal engine repair and overhaul, carburetor overhaul, and detailed propeller repair require the respective manufacturer's publications. Slick magneto coverage concerns installation and timing to the engine; the sealed units are not field-overhauled.
Instrument Diagnosis, Electrical Circuits, and Structural Repairs
Static Test Equipment illustrations accompany leak testing. Vacuum-system troubleshooting covers the pump, relief valve, and central air filters. Instrument coverage focuses on system faults and replacement; internal instrument repairs belong with instrument specialists.
Electrical sections include charging-system and lighting fault charts. The wiring chapter separates earlier circuits from the 1976 installations, including electric-flap diagrams. Optional wing-leveler rigging is covered. Nav-O-Matic autopilots and electronic communications and navigation equipment require separate manuals.
Structural repair coverage addresses skins, ribs, spars, landing-gear bulkheads, and hard-landing damage. Control Surface Balancing illustrations cover checks following repair or painting, alongside repair-jig information and exterior finish guidance.
Aircraft service, structural adjustments, and repairs must be performed by appropriately qualified aviation personnel, with particular care around the propeller and ignition system.
A Sample of Control-Cable and Trim Inspection Data
These are two examples of the rigging and inspection specifications included in the manual.
Aileron carry-through cable tension is specified at 40 ± 10 lb at the average temperature for the area.
With the elevators and trim tab neutral, maximum trim-tab free play is 0.112 inch total up-and-down movement measured at the trailing edge.
Bookmarked PDF and Wiring-Sheet Readability
Section access and diagram detail: Embedded bookmarks link the introductory material and system sections. Manual pages do not support PDF text search. Small wiring labels require zooming; some tiny handwritten notes and crowded table entries remain difficult to distinguish.
Supplied as one printable, 358-page PDF. The total includes the cover, preliminary material, revision inserts, 23 blank pages, and the single Temporary Change 1 replacement page; these pages are already included in the total.
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