Cessna 150F Model Reference

Generation and Certification

The similarly named Reims F150F is a separate identity under a different certification source. A shared letter and related design history do not justify merging their serials or automatically transferring technical limits. Use the aircraft origin and exact model before selecting the handbook or interpreting a component application.

The 150F brings the documented swept vertical stabilizer, wider and deeper doors, electric flaps and enlarged baggage arrangement. It therefore changes both external identification and several cockpit/maintenance questions while retaining the D-F 1,600-lb certified limit and 100-hp O-200-A. The year summary lists a 23 ft length and 32 ft 8.5 in span, compared with the E's 21 ft 7 in and 33 ft 6 in entries. Those are published configuration descriptions; they should not be used to infer a dimensional change from a photograph alone.

Serial Numbers and Production

For 150F, the ordinary source assignments are 1966: 15061533 through 15064532. The serial guide retains source conflicts and exceptional identities alongside these intervals.

Engine, Propeller and Equipment Changes

The electric-flap installation is not one unchanging F-model assembly. The systems source identifies a right-wing relay for serials 15062291-15063135, followed by an improved motor with the relay deleted from 15063136 onward. The separate engine-mount/doubler change starts at 15061640. These boundaries show why the broad 1966 redesign and exact component effectivity need separate treatment. A mechanic tracing an electrical fault or ordering structural parts needs the relevant serial and installed assembly, not just confirmation that the aircraft has the swept tail associated with the F generation.

The 150F factory installation groups specify 1966: O-200-A, 100 hp at 2750 RPM. Its named propeller applications are 69CK-0-48L / -50L / -52L; 1A100/MCM6950; 1A101/DCM6950. Their diameter, static-RPM and configuration conditions are preserved together below.

Specifications, Fuel and Loading

The 1966 summary separates a 970-lb Standard example from a 1,060-lb Commuter example. A larger cabin or baggage arrangement does not increase the certified gross weight beyond 1,600 lb, and the difference in equipment weight can consume some of the practical cabin-load margin. The F performance entries retain standard/long-tank range conditions as well as cruise and runway figures. Keep those conditions visible when comparing a manual-flap E with an electric-flap F; a design-generation change alone does not quantify the takeoff or landing result for a particular load and day.

The F's three propeller applications offer a useful example of why static RPM belongs to an installation. The Sensenich entry gives a 2,320-2,470-RPM static window; the McCauley 1A100/MCM6950 gives 2,375-2,475; the 1A101/DCM6950 gives 2,500-2,600. Their shared 69-inch maximum and 67.5-inch minimum diameters do not make those RPM windows interchangeable. A static-RPM observation should therefore be reconciled with the actual propeller and controlling application, not judged against whichever early-model row is closest. The flap changes add another independent inspection question: an F before the named right-wing relay interval is not automatically described by either the interval's relay configuration or the later relay-deleted arrangement. The source must establish the exact installation. This is particularly relevant when an aircraft has had a motor or wing replaced. Comparing the F with the following G should also preserve the distinction between the F's electric-flap introduction and the G's alternator/cabin-heating refinement. Neither change proves present equipment after later alterations. The F model page is thus most useful as a map of distinct design, component and operating boundaries, rather than a single list of features assumed to have arrived together on every 1966 aircraft.

Performance and Comparison Conditions

One published 150F example is 1966 cruise speed: 120 mph (power % 75; altitude ft 7500). The table keeps each metric's year, units, power, altitude, fuel and reserve columns together. Use the performance guide to distinguish headline comparisons from handbook operating calculations; no unreported condition is supplied for 150F.

Manuals, Maintenance and Research

The F-model year is the opening boundary of the 1966-1986 fin-attachment advisory context recorded in the known-issues guide. That provides a specific tail-structure research lead, not a declaration of damage or a substitution of an advisory for an AD. The Reims F150F also begins in 1966 but has its own prefix, certification identity and electric-flap serial boundaries. D326-13 is a recognized publication-family mapping for the related models; the applicable authority and aircraft coverage still distinguish a U.S. 150F from a French-built F150F. The positive 150F publication leads are 1966: D326-13 (Owner's Manual).