Cessna 150G Model Reference

The 150G requires unusual care because an explicit A150M identity lies numerically inside its ordinary sequence. The excluded serial must never be returned as a 150G merely because it falls between the endpoints. The source also distinguishes landplane and approved seaplane context, making configuration evidence particularly important for this model.

Cessna 150J D-EJLP in side profile at Portimão Airport
Cessna 150J D-EJLP at Portimão. The side view shows the high wing, supporting strut and fixed landing gear. Photo: Robbie Klinkenberg · Wikimedia Commons · CC BY-SA 4.0. Resized, WebP.

Refinement after the F redesign

The 1967 150G develops the newly swept-tail aircraft introduced by the 150F. The recorded alternator, cabin and heating refinements shift attention toward the aircraft's electrical supply and occupied space. The 150H follows in 1968. The G therefore belongs to the refinement of an established outline, rather than a repeat of the F's first electric-flap and swept-tail transition.

That distinction is useful when comparing surviving aircraft with similar silhouettes. The F-to-G comparison asks what changed within that familiar shape, and the electrical article explains why generation and current installed equipment must be distinguished. The G's approved float context adds a different configuration branch; it is not a general description of every G landplane.

Before those comparisons can be applied to a particular serial, the exceptional A150M assignment inside the ordinary G interval has to be resolved. This is an identity exception, not evidence of an unusual G with later Aerobat equipment. The distinction lets the visible development story and the legal-model record work together without one replacing the other.

150G: identity at a glance
Model Years1967
Certification CategoryUtility
Certified Serial Eligibility15064533-15067198 except 15064970
Type-design engine contextContinental O-200-A

Generation and Certification

The historical record describes cabin refinement and float-related development, while the propeller and loading records retain separate configuration conditions. A float-related value is not an upgrade to every 150G landplane. For buyers and mechanics, the correct combination of identity, installed configuration and approval records is more useful than a single generic model specification.

For 1967, the 150G change record identifies an alternator, a wider cabin, heating/defroster changes and optional floats. This follows the F's electric-flap and swept-tail redesign rather than repeating that introduction. The alternator distinction matters for electrical-system research, while cabin and heater changes matter to the installed equipment and occupant environment. The standard landplane remains in the 1,600-lb group. Optional float approval creates a separate configuration enquiry; it does not make the sea weight or float propeller a generic G-model specification.

150G: certification models
ModelTCCategoryInitial Model Approval DateCore Cert BasisCertification / Identity NoteReference
150G3A19Utility1966-05-05CAR 3 (1956-05-15) amended 3-4Separate seaplane configuration approval appears in TCDS.[1]
Instrument panel and open doorway of Cessna 150L SP-KNC
The cockpit of Cessna 150L SP-KNC. Instruments, controls and cabin fittings shown here belong to this photographed aircraft. Photo: Wlodek k1 · Wikimedia Commons · CC BY-SA 3.0. Resized, WebP.

Serial Numbers and Production

For 150G, the ordinary source assignments are 1967: 15064533 through 15067198 (excluding 15064970). The serial guide retains source conflicts and exceptional identities alongside these intervals.

150G: serial ranges
Model YearOfficial ModelSerial StartSerial EndExcluded / Override SerialsNotesPrimary Source
1967150G15064533150671981506497015064970 is explicitly excluded from 150G identity and assigned to A150M.[1]

Engine, Propeller and Equipment Changes

The G-model propeller evidence separates the landplane application from approved-seaplane conditions. Read that distinction alongside the two weight-and-balance groups before comparing an aircraft that has operated on floats with one that has always been a landplane. A previous float installation may be a records and configuration question even when the aircraft is currently on wheels. The source also records a Model 22-374-series Weston-Garwin Carruth altimeter AD lead among G-model equipment examples. Applicability depends on the actual unmodified instrument, not on the presence of a 150G data plate.

The 150G factory installation groups specify 1967: O-200-A, 100 hp at 2750 RPM. Its named propeller applications are 69CK family / 1A100/MCM6950 / 1A101/DCM6950; 1A90/CF. Their diameter, static-RPM and configuration conditions are preserved together below.

150G: engine serial ranges
OriginModel YearAircraft ModelFactory EngineInstalled hpRPM LimitFirst Serial in GroupLast Serial in GroupApplicability BasisAircraft Source
USA1967150GO-200-A10027501506453315067198Factory / type-design[1]
150G: propeller applications
Aircraft ModelModel Year / ConfigEngineExact Propeller ApplicationMax DiaMin DiaStatic MinStatic MaxNotesPrimary Authority
150G through 150KLandplaneO-200-A69CK family / 1A100/MCM6950 / 1A101/DCM69506967-67.52320/2375/25002470/2475/2600Use propeller-specific static range.[1]
150G through 150KSeaplaneO-200-A1A90/CF7573.525002600Seaplane only.[1]
150G: major changes
YearModelMajor ChangeSerial Specific?Source
1967150GAlternator, wider cabin, heating/defroster changes, optional floatsNo[1]

Specifications, Fuel and Loading

The normal G-model interval contains an explicit exclusion: 15064970 belongs to A150M. This is more than a historical curiosity because a numeric-only lookup would otherwise assign the wrong legal model and category. The 1967 performance entries must stay with the ordinary G identity and their own power/altitude conditions. The published 975-lb Standard and 1,060-lb Commuter empty weights are comparison examples rather than loading evidence for the excluded aircraft. Use the correct legal model before selecting a certified-limit or handbook group, even when the serial appears comfortably inside the G endpoints.

The ordinary G range must exclude 15064970 before it is used for an aircraft identity count or technical assignment. The exception is not a special G-model year; it redirects to the A150M legal identity. This distinguishes it from a short special serial whose year simply remains unresolved. The D397 handbook lineage, land/sea propeller separation and alternator/heating history then become relevant only after the ordinary G identity is established. For a former float aircraft, records connecting the approved sea configuration and any return to land operation are more useful than assuming that the G's optional-float history makes both weight groups simultaneously applicable.

150G: certified limits
ModelsCategorySpeed BasisVneVnoVaVfeMTOW Land lbMTOW Sea lbBaggage lbSource
150G/150H/150J/150KUtilityCAS141 kt / 162 mph104 kt / 120 mph95 kt / 109 mph87 kt / 100 mph16001650120[1]
150G: weight balance groups
Models / Serial ApplicabilityConfigCategoryRamp lbTO lbLanding lbFwd CG lightLight wtFwd CG heavyHeavy wtAft CGBaggageDatum / ReferenceLevelingSource
150G, H, J, KLandUtility-1600160031.5128032.9160037.5120 lb, reference W&B dataCertified datumTop of tailcone[1]
150G, H, J, K with approved seaplane configurationSeaUtility-1650165033140033.8165036.5120 lb, reference W&B dataCertified datumTop of tailcone[1]
150G: model year specifications
YearModel(s)Max SpeedCruiseROC SLCeilingPublished Gross / MTOWPublished Empty WeightBaggageNotesSource
1967150G123 mph; 125 Commuter120 mph @75% /7500; 122 Commuter670 fpm12,650 ft1600 lb975 Std; 1060 Commuter120 lbDetailed secondary page.[1]
Continental O-200-A installed in a Cessna 150H with the cowling removed
Continental O-200-A in a Cessna 150H, viewed from above and to the left with the cowling removed. Photo: YSSYguy at English Wikipedia · Wikimedia Commons · CC BY-SA 4.0. Resized, WebP.

Performance and Comparison Conditions

One published 150G example is 1967 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 150G.

150G: performance
YearModelValueUnitsPower %Altitude ftFuel Usable galReserve BasisObstacle ftCondition NoteSource
1967150G123mph-----Published headline value[1]
1967150G120mph757500---Published headline condition[1]
1967150G670fpm------[1]
1967150G12650ft------[1]
1967150G735ft------[1]
1967150G1385ft----50-[1]
1967150G445ft------[1]
1967150G1075ft----50-[1]

Manuals, Maintenance and Research

The D397-13 handbook family retains a documented distinction from the later D397-1 lineage. A similar publication number in a listing does not settle revision or effectivity. For a G-model buyer, a productive records review connects that handbook question with the alternator installation, cabin-heating system, land/sea configuration and actual altimeter identification. The following 150H continues the swept-tail generation, but its shorter available performance coverage is not a reason to backfill H-model operating values from this G page. Exact model identity remains the basis for choosing the next technical reference. The positive 150G publication leads are 1967: D397-13 family (Owner's Manual).

150G: handbook applicability
Family / YearModelPublicationDocument ClassSerial / Year EffectivityAuthority BasisOperational StatusSpecial BoundaryReference
1967150G / F150GD397-13 familyOwner's Manual1967 equivalent Cessna/Reims mappingCAA TAR 98/08Authority-recognized base familyD397 vs later D397-1 lineage retained[1]

Related Models and Technical Research

The 150 seaplane configuration reference keeps float-related loading and propeller eligibility separate from this model's landplane identity. The 150F-versus-150G comparison distinguishes the electric-flap redesign from the following alternator and cabin refinements.