Cessna 150K Model Reference

The standard 150K should be distinguished from the A150K Aerobat rather than treated as the same model with a different public name. The standard model retains its own certification category and ordinary serial sequence. The source also identifies a spinner change within the model, providing a more precise research boundary than the year label alone.

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.

The standard aircraft beside the first Aerobat

Two distinct U.S. K-model stories begin in the 1970 model-year group. This 150K continues the standard line after the 150J, while the A150K opens the Aerobat branch. The next standard model is 150L. The K's historical setting is therefore a branching family, not the conversion of the standard model into an Aerobat.

The K-versus-A150K comparison makes the distinction visible despite their shared period and engine family. Category, serial identity and approved operating information remain separate. Looking forward to the L adds another question: its tubular-main-gear generation is later development, not a feature to infer on every K. The spinner change inside the standard K interval is narrower again and belongs to its own component enquiry.

150K: identity at a glance
Model Years1970
Certification CategoryUtility
Certified Serial Eligibility15071129-15072003
Type-design engine contextContinental O-200-A

Generation and Certification

A shared model-year context does not authorize borrowing Aerobat limitations or assuming identical installed equipment. Follow the standard-model serial, applicable propeller entry and actual component identification. The spinner-related trigger explains why a parts question may need more detail than the official model designation.

The 1970 150K is the standard model alongside the new A150K Aerobat. That parallel introduction is the key historical comparison: the standard aircraft does not acquire an Acrobatic category because the same year includes an Aerobat version. Standard K limits remain 141 kt Vne and 104 kt Vno on the recorded CAS basis, whereas the A150K group lists higher acrobatic-category values. Both aircraft can be described as 100-hp 150s, so engine power alone is a poor guide to their operating-document and limitation differences.

150K: certification models
ModelTCCategoryInitial Model Approval DateCore Cert BasisCertification / Identity NoteReference
150K3A19Utility1969-06-05CAR 3 (1956-05-15) amended 3-4-[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 150K, the ordinary source assignments are 1970: 15071129 through 15072003. The serial guide retains source conflicts and exceptional identities alongside these intervals.

150K: serial ranges
Model YearOfficial ModelSerial StartSerial EndExcluded / Override SerialsNotesPrimary Source
1970150K1507112915072003--[1]

Engine, Propeller and Equipment Changes

The standard K's spinner change begins at serial 15071711, inside its 15071129-15072003 ordinary interval. A propeller/spinner parts enquiry should therefore preserve the serial breakpoint as well as the actual installed assembly. This is distinct from the later L-series landing-gear generation and from the Aerobat's separate certification identity. The K propeller evidence also retains configuration conditions rather than a universal pitch specification. It is possible for two standard K aircraft to share the same model-year description while requiring different investigation because of original effectivity or later recorded alterations.

The 150K factory installation groups specify 1970: 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.

150K: engine serial ranges
OriginModel YearAircraft ModelFactory EngineInstalled hpRPM LimitFirst Serial in GroupLast Serial in GroupApplicability BasisAircraft Source
USA1970150KO-200-A10027501507112915072003Factory / type-design[1]
150K: 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]
150K: serial break changes
YearModelSerial TriggerChangeEffectivitySystemSource
1970150K15071711Spinner changed15071711 and onPropeller/spinner[1]

Specifications, Fuel and Loading

The K remains at a 1,600-lb standard landplane limit, with a 26-gallon total and 22.5-gallon usable fuel entry in the certified group. The Patroller option appears separately in historical year context. Compare the published 975-lb Standard and 1,060-lb Commuter examples as equipment descriptions rather than two different gross-weight approvals. For operating comparisons with the A150K, the standard-model cruise table is not Aerobat performance evidence. Retaining category, tank configuration and source conditions avoids making the superficially similar aircraft appear interchangeable in a loading or performance question.

The standard K and A150K also demonstrate why an engine comparison is insufficient for an Aerobat purchase. Their nominal O-200-A power is similar, but the category, serial sequence, propeller relationship and operating limitations are separately established. The standard K's spinner breakpoint is a component distinction inside its own range, not a rule for the A150K or French K sequences. If a records collection uses only the phrase "1970 150", resolve which identity it actually concerns before interpreting the combined D727-13 / D740-13 manual lead. The source should decide the relationship, not the apparent similarity of the aircraft or handbook cover.

150K: 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]
150K: 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]
150K: model year specifications
YearModel(s)Max SpeedCruiseROC SLCeilingPublished Gross / MTOWPublished Empty WeightBaggageNotesSource
1970150K/A150K122 mph; 125 Commuter117 mph @75% /7000 ft670 fpm12,650 ft1600 lb975 Std; 1060 Commuter120 lbA150 certification limits stored separately.[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 150K example is 1970 cruise speed: 117 mph (power % 75; altitude ft 7000). 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 150K.

150K: performance
YearModelValueUnitsPower %Altitude ftFuel Usable galReserve BasisObstacle ftCondition NoteSource
1970150K122mph-----Published headline value[1]
1970150K117mph757000---Published headline condition[1]
1970150K670fpm------[1]
1970150K12650ft------[1]
1970150K735ft------[1]
1970150K1385ft----50-[1]
1970150K445ft------[1]
1970150K1075ft----50-[1]

Manuals, Maintenance and Research

The K publication lead lists D727-13 / D740-13 as a combined standard/Aerobat family. It deliberately does not authorize using either copy for every K-marked aircraft. Resolve the title, aircraft coverage and amendments, then use the serial record and spinner boundary to orient the parts research. The next standard generation is the multi-year 150L; its tubular-gear history belongs in that comparison rather than being attributed to the K. The Reims F150K and FA150K add another authority and serial namespace, so a bare "K model" description is insufficient for document selection. The positive 150K publication leads are 1970: D727-13 / D740-13 (Owner's Manual).

150K: handbook applicability
Family / YearModelPublicationDocument ClassSerial / Year EffectivityAuthority BasisOperational StatusSpecial BoundaryReference
1970150K/A150K/F150K/FA150KD727-13 / D740-13Owner's ManualStandard vs Aerobat familyCAA TAR 98/08 + FAA 3A19Authority-recognized familyA150K acrobatic speeds differ[1]

Related Models and Technical Research

Use the 150K-versus-150L comparison to separate the landing-gear generation from smaller serial-dependent component changes. The 150K and A150K comparison explains why a shared engine and model year do not establish the same certified identity.