Reims/Cessna FRA150L Aerobat Model Reference
The FRA150L is a configuration-sensitive Reims identity associated with a higher-power engine context. The source explicitly connects it with eligible FA150L aircraft under the prescribed kit conditions. Serial eligibility therefore narrows the question but does not by itself establish the configuration of an individual aircraft.

A higher-power French branch with conditional identity
FRA150L belongs to the 1972-1974 higher-power Reims Aerobat story, ahead of FRA150M. Its relationship to FA150L is not simply the next letter in a standard model series. The documented kit conditions connect eligible FA identities with the FRA configuration, and the O-240 context distinguishes the branch from the familiar O-200-powered Aerobats.
The Reims development history describes why this aircraft deserves more than the label French 150. Its engine, aircraft approval and dedicated flight-manual relationships form a coherent configuration question. The engine-installation references provide the broader comparison, but an eligible serial still does not establish which equipment is present. The distinction between a possible configuration and an established aircraft identity is central to reading this profile.
| Model Years | 1972-1974 |
|---|---|
| Certification Category | Acrobatic |
| Certified Serial Eligibility | FRA1500121-FRA1500261; or FA1500121-FA1500261 when equipped with FKA150-2311 and FKA150-2316 |
| Type-design engine context | Rolls-Royce Continental O-240-A |
Generation and Certification
This model has its own engine, propeller and authority-recognized flight-manual relationships. Those relationships are the useful reason for a separate technical reference. They must be applied as a coherent configuration rather than mixed with base FA150L values or U.S. Aerobat documents. The actual kit and aircraft records remain necessary.
FRA150L covers the 1972-1974 higher-power Reims Aerobat identity. Its certification eligibility includes FRA1500121-FRA1500261 and the corresponding FA-prefix range when the prescribed kits are installed. This is not a second batch of aircraft to add to the FA history. It is a configuration-qualified way to establish the legal identity. The relationship differs from both standard F150L and the ordinary 1971 FA150L interval, which is why the full prefix and equipment evidence matter in a model comparison.
FRA150L is recorded as Aerobat / higher-power configuration in the Acrobatic category, with model years 1972-1974 and approval context A13EU. The manufacturer entry is Reims Aviation S.A. (Reims-Cessna); the manufacture/assembly location is Reims-Prunay, France. Its approval date is 1971-12-03, a model approval event rather than an individual aircraft's manufacture date.
| Model | TC | Category | Initial Model Approval Date | Core Cert Basis | Certification / Identity Note | Reference |
|---|---|---|---|---|---|---|
| FRA150L | A13EU | Acrobatic | 1971-12-03 | CAR 3 (1956-05-15) amended 3-4 | Higher-power Rolls-Royce Continental O-240 configuration | [1] |

Serial Numbers and Production
For FRA150L, the ordinary source assignments are 1972: FRA1500121 through FRA1500166; 1973: FRA1500167 through FRA1500211; 1974: FRA1500212 through FRA1500261. The serial guide retains source conflicts and exceptional identities alongside these intervals.
| Model Year | Official Model | Serial Start | Serial End | Excluded / Override Serials | Notes | Primary Source |
|---|---|---|---|---|---|---|
| 1972 | FRA150L | FRA1500121 | FRA1500166 | - | - | [1] |
| 1973 | FRA150L | FRA1500167 | FRA1500211 | - | - | [1] |
| 1974 | FRA150L | FRA1500212 | FRA1500261 | - | - | [1] |
| Range / Serial Family | Base Prefix Identity | Possible Certified Identity | Condition | Primary Source |
|---|---|---|---|---|
| FA1500121-FA1500261 | FA150L | FRA150L | With FKA150-2311 and FKA150-2316 per A13EU. | [1] |
Engine, Propeller and Equipment Changes
The O-240 installation is the central technical reason to follow the FRA150L reference instead of borrowing O-200 Aerobat specifications. It has its own power/RPM context and propeller application. A higher engine-manufacturer rating must still be distinguished from the aircraft-installed rating stated in the records below. The two named kits, FKA150-2311 and FKA150-2316, remain part of the eligibility condition for FA-prefix aircraft. An engine description in an advertisement alone does not establish that complete approval relationship.
The FRA150L factory installation groups specify 1972: O-240-A, 130 hp at 2800 RPM; 1973: O-240-A, 130 hp at 2800 RPM; 1974: O-240-A, 130 hp at 2800 RPM. Its named propeller applications are 1A135/BRM7150. Their diameter, static-RPM and configuration conditions are preserved together below.
| Origin | Model Year | Aircraft Model | Factory Engine | Installed hp | RPM Limit | First Serial in Group | Last Serial in Group | Applicability Basis | Aircraft Source |
|---|---|---|---|---|---|---|---|---|---|
| France | 1972 | FRA150L | O-240-A | 130 | 2800 | FRA1500121 | FRA1500166 | A13EU FRA150L / eligible FA150L with FKA150-2311 and FKA150-2316 | [1] |
| France | 1973 | FRA150L | O-240-A | 130 | 2800 | FRA1500167 | FRA1500211 | A13EU FRA150L / eligible FA150L with FKA150-2311 and FKA150-2316 | [1] |
| France | 1974 | FRA150L | O-240-A | 130 | 2800 | FRA1500212 | FRA1500261 | A13EU FRA150L / eligible FA150L with FKA150-2311 and FKA150-2316 | [1] |
| Aircraft Model | Model Year / Config | Engine | Exact Propeller Application | Max Dia | Min Dia | Static Min | Static Max | Notes | Primary Authority |
|---|---|---|---|---|---|---|---|---|---|
| FRA150L | FRA configuration | O-240-A | 1A135/BRM7150 | 71 | 70 | 2400 | 2500 | 130 hp Reims Aerobat configuration. | [1] |

Manuals, Maintenance and Research
D1015-13GB is the dedicated SGAC-approved AFM family for the L configuration. Its role differs from the standard/Aerobat owner's-manual families listed for the base models. Exact U.S. 150L performance, CG and speed tables are not substitutes for that AFM. Before comparing an FRA150L with the later FRA150M, identify the engine variant, applicable propeller and complete flight-manual coverage. This produces a coherent higher-power-aircraft comparison while leaving unresolved limits explicit rather than assembling a favorable specification from unrelated variants. The positive FRA150L publication leads are 1972-74: D1015-13GB (SGAC-approved AFM).
| Family / Year | Model | Publication | Document Class | Serial / Year Effectivity | Authority Basis | Operational Status | Special Boundary | Reference |
|---|---|---|---|---|---|---|---|---|
| 1972-74 | FRA150L | D1015-13GB | SGAC-approved AFM | FRA1500121-FRA1500261 | CAA TAR 96/09 / Reims SGAC basis | Dedicated approved AFM family | Never inherit U.S. 150L/A150L performance automatically | [1] |
| Publication | Title | Document Class | Model Applicability | Years | Serial Effectivity | Revision Context | Authority Status | Use Boundary | Reference |
|---|---|---|---|---|---|---|---|---|---|
| D1015-13GB | Reims/Cessna FRA150L SGAC-Approved Aircraft Flight Manual | Aircraft Flight Manual | FRA150L | 1972-1974 | FRA1500121 through FRA1500261 | SGAC-approved publication family | Approved Reims flight manual | Authority-recognized flight manual; exact aircraft supplements/amendments control | [1] |
Related Models and Technical Research
The F150L-versus-FRA150L comparison distinguishes the standard engine path from the O-240 Aerobat configuration and its document evidence.