Reims/Cessna F150L Model Reference
The F150L spans several Reims model-year groups and multiple propeller-application conditions. That makes a single generic L-series specification particularly unhelpful. The exact year/configuration field should remain visible when a reader compares an application or selects a handbook family.

Four French model years within one standard identity
The standard French L spans 1971-1974 between F150K and F150M. It is a longer production chapter than the preceding annual letter groups. Within that chapter, handbook and propeller applications retain their year or configuration qualifications. The shared L suffix with the U.S. aircraft is historical orientation, not proof that a U.S. component breakpoint is also a French one.
The distinction from FA and FRA aircraft is especially useful during these years. F150L remains the standard Reims line, while FA150L and FRA150L address Aerobat and conditional higher-power identities. The engine overview explains the larger installation families. A reader can then compare the French L branches without mistaking their common period for a common engine, category or operating-document approval.
| Model Years | 1971-1974 |
|---|---|
| Certification Category | Utility |
| Certified Serial Eligibility | F15000659-F15001143 |
| Type-design engine context | Rolls-Royce Continental O-200-A |
Generation and Certification
The standard F150L is distinct from the FA150L/FRA150L configuration-dependent relationship. A common letter does not prove the higher-power configuration or its associated documents. This page retains only the exact F150L relationships and leaves unsupported U.S.-to-Reims technical inheritance unresolved.
F150L is the multi-year standard Reims L identity, covering 1971-1974 rather than one annual French model. The F15000659-F15001143 eligibility contains successive year groups and application conditions. A comparison with F150K should therefore focus on the expanded year/document coverage as well as the L-generation context. Standard U.S. L gear and cockpit changes require their own evidence before being described as French serial changes; the shared suffix does not provide that evidence by itself.
F150L is recorded as Standard in the Utility category, with model years 1971-1974 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 1970-10-09, 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 |
|---|---|---|---|---|---|---|
| F150L | A13EU | Utility | 1970-10-09 | CAR 3 (1956-05-15) amended 3-4 | - | [1] |

Serial Numbers and Production
For F150L, the ordinary source assignments are 1971: F15000659 through F15000738; 1972: F15000739 through F15000863; 1973: F15000864 through F15001013; 1974: F15001014 through F15001143. 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 |
|---|---|---|---|---|---|---|
| 1971 | F150L | F15000659 | F15000738 | - | - | [1] |
| 1972 | F150L | F15000739 | F15000863 | - | - | [1] |
| 1973 | F150L | F15000864 | F15001013 | - | - | [1] |
| 1974 | F150L | F15001014 | F15001143 | - | - | [1] |
Engine, Propeller and Equipment Changes
The F150L propeller table contains multiple year/configuration entries. Their dates and conditions are valuable because a single "O-200 propeller" description cannot choose among them. The standard F150L remains separate from the FA150L/FRA150L higher-power question, whose base prefix and kit conditions are different. Retaining these relationships makes the page useful to an owner comparing two French L aircraft: the correct handbook and propeller context can differ even before later modifications are considered.
The F150L factory installation groups specify 1971: O-200-A, 100 hp at 2750 RPM; 1972: O-200-A, 100 hp at 2750 RPM; 1973: O-200-A, 100 hp at 2750 RPM; 1974: O-200-A, 100 hp at 2750 RPM. Its named propeller applications are 1A101/GCM6948; 1A101/HCM6948; 1A101/PCM6948; 1A102/OCM6948. 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 | 1971 | F150L | O-200-A | 100 | 2750 | F15000659 | F15000738 | Factory / type-design | [1] |
| France | 1972 | F150L | O-200-A | 100 | 2750 | F15000739 | F15000863 | Factory / type-design | [1] |
| France | 1973 | F150L | O-200-A | 100 | 2750 | F15000864 | F15001013 | Factory / type-design | [1] |
| France | 1974 | F150L | O-200-A | 100 | 2750 | F15001014 | F15001143 | Factory / type-design | [1] |
| Aircraft Model | Model Year / Config | Engine | Exact Propeller Application | Max Dia | Min Dia | Static Min | Static Max | Notes | Primary Authority |
|---|---|---|---|---|---|---|---|---|---|
| F150L | 1971-1973 | O-200-A | 1A101/GCM6948 | 69 | 67 | 2500 | 2600 | - | [1] |
| F150L | 1973-1974 | O-200-A | 1A101/HCM6948 | 69 | 67 | 2500 | 2600 | Different from U.S. year effectivity. | [1] |
| F150L | 1974 | O-200-A | 1A101/PCM6948 | 69 | 67 | 2500 | 2600 | - | [1] |
| F150L | 1971-1974 | O-200-A | 1A102/OCM6948 | 69 | 67.5 | 2460 | 2560 | - | [1] |

Manuals, Maintenance and Research
The recognized manual leads progress through the 1971, 1972, 1973 and 1974 publication families. The last mapping explicitly excludes automatic FRA inheritance. Use the aircraft's year/serial relationship to select a candidate copy, then establish the French authority and supplement coverage. Exact F150L certified CG and performance tables are not supplied by the U.S. L summaries. The succeeding standard F150M offers another year and handbook boundary; the dedicated Reims guide provides the broader explanation of why these French identities remain distinct. The positive F150L publication leads are 1971: D836-13 / D839-13 (Owner's Manual); 1972: D901-13 / D900-13 (Owner's Manual); 1973: D962-13 / D963-13 (Owner's Manual); 1974: D1013-13 / D1014-13 (Owner's Manual).
| Family / Year | Model | Publication | Document Class | Serial / Year Effectivity | Authority Basis | Operational Status | Special Boundary | Reference |
|---|---|---|---|---|---|---|---|---|
| 1971 | 150L/A150L/F150L/FA150L | D836-13 / D839-13 | Owner's Manual | Standard vs Aerobat family | CAA TAR 98/08 + FAA 3A19 | Authority-recognized family | A150L acrobatic category | [1] |
| 1972 | 150L/A150L/F150L/FA150L | D901-13 / D900-13 | Owner's Manual | Standard vs Aerobat family | CAA TAR 98/08 + FAA 3A19 | Authority-recognized family | Argentina technical equivalence only | [1] |
| 1973 | 150L/A150L/F150L/FA150L | D962-13 / D963-13 | Owner's Manual | Standard vs Aerobat family | CAA TAR 98/08 + FAA 3A19 | Authority-recognized family | Argentina technical equivalence only | [1] |
| 1974 | 150L/A150L/F150L | D1013-13 / D1014-13 | Owner's Manual | Standard vs Aerobat family | CAA TAR 98/08 + FAA 3A19 | Authority-recognized family | No FRA inheritance | [1] |
Related Models and Technical Research
Consult the GCM/HCM/PCM application comparison for the Reims HCM year range, which differs from the U.S. entry. The F150L-versus-FRA150L comparison distinguishes the standard engine path from the O-240 Aerobat configuration and its document evidence.