Cessna A152 Aerobat: Identity, Exceptions and Technical Guide
The U.S. A152 Aerobat is a separate Acrobatic-category identity with two exceptional serial cases and its own certified-speed group. It was approved alongside the standard 152, but it should not be treated as a standard aircraft with a sales label added. Serial research, loading groups and handbook selection all need the Aerobat relationship to remain explicit.

The U.S. Aerobat enters the O-235 era
After A150M, the A152 carries the U.S. Aerobat branch into the later Lycoming-powered family. Its 1978-1985 model-year span runs alongside the standard 152, with the separate Acrobatic identity retained. This is a succession within the Aerobat line, not evidence that the standard 152 became aerobatic when the A152 was introduced.
The 152-versus-A152 comparison answers the category question within the same period. Comparing A152 with the earlier A150M adds an engine-generation question, while comparing it with French FA152 adds origin and approval context. Keeping those comparisons separate makes a broad Aerobat search considerably more informative.
The exceptional A150-prefixed identity and the short-serial notation case are particularly important here because they can obscure which generation an aircraft belongs to. They do not create additional model variants. The flying explanation connects the general aircraft concepts with the need for precise approval context, while this page retains the exact exceptions, engine relationships and Aerobat documentation.
| Model Years | 1978-1985 |
|---|---|
| Certification Category | Acrobatic |
| Certified Serial Eligibility | A1500433; 681; A1520735-A1521049 |
| Type-design engine context | Lycoming O-235-L2C through A1521014; O-235-N2C from A1521015 and on, or aircraft reworked per SK152-15 / SK152-16 |
Compare it with the standard U.S. 152 and Reims FA152 without merging their authority or document scope. The family model guide explains those distinctions, while the serial reference preserves the full exceptional-identity evidence.
Certification and Model-Year Context
the identity records 1978-1985 model-year coverage and approval on 16 March 1977 under 3A19. Approval date is a certification event, while model-year ranges organize production identity. Neither establishes an individual aircraft's delivery date or present configuration.
| Official Model | Public Name | Model Years | Variant Type | Certification Category | Historical Manufacturer | Country of Manufacture | Primary Type Certificate |
|---|---|---|---|---|---|---|---|
| A152 | Cessna A152 Aerobat | 1978-1985 | Aerobat | Acrobatic | Cessna Aircraft Company | United States | 3A19 |
| Model | TC | Category | Initial Model Approval Date | Core Cert Basis | Certification / Identity Note | Reference |
|---|---|---|---|---|---|---|
| A152 | 3A19 | Acrobatic | 1977-03-16 | CAR 3 (1956-05-15) amended 3-4 | Special S/N 681 is part of the later FAR 23.1559 trigger set. | [1] |

A1500433 and the 681 Notation Case
A1500433 belongs to A152 despite its A150 prefix and is excluded from the A150L ordinary range. The exceptional identity must take priority over a prefix or interval-only lookup. Otherwise, later engine, manual and loading research could start from the wrong legal model.
The short serial 681 and later notation A15200681 are retained as one source-qualified exceptional case. Their coexistence is not evidence of two aircraft. Do not invent a general zero-padding rule from this particular relationship or count every spelling as separate physical production.
| Serial | Legal Model | Model Year | Effect | Primary Source |
|---|---|---|---|---|
| A1500433 | A152 | 1978 | Explicitly excluded from A150L and carried as A152. | [1] |
| 681 / A15200681 | A152 | 1979 | TCDS uses 681; later FAA material may normalize as A15200681. | [1] |
| Model Year | Official Model | Serial Start | Serial End | Excluded / Override Serials | Notes | Primary Source |
|---|---|---|---|---|---|---|
| 1978 | A152 | A1520735 | A1520808 | - | - | [1] |
| 1979 | A152 | A1520809 | A1520878 | - | - | [1] |
| 1980 | A152 | A1520879 | A1520943 | - | FAA TCDS assigns A1520879-A1520943 to 1980; Cessna 152 Service Manual extends 1980 through A1520948. | [1] |
| 1981 | A152 | A1520944 | A1520983 | - | FAA TCDS assigns A1520944-A1520983 to 1981; Cessna 152 Service Manual begins 1981 at A1520949. | [1] |
| 1982 | A152 | A1520984 | A1521014 | - | - | [1] |
| 1983 | A152 | A1521015 | A1521025 | - | - | [1] |
| 1984 | A152 | A1521026 | A1521027 | - | - | [1] |
| 1985 | A152 | A1521028 | A1521049 | - | - | [1] |
A Disputed Model-Year Boundary
The source preserves disagreement over A1520944-A1520948 between the FAA and manufacturer year boundaries. Its primary treatment follows the TCDS while keeping the competing evidence visible. This is a model-year research distinction, not proof of an exact calendar manufacture date.
For a handbook or service-table question in that interval, retain the conflict and examine the aircraft documents. A convenient adjacent-year copy is not an adequate reason to suppress the discrepancy. The manuals guide explains the additional title-page and revision checks.
| Subject | Affected Serials | Source A Result | Source B Result | Model assignment | Reason | Source A | Source B |
|---|---|---|---|---|---|---|---|
| A152 1980/1981 model-year boundary | A1520944-A1520948 | FAA TCDS: 1980 A1520879-A1520943; 1981 A1520944-A1520983 | Cessna SM: 1980 through A1520948; 1981 starts A1520949 | Use FAA TCDS for primary year lookup; flag A1520944-A1520948. | TCDS is certification authority; manufacturer conflict is preserved. | [1] | [2] |
| A150L sequence override | A1500433 | A1500433 excluded from A150L | Naive range includes it | Special override to A152. | Explicit authority listing overrides numeric inference. | [1] | [3] |
Engine and Propeller Relationships
The source changes the factory engine relationship from O-235-L2C through A1521014 to N2C from A1521015, while also recognizing approved rework. The engine guide distinguishes the aircraft ratings from engine-manufacturer figures. The installed engine must still be established from its identification and records.
The McCauley application remains attached to its actual engine and aircraft conditions. Shared propeller values do not erase the Aerobat's separate operating category or prove component compliance. The propeller guide provides the installation and hub-research context.
| Origin | Model Year | Aircraft Model | Factory Engine | Installed hp | RPM Limit | First Serial in Group | Last Serial in Group | Applicability Basis | Aircraft Source |
|---|---|---|---|---|---|---|---|---|---|
| USA | 1978 | A152 | O-235-L2C | 110 | 2550 | A1520735 | A1520808 | Factory / type-design | [1] |
| USA | 1978 | A152 | O-235-L2C | 110 | 2550 | A1500433 | A1500433 | Factory / type-design special serial | [1] |
| USA | 1979 | A152 | O-235-L2C | 110 | 2550 | A1520809 | A1520878 | Factory / type-design | [1] |
| USA | 1979 | A152 | O-235-L2C | 110 | 2550 | 681 | A15200681 | Factory / type-design special serial | [1] |
| USA | 1980 | A152 | O-235-L2C | 110 | 2550 | A1520879 | A1520943 | Factory / type-design | [1] |
| USA | 1981 | A152 | O-235-L2C | 110 | 2550 | A1520944 | A1520983 | Factory / type-design | [1] |
| USA | 1982 | A152 | O-235-L2C | 110 | 2550 | A1520984 | A1521014 | Factory / type-design | [1] |
| USA | 1983 | A152 | O-235-N2C | 108 | 2550 | A1521015 | A1521025 | Factory/approved rework per 3A19 | [1] |
| USA | 1984 | A152 | O-235-N2C | 108 | 2550 | A1521026 | A1521027 | Factory/approved rework per 3A19 | [1] |
| USA | 1985 | A152 | O-235-N2C | 108 | 2550 | A1521028 | A1521049 | Factory/approved rework per 3A19 | [1] |
| Aircraft Model | Model Year / Config | Engine | Exact Propeller Application | Max Dia | Min Dia | Static Min | Static Max | Notes | Primary Authority |
|---|---|---|---|---|---|---|---|---|---|
| 152/A152 | All | O-235-L2C/N2C | 1A103/TCM6958 | 69 | 67.5 | 2280 | 2380 | Spinner Dwg 0450073 in aircraft TCDS. | [1] |

Aerobat Limits and Loading
The A152 certified-speed group is separate from standard Model 152. Its weight-and-balance groups also expressly place A1500433 in the early group and 681 in the later group. Those relationships demonstrate why exceptional identities must survive every later technical lookup.
A later ramp allowance is not a higher takeoff allowance, and a shared weight figure does not establish every operating or maneuver condition. Current aircraft documentation, actual empty weight and configuration are needed. An installed alteration can also introduce limitations that the Aerobat model name does not cancel.
| Models | Category | Speed Basis | Vne | Vno | Va | Vfe | MTOW Land lb | MTOW Sea lb | Baggage lb | Source |
|---|---|---|---|---|---|---|---|---|---|---|
| A152 | Acrobatic | IAS | 172 kt | 125 kt | 108 kt | 85 kt | 1670 | - | 120 | [1] |
| Models / Serial Applicability | Config | Category | Ramp lb | TO lb | Landing lb | Fwd CG light | Light wt | Fwd CG heavy | Heavy wt | Aft CG | Baggage | Datum / Reference | Leveling | Source |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| A1500433; A1520735-A1520808 | Land | Acrobatic | - | 1670 | 1670 | 31 | 1350 | 32.65 | 1670 | 36.5 | Area 1 120; Area 2 40; combined 120 | Firewall front face Sta 0.0 | Jig points +94.63/+132.94 | [1] |
| 681; A1520809 and on | Land | Acrobatic | 1675 | 1670 | 1670 | 31 | 1350 | 32.65 | 1670 | 36.5 | Area 1 120; Area 2 40; combined 120 | Firewall front face Sta 0.0 | Jig points +94.63/+132.94 | [1] |
Publications and Remaining Evidence Boundaries
The handbook and document rows below explicitly name A152, including standard/Aerobat family boundaries. A paired publication entry is not permission to choose either manual without checking its model and aircraft scope. The 3A19 reference supplies identity authority rather than a complete operational document.
| Family / Year | Model | Publication | Document Class | Serial / Year Effectivity | Authority Basis | Operational Status | Special Boundary | Reference |
|---|---|---|---|---|---|---|---|---|
| 1978 | 152/A152 | D1107-13 / D1108-13 | POH/AFM | 1978 serial ranges | FAA 3A19 + CAA TAR | Approved handbook basis | A152 acrobatic category | [1] |
| 1979 | 152/A152 | D1136-13PH / D1137-13PH | POH/AFM | 1979 serial ranges | FAA 3A19 + CAA TAR | Approved handbook basis | Generic Information Manual not legal substitute | [2] |
| 1980 | 152/A152 | D1170-13PH / D1171-13PH | POH/AFM | 1980 serial ranges | FAA 3A19 + CAA TAR | Approved base family | Information-manual warning applies | [1] |
| 1981 | 152/A152 | D1190-13PH / D1191-13PH | POH/AFM | 1981 serial ranges | FAA 3A19 + CAA TAR | Approved base family | Aircraft title-page serial controls | [3] |
| 1982 | 152/A152 | D1210-13PH / D1211-13PH | POH/AFM | 1982 serial ranges | FAA 3A19 + CAA TAR | Approved base family | A152 D1211-1 lineage known | [1] |
| 1983 | 152/A152 | D1229-13PH / D1230-13PH | POH/AFM | 1983 serial ranges | FAA 3A19 + CAA TAR | Approved family | O-235-N2C transition | [4] |
| 1984 | 152/A152 | D1249-13PH / D1250-13PH | POH/AFM | 1984 serial ranges | FAA 3A19 + CAA TAR | Approved family | Do not infer full table from checklist alone | [5] |
| 1985 / Reims 1986 serials | 152/A152/F152/FA152 | D1270-13PH / D1271-13PH | POH/AFM | 1985 U.S.; authority serial effectivity includes Reims 1986 production | FAA 3A19 + CAA TAR | Approved/authority-recognized family | Reims serial effectivity, not production-year guess | [6] |
| Publication | Title | Document Class | Model Applicability | Years | Serial Effectivity | Revision Context | Authority Status | Use Boundary | Reference |
|---|---|---|---|---|---|---|---|---|---|
| D1108-13 | A152 / FA152 (1978) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1978 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D1137-13PH | A152 / FA152 (1979) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1979 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D1171-13PH | A152 / FA152 (1980) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1980 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D1191-13PH | A152 / FA152 (1981) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1981 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D1211-13PH | A152 / FA152 (1982) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1982 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D1230-13PH | A152 / FA152 (1983) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1983 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D1250-13PH | A152 / FA152 (1984) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1984 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D1271-13PH | A152 / FA152 (1985) Pilot's Operating Handbook | Pilot's Operating Handbook | A152 / FA152 | 1985 | Model-year / exact serial-specific handbook controls | Publication family | Current historical publication family | FAA-approved aircraft handbook when issued for the specific airplane; generic information manual is not a replacement | [1] |
| D2064-1-13 | Model 152 Series 1978 Thru 1985 Service Manual | Service Manual | 152, A152, F152, FA152 | 1978-1986 Reims coverage noted in manual | Use the effectivity/cross-reference pages inside the publication; do not infer from model family alone | Revision 1 | Technical publication family | Maintenance/parts reference; latest revision/temporary revision controls | [2] |
| P692-12 | 152 (1978-1985) Parts Catalog | Illustrated Parts Catalog | 152 / A152 / F152 / FA152 | 1978-1985 | Use the effectivity/cross-reference pages inside the publication; do not infer from model family alone | Original issue | Technical publication family | Maintenance/parts reference; latest revision/temporary revision controls | [3] |
| D4601-13 | 152/A152/172/R172/172RG (1979-1982) Avionics Installation Service/Parts Manual | Avionics Installation / Parts | 152/A152 | 1979-1982 | Aircraft/configuration-specific where applicable | Original issue | Technical publication / aircraft record | Use only where configuration/effectivity matches; serialized records take precedence | [1] |
| D4608-13 | 152/A152/172/R172/172RG (1983-1984) Avionics Installation Service/Parts Manual | Avionics Installation / Parts | 152/A152 | 1983-1984 | Aircraft/configuration-specific where applicable | Original issue + TR1 | Technical publication / aircraft record | Use only where configuration/effectivity matches; serialized records take precedence | [1] |
The detailed performance series in the family reference names standard Model 152 and is not inherited here. Use the actual Aerobat handbook and supplements for performance. Likewise, ADs and known issues require their own installed-equipment and effectivity decisions. This page establishes source relationships, not current equipment, condition or compliance.
Compare the Four Model Identities
The AD 80-06-03 reference explicitly retains A1500433 in its A152 cable-clamp context. The prefix must not override the accepted special identity. The 152-versus-A152 comparison connects category, engine effectivity and exceptional serials with the correct aircraft records.