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2020-25-12: Reciprocating Engine Power Section

FAA order 2020-25-12 is an airworthiness directive in force since January 15, 2021. The FAA's subject line: Reciprocating Engine Power Section. It names the Lycoming AEIO-360-H1A, Lycoming IO-360-B1B, Lycoming IO-360-B1D, Lycoming IO-360-B1E, Lycoming IO-360-B1F, Lycoming IO-360-B2F, Lycoming IO-360-L2A, Lycoming IO-360-M1A, Lycoming IO-360 series, Lycoming O-360-A1A, Lycoming O-360-A1D, Lycoming O-360-A2A, Lycoming O-360-A2D, Lycoming O-360-A2F, Lycoming O-360-A2G, Lycoming O-360-B2A, Lycoming O-360-C1A, Lycoming O-360-C1E, Lycoming O-360-C1F, Lycoming O-360-C1G, Lycoming O-360-C2A, Lycoming O-360-C2C, Lycoming O-360-C2D, Lycoming O-360-C2E, Lycoming O-360-D2A, Lycoming O-360 series, Superior Air Parts IO-360-B1A2, Superior Air Parts IO-360 series, Superior Air Parts O-360-A3A2, Superior Air Parts O-360 series, Superior Air Parts O360B1A2 engines: about 15,399 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Engine
Makes
Superior Air Parts Inc.; Lycoming Engines
Models
IO-360-A1A1, IO-360-A1A2, IO-360-A2A1, IO-360-A2A2, IO-360-A3A1, IO-360-A3A2, IO-360-A4A1, IO-360-A4A2, IO-360-A5A1, IO-360-A5A2, IO-360-A6A1, IO-360-A6A2, IO-360-B1A1, IO-360-B1A2, IO-360-B2A1, IO-360-B2A2, IO-360-B3A1, IO-360-B3A2, IO-360-B4A1, IO-360-B4A2, IO-360-B5A1, IO-360-B5A2, IO-360-B6A1, IO-360-B6A2, IO-360-C1A1, IO-360-C1A2, IO-360-C2A1, IO-360-C2A2, IO-360-C3A1, IO-360-C3A2, IO-360-C4A1, IO-360-C4A2, IO-360-C5A1, IO-360-C5A2, IO-360-C6A1, IO-360-C6A2, IO-360-D1A1, IO-360-D1A2, IO-360-D2A1, IO-360-D2A2, IO-360-D3A1, IO-360-D3A2, IO-360-D4A1, IO-360-D4A2, IO-360-D5A1,...
Engine series
Lycoming AEIO-360-H1A 8 aircraft
Lycoming IO-360-B1B 67 aircraft
Lycoming IO-360-B1D 2 aircraft
Lycoming IO-360-B1E 184 aircraft
Lycoming IO-360-B1F 8 aircraft
Lycoming IO-360-B2F 1 aircraft
Lycoming IO-360-L2A 2,634 aircraft
Lycoming IO-360-M1A 549 aircraft
Lycoming IO-360 series 8,560 aircraft
Lycoming O-360-A1A 600 aircraft
Lycoming O-360-A1D 1,057 aircraft
Lycoming O-360-A2A 38 aircraft
Lycoming O-360-A2D 5 aircraft
Lycoming O-360-A2F 13 aircraft
Lycoming O-360-A2G 3 aircraft
Lycoming O-360-B2A 3 aircraft
Lycoming O-360-C1A 7 aircraft
Lycoming O-360-C1E 5 aircraft
Lycoming O-360-C1F 102 aircraft
Lycoming O-360-C1G 142 aircraft
Lycoming O-360-C2A 19 aircraft
Lycoming O-360-C2C 6 aircraft
Lycoming O-360-C2D 2 aircraft
Lycoming O-360-C2E 5 aircraft
Lycoming O-360-D2A 4 aircraft
Lycoming O-360 series 1,066 aircraft
Superior Air Parts IO-360-B1A2 9 aircraft
Superior Air Parts IO-360 series 201 aircraft
Superior Air Parts O-360-A3A2 3 aircraft
Superior Air Parts O-360 series 92 aircraft
Superior Air Parts O360B1A2 4 aircraft

Dates and paperwork

In force since
January 15, 2021
Published
December 11, 2020 (signed December 3, 2020)
Docket
FAA-2018-1077
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for all Superior Air Parts, Inc. (SAP) Model IO-360-series and O-360-series reciprocating engines and certain Lycoming Engines (Lycoming) Model AEIO-360-, IO-360-, and O-360-series reciprocating engines with a certain SAP crankshaft assembly installed. This SAP crankshaft assembly is installed as original equipment on the affected SAP engines and as a replacement part under parts manufacturer approval (PMA) on the affected Lycoming engines. This AD was prompted by three crankshaft assembly failures that resulted in the loss of engine power and immediate or emergency landings. This AD requires the removal from service of all affected crankshaft assemblies. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,265 characters)
The Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive: \n\n2020-25-12 Superior Air Parts, Inc.: Amendment 39-21354; Docket No. FAA-2018-1077; Project Identifier 2018-NE-40-AD. \n\n(a) Effective Date \n\n\n\tThis airworthiness directive (AD) is effective January 15, 2021. \n\n(b) Affected ADs \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to the reciprocating engine models identified in paragraphs (c)(1) and (2) of this AD with a Superior Air Parts, Inc. (SAP) crankshaft assembly, part number (P/N) SL36500-A20 or P/N SL36500-A31, with serial numbers 82976-01; 82976-02; SP12-0003 through SP12-0089, inclusive; SP13-0034 through SP13-0150, inclusive; or SP14-0151 through SP14-0202, inclusive; installed. \n\t(1) With SAP crankshaft assembly, P/N SL36500-A20, installed: \n\t(i) SAP Model IO-360-series and O-360-series reciprocating engines. \n\t(ii) Lycoming Engines (Lycoming) Model IO-360-B2F, IO-360-L2A, O-360, O-360-A2A, O-360-A2D, O-360-A2E, O-360-A2F, O-360-A2G, O-360- B2A, O-360-C2A, O-360-C2C, O-360-C2D, O-360-C2E, O-360-D2A, and O- 360-D2B reciprocating engines. \n\t(2) With SAP crankshaft assembly, P/N SL36500-A31, installed: \n\t(i) SAP Model IO-360-series and O-360-series reciprocating engines. \n\t(ii) Lycoming Model AEIO-360-H1A, IO-360-B1A, IO-360-B1B, IO- 360-B1D, IO-360-B1E, IO-360-B1F, IO-360-M1A, O-360, O-360-A1A, O- 360-A1C, O-360-A1D, O-360-A2A, O-360-C1A, O-360-C1G, O-360-C1C, O- 360-C1E, and O-360-C1F reciprocating engines. \n\tNote 1 to paragraph (c): This SAP crankshaft assembly may be installed as a replacement part under parts manufacturer approval on the affected Lycoming engines. \n\n(d) Subject \n\n\n\tJoint Aircraft System Component (JASC) Code 8520, Reciprocating Engine Power Section. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by three crankshaft assembly failures that resulted in the loss of engine power and immediate or emergency landings. The FAA is issuing this AD to prevent failure of the crankshaft assembly. The unsafe condition, if not addressed, could result in failure of the engine, in-flight shutdown, and loss of the airplane. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Required Action \n\n\n\tWithin 25 engine operating hours after the effective date of this AD, remove the crankshaft assembly from service. \n\n(h) Special Flight Permit \n\n\n\tA one-time special flight permit may be issued to fly the aircraft to a maintenance facility to perform the actions of this AD with the following limitations: No passengers, visual flight rules (VFR) day conditions only, and avoid areas of known turbulence. \n\n(i) Alternative Methods of Compliance (AMOCs) \n\n\n\t(1) The Manager, Fort Worth ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in Related Information. \n\t(2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. \n\n(j) Related Information \n\n\n\tFor more information about this AD, contact Justin Carter, Aviation Safety Engineer, Fort Worth ACO Branch, FAA, 10101 Hillwood Parkway, Fort Worth, TX 76177; phone: (817) 222-5146; fax: (817) 222-5245; email: justin.carter@faa.gov.(k) Material Incorporated by Reference \n\n\n\tNone. \n\n\n\tIssued on December 3, 2020. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. (FR Doc. 2020-27149 Filed 12-10-20; 8:45 am) BILLING CODE 4910-13-P

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2020-25-12.json · aircraft systems.