Public Record · As of May 5, 2026
N2865H
Ercoupe 415-C · 1946 View Type →
Status
Registration Valid
Type
Fixed Wing Single Engine
Engine
CONT MOTOR A&C75 SERIES
Last Cert Issue
—
Aircraft Resources
01 / Registration
Filed with the Federal Aviation Administration
Every cell below is a literal field from the FAA Aircraft Registry. Click any value to open the FAA registry record for N2865H.
Tail Number
N2865H
Serial Number
3490
Make
ERCOUPE
Model
415-C
Year of Manufacture
1946
Mfr / Model Code
0420322
Type Aircraft
Fixed Wing Single Engine
Type Engine
Reciprocating
Engines
1
Seats
2
Engine Manufacturer
CONT MOTOR
Engine Model
A&C75 SERIES
Horsepower
75 hp
Weight Class
CLASS 1
Certification
Standard · code 1
Registrant
BAYNE WILLIAM R · Individual
Address
12087 FM 2860 · KAUFMAN, TX 75142-7801
FAA Region
2 · County 257
Status
Registration Valid
Airworthiness Date
—
Cert Issue Date
—
Expiration Date
—
Last FAA Action
—
Mode S Hex (ICAO24)
A2E754
Mode S (Octal)
50563524
Live position via ICAO24 A2E754
External services. Live tracks are unaffiliated with TallyAero or the FAA.
02 / NTSB Records
Events on file with the National Transportation Safety Board
-
Sep 22, 1983
HESPERIA, California
Airport · L26 HESPERIA AIR LODGE
03 / Airworthiness Directives
Applicable to ERCOUPE 415-C
Federal Aviation Administration airworthiness directives matched to make and model. Each entry links to the Federal Register publication.
-
Nov 13, 2012
Federal Register →Airworthiness Directives; Univair Aircraft Corporation Airplanes
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to certain Univair Aircraft Corporation Models (ERCO) 415-C, 415-CD, 415-D, E, G; (Forney) F-1 and F-1A; (Alon) A-2 and A2-A; and (Mooney) M10 airplanes. All references to Ercoupe Service Memorandum No. 20, Revision A, dated September 1, 2008, in th…
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Aug 29, 2012
Federal Register →Airworthiness Directives; Univair Aircraft Corporation Airplanes
We are superseding an existing airworthiness directive (AD) for certain Univair Aircraft Corporation Models (ERCO) 415-C, 415-CD, 415-D, E, G; (Forney) F-1 and F-1A; (Alon) A-2 and A2-A; and (Mooney) M10 airplanes. That AD currently requires an inspection of the aileron balance assembly and ailerons for cracks and excessive looseness of associated parts wit…
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Apr 14, 2011
Federal Register →Airworthiness Directives; Univair Aircraft Corporation Models (ERCO) 415-C, 415-CD, 415-D, E, G; (Forney) F-1 and F-1A; (Alon) A-2 and A2-A; and (Mooney) M10 Airplanes
We propose to supersede an existing airworthiness directive (AD) that applies to Univair Aircraft Corporation Models (ERCO) 415-C, 415-CD, 415-D, E, G; (Forney) F-1 and F-1A; (Alon) A-2 and A2-A; and (Mooney) M10 Airplanes. The existing AD currently requires an inspection of the aileron balance assembly and ailerons for cracks and excessive looseness of ass…
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Apr 12, 1994
Federal Register →Airworthiness Directives: Univair Aircraft Corporation Models Ercoupe 415-C, 415-CD, 415-D, 415-E, and 415-G, Forney F-1 and F-1A, Alon A-2 and A-2A, and Mooney M10 Airplanes
This document proposes to adopt a new airworthiness directive (AD) that would apply to Univair Aircraft Corporation (Univair) Models Ercoupe 415-C, 415-CD, 415-D, 415-E, and 415-G, Forney F-1 and F-1A, Alon A-2 and A-2A, and Mooney M10 airplanes. The proposed action would require installing inspection openings in the outer wing panels, inspecting (one-time)…
04 / Service Difficulty Reports
FAA SDR filings
The FAA does not currently expose a public API for Service Difficulty Reports. We do not back-fill or paraphrase. Search the FAA SDR portal directly →
05 / Sources & Methodology
Every fact on this page links to its primary US-government source
- FAA Aircraft Registry →
Refreshed May 5, 2026
Available
- NTSB CAROL →
Refreshed May 5, 2026
Available
- Federal Register (FAA Airworthiness Directives) →
Refreshed May 5, 2026
Available
- FAA Service Difficulty Reports →
Refreshed May 5, 2026
Unavailable
We render only what the agency publishes. Found a factual error? Report it → We acknowledge within 5 business days and resolve within 14.