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Registered aircraft · FAA record as of October 2, 2026
N86SD

Bell 47G-5A

Valid Florida

N86SD is a Bell 47G-5A, a rotorcraft with a piston engine (a helicopter or multicopter), built in 1973. It has 3 seats. It is registered to an individual in Clearwater Beach, Florida. The registration is valid: it was issued on May 20, 2014 and expires on May 31, 2027. It holds a standard airworthiness certificate for normal, dated May 14, 1973.

Aircraft

Maker
Bell
Model
47G-5A · all 47G-5As and related versions
Serial number
25118
Type
Rotorcraft
Power
Piston (reciprocating), 1 motor · Lycoming VO-435 SERIES · 260 hp
Seats
3
Year built
1973
Cruising speed
78 mph
Transponder code
ABCE12 (octal 52747022)

Registration

Status
Valid registration
Certificate issued
May 20, 2014
Expires
May 31, 2027
Last FAA action
January 22, 2023
Airworthiness
Standard · Normal · May 14, 1973
FAA region
Southern
FAA record id
00570842

Owner as the FAA publishes it

Name
Young Randall K
Type
Individual
Address
805 Mandalay Ave
Clearwater Beach, FL 33767-1325

Owners can ask the FAA to withhold their name and address from public files. When they do, those fields are blank here as well. How that works.

Documents on file 0

No bills of sale, loans or other documents are indexed against this tail number.

Earlier use of this number 1

1994-07-14Mitsubishi MU-2B-60 · Triennial registration form was mailed and has not been returned by the Post Office

Records check free · 2 to understand · 3 clear

The public federal record on N86SD, read the way a buyer, lender or insurer reads it: FAA registration, prior tail numbers keyed on the serial number, reuse of the tail number, recent registry filings, and the NTSB accident record under this and every earlier registration.

CLEARRegistration and identity

Valid registration to Young Randall K, an individual, certificate issued May 20, 2014, expires May 31, 2027. No fractional interest recorded. [1]

CLEARAirworthiness certificate

Standard certificate for normal, dated May 14, 1973, consistent with the 1973 manufacture year. [1]

CLEARPrior registrations of this airframe

No earlier tail number is recorded against serial 25118 for this model in the deregistered file. [2]

ATTENTIONTail number reuse

N86SD was previously assigned to 1 other aircraft: Mitsubishi MU-2B-60 (serial 765SA, cancelled July 14, 1994). Histories keyed to the tail number alone can mix aircraft up; this check keys on the serial number. [2]

NOTERecent registry documents

No bills of sale, loans or releases have reached the registry in recent weeks. The index covers only recent filings; older liens are in the records file. [3]

ATTENTIONAccident and incident record

1 NTSB record under N86SD: Accident on April 19, 1993 at Zwingle, IA: fatal, destroyed (8 fatal). Details below. [4]

PENDINGTitle chain, liens and 337 forms

These live in the FAA aircraft records file (every document ever filed against the aircraft) and, for larger aircraft, the International Registry. Part of the full report.

PENDINGAirworthiness directives and utilization

AD compliance against the logbooks and flight-activity reconciliation are researched layers of the full report.

NTSB records 1

DCA93GA042Accident on April 19, 1993 at Zwingle, IA: fatal, destroyed (8 fatal).serial on NTSB record: 765 S.A.

Aircraft on the NTSB record: Mitsubishi MU-2B-60 · operated under PUBU

THE FATIGUE CRACKING AND FRACTURE OF THE PROPELLER HUB ARM. THE RESULTANT SEPARATION OF THE HUB ARM AND THE PROPELLER BLADE DAMAGED THE ENGINE, NACELLE, WING, AND FUSELAGE, THEREBY CAUSING SIGNIFICANT DEGRADATION TO AIRCRAFT PERFORMANCE AND CONTROL THAT MADE A SUCCESSFUL LANDING PROBLEMATIC. THE CAUSE OF THE PROPELLER HUB ARM FRACTURE WAS A REDUCTION IN THE FATIGUE STRENGTH OF THE MATERIAL BECAUSE OF MANUFACTURING AND TIME-RELATED FACTORS (DECARBURIZATION, RESIDUAL STRESS, CORROSION, MIXED MICROSTRUCTURE, AND MACHINING/SCORING MARKS) THAT REDUCED THE FATIGUE RESISTANCE OF THE MATERIAL, PROBABLY COMBINED WITH EXPOSURE TO HIGHER-THAN-NORMAL CYCLIC LOADS DURING OPERATION OF THE PROPELLER AT A CRITICAL VIBRATION FREQUENCY (REACTIONLESS MODE), WHICH WAS NOT APPROPRIATELY CONSIDERED DURING THE AIRPLANE/PROPELLER CERTIFICATION PROCESS.

Full record in plain English · Docket and reports at the NTSB

CLEAR the source was checked and shows no adverse findingATTENTION a fact a buyer or lender should understand, often routineNOTE context onlyPENDING covered by the full report
  1. FAA Releasable Aircraft Database, master file, file of October 2, 2026. registry.faa.gov/
  2. FAA deregistered aircraft file (part of the same download), file of October 2, 2026. registry.faa.gov/
  3. FAA document index: registry documents received in recent weeks, file of October 2, 2026. registry.faa.gov/
  4. NTSB aviation accident database (CAROL), records through September 30, 2026. data.ntsb.gov/carol-main-public/basic-search

This automated check reads the public federal record. Nothing here is a legal opinion, an appraisal or a statement about the aircraft's condition; a CLEAR line is a statement about the searched record, not the aircraft.

Source: FAA Civil Aviation Registry, Releasable Aircraft Database, October 2, 2026. See this record on the FAA site · This record as data