Piston helicopter

N8135J

1972 Bell 47G-5A

Registered 1 NTSB/FAA record
Built
1972
Serial
25060
Class
Piston helicopter
Engines
Lycoming VO-435 series
Status
Current as of October 2026
Registered owner
Wilbur-Ellis Co (Corporation)
Based
Salinas, CA
Registration record

N8135J on the FAA register

Type
1972 Bell 47G-5A
Serial
25060
Engines
Lycoming VO-435 series
Registered owner
Wilbur-Ellis Co
Salinas, CA
Certificate issued
2010-06-24
Airworthiness date
1972-02-22
Registration expires
2028-01-31
Airworthiness class
Standard · normal
Mode S (hex)
AB1791
Mode S (octal)
52613621
Seats (type)
3
Weight class
up to 12,499 lb
Range (type)
214 nm
Cruise (type)
73 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2028-01-31
    Registration expires (renewal due).
  • 2010-06-24
    Certificate of registration issued as N8135J.
  • 1996-10-07
    Accident at King City, CA; damage: substantial.
  • 1972-02-22
    Airworthiness date on the current FAA record (standard category (normal)).
Overview

About N8135J

N8135J is a 1972 Bell 47G-5A, serial number 25060. The FAA register lists Wilbur-Ellis Co as the registrant in Salinas, California. The current certificate of registration was issued on June 24, 2010 and expires on January 31, 2028.

The FAA aircraft reference file describes the type as a piston helicopter, one Lycoming VO-435 series engine and 3 seats. Published figures for the type give a cruise speed of about 73 knots and a range of about 214 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal), dated February 22, 1972.

N8135J has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
73 kt
Range
214 nm
Fuel burn
7 gph

Published figures for the Bell 47G-5A type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

1996-10-07 Accident · King City, CA Damage: Substantial NTSB · LAX97LA006
Reported aircraft: Bell 47G-5A
Probable cause: the pilot's failure to maintain adequate rotor rpm during the takeoff initial climb.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.