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Type Record · As of May 3, 2026

VERTOL 107

Rotorcraft · GE CT58 SERIES

Registered

1

Year Range

1965–1965

NTSB Events

1

Airworthiness Directives

11

01 /  Distribution

Where the fleet lives and was built

Counts of currently-registered VERTOL 107 aircraft by US state and decade of manufacture, sourced from the FAA Aircraft Registry.

By State (top 10)

  • OR 100.0% 1

By Decade of Manufacture

  • 1960s 100.0% 1

02 /  NTSB Records

Events involving VERTOL 107 aircraft

1 event(s) on file. Showing the most recent 1.

02c /  Academic Research

Scholarly work mentioning VERTOL 107

Papers and reports across NASA, NTSB, FAA CAMI, AOPA ASI, Embry-Riddle, arXiv, and the broader academic graph that mention this airframe. Title or keyword match — drill into each for full abstract + author list + PDF link.

Browse the full corpus — academia portal ↗

03 /  Airworthiness Directives

FAA directives applicable to VERTOL 107

11 directive(s) on file. Showing the most recent 11.

  • Jul 23, 2012

    Airworthiness Directives; Boeing Vertol (Type Certificate Currently Held by Columbia Helicopters, Inc. (CHI)) and Kawasaki Heavy Industries, Limited Helicopters (Kawasaki)

    We are adopting a new airworthiness directive (AD) for CHI Model 107-II and Kawasaki Model KV107-II and KV107-IIA helicopters. This AD requires, before further flight, replacing certain upper collective pitch control yoke bolts. This AD is prompted by three failures of the affected bolts. These actions are intended to…

  • Nov 23, 2005

    Airworthiness Directives; Boeing Vertol Model 107-II Helicopters

    This amendment adopts a new airworthiness directive (AD) for Boeing Vertol (Boeing) Model 107-II helicopters. This action requires a visual and magnetic particle inspection of the quill shaft. This amendment is prompted by the discovery of cracks in a quill shaft during a routine inspection. The actions specified in t…

  • Feb 23, 2004

    Airworthiness Directives; General Electric Company CT58 Series and T58 Series Turboshaft Engines

    The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) CT58-100-2, CT58-140-1, -140-2, and T58-GE-1, -3, -5, -8E, -8F, -10, -100, and -402 turboshaft engines. This AD requires the removal from service of certain fuel flow divider assemblies. This AD results from a report that…

  • Sep 13, 2001

    Airworthiness Directives; General Electric Company T58 and CT58 Series Turboshaft Engines

    This amendment surpersedes two existing airworthiness directives (AD's), applicable to General Electric Company (GE) T58 and CT58 series turboshaft engines. The current AD's revised the counting method for hours in repetitive heavy-lift (RHL) service and reduced the life limit for rotating components. Life-limited rot…

  • Jun 15, 2001

    Airworthiness Directives; General Electric Company CT58 Series and Former Military T58 Series Turboshaft Engines

    This amendment adopts a new airworthiness directive (AD) that is applicable to certain General Electric Company (GE) CT58 series and former military T58 series turboshaft engines. This action requires the removal from service of certain fuel flow divider assemblies, and replacement with serviceable parts. This amendme…

  • Apr 3, 2000

    Airworthiness Directives; General Electric Company CT58 Series Turboshaft Engines

    This document proposes the adoption of a new airworthiness directive that would supersede two existing airworthiness directives (AD's), applicable to General Electric Company (GE) CT58 series turboshaft engines. The current AD's revised the counting method for hours in repetitive heavy-lift (RHL) service and reduced t…

  • Oct 20, 1997

    Airworthiness Directives; General Electric Company CT58 Series Turboshaft Engines

    This amendment adopts a new airworthiness directive (AD), applicable to General Electric Company CT58 series turboshaft engines, that requires removal from service of certain stage 1 and 2 forward cooling plates, and stage 2 aft cooling plates, and replacement with serviceable parts. This amendment is prompted by repo…

  • Sep 29, 1997

    Airworthiness Directives; General Electric Company CT58 Series Turboshaft Engines

    This amendment adopts a new airworthiness directive (AD), applicable to General Electric Company CT58 series turboshaft engines, that requires removal from service of certain compressor rear shafts, initial and repetitive inspections of specific critical rotating parts, and replacement if found cracked, until those pa…

  • Jun 9, 1997

    Airworthiness Directives; General Electric Company CT58 Series Turboshaft Engines

    This document proposes the adoption of a new airworthiness directive (AD) that is applicable to General Electric Company CT58 series turboshaft engines. This proposal would require removal from service of certain stage 1 and 2 forward cooling plates, and stage 2 aft cooling plates, and replacement with serviceable par…

  • Apr 3, 1997

    Airworthiness Directives; General Electric Company CT58 Series Turboshaft Engines

    This document proposes the adoption of a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CT58 series turboshaft engines. This proposal would require removal from service of compressor rear shafts, initial and repetitive inspections of ten rotating parts, and replacement if found cr…

  • Apr 4, 1994

    Airworthiness Directives; General Electric Company CT58 Series Turboshaft Engines

    This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CT58-110 and -140 series turboshaft engines. This action supersedes priority letter AD 93-10-09 that currently requires inspection of the forward and aft cooling plate locating groove or channel (rabbet groove)…

07 /  PMA replacement parts

FAA-approved replacement parts for VERTOL 107

5 parts on file from the FAA Parts Manufacturer Approval database. Each is a non-OEM part the FAA has authorized for use as a replacement on this aircraft type.

  • 0101383-4#https://drs.faa.gov/browse/excelExternalWindow/06EED5A5DB807DBF86257DFD007026C1.0001##

    Inertia Reel Assembly

    Meggitt Safety Systems Inc replaces 0101383-4

    PMA holder →
  • 1501111-0#https://drs.faa.gov/browse/excelExternalWindow/789F27287788FA5D86257DFD007026BE.0001##

    Pedal Link Adjuster

    Meggitt Safety Systems Inc replaces 1501111-0

    PMA holder →
  • 0106926#https://drs.faa.gov/browse/excelExternalWindow/68ABC5D557F35E6E86257DFD007026BF.0001##

    Inertia Reel Assembly

    Meggitt Safety Systems Inc replaces 0106926

    PMA holder →
  • AC325848HM2#https://drs.faa.gov/browse/excelExternalWindow/7E225B09E5257D6D86257A610055E850.0001##

    Hydraulic Filter Assembly

    Pall Aeropower Corporation replaces AC-3258-48HM2

    PMA holder →
  • AC325568HM2#https://drs.faa.gov/browse/excelExternalWindow/2E12E11CCCAAC23486257A610055E851.0001##

    Hydraulic Filter Assembly

    Pall Aeropower Corporation replaces AC-3255-68HM2

    PMA holder →

05 /  Aircraft of this type

All 1 registered N-numbers

Every tail currently on the FAA registry for this make/model. Click an N-number to query the FAA Aircraft Inquiry; rows flagged have NTSB events on file. Tails seeded with full TallyAero pages link directly.

1 of 1
N-number St Year NTSB FAA
N196CH OR 1965 Look up ↗

Source — FAA Aircraft Registry · click "Look up" to query the live registry record (owner, address, last airworthiness)

05 /  Sources & Methodology

Every count traces back to a primary US-government source

We render counts and lists as the agency publishes them. Read the methodology →