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Type Record · As of May 3, 2026

CONSTRUCCIONES AERONAUTICAS SA CN-235

Fixed Wing Multi Engine · GE CT7-9C3

Registered

4

Year Range

1991–2007

NTSB Events

0

Airworthiness Directives

14

01 /  Distribution

Where the fleet lives and was built

Counts of currently-registered CONSTRUCCIONES AERONAUTICAS SA CN-235 aircraft by US state and decade of manufacture, sourced from the FAA Aircraft Registry.

By State (top 10)

  • CO 50.0% 2
  • MT 50.0% 2

By Decade of Manufacture

  • 1990s 25.0% 1
  • 2000s 75.0% 3

02 /  NTSB Records

Events involving CONSTRUCCIONES AERONAUTICAS SA CN-235 aircraft

No NTSB-recorded events match CONSTRUCCIONES AERONAUTICAS SA CN-235 in the indexed corpus.

03 /  Airworthiness Directives

FAA directives applicable to CONSTRUCCIONES AERONAUTICAS SA CN-235

14 directive(s) on file. Showing the most recent 14.

  • Apr 9, 2007

    Airworthiness Directives; General Electric Company CT7-5, -7, and -9 Series Turboprop Engines

    The FAA is superseding an existing airworthiness directive (AD) for General Electric Company (GE) CT7-5A2, -5A3, -7A, -7A1, -9B, - 9B1, and -9B2, -9C, -9C3, -9D, and -9D2 turboprop engines, with certain part number (P/N) and serial number stage 2 turbine aft cooling plates installed. That AD currently requires a oneti…

  • Mar 31, 2006

    Airworthiness Directives; General Electric Company CT7-5, -7, and -9 Series Turboprop Engines

    The FAA proposes to supersede an existing airworthiness directive (AD) for General Electric Company (GE) CT7-5A2, -5A3, -7A, - 7A1, -9B, -9B1, and -9B2 turboprop engines, with certain part number (P/N) and serial number stage 2 turbine aft cooling plates installed. That AD currently requires a onetime eddy current ins…

  • Sep 19, 2005

    Airworthiness Directives; General Electric Company CT7-5, -7, and -9 Series Turboprop Engines

    The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CT7-5A2, -5A3, -7A, -7A1, -9B, -9B1, and -9B2 turboprop engines, with stage 2 turbine aft cooling plate, part number (P/N) 6064T07P01, 6064T07P02, 6064T07P05, or 6068T36P01 installed. This AD requires a onetime eddy current inspec…

  • Apr 15, 2005

    Airworthiness Directives; General Electric Company CT7-5, -7, and -9 Series Turboprop Engines

    The FAA proposes to adopt a new airworthiness directive (AD) for General Electric Company (GE) CT7-5A2, -5A3, -7A, -7A1, -9B, -9B1, and -9B2 turboprop engines, with stage 2 turbine aft cooling plate, part number (P/N) 6064T07P01, 6064T07P02, 6064T07P05, or 6068T36P01 installed. This proposed AD would require a onetime…

  • Jan 8, 2002

    Airworthiness Directives; GE Aircraft Engines CT7 Series Turboprop Engines

    This amendment adopts a new airworthiness directive (AD), that is applicable to GE Aircraft Engines (GE) CT7 series turboprop engines. This amendment requires removal of stage 2 turbine aft cooling plates of a certain part number (P/N) and installation of cooling plates of a new design. This amendment is prompted by a…

  • May 2, 2001

    Airworthiness Directives; GE Aircraft Engines CT7 Series Turboprop Engines

    The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to GE Aircraft Engines (GE) CT7 series turboprop engines. This proposal would require removal of stage 2 turbine aft cooling plates of a certain part number (P/N) and installation of cooling plates of a ne…

  • Jan 13, 1998

    Airworthiness Directives; GE Aircraft Engines CT7 Series Turboprop Engines

    This amendment supersedes an existing airworthiness directive (AD), applicable to GE Aircraft Engines (GE) CT7 series turboprop engines, that currently requires eddy current inspection (ECI) of disk holes of stage 1 and 2 gas generator turbine (GGT) disks for cracks, and, if necessary, replacement with serviceable par…

  • Mar 31, 1997

    Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines

    This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Aircraft Engines (GE) CT7 series turboprop engines. This action requires eddy current inspection of disk holes of stage 1 and 2 gas generator turbine (GGT) disks for cracks, and, if necessary, replacement with serviceable p…

  • Dec 13, 1995

    Airworthiness Directives; Hamilton Standard 14RF and 14SF Series, and Hamilton Standard/British Aerospace Model 6/5500/F Propellers

    This document proposes the adoption of a new airworthiness directive (AD) that is applicable to Hamilton Standard 14RF and 14SF series, and Hamilton Standard/British Aerospace Model 6/5500/F propellers. This proposal would require initial and repetitive inspections of critical components, and removal, and replacement…

  • Mar 8, 1995

    Airworthiness Directives; Hamilton Standard 14RF Series, 14SF Series, and Hamilton Standard/British Aerospace Model 6/5500/F Propellers

    This amendment supersedes an existing airworthiness directive (AD), applicable to Hamilton Standard 14RF series, 14SF series, and Hamilton Standard/British Aerospace 6/5500/F series propellers, that currently requires a one-time ultrasonic shear wave inspection for cracks in the propeller blade taper bore. This amendm…

  • Nov 4, 1994

    Airworthiness Directives; Hamilton Standard 14RF, 247F, 14SF, and P6/5500/F Series Propellers

    This amendment supersedes an existing airworthiness directive (AD), applicable to Hamilton Standard 14RF, 247F, 14SF, and 6/5500/F (formerly Hamilton Standard/British Aerospace 6/5500/F) series propellers, that currently requires initial and repetitive inspections of the propeller control unit (PCU) servo ballscrew in…

  • Jul 20, 1994

    Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines

    This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Aircraft Engines (GE) CT7 series turboprop engines. This action requires a one-time ultrasonic inspection of a suspect population of propeller shafts for metallurgical defects, and if necessary, replacement with a serviceab…

  • May 27, 1994

    Airworthiness Directives; Hamilton Standard 14RF, 247F, 14SF, and 6/5500/F Series Propellers

    This document proposes the supersedure of an existing airworthiness directive (AD), applicable to Hamilton Standard 14RF, 247F, 14SF, and 6/5500/F (formerly Hamilton Standard/British Aerospace 6/5500/F) series propellers, that currently requires initial and repetitive inspections of the propeller control unit (PCU) se…

  • Apr 22, 1994

    Airworthiness Directives; Hamilton Standard 14RF Series, 14SF Series, and Hamilton Standard/British Aerospace 6/5500/F Series Propellers

    This amendment adopts a new airworthiness directive (AD) that is applicable to Hamilton Standard 14RF series, 14SF series, and Hamilton Standard/British Aerospace 6/5500/F series propellers. This action requires a one-time inspection for cracks in the propeller blade taper bore. This amendment is prompted by reports o…

04 /  Type Certificate Data Sheets

FAA TCDS for CONSTRUCCIONES AERONAUTICAS SA CN-235

The TCDS is the legal certification document — weight limits, performance, equipment, AD compliance times, operating limitations. 1 match in the FAA catalog.

  • A21NM Historical Rev 6 · 12/30/1998

    Construcciones Aeronauticas S.A.

    Models: CN-235-100, CN-235, C-295, CN-235-300 + 1 more

06 /  Supplemental Type Certificates

Modifications approved for CONSTRUCCIONES AERONAUTICAS SA CN-235

19 STCs on file — every FAA-approved modification, alteration, or installation for this aircraft. STOL kits, avionics, fuel systems, floats, engine swaps, you name it.

  • 08/23/2010

    STC ST03537AT

    Installation of a Single Class-A Sandel ST3400 Terrain Awareness Warning System with Remote Magnetic Indicator Function on copilot upper left instrument panel.

    Presidential Airways Inc.

  • 02/10/2010

    STC ST03537AT

    Installation of a Single Class-A Sandel ST3400 Terrain Awareness Warning System with Remote Magnetic Indicator Function on copilot upper left instrument panel.

    Presidential Airways Inc.

  • 02/28/2008

    STC ST00266BO

    Installation of a BAE Systems AN/AAR-57 Missile Warning System with an AN/ALE-47 Threat Adaptive Countermeasures Dispensing System

    BAe Systems Info & Electronic Systems

  • 02/15/2008

    STC ST00266BO

    Installation of a BAE Systems AN/AAR-57 Missile Warning System with an AN/ALE-47 Threat Adaptive Countermeasures Dispensing System

    Pro Star Aviation LLC

  • 01/31/2008

    STC ST03537AT

    Installation of a Single Class-A Sandel ST3400 Terrain Awareness Warning System with Remote Magnetic Indicator Function on copilot upper left instrument panel.

    Southeast Aerospace Inc

  • 02/28/2007

    STC ST01305WI-D

    Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Dr…

    Rockwell Collins Inc

  • 07/20/2006

    STC ST00844WI-D

    Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system insta…

    Rockwell Collins Inc

  • 07/10/2006

    STC ST00234BO

    Installation of a modified exhaust.

    BAe Systems Info & Electronic Systems

  • 09/15/2005

    STC ST01142WI-D

    Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S T…

    Rockwell Collins Inc

  • 06/28/2005

    STC ST01307WI-D

    Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation

    Rockwell Collins Inc

  • 02/16/2005

    STC ST01307WI-D (1 OF 2)

    Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation in accordance with Collins Drawing Index as listed on AML No. ST01307WI-D, Revision -, or late…

    Rockwell Collins Inc

  • 02/07/2005

    STC ST01305WI-D

    Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Dr…

    Rockwell Collins Inc

  • 01/06/2005

    STC ST01142WI-D

    Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S T…

    Rockwell Collins Inc

  • 12/14/2004

    STC ST00844WI-D

    Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system insta…

    Rockwell Collins Inc

  • 02/24/2003

    STC ST01142WI-D

    Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S T…

    Rockwell Collins Inc

  • 08/21/2002

    STC ST01142WI-D

    Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S T…

    Rockwell Collins Inc

  • 07/29/2002

    STC SA9169SC-D

    Incorporated GPS approach capability to the existing certified GPS and EFIS installation.

    L-3 Communications Integrated Systems LP

  • 03/10/2000

    STC ST00844WI-D

    Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system insta…

    Rockwell Collins Inc

  • 05/14/1999

    STC ST00673WI-D

    Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter…

    Rockwell Collins Inc

07 /  PMA replacement parts

FAA-approved replacement parts for CONSTRUCCIONES AERONAUTICAS SA CN-235

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.

  • P-1115-1#https://drs.faa.gov/browse/excelExternalWindow/5BC819E140DAD7EE86257B4000546D6E.0001##

    Filter, Element

    Western Filter A Division of Donalson Company Inc replaces 147240-1

    PMA holder →
  • P-1115-1#https://drs.faa.gov/browse/excelExternalWindow/484F36DF0A089C8E8625763F006873ED.0001##

    Filter, Element

    Western Filter A Division of Donalson Company Inc replaces 147240-1

    PMA holder →
  • P-1115-1#https://drs.faa.gov/browse/excelExternalWindow/F89FE76E35BC0F09862575D30063538D.0001##

    Filter, Element

    Western Filter A Division of Donalson Company Inc replaces 147240-1

    PMA holder →
  • 756500017#https://drs.faa.gov/browse/excelExternalWindow/46DAFD1C4D04632F862576C5006354B6.0001##

    Power Supply

    Max-Viz, Inc replaces 756500017

    PMA holder →
  • 756500006#https://drs.faa.gov/browse/excelExternalWindow/F2B0BE612CC3A953862576C5006354A0.0001##

    Camera Assy

    Max-Viz, Inc replaces 756500006

    PMA holder →

05 /  Aircraft of this type

All 4 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.

4 of 4
N-number St Year NTSB FAA
N252QA CO 2004 · Look up ↗
N383EC MT 2007 · Look up ↗
N385RS MT 1991 · Look up ↗
N595QA CO 2004 · 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 →