FAIRCHILD SA227-DC

01 /  Distribution

Where the fleet lives and was built

Counts of currently-registered FAIRCHILD SA227-DC aircraft by US state and decade of manufacture, sourced from the FAA Aircraft Registry.

02 /  NTSB Records

Events involving FAIRCHILD SA227-DC aircraft

4 event(s) on file. Showing the most recent 4.

• Nov 4, 1998

  N5LN

  ROCK, Kansas Fatal

  NTSB Docket →

• Aug 19, 1979

  N3532Q

  MERRITT, North Carolina

  NTSB Docket →

• Jul 25, 1970

  N3532Q

  THOMSON, Georgia

  NTSB Docket →

• Aug 11, 1969

  N3532Q

  LOUISVILLE, Georgia

  NTSB Docket →

03 /  Airworthiness Directives

FAA directives applicable to FAIRCHILD SA227-DC

33 directive(s) on file. Showing the most recent 25 · 8 more in the Federal Register.

• Mar 4, 2016

  Airworthiness Directives; M7 Aerospace LLC Airplanes

  We are adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA26-AT, SA226-T(B), SA226-AT, SA226-T, SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C- 26B), and SA227-TT airplanes. This AD was prompted by information that the airplane flight manual (AFM) does not prov…

  Atlas AD → Federal Register ↗

• Sep 29, 2015

  Airworthiness Directives; M7 Aerospace LLC Airplanes

  We are superseding Airworthiness Directive (AD) 97-02-02 for certain Models SA26-AT, SA26-T, SA226-AT, SA226-T, SA226-T(B), SA226- TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes. AD 97-02-02 required applying torque to the control column pitch bearing attaching nut…

  Atlas AD → Federal Register ↗

• Aug 25, 2015

  Airworthiness Directives; M7 Aerospace LLC Airplanes

  We propose to adopt a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA26-AT, SA226-T, SA226-AT, SA226-T(B), SA226- TC, SA227-AT, SA227-TT, SA227-AC (C-26A), SA227-BC (C-26A), SA227-CC, and SA227-DC (C-26B) airplanes. This proposed AD was prompted by information that the airplane flight manual (AFM)…

  Atlas AD → Federal Register ↗

• Jun 16, 2015

  Airworthiness Directives; M7 Aerospace LLC Airplanes

  We propose to supersede Airworthiness Directive (AD) 97-02-02, which applies to certain Models SA26-AT, SA26-T, SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes. AD 97-02-02 currently requires applying torque to the control column…

  Atlas AD → Federal Register ↗

• Sep 6, 2012

  Airworthiness Directives; M7 Aerospace LLC Airplanes

  We are adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), SA227-AT, and SA227-TT airplanes. This AD requires repetitively inspecting the left and right forward (main) and aft spar wing-to-f…

  Atlas AD → Federal Register ↗

• Jan 12, 2011

  Airworthiness Directives; M7 Aerospace LP (Type Certificate Previously Held by Fairchild Aircraft Incorporated) Models SA26-AT, SA26-T, SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT Airplanes

  We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires repetitively inspecting the cockpit heated windshields for damage and replacing damaged windshields. This AD was prompted by reports from the windshield manufacturer of inner glass ply fracture. We are issuing this AD to…

  Atlas AD → Federal Register ↗

• May 28, 2009

  Airworthiness Directives; M7 Aerospace LP Models SA226-AT, SA226-T, SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, and SA227-DC (C-26B) Airplanes

  We are adopting a new airworthiness directive (AD) to supersede AD 2008-12-16, which applies to certain M7 Aerospace LP SA226 and SA227 series airplanes. AD 2008-12-16 currently requires you to inspect wires and tube assemblies for chafing, arcing, or insufficient clearance between components. If chafing, arcing, or i…

  Atlas AD → Federal Register ↗

• Feb 12, 2009

  Airworthiness Directives; M7 Aerospace LP Models SA226-AT, SA226-T, SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, and SA227-DC (C-26B) Airplanes

  We propose to supersede Airworthiness Directive (AD) 2008-12- 16, which applies to certain M7 Aerospace LP SA226 and SA227 series airplanes. AD 2008-12-16 currently requires you to inspect wires and tube assemblies for chafing, arcing, or insufficient clearance between components. If chafing, arcing, or insufficient c…

  Atlas AD → Federal Register ↗

• Jun 18, 2008

  Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes

  We are adopting a new airworthiness directive (AD) for certain M7 Aerospace LP SA226 and SA227 series airplanes. This AD requires you to inspect electrical wires/components, hydraulic and bleed air tube assemblies at left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas, LH/RH wing stations 51…

  Atlas AD → Federal Register ↗

• Mar 14, 2008

  Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes

  We propose to adopt a new airworthiness directive (AD) for certain M7 Aerospace LP SA226 and SA227 series airplanes. This proposed AD would require you to inspect electrical wires/components, hydraulic and bleed air tube assemblies at left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas, LH/R…

  Atlas AD → Federal Register ↗

• Aug 3, 2007

  Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes

  We are adopting a new airworthiness directive (AD) to supersede AD 98-19-15 R1 and AD 2000-03-17, which apply to M7 Aerospace LP SA226 and SA227 series airplanes equipped with certain pitch trim actuators. AD 98-19-15 R1 currently requires you to incorporate changes into the Limitations Section of the FAA-approved air…

  Atlas AD → Federal Register ↗

• Apr 30, 2007

  Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes

  We propose to supersede Airworthiness Directive (AD) 98-19-15 R1 and AD 2000-03-17, which apply to M7 Aerospace LP SA226 and SA227 series airplanes equipped with certain pitch trim actuators. AD 98-19- 15 R1 currently requires you to incorporate changes into the Limitations Section of the FAA-approved Airplane Flight…

  Atlas AD → Federal Register ↗

• Mar 21, 2005

  Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes

  The FAA is adopting a new Airworthiness Directive (AD) to supersede AD 99-06-02, which currently applies to certain Fairchild Aircraft (Fairchild) SA226 and SA227 series airplanes. AD 99-06-02 requires you to repetitively inspect the wing spar center web cutout on both wings for cracks between Wing Station (WS) 8 and…

  Atlas AD → Federal Register ↗

• Jan 19, 2005

  Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

  The FAA is adopting a new airworthiness directive (AD) to supersede Airworthiness Directive 2004-10-15, which applies to certain GTX 330 and GTX 330D Mode S transponders that are installed on airplanes. AD 2004-10-15 currently requires you to install GTX 330/330D Software Upgrade Version 3.03, 3.04, or 3.05. This AD a…

  Atlas AD → Federal Register ↗

• Oct 7, 2004

  Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

  The FAA proposes to supersede Airworthiness Directive (AD) 2004-10-15, which applies to certain GTX 330 and GTX 330D Mode S transponders that are installed on airplanes. AD 2004-10-15 currently requires you to install GTX 330/330D Software Upgrade Version 3.03, 3.04, or 3.05. This proposed AD applies to certain GTX 33…

  Atlas AD → Federal Register ↗

• May 21, 2004

  Airworthiness Directives; GARMIN International Inc. GTX 330 Mode S Transponders and GTX 330D Diversity Mode S Transponders

  The FAA adopts a new airworthiness directive (AD) for certain GARMIN International Inc. GTX 330/GTX 330D Mode S transponders that are installed on aircraft. This AD requires you to install GTX 330/330D Software Upgrade Version 3.03, 3.04, or 3.05. This AD is the result of observations that the GTX 330 and GTX 330D may…

  Atlas AD → Federal Register ↗

• Dec 30, 2003

  Airworthiness Directives; GARMIN International Inc. GTX 330 Mode S Transponders and GTX 330D Diversity Mode S Transponders

  The FAA proposes to adopt a new airworthiness directive (AD) for certain GARMIN International Inc. GTX 330/GTX 330D Mode S transponders. This proposed AD would require you to install GTX 330/ 330D Software Upgrade Version 3.03. This proposed AD is the result of observations that the GTX 330 and GTX 330D may detect, fr…

  Atlas AD → Federal Register ↗

• Sep 23, 2003

  Airworthiness Directives; Fairchild Aircraft, Inc., SA226 Series and SA227 Series Airplanes

  This amendment adopts a new airworthiness directive (AD) that applies to all Fairchild Aircraft, Inc. (Fairchild Aircraft) SA226 and SA227 series airplanes. This AD requires you to inspect the fuel boost pump wiring for any chafing, cracked insulation material, or evidence of bare wire(s) (referred to herein as damage…

  Atlas AD → Federal Register ↗

• Oct 15, 2002

  Airworthiness Directives; Fairchild Aircraft, Inc., SA226 Series and SA227 Series

  This document proposes to adopt a new airworthiness directive (AD) that would apply to all Fairchild Aircraft, Inc. (Fairchild Aircraft) SA226 and SA227 series airplanes. This proposed AD would require you to inspect the fuel boost pump wiring for any chafing, cracked insulation material, or evidence of bare wire(s) (…

  Atlas AD → Federal Register ↗

• Feb 17, 2000

  Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes

  This amendment supersedes Airworthiness Directive (AD) 97-23- 01, which currently requires the following on Fairchild Aircraft, Inc. (Fairchild Aircraft) SA226 and SA227 series airplanes that are equipped with a certain Simmonds-Precision pitch trim actuator or a certain Barber-Colman pitch trim actuator: repetitively…

  Atlas AD → Federal Register ↗

• Oct 12, 1999

  Airworthiness Directives; Fairchild Aircraft Corporation SA226 and SA227 Series Airplanes

  This document proposes to adopt a new airworthiness directive (AD) that would apply to all Fairchild Aircraft Corporation (Fairchild) SA226 and SA227 series airplanes. The proposed AD would require revising the Airplane Flight Manual (AFM) to include requirements for activation of the airframe pneumatic deicing boots.…

  Atlas AD → Federal Register ↗

• Oct 6, 1999

  Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes

  This document proposes to supersede Airworthiness Directive (AD) 97-23-01, which currently requires the following on Fairchild Aircraft, Inc. (Fairchild Aircraft) SA226 and SA227 series airplanes that are equipped with a certain Simmonds-Precision pitch trim actuator or a certain Barbar-Colman pitch trim actuator: rep…

  Atlas AD → Federal Register ↗

• Sep 23, 1999

  Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes

  This document proposes to revise Airworthiness Directive (AD) 98-19-15, which currently requires incorporating information into the Limitations Section of the airplane flight manual (AFM) that imposes a speed restriction and a minimum pilot requirement for Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series ai…

  Atlas AD → Federal Register ↗

• Apr 23, 1999

  Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes

  This document proposes to supersede Airworthiness Directive (AD) 99-06-02, which currently requires repetitively inspecting the wing spar center web cutout on both wings for cracks between Wing Station (WS) 8 and WS 17.5 on certain Fairchild Aircraft (Fairchild) SA226 and SA227 series airplanes, and immediately repair…

  Atlas AD → Federal Register ↗

• Mar 10, 1999

  Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes

  This amendment adopts a new airworthiness directive (AD) that applies to certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes. This AD requires repetitively inspecting the wing spar center web cutout on both wings for cracks between Wing Station (WS) 8 and WS 17.5, and immediately repairing an…

  Atlas AD → Federal Register ↗

04 /  Type Certificate Data Sheets

FAA TCDS for FAIRCHILD SA227-DC

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

• A18SW Historical Rev 3 · 12/01/2000

  Fairchild Aircraft Corporation

  Models: SA227-DC (C-26B), SA227-CC

  Atlas TCDS → DRS ↗

06 /  Supplemental Type Certificates

Modifications approved for FAIRCHILD SA227-DC

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

• 11/09/2022

  STC ST00789WI

  Installation of the Fairchild Digital Data Flight Recorder Model F800 or F1000.

  Worldwide Aircraft Services LLC

  Atlas STC → DRS ↗

• 07/16/2019

  STC SA01861SE (PAGE 2)

  Fabrication and installation of Landing Light Controller

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 07/16/2019

  STC SA01800SE (PG 2)

  Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 07/14/2017

  STC SA01800SE (PG 2)

  Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 09/01/2016

  STC SA1542GL

  Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 126 using Installation Kit P/N 805

  Paul/ Lanna Egan LLC

  Atlas STC → DRS ↗

• 12/01/2011

  STC SA01861SE (PAGE 2)

  Fabrication and installation of Landing Light Controller

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 12/01/2011

  STC SA01800SE (PG 2)

  Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 07/21/2011

  STC SA00243BO (1 OF 5)

  Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).

  Icarus Avionics, LLC

  Atlas STC → DRS ↗

• 01/11/2010

  STC SA02254AK (1 OF 2)

  Installation of Single Screen, or 2 or 3 Screen FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV) configurations

  Chelton Flight Systems Inc.

  Atlas STC → DRS ↗

• 01/09/2009

  STC SA01861SE (PAGE 2)

  Fabrication and installation of Landing Light Controller

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 01/08/2009

  STC SA01800SE (PG 2)

  Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 07/22/2008

  STC SA01861SE (PAGE 2)

  Fabrication and installation of Landing Light Controller

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 05/21/2008

  STC SA01473SE (3 OF 5)

  Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde

  Garmin AT Inc.

  Atlas STC → DRS ↗

• 01/04/2008

  STC SA01800SE (PG 2)

  Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 01/04/2008

  STC SA01800SE (PG 3)

  Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.

  Seaton Engineering Corp.

  Atlas STC → DRS ↗

• 04/30/2007

  STC SA01692SE (Page 1)

  Installation of a Garmin GMX200 Multi Function Display.

  Garmin AT Inc.

  Atlas STC → DRS ↗

• 02/15/2007

  STC SA01695SE (3 OF 5)

  Installation of an antenna

  Garmin AT Inc.

  Atlas STC → DRS ↗

• 11/05/2006

  STC SA01933LA (2 OF 5)

  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System

  Garmin AT Inc.

  Atlas STC → DRS ↗

• 10/23/2006

  STC SA00243BO (1 OF 5)

  Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).

  Centurion Consulting Inc

  Atlas STC → DRS ↗

• 08/30/2006

  STC SA01695SE (3 OF 5)

  Installation of an antenna

  Garmin AT Inc.

  Atlas STC → DRS ↗

• 08/10/2006

  STC SA1542GL

  Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 126 using Installation Kit P/N 805

  Aero Medical Products Mfg

  Atlas STC → DRS ↗

• 05/24/2006

  STC SA01141WI-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-94 Mode S Tr…

  Rockwell Collins Inc

  Atlas STC → DRS ↗

• 03/27/2006

  STC SA02254AK (1 OF 2)

  Installation of Single Screen, or 2 or 3 Screen FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV) configurations

  Chelton Flight Systems Inc.

  Atlas STC → DRS ↗

• 09/21/2005

  STC SA02254AK (1 OF 2)

  Installation of Single Screen, or 2 or 3 Screen FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV) configurations

  Chelton Flight Systems Inc.

  Atlas STC → DRS ↗

• 09/15/2005

  STC SA01141WI-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-94 Mode S Tr…

  Rockwell Collins Inc

  Atlas STC → DRS ↗

• 06/16/2005

  STC SA01900NY

  Installation of a Honeywell MK VI EGPWS.

  Western Avionics

  Atlas STC → DRS ↗

• 05/02/2005

  STC SA10352SC

  Installation of an Aviation Communication & Surveillance Systems (ACSS) TCAS II, dual ACSS Mode-S transponders and dual Sextant VSI/TCAS display in accordance with BHE & Associates…

  M7 Aerospace LP

  Atlas STC → DRS ↗

• 02/07/2005

  STC SA00161BO (2 OF 3

  Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.

  Avidyne Corporation

  Atlas STC → DRS ↗

• 12/19/2004

  STC SA01487SE (2 OF 5)

  Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20,…

  Garmin AT Inc.

  Atlas STC → DRS ↗

• 11/05/2004

  STC SA01900NY

  Installation of a Honeywell MK VI EGPWS.

  Western Avionics

  Atlas STC → DRS ↗

+ 23 more STCs on file

07 /  PMA replacement parts

FAA-approved replacement parts for FAIRCHILD SA227-DC

11 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.

• AD325568Y14#https://drs.faa.gov/browse/excelExternalWindow/00EA7A6FAA2010EF86257A610055E806.0001##

  Hydraulic Filter Assembly

  Pall Aeropower Corporation replaces AD-3255-68Y14

  PMA holder →

• M18003-00#https://drs.faa.gov/browse/excelExternalWindow/EB6F060AA1A7F54D8625777B00526404.0001##

  O-Ring

  Ametek Ameron, LLC d/b/a Mass Systems replaces 18003-00

  PMA holder →

• 802040-03#https://drs.faa.gov/browse/excelExternalWindow/E0CBCFBAD875A41F862574EF004CD523.0001##

  Outlet Assembly

  AVOX Systems Inc replaces 802040-03

  PMA holder →

• 804023-01#https://drs.faa.gov/browse/excelExternalWindow/4EE3D944D199318F862574EF004CD589.0001##

  KS Mask with Bag

  AVOX Systems Inc replaces 804023-01

  PMA holder →

• 4500S-A2#https://drs.faa.gov/browse/excelExternalWindow/C91233BB3143424A862574EF004CD4F9.0001##

  Valve & Control Arm Assembly

  AVOX Systems Inc replaces 4500S-A2

  PMA holder →

• 803272-08#https://drs.faa.gov/browse/excelExternalWindow/B21D4FA7C79DF3BA862574EF004CD55A.0001##

  Bracket Assembly

  AVOX Systems Inc replaces 803272-08

  PMA holder →

• 895-49050#https://drs.faa.gov/browse/excelExternalWindow/18F799CE38E359DE862574EF004CD5E0.0001##

  Cylinder & Regulator

  AVOX Systems Inc replaces 895-49050

  PMA holder →

• 895-49015#https://drs.faa.gov/browse/excelExternalWindow/2037CACDFC1F8D61862574EF004CD5B7.0001##

  Cylinder & Regulator

  AVOX Systems Inc replaces 895-49015

  PMA holder →

• H8820-10#https://drs.faa.gov/browse/excelExternalWindow/0D36775D7A7CAE7E862572AD0047C7F2.0001##

  Filter

  HRD Aerosystems Inc replaces 8820-10

  PMA holder →

• H24202-01#https://drs.faa.gov/browse/excelExternalWindow/5F2F9DD468A615BD862572AD0047C6EE.0001##

  Filter

  HRD Aerosystems Inc replaces 24202-01

  PMA holder →

• H800207#https://drs.faa.gov/browse/excelExternalWindow/959E11F25CDF8778862572AD0047C743.0001##

  Valve Assy.

  HRD Aerosystems Inc replaces 800207-00

  PMA holder →

04 /  Regulations watching this type

Advisory Circulars and Federal Register activity for FAIRCHILD SA227-DC

05 /  Aircraft of this type

All 12 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.

05 /  Sources & Methodology

Every count traces back to a primary US-government source

• FAA Aircraft Registry →

  Refreshed Apr 27, 2026

  Available

• NTSB CAROL →

  Refreshed Apr 27, 2026

  Available

• Federal Register (FAA Airworthiness Directives) →

  Refreshed Apr 27, 2026

  Available

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