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Public Record · As of May 5, 2026

N619BA

Fairchild SA227-AC · 1985 View Type →

Status

Registration Valid

Type

Fixed Wing Multi Engine

Engine

GARRETT TPE331-11UA

Last Cert Issue

02 /  NTSB Records

Events on file with the National Transportation Safety Board

03 /  Airworthiness Directives

Applicable to FAIRCHILD SA227-AC

Federal Aviation Administration airworthiness directives matched to make and model. Each entry links to the Federal Register publication.

  • 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 provide adequate guidance in the handling of…

    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 nuts, inspecting the bearing assembly, insp…

    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) does not provide adequate guidance in th…

    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 pitch bearing attaching nuts, inspectin…

    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-fuselage attach fittings for cracks and r…

    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 detect and correct damage to the cockpi…

    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 insufficient clearance between components…

    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 clearance between components is found, 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 51.167 to 81.174, and at all feed-through…

    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/RH wing stations 51.167 to 81.174, and at…

    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 airplane flight manual (AFM) if certain par…

    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 Manual (AFM) if certain part number (P/N…

    Federal Register →
  • Sep 9, 2005

    Airworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers

    The FAA is adopting a new airworthiness directive (AD) for Goodrich De-icing and Specialty Systems "FASTprop" propeller de- icers, part numbers P4E1188 series, P4E1601 series, P4E2200 series, P4E2271-10, P4E2575-7, P4E2575-10, P4E2598-10, P5855BSW, P6199SW, P6592SW, P6662SW, and P6975-11, installed. This AD requires inspection, repair, or replacement of tho…

    Federal Register →
  • Apr 6, 2005

    Airworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers

    The FAA proposes to adopt a new airworthiness directive (AD) for Goodrich De-icing and Specialty Systems "FASTprop" propeller de- icers, part numbers P4E1188 series, P4E1601 series, P4E2200 series, P4E2271-10, P4E2575-7, P4E2575-10, P4E2598-10, P5855BSW, P6199SW, P6592SW, P6662SW, and P6975-11, installed. This proposed AD would require inspection, repair, o…

    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 WS 17.5. That AD also requires you to re…

    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 applies to certain GTX 33, GTX 33D, GTX 3…

    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, GTX 33D, GTX 330, and GTX 330D Mode S…

    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 detect, from other aircraft, the S1 (su…

    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, from other aircraft, the S1 (suppression)…

    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), and replace any damaged wiring. This…

    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) (referred to herein as damage), and repla…

    Federal Register →
  • Apr 19, 2002

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

    This amendment supersedes Airworthiness Directive (AD) 2001- 20-14, which currently requires you to replace the brake shuttle valves with parts of improved design and install a shield over the hydraulic lines on certain Fairchild Aircraft SA226 and SA227 series airplanes. AD 2001-20-14 also requires you to replace the rubber fuel hose with a metal device fo…

    Federal Register →
  • Apr 17, 2002

    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 equipped with Skidmore-Wilheim Manufacturing Co. (Skidmore-Wilheim) (formerly Hydromotive) Model V1-15-1000 brake master cylinders. This AD requires you to replace these brake master cylinders with new or ove…

    Federal Register →
  • Jan 30, 2002

    Airworthiness Directives; Fairchild Aircraft, Inc. SA26, SA226, and SA227 Series Airplanes

    This amendment supersedes Airworthiness Directive (AD) 86-24- 11 and AD 86-25-04, which require you to incorporate, into the Limitations Section of the pilot's operating handbook and airplane flight manual (POH/AFM) of Fairchild Aircraft, Inc. (Fairchild Aircraft) SA226 and SA227 series airplanes, procedures for preventing an engine flameout while in icing…

    Federal Register →
  • Dec 27, 2001

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

    This document proposes to supersede Airworthiness Directive (AD) 2001-20-14, which currently requires you to replace the brake shuttle valves with parts of improved design and install a shield over the hydraulic lines on certain Fairchild Aircraft SA226 and SA227 series airplanes. AD 2001-20-14 also requires you to replace the rubber fuel hose with a metal…

    Federal Register →
  • Dec 20, 2001

    Airworthiness Directives; Fairchild Aircraft Incorporated SA226 and SA227 Series Airplanes

    This document proposes to revise an earlier proposed airworthiness directive (AD) that would apply to certain Fairchild Aircraft Incorporated (Fairchild Aircraft) SA226 and SA227 series airplanes equipped with Skidmore-Wilheim Manufacturing Co. (Skidmore- Wilheim) (formerly Hydromotive) Model V1-15-1000 brake master cylinders. The earlier NPRM would have re…

    Federal Register →
  • Oct 12, 2001

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

    This amendment adopts a new airworthiness directive (AD) that applies to certain Fairchild Aircraft SA226 and SA227 series airplanes. This AD requires you to replace the brake shuttle valves with parts of improved design and install a shield over the hydraulic lines. This AD also requires replacing the rubber fuel hose with a metal device for certain SA226…

    Federal Register →
  • May 30, 2001

    Airworthiness Directives; Fairchild Aircraft, Inc. SA26, SA226, and SA227 Series Airplanes

    This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Fairchild Aircraft, Inc. (Fairchild Aircraft) SA26, SA226, and SA227 series airplanes. The proposedAD would require you to modify the negative torque sensing test system to allow the igniters to automatically turn when an engine senses low torque. The proposed AD…

    Federal Register →
  • Dec 5, 2000

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

    This document proposes to revise an earlier proposed airworthiness directive (AD) that would apply to certain Fairchild Aircraft SA226 and SA227 series airplanes. The earlier NPRM would have required you to replace the brake shuttle valves with parts of improved design and install a shield over the hydraulic lines. The earlier NPRM resulted from a report of…

    Federal Register →
  • Sep 1, 2000

    Airworthiness Directives; Fairchild Aircraft, Inc., SA226 Series 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 equipped with certain Ozone Industries, Inc., main landing gear (MLG) assemblies. This AD requires you to repetitively inspect the MLG drag brace assembly (consists of both brace and links) for cracks, and re…

    Federal Register →
  • Aug 22, 2000

    Airworthiness Directives; Fairchild Aircraft, Inc. Models SA226-T, SA226-AT, SA226-T(B), SA226-TC, SA227-AT, SA-227-TT, and SA-227-AC Airplanes

    This amendment supersedes Airworthiness Directive (AD) 92-01- 02, which currently requires you to accomplish the following on certain Fairchild Aircraft SA226 and SA227 series airplanes: modify the parking brake system; and inspect (repetitively) certain landing gear brake assemblies. That AD resulted from wheel brake system malfunctions on several of the a…

    Federal Register →
  • Aug 3, 2000

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

    This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Fairchild Aircraft SA226 and SA227 series airplanes. The proposed AD would require you to replace the brake shuttle valves with parts of improved design; and would require you to install a shield over the hydraulic lines. The proposed AD is the result of the wheel…

    Federal Register →
  • Feb 16, 2000

    Airworthiness Directives; Fairchild Aircraft, Inc. Models SA226-T, SA226-AT, SA226-T(B), SA226-TC, SA227-AT, SA-227-TT, and SA-227-AC Airplanes

    This document proposes to supersede Airworthiness Directive (AD) 92-01-02, which currently requires you to accomplish the following on certain Fairchild Aircraft SA226 and SA227 series airplanes: modify the parking brake system; and inspect (repetitively) certain landing gear brake assemblies. That AD resulted from wheel brake system malfunctions on several…

    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. The proposed AD is the result of report…

    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 airplanes equipped with Barber-Colman pitc…

    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 repairing any area found cracked. The repair w…

    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 any area found cracked. This repair will e…

    Federal Register →
  • Sep 24, 1998

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

    This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 98-19-15, which was sent previously to all known U.S. owners and operators of Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes. The AD applies to those airplanes that are equipped with Barber-Colman pitch trim actuators, part number (P/N)…

    Federal Register →
  • Jul 31, 1998

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

    This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes. The proposed AD would require 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 any area found…

    Federal Register →
  • Apr 17, 1998

    Airworthiness Directives; AlliedSignal Aerospace Bendix/King Model KSA 470 Autopilot Servo Actuators, Part Numbers 065-0076-10 Through 065-0076-15

    This amendment adopts a new airworthiness directive (AD) that applies to certain AlliedSignal Aerospace Bendix/King Model KSA 470 autopilot servo actuators, part numbers 065-0076-10 through 065-0076- 15, that are installed on aircraft. This AD requires replacing the autopilot servo actuator with a modified actuator. This is the result of two reports of the…

    Federal Register →
  • Mar 20, 1998

    Airworthiness Directives; Fairchild Aircraft Inc. Models SA226- AT, SA226-TC, SA227-AC, and SA227-AT Airplanes

    This amendment adopts a new airworthiness directive (AD) that applies to Fairchild Aircraft Inc. (Fairchild) Models SA226-AT, SA226- TC, SA227-AC, and SA227-AT airplanes. This action would require inspecting the cargo door lower belt frames at the cargo latch receptacles for cracks in the belt frames, repairing any cracks, and reinforcing the cargo door low…

    Federal Register →
  • Dec 19, 1997

    Airworthiness Directives; AlliedSignal Aerospace Bendix/King Model KSA 470 Autopilot Servo Actuators, Part Numbers 065-0076-10 Through 065-0076-15

    This document proposes to adopt a new airworthiness directive (AD) that would apply to certain AlliedSignal Aerospace Bendix/King Model KSA 470 autopilot servo actuators, part numbers 065-0076-10 through 065-0076-15, that are installed on aircraft. The proposed AD would require replacing the autopilot servo actuator with a modified actuator. The proposed AD…

    Federal Register →
  • Jun 4, 1997

    Airworthiness Directives; Fairchild Aircraft Incorporated Models SA226-AT, SA226-TC, SA227-AC, and SA227-AT Airplanes

    This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Fairchild Aircraft Incorporated (Fairchild) Models SA226-AT, SA226-TC, SA227-AC, and SA227-AT airplanes. The proposed action would require inspecting the cargo door lower belt frames at the cargo latch receptacles for cracks in the belt frames, repairing the crack…

    Federal Register →
  • May 29, 1997

    Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes

    This amendment adopts a new airworthiness directive (AD) that applies to certain Fairchild Aircraft SA226 and SA227 series airplanes. This AD requires modifying the electrical power generation system. The AD results from reports of both generators going off-line during flight on three of the affected airplanes. The actions specified by this AD are intended…

    Federal Register →
  • May 13, 1997

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

    This amendment supersedes Airworthiness Directive (AD) 96-21- 05, which currently requires the following on certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes that do not have a certain elevator torque tube installed: drilling inspection access holes in the elevator torque tube arm, inspecting the elevator torque tube for corrosio…

    Federal Register →
  • Jan 29, 1997

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

    This document proposes to supersede AD 96-21-05, which currently requires the following on certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes that do not have a certain elevator torque tube installed: drilling inspection access holes in the elevator torque tube arm, inspecting the elevator torque tube for corrosion, replacing any…

    Federal Register →
  • Jan 17, 1997

    Airworthiness Directives; Fairchild Aircraft, Inc. SA26, SA226, and SA227 Series Airplanes

    This amendment adopts a new airworthiness directive (AD) that applies to Fairchild Aircraft, Inc. (Fairchild) SA26, SA226, and SA227 series airplanes. This action requires applying torque to the control column pitch bearing attaching nuts, inspecting for any looseness or movement of the bearing assembly, and inspecting the elevator control rod end bearing r…

    Federal Register →

Advisory Circulars naming this type

FAA guidance that explicitly references FAIRCHILDSA227-AC

04 /  Service Difficulty Reports

FAA SDR filings

The FAA does not currently expose a public API for Service Difficulty Reports. We do not back-fill or paraphrase. Search the FAA SDR portal directly →

05 /  Sources & Methodology

Every fact on this page links to its primary US-government source

We render only what the agency publishes. Found a factual error? Report it → We acknowledge within 5 business days and resolve within 14.