Sikorsky S-92A

1,122 parts applicable to this airframe — helicopter

Part NumberStatus
SH3319NMOEM
SH3319NM (1 OF 2)OEM
SR00086IBOEM
SR00160IBOEM
SR00362BOOEM
SR00826DEOEM
SR00917DEOEM
SR00925DEOEM
SR01934LAOEM
SR01948LAOEM
SR01973NY-DOEM
SR02108NY-DOEM
SR02113NY-DOEM
SR02115NY-DOEM
SR02132NY-DOEM
SR02158LAOEM
SR02402NYOEM
SR02404NY-DOEM
SR02407NY-DOEM
SR02413NY-DOEM
SR02428NY-DOEM
SR02433NY-DOEM
SR02435NY-DOEM
SR02436NY-DOEM
SR02442NY-DOEM
SR02448NY-DOEM
SR02547SESTC
SR02553NYOEM
SR02560NYOEM
SR02573NY-DOEM
SR02575NY-DOEM
SR02594NY-DOEM
SR02596NY-DOEM
SR02597NY-DOEM
SR02598NY-DOEM
SR02606NY-DOEM
SR02607NY-DOEM
SR02629LAOEM
SR02666CHSTC
SR02685CHOEM
SR03370ATOEM
SR04337NYOEM
SR04350NYOEM
SR04485NYOEM
SR04564NYOEM
SR04583CHOEM
SR09469RCOEM
SR09470RCOEM
SR09471RCOEM
SR09926ACOEM

Airworthiness Directive activity

FAA / EASA public regulatory data

4airworthiness directives affecting this fleet — recurring compliance demand for the parts and shops that serve it
Most recent
  • FAA AD 2023-09-07effective Jun 29, 2023Mixed actions

    The FAA is superseding Airworthiness Directive (AD) 2022-02-01 for Sikorsky Aircraft Corporation Model S-92A helicopters with certain part-numbered main rotor stationary swashplate assemblies (swashplate assemblies) that had accumulated 1,600 or more total hours time-in- service (TIS) installed. AD 2022-02-01 required visually inspecting the swashplate assembly at specified intervals and depending on the results, removing the swashplate assembly from service. Since the FAA issued AD 2022-02-01, the FAA determined it was necessary to expand the applicability and require more detailed inspections to address the unsafe condition. This AD retains the actions of AD 2022-02-01, expands the applicability, adds a detailed recurring visual inspection, and requires either eddy current inspections (ECI) or fluorescent penetrant inspections (FPI). The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2022-11-04effective Jun 27, 2022Prohibition

    The FAA is superseding Airworthiness Directive (AD) 2020-26- 13, which applied to certain Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. AD 2020-26-13 required establishing the life limit for certain part-numbered horizontal stabilizer root fittings FWD (forward root fittings) and certain part-numbered stabilizer strut fittings. AD 2020-26-13 also required repetitively inspecting certain parts, and depending on the inspection results, removing parts from service. Finally AD 2020-26-13 prohibited installing certain stabilizer assemblies on any helicopter. Since the FAA issued AD 2020-26-13, the manufacturer notified the FAA that due to an error in the service information, certain part numbers in AD 2020-26-13 are incorrect. Also, the FAA determined that additional inspections are required to address the unsafe condition. This AD retains certain requirements and the prohibition for installing certain stabilizer assemblies on any helicopter from AD 2020-26-13, corrects certain part numbers, and requires additional repetitive inspections. The actions of this AD are intended to address an unsafe condition on these products.

  • FAA AD 2022-02-01effective Feb 18, 2022Mixed actions

    The FAA is adopting a new airworthiness directive (AD) for certain Sikorsky Aircraft Corporation Model S-92A helicopters. This AD was prompted by a cracked main rotor stationary swashplate assembly (swashplate assembly). This AD requires visually inspecting the swashplate assembly at specified intervals and depending on the results, removing the swashplate assembly from service. The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2021-19-17effective Nov 22, 2021Prohibition

    The FAA is adopting a new airworthiness directive (AD) for certain Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This AD was prompted by an incident of a side facing utility seat detaching from wall attachment points. This AD requires modifying certain side facing utility seats and observer seats, and prohibits installing those seats unless the modification has been accomplished. The FAA is issuing this AD to address the unsafe condition on these products.

Directives linked to this airframe family in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) across the fleet; inspection directives are not replacement directives, and none of this is a prediction that any part will fail.