Sikorsky S-92A

1,122 parts applicable to this airframe — helicopter

Part NumberStatus
20715-108PMA
2119048-3OEM
2222192-1-1OEM
2B103-2-AOEM
3213850-6OEM
3505974-1OEM
3617337-3OEM
3617731-4OEM
3800754-3unknown
44311-10-1OEM
44311-10-11PMA
44311-10-13PMA
44311-10-14PMA
44311-10-15PMA
44311-10-17PMA
44311-10-2OEM
44311-121OEM
44311-42-1PMA
44311-42-10OEM
44311-42-11OEM
44311-42-12PMA
44311-42-14PMA
44311-42-2PMA
44311-42-6OEM
44311-42-8OEM
44311-530OEM
44311-550OEM
44311-552OEM
44311-700OEM
44311-721OEM
44311-805-3OEM
44311-826PMA
565-0046-2OEM
570-0007-4OEM
595-0009-2OEM
6431556-1OEM
81-014-01PMA
92550-0214-107OEM
92550-0214-108OEM
92550-04803-041OEM
92600-01801-108OEM
92631-03804-101OEM
FT258661ZZOEM
FT258661ZZCTXPMA
LB4-1225-14-1PMA
LB6-1225-17-1PMA
LB6-1225-18-1PMA
SR02443NY-DOEM
SR09460RCOEM
SRP-110-010OEM

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.