205A

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NUT,PLAIN,CASTELLATED,HEXAGON

GENERAL MOTORS LLC DBA GENERAL MOTORS LLCATA 20

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Documentation

General information based on part classification, not a certification determination. Your operator's quality manual governs.

OEM / Production Approval Holder Part8130-3 Eligible

What to ask the seller for

  • FAA Form 8130-3 from the PAH or an authorized release traceable to the PAH
  • Manufacturer's CofC if a Form 8130-3 was not issued

Governing reference: FAA Order 8130.21J

PMA Alternatives

No PMA alternatives found for this part. This does not mean none exist — only that none are currently in our database.

Supplemental Type Certificates6 found

FAA-approved modifications that reference this part number

SH2394NM ↗Hillsboro Aviation Inc
Rev: 2016-06-07

Installation of AlliedSignal T5371A and T5317B engines in a Bell 205A-1 helicopter.

Aircraft: 205A-1, 205B

SH5977NM ↗Hillsboro Aviation Inc
Rev: 2016-06-07

This supplemental type certificate (STC) applies to the model 205A-1 with either the T5317A or T5317B engine modified by STCs SH2394NM and SH5132NM, and the 210 helicopters (no modifications required) when operated with nine (9) or less passengers

Aircraft: 205A-1, 210

SR01549SE ↗Dart Aerospace USA Inc.
Rev: 2005-05-19

Installation, maintenance, and operation of Nightsun SX-16 searchlight and Bell BHT 214-706-003-107 Two Speed Internal Hoist and/or BHT 205-706-091-101 Hoist Provisions and/or AAI 412-830-101 SX-16 Nightsun Kit Two Speed Internal Hoist in accordance with Dart Aerospace USA, Inc. Master Document List MDL-D205-737, Revision A, dated April 4, 2005, or later FAA approved revision. Approved for model 205A-1, serial numbers 30013 and 30121.

Aircraft: 205A-1

SR02058NY ↗Dart Aerospace Limited
Rev: 2005-02-24

The installation of replacement window kits in accordance with Dart Aerospace Ltd. Installation Instructions IIN-D412-709, Rev. A dated December 5, 2003 on Bell models 205A, 205A-1, 205B, 212, 412, 412CF, 412EP, 214B and 214B-1 aircraft.

Aircraft: 205A, 205A-1, 205B, 212 +5 more

SH201WE ↗Dallwig Barry C
Rev: 2001-03-15

Installation of stirrup assemblies to directional control pedals for operation by handicapped pilot. (US ARMY OH-13E 205A)

Aircraft: UH-1B, 204B, 205A-1, 205A +42 more

SA973NE ↗L P Aero Plastics, Inc
Rev: 1992-05-15

Installation of .250-inch thick windshield with L.P. Aero Plastics, Inc. single piece windshield. (210-5A (205A) (210 21058221 THRU 21058510) (210-5(205) S/N 205-0001 THRU 205-0480) (210B S/N 21057841 THRU 21058085) (210C S/N 21058086 THRU 2105813) (210 E S/N 21058511 THRU 21058715)

Aircraft: 210B, 210-5A (205A), 210C, 210D +2 more

Airworthiness Directives

Synced 40 days ago (09/27/2026)

No Active Airworthiness Directives

No FAA or EASA ADs are linked to this part number. Always verify against the aircraft's maintenance records before install.

Service Difficulty Reports

No Service Difficulty Reports

No failure reports found for this part number in the FAA SDR database.

Suspect-Parts Alerts (SUP/UPN)

No Suspect-Parts Alerts

This manufacturer is not named in any active FAA Suspect Unapproved Parts (SUP/UPN) notification.

NSN Cross-References1 NSN — DLA WebFLIS

National Stock Numbers assigned to this part number by the U.S. Defense Logistics Agency

NSNStandardized NameFSCDLA List Price (gov't catalog)CAGE / Manufacturer
5310-00-010-9879NUT,PLAIN,CASTELLATED,HEXAGON5310—7X677GENERAL MOTORS LLC DBA GENERAL MOTORS LLC

DLA PUBLOG published list price — government procurement catalog, not a commercial market price. Prices may differ from current commercial availability.

Government Award Prices

U.S. government contract award prices from FPDS — unit prices for NSN purchases by DoD/DLA agencies

No government contract award price data found for this part number.

Identifiers

Manufacturer

GENERAL MOTORS LLC DBA GENERAL MOTORS LLC

Source

DLA WebFLIS

ATA Chapter

20

Type

OEM

Part ID: nsn:205A | Source: DLA WebFLIS | Last updated: 2026-11-07