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1620-00-093-9071
Landing Gear Direct Action Shock Absorber
1620000939071 000939071 188600
A pneumatically or hydraulically damped coupling used to absorb forces generated by the contact of aircraft landing gear with a landing surface. View more Landing Gear Direct Action Shock Absorber
January 2023
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Related Documents 1620-00-093-9071 5+ Documents (More...)
United States (US) 4. 1620-00-093-9071 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1620-00-093-9071 RQST Updated Every Day 1620-00-093-9071 RQST NE Related Documents
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Restrictions 1620-00-093-9071
1620-00-093-9071 is a Landing Gear Direct Action Shock Absorber that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. The precious metals content of this item is unknown.
Import and Export 1620-00-093-9071
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1620-00-093-9071
- France (ZF01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 1620-00-093-9071
- Part Number
- Manufacturer
- Status
- 188600
- Manufacturer
- 7EK50 - Textron Aviation Inc (Active)
- Primary Buy
- Primary Buy
- 188600
- 70898 - Beechcraft Corporation (Replaced)
- Original Design
- Original Design
Datasheet 1620-00-093-9071
- Characteristic
- Specifications
- FIIG
- Specifications
- T312-X
- Operation Method [APHE]
- Hydraulic
- Compressed Length [AMQZ]
- 14.187 Inches Nominal
- Extended Length [ATEM]
- 22.187 Inches Nominal
- Stroke Length [AMWL]
- 8.000 Inches Nominal
- End Item Identification [AGAV]
- C-45 Beechcraft Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Shock Absorber Assembly
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Freight Information 1620-00-093-9071
1620-00-093-9071 has freight characteristics.. 1620-00-093-9071 has a variance between NMFC and UFC when transported by rail and the description should be consulted.