1615-00-132-4932

Description: Tail Rotor Trunnion Assembly

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MILSPEC: Drive Mechanisms And Components Helicopter Rotor Blades

 Export Restrictions

Any part(s) quoted or sold by MilSpec.parts and re-sold (to a third party) CANNOT be sold to a USA embargoed country, company, entity, or person(s). Depending on the ECCN, these commodities may require export license or exception. Diversion contrary to U.S. law is prohibited. Unless otherwise noted, this sale, order or quote may include Munitions List Items (MLI) or Commerce Controlled List Items (CCLI). MLI/CCLI property is controlled by the US Government and in many cases cannot be transferred (exported, sold or given) to a foreign country, a non-US Citizen/National or a non- Permanent US Resident without a valid State/Commerce Department export authorization. It is the responsibility of (the Purchaser) to determine what the applicable requirements may be, to obtain all necessary authorizations, licenses or approvals and are subject to both review and acceptance by MilSpec.parts. The use, disposition, export and re-export of the property covered or included in this sale, order or quote is subject to the provisions of law referenced in End-Use Certificate DLA form 1822, DEC 2001, including, but not limited to, the Arms Export Control Act (22 USC 2751 et seq.); Export Administration Act of 1979 (50 USC App. 2401 et seq.) as contained under Executive Order 12924; International Traffic in Arms Regulations (22 CFR 120 et seq.); Export Administration Regulations (15 CFR 730 et seq.); Foreign Assets Control Regulations (31 CFR 500 et seq.) and the Espionage Act (18 USC 793 et seq.)

1615-00-132-4932 Properties

  • NSN:
    1615-00-132-4932
  • Description:
    Tail Rotor Trunnion Assembly
  • Shelf Life:
    N/A
  • DEMIL:
    DEMIL/MLI
  • UOM:
    1 EA
  • General Description:
    Fsteel, ams6414 comp aisi 4340 body, cadmium-plated o/a except splines, steel inner race no. Ra42584 torrington, dim., 3.950 in. Min, 3.960 in. Max o/a lg, 1.630 in. Min, 1.700 in. Max center w, 0.9378 in. Min, 0.9382 in. Max left and right arm thickness, 1.845 in. Min, 1.855 in. Max left and right arm spherical radius, 1.150 in. Min, 1.160 in. Max left and right arm lg, 0.635 in. Diameter arm ends by 0.317 in. Lg, trunnion internal spline data, involute flat root spline, side bearing sliding class a fit, 40 teeth theoretical, 32/64 diametral pitch, 30.0 degrees pressure angle, 1.2500 in. Pitch dia, 1.2188 in. Min 1.2203 in. Min minor dia, 1.2915 in. Min, 1.2996 in. Max major dia, trunnion arms fitted w/torrington no. Ra24584 inner race
Manufacturers and Part Numbers
Part Number
Brand
204-011-737-5
Bell Helicopter Textron .
Major Organizational Entities (MOE)
Entity
MOE Code
MOE Rule
PICA
DSOR
User:
SPAIN Spain
MOE_CD:
YB
MOE_RL:
YB01
PICA:
YB
DSOR:
Part Identification
INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
77777
FIIG:
Concept No.:
App. Key:
Cond. Code:
Status:
Material and Special Handling
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
---
CRITL:
X
Hazmat (HMIC): N
Indicates there is no data in the hmirs and the nsn is in a fsc not generally suspected of containing hazardous materials.
Precious Metals (PMIC): A
Item does not contain precious metal.
Criticality (CRITL): X
The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Packaging and Dimensions
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Package Weight
Part Weight
Part Dimensions (approx.)
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Item Weight:
--
Item Dim:
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Container
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LVL B
LVL C
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LVL B:
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CUSH
MOP
CATEG.
PRESS MAT
CUSH:
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WRAP MAT
ICQ
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UCL
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Packaging Code Definitions
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Cushion Material (CUSH):
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