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62-23-02: Main Rotor Mast Thrust Bearing

FAA order 62-23-02 is an airworthiness directive in force since October 29, 1962. The FAA's subject line: Main Rotor Mast Thrust Bearing. It names Bell-Carson 47, Bell 47: about 483 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: rotorcraft systems.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Scotts-Bell 47 Inc
Models
47, 47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A, 47H-1, 47J, 47J-2, 47J-2A, 47K
On this site
Bell-Carson 47 5 registered
Bell 47 478 registered

Dates and paperwork

In force since
October 29, 1962
Published
October 23, 1962
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (1,570 characters)
62-23-02 BELL: Amdt. 498 Part 507 Federal Register October 23, 1962. Applies to Model 47 Series Helicopters Equipped with Main Rotor Mast Thrust Bearing, P/N 47-130-110-1. Compliance required as indicated. Excessive wear and evidence of impending failure of the main rotor mast thrust bearing have occurred. To preclude progression of bearing deterioration to a hazardous degree, accomplish the following: (a) Within the next 25 hours' time in service following the effective date of this AD and thereafter at periods not to exceed 25 hours, conduct a close visual inspection of the engine oil filter. (b) If metal particles are found during any inspection of the engine oil filter, the following shall be accomplished prior to further flight: (1) The source of the contaminant shall be located and eliminated and other components of the engine and transmission which may be jeopardized by metal particles shall be inspected and overhauled as prescribed by the appropriate Bell maintenance manual; and (2) The main rotor mast thrust bearing, P/N 47-130-110-1, shall be thoroughly inspected and replaced with a like component if found not to be in a serviceable condition. (c) Clean engine oil filter carefully before reinstalling. NOTE: For the purpose of this AD, the operations outlined under (a) and (c) are considered to be preventive maintenance and may, therefore, be accomplished by persons specified in Section 18.10(c) of the Civil Air Regulations. This directive effective October 29, 1962. Revised September 16, 1966.

Related safety bulletins advice on the same designs, not orders

2001-02-09SW-01-13 ·

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 23, 2026. Connections as data: /graph/directive/62-23-02.json · aircraft systems.