AD 97-05-06

final rule
Data completeness: 70%

Airworthiness Directives; Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B, and TH-55A Helicopters

AD Number
97-05-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
94-SW-17-AD
FR Citation
Federal Register: March 03, 1997 (Volume 62, Number 41)

Applicability

TypeManufacturerModelDetails
aircraft Schweizer Aircraft Corporation 269A Airworthiness Directives; Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B, and TH-55A Helicopters
aircraft Schweizer Aircraft Corporation 269A-1 Airworthiness Directives; Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B, and TH-55A Helicopters
aircraft Schweizer Aircraft Corporation 269B Airworthiness Directives; Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B, and TH-55A Helicopters

Unsafe Condition

Failure of the main rotor thrust bearing (bearing), loss of the main rotor, and subsequent loss of control of the helicopter.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Determine the time-in-service (TIS) of the bearing part numbers 269A5050-50, -51, or -73. Replace bearings with TIS equal to or exceeding 300 hours (for P/N -50/-51) or 3,000 hours (for P/N -73) before further flight. Inspect bearings for rotational roughness, corrosion, inadequate lubrication, physical damage, moisture, or zinc chromate paste buildup per SSN N-59. Inspect and modify thrust bearing nut and main rotor mast as required.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Required within 25 hours time-in-service (TIS) after the effective date of this AD, unless accomplished previously.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A (S/N 0011-1109), 269A-1 (S/N 0001-0041), 269B (S/N 0001-0444), and TH-55A helicopters with main rotor thrust bearing part numbers 269A5050-50, -51, or -73 installed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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